Technical Field
[0001] The present invention relates to the structure of a propeller cap and, more particularly
to a combined propeller cap for reducing rotational flow and hub vortex and enhancing
propulsive efficiency, whereby the propeller cap reduces noise and vibration in a
vessel by decreasing hub vortex cavitation behind a propeller for propelling the vessel,
prevents erosion and corrosion of a rudder, and enhances propulsive efficiency to
save fuel.
[0002] Further, the present invention relates to a combined propeller cap for reducing rotational
flow and hub vortex and improving propulsive efficiency, the combined propeller cap
being capable of reducing hub vortex cavitation that is generated behind a propeller
by using a combined propeller cap structure in which a diffusion type propeller cap
is coupled to the end of a contraction type propeller cap in order to solve the problem
with a PBCF (Propeller Boss Cap Fin) in the related art, which is difficult to manufacture
and is expensive due to precise machining for designing and manufacturing fins caused
by a configuration of attaching a plurality of small fins to a propeller cap to reduce
hub vortex, and being capable of being easily manufactured with a low cost in a simple
structure as compared with the PBCF.
[0003] Further, the present invention relates to a combined propeller cap for reducing rotational
flow and hub vortex and improving propulsive efficiency, the combined propeller cap
being capable of additionally reducing hub vortex cavitation by forming a combined
propeller cap structure, in which a diffusion type propeller cap is coupled to the
end of a contraction type propeller cap, and by attaching plate-shaped guide fins
at a contractive section or between an contractive section and a diffusive section
of the propeller cap, whereby it can reduce rotational flow and hub vortex cavitation
that are generated behind a propeller and can be easily manufactured at a low cost
in a simple configuration, as compared with an existing PBCF.
Background Art
[0004] In general, sea vessels are moved forward by a thruster such as a propeller that
generates propulsion and such a propeller type thruster is connected to a rotary shaft
of an engine of a vessel and rotated by power from the engine.
[0005] In detail, a propeller type thruster is largely includes a propeller cap connected
to the rotary shaft of an engine to form the body of a propeller and a plurality of
blades formed around the propeller cap, and propulsion and torque is generated by
the flows passing the blades, whereby a vessel is moved forward by the propulsion
with the torque offset by power from the engine.
[0006] In general, the propellers of vessels use only 70% of the power from a main engine
as propulsion for moving the vessels forward and the other power from the engine is
wasted as friction, a thermal loss, a vortex behind the propeller, and a propeller
hub vortex.
[0007] In these factors, the rotational flow and the hub vortex behind the propeller consume
about 5 ∼ 7% and 1 ∼ 3% of the power. Further, a strong hub vortex generates hub vortex
cavitation, which causes problems such as noise, vibration, erosion and corrosion
of a rudder. Accordingly, various devices have been developed in the related art to
solve problems with restoration of wasted energy and cavitation.
[0008] For example, a "Ship propulsion device and ship with same" has been disclosed in
Korean Patent Application Publication No.
10-2011-0120267 to increase propulsion and save fuel by decreasing hub vortex cavitation behind a
propeller.
[0009] In detail, Korean Patent Application Publication No.
10-2011-0120267 relates to a ship propulsion device that has fins formed on a propeller boss cap
mounted at the rear of a propeller boss of a screw propeller and disposed behind and
between the blades of the propeller and that can be easily manufactured with high
efficiency and low weight by cutting straight the rear end of the propeller boss cap
or, by recessing the rear end of the propeller boss cap within 20% of the entire length
of the propeller boss cap from the edge, making the entire length of the propeller
boss cap 0.28 ∼ 0.76 times the diameter of the front end of the cap, and by making
the diameter of the rear end of the propeller boss cap 0.35 ∼ 0.95 times the diameter
of the front end of the cap, and a ship equipped with the ship propulsion device.
[0010] Further, a "Propeller boss cap of the ship" for improving propulsion and saving fuel
by reducing hub vortex cavitation behind a propeller has been disclosed in Korean
Patent Application Publication No.
10-2012-0134647.
[0011] In detail, the propeller boss cap for a ship disclosed in 10-2012-0134647 is designed
to be mounted on the rear side of a propeller boss, which is connected to the shaft
of a propeller, to prevent corrosion of a rudder by suppressing hub vortex cavitation
due to a flow behind the propeller without increasing additional resistance by the
boss cap, by forming a boss groove deep such that the center and the edge thereof
are not at the same level, on a rudder-side surface of the boss cap.
[0012] As described above, there have been various studies for increasing propulsion and
saving fuel by decreasing rotational flow and hub vortex cavitation. However, according
to these methods of the related art, propeller caps are formed in specific shapes
different from those existing before or forming a plurality of fins separate from
the blades of propellers, so the configuration is complicated, whereby it is difficult
to design and manufacture a propeller, and the manufacturing cost is also increased.
[0013] In detail, as for a device for restoring rotational energy behind a propeller, as
described above, there are a CRP (Contra-Rotating Propeller), a pre-swirl stator,
a postswirl stator, a vane-wheel, and a rudder thrust (bulb) fin). These devices have
been known to save energy by about 2 - 5%, but they are relatively large structures,
so they are expensive to install and mount and have a structural danger.
[0014] Further, for example, there is a PBCF (Propeller Boss Cap Fin) and a rudder bulb
that are devices for overcoming the problem with hub vortex cavitation by a propeller.
These devices have an energy saving effect of about 1 ∼ 3% and have a small and simple
configuration, as compared with the devices for restoring rotational energy behind
a propeller, so they can be easily mounted and manufactured at low cost.
[0015] The PBCF, which was been developed in the 1970s, improves propeller efficiency about
1 ∼ 3% by absorbing hub vortex energy using small fins on a propeller cap on the hub
at the rear portion of a propeller and, reduces noise and erosion and corrosion of
a rubber due to hub vortex cavitation by decreasing hub vortex cavitation by the propeller.
[0016] However, the fins for the PBCF have to be designed in different ways every time to
have appropriate characteristics, depending on the types of vessels and the use environment,
require very precise design, and should be manufactured substantially in the same
way as a propeller after being designed. Accordingly, a large manufacturing cost is
needed, as compared with the rudder bulb.
[0017] Therefore, in order to solve the problems with the methods of reducing hub vortex
cavitation by a propeller using the PBCF that requires precise design for each vessel,
which should be manufactured in the same way as propellers, and thus is not easy to
manufacture and which increases the manufacturing cost, it is required to develop
a new propeller structure that can be manufactured at a low cost with a simpler configuration,
can reduce hub vortex cavitation generated behind the propeller, thereby being able
to reduce noise and vibration in a vessel, prevent erosion and corrosion of a rudder,
and save fuel by improving propulsive efficiency.
Documents of Related Art
Disclosure
Technical Problem
[0019] An object of the present invention is to provide a combined propeller cap for reducing
rotational flow and hub vortex and improving propulsive efficiency, the combined propeller
cap being capable of reducing hub vortex cavitation that is generated behind a propeller
by using a combined propeller cap structure in which a diffusion type propeller cap
is coupled to the end of a contraction type propeller cap in order to solve the problem
with a PBCF (Propeller Boss Cap Fin) in the related art, which is difficult to manufacture
and is expensive due to precise machining for designing and manufacturing fins caused
by a configuration of attaching a plurality of small fins to a propeller cap to reduce
hub vortex cavitation, and being capable of being easily manufactured with a low cost
in a simple structure as compared with the PBCF.
[0020] Another object of the present invention is to provide a combined propeller cap for
reducing rotational flow and hub vortex and improving propulsive efficiency that is
configured not only to reduce hub vortex cavitation that is generated behind a propeller
through a combined propeller cap structure in which a diffusion type propeller cap
is coupled to the end of a contraction type propeller cap, but also to additionally
reduce hub vortex cavitation by attaching plate-shaped guide fins to the contractive
section or between the contractive section and the diffusive section of the propeller
cap, whereby it is possible to reduce rotational flow and hub vortex cavitation that
are generated behind a propeller, to easily manufacture the propeller cap at a low
cost in a simple configuration, as compared with the existing PBCF, to reduce noise
and vibration in a vessel and prevent erosion and corrosion of a rudder, and to save
fuel by improving propulsive efficiency.
Technical Solution
[0021] In order to achieve the objects of the present invention, according to an aspect
of the present invention, there is provided a combined propeller cap for reducing
rotational flow and hub vortex and improving propulsive efficiency. The combined propeller
cap has: a contractive section having a diameter that decreases as it goes away from
a propeller; and a diffusive section extending from the contractive section and having
a diameter that increases as it goes away from the propeller, in which pressure of
a flow from the propeller is recovered by the shape of the contractive section having
the decreasing diameter, so propulsive efficiency is improved, and rotational flow
(vortex) is weakened by the shape of the diffusive section having the increasing diameter
at an end of the propeller cap.
[0022] The inclination angle of the contractive section may be set to 0 ∼ 40°.
[0023] A side of the contractive section may be formed straight, or the side of the contractive
section may be curved to be convex outwardly with a predetermined curvature, or the
side of the contractive section may be curved to be convex inwardly with a predetermined
curvature.
[0024] According to another aspect of the present invention, there is provide a combined
propeller cap for reducing rotational flow and hub vortex and improving propulsive
efficiency. The combined propeller cap has: a first diffusive section having a diameter
that increases from an end of a propeller as it goes toward the propeller; a straight
section horizontally extending from the first diffusive section; a contractive section
extending from the straight section and having a diameter that decreases as it goes
away from the propeller; and a second diffusive section extending from the contractive
section and having a diameter that increases as it goes away from the propeller, in
which the combined propeller cap is convexly formed at a front portion by the first
diffusive section, so pressure at a pressure side of the propeller increases and propulsive
efficiency is improved, pressure of a flow passing the propeller cap from the propeller
is recovered by the contractive section, so the propulsive efficiency is improved,
and rotational flow (vortex) of a flow from the propeller is weakened by the second
diffusive section, so hub vortex cavitation is reduced.
[0025] The inclination angles of the first diffusive section and the second diffusive section
may be set to 0 ∼ 40°.
[0026] A side of the contractive section may be formed straight, or the side of the contractive
section may be curved to be convex outwardly with a predetermined curvature, or the
side of the contractive section may be curved to be convex inwardly with a predetermined
curvature.
[0027] According to another aspect of the present invention, there is provided a combined
propeller cap for reducing rotational flow and hub vortex and improving propulsive
efficiency. The combined propeller cap has: a contractive section having a diameter
that decreases as it goes away from a propeller; a diffusive section extending from
the contractive section and having a diameter that increases as it goes away from
the propeller; and a plurality of guide fins formed in a thin plate shape having a
rectangular or curved cross-section with a predetermined uniform thickness and, disposed
with regular intervals between the contractive section and the diffusive section;
in which pressure of a flow from the propeller is recovered by the shape of the contractive
section having the decreasing diameter, so propulsive efficiency is improved, rotational
flow (vortex) is weakened by the shape of the diffusive section having the increasing
diameter at an end of the propeller cap, and rotational flow by rotation of the propeller
is changed into a straight flow in a rotational axial direction, so the hub vortex
cavitation is further reduced.
[0028] The inclination angle of the contractive section may be set to 0 ∼ 40°.
[0029] A side of the contractive section may be formed straight, or the side of the contractive
section may be curved to be convex outwardly with a predetermined curvature, or the
side of the contractive section may be curved to be convex inwardly with a predetermined
curvature.
[0030] The guide fins may be formed in a thin rectangular plate shape and attached between
the contractive section and the diffusive section of the propeller cap by simple welding,
and a size of the guide fins may be determined to correspond to the diameter of the
diffusive section in order to avoid an increase in resistance due to the guide fins.
[0031] The guide fins may be formed in a thin pentagonal plate shape and attached between
the contractive section and the diffusive section of the propeller cap by simple welding,
and a length of a portion extending from an end of the diffusive section may be within
two times the diameter of the diffusive section.
[0032] The guide fins may be formed in a thin trapezoidal plate shape and attached between
the contractive section and the diffusive section of the propeller cap by simple welding,
and a length of a shortest portion of portions extending from a side of the contractive
section may be within two times the diameter of the diffusive section.
[0033] Two to eight guide fins may be disposed at the contractive section or between the
contractive section and the diffusive section of the propeller cap, and the guide
fins may be attached with a tolerance of +10 ∼ -10 degrees or +20 ∼ -20 degrees with
respect to 0 degree when seen from vertically above.
[0034] According to another aspect of the present invention, there is provided a combined
propeller cap for reducing rotational flow and hub vortex and improving propulsive
efficiency. The combined propeller cap has: a first diffusive section having a diameter
that increases from an end of a propeller as it goes toward the propeller; a straight
section horizontally extending from the first diffusive section; a contractive section
extending from the straight section and having a diameter that decreases as it goes
away from the propeller; a second diffusive section extending from the contractive
section and having a diameter that increases as it goes away from the propeller; and
a plurality of guide fins formed in a thin plate shape having a rectangular or curved
cross-section with a predetermined uniform thickness and, disposed with regular intervals
at the contractive section or between the contractive section and the diffusive section,
in which the combined propeller cap is convexly formed at a front portion by the first
diffusive section, so pressure at a pressure side of the propeller increases and propulsive
efficiency is improved, pressure of a flow passing the propeller cap from the propeller
is recovered by the contractive section, so the propulsive efficiency is improved,
rotational flow (vortex) of a flow from the propeller is weakened by the second diffusive
section, so hub vortex cavitation is reduced, and rotational flow by rotation of the
propeller is changed into a straight flow in a rotational axial direction, so the
hub vortex cavitation is further reduced.
[0035] The inclination angles of the first diffusive section and the contractive section
may be set to 0 ∼ 40°.
[0036] A side of the contractive section may be formed straight, or the side of the contractive
section may be curved to be convex outwardly with a predetermined curvature, or the
side of the contractive section may be curved to be convex inwardly with a predetermined
curvature.
[0037] The guide fins may be formed in a thin rectangular plate shape and attached between
the contractive section and the second diffusive section of the propeller cap by simple
welding, and a size of the guide fins may be determined to correspond to the diameter
of the diffusive section in order to avoid an increase in resistance due to the guide
fins.
[0038] The guide fins may be formed in a thin pentagonal plate shape and attached between
the contractive section and the second diffusive section of the propeller cap by simple
welding, and a length of a portion extending from an end of the second diffusive section
may be within two times the diameter of the second diffusive section.
[0039] The guide fins may be formed in a thin trapezoidal plate shape and attached between
the contractive section and the diffusive section of the propeller cap by simple welding,
and a length of a shortest portion of portions extending from a side of the contractive
section may be within two times the diameter of the second diffusive section.
[0040] Two to eight guide fins may be disposed at the contractive section or between the
contractive section and the second diffusive section of the propeller cap, and the
guide fins may be attached with a tolerance of +10 ∼ -10 degrees or +20 ∼ -20 degrees
with respect to 0 degree when seen from vertically above.
[0041] According to another aspect of the present invention, there is provided a propeller
for a vessel, which uses the combined propeller caps described above, in which as
compared with existing propellers, energy loss due to hub vortex cavitation and a
propeller cap shape is prevented and propulsive efficiency is improved, vibration
and noise are reduced, and erosion and corrosion of a rudder by the hub vortex cavitation
are prevented, and in comparison to existing PBCFs, manufacturing cost is reduced.
Advantageous Effects
[0042] According to the present invention, there is provided a combined propeller cap for
reducing rotational flow and hub vortex and improving propulsive efficiency, the combined
propeller cap being capable of reducing hub vortex cavitation that is generated behind
a propeller and being capable of being easily manufactured at a low cost in a simple
configuration, as compared with the existing PBCF, through a combined propeller cap
structure in which a diffusion type propeller cap is coupled to the end of a contraction
type propeller cap, whereby it is possible to solve the problem with a PBCF (Propeller
Boss Cap Fin) in the related art, whereby manufacturing is difficult and expensive
due to precise machining for designing and manufacturing fins caused by a configuration
of attaching a plurality of small fins to a propeller cap to reduce hub vortex cavitation.
[0043] Further, according to the present invention, as described above, there is provided
a combined propeller cap for reducing rotational flow and hub vortex and improving
propulsive efficiency that is configured not only to reduce hub vortex cavitation
that is generated behind a propeller through the combined propeller cap in which a
diffusion type propeller cap is coupled to the end of a contraction type propeller
cap, but also to additionally reduce hub vortex cavitation by attaching plate-shaped
guide fins to the contractive section or between the contractive section and the diffusive
section of the propeller gap. Accordingly, it is possible to reduce rotational flow
and hub vortex cavitation that are generated behind a propeller, to easily manufacture
the propeller cap at a low cost in a simple configuration, as compared with the existing
PBCF, to reduce noise and vibration in a vessel and prevent erosion and corrosion
of a rudder, and to save fuel by improving propulsive efficiency.
Description of Drawings
[0044]
FIG. 1 is a view schematically showing the structure of a propeller cap of the related
art.
FIG. 2 is a view schematically showing the entire configuration of a combined propeller
cap according to a first embodiment of the present invention.
FIG. 3 is a view schematically showing the entire configuration of a combined propeller
cap according to a second embodiment of the present invention.
FIG. 4 is a view comparing efficiency of a propeller equipped with a propeller cap
of the related art and a propeller equipped with the combined propeller cap according
to the first embodiment of the present invention shown in FIG. 2.
FIG. 5 is a view schematically showing the entire configuration of a combined propeller
cap according to a third embodiment of the present invention.
FIG. 6 is a view schematically showing the entire configuration of a combined propeller
cap according to a fourth embodiment of the present invention.
FIG. 7 is a view comparing efficiency of a propeller equipped with a propeller cap
of the related art and a propeller equipped with the combined propeller caps according
to the third and fourth embodiments of the present invention shown in FIGS. 5 and
6.
FIG. 8 is a view schematically showing the entire configuration of a combined propeller
cap according to a fifth embodiment of the present invention.
FIG. 9 is a view comparing propulsion, torque, and efficiency of a propeller equipped
with a propeller cap of the related art and a propeller equipped with the combined
propeller cap according to the fifth embodiment of the present invention shown in
FIG. 8.
FIG. 10 is a view schematically showing the entire configuration of a combined propeller
cap according to a sixth embodiment of the present invention.
FIG. 11 is a view schematically showing the entire configuration of a combined propeller
cap according to a seventh embodiment of the present invention.
FIG. 12 is a view comparing efficiency of a propeller equipped with a propeller cap
of the related art and a propeller equipped with the combined propeller cap according
to the seventh embodiment of the present invention shown in FIG. 11.
FIG. 13 is a view schematically showing the entire configuration of a combined propeller
cap according to an eighth embodiment of the present invention.
FIG. 14 is a view schematically showing the entire configuration of a combined propeller
cap according to a ninth embodiment of the present invention.
FIG. 15 is a view schematically showing the entire configuration of a combined propeller
cap according to a tenth embodiment of the present invention.
FIG. 16 is a view comparing propulsion, torque, and efficiency of a propeller equipped
with a propeller cap of the related art and a propeller equipped with the combined
propeller cap according to the ninth embodiment of the present invention shown in
FIG. 14.
Best Mode
[0045] Hereinafter, detailed embodiments of a combined propeller cap for reducing rotational
flow and hub vortex and improving propulsive efficiency according to the present invention
are described with reference to accompanying drawings.
[0046] It should be understood that the following description is just an example for accomplishing
the present invention and the present invention is not limited thereto.
[0047] Further, it should be understood that components that is determined as being the
same as or similar to those in the related art or as being easily understood and achieved
by those skilled in the art are not described in detail for simple description in
the following description about embodiments of the present invention.
[0048] Further, in the following description about embodiments of the present invention,
it should be understood that the same or similar components are given the same reference
numerals and are not described in detail for simple description.
[0049] Further, as described below, the present invention relates to a combined propeller
cap for reducing rotational flow and hub vortex and improving propulsive efficiency,
the combined propeller cap being capable of reducing hub vortex cavitation that is
generated behind a propeller by using a combined propeller cap structure in which
a diffusion type propeller cap is coupled to the end of a contraction type propeller
cap in order to solve the problem with a PBCF (Propeller Boss Cap Fin) in the related
art, whereby manufacturing is difficult and expensive due to precise machining for
designing and manufacturing fins caused by a configuration of attaching a plurality
of small fins to a propeller cap to reduce hub vortex cavitation, and being capable
of being easily manufactured with a low cost in a simple structure as compared with
the PBCF.
[0050] Further, as described below, the present invention relates to a combined propeller
cap for reducing rotational flow and hub vortex and improving propulsive efficiency
that is configured not only to reduce hub vortex cavitation that is generated behind
a propeller through a combined propeller cap structure in which a diffusion type propeller
cap is coupled to the end of a contraction type propeller cap, but also to additionally
reduce hub vortex cavitation by attaching plate-shaped guide fins to the contractive
section or between the contractive section and the diffusive section of the propeller
cap, whereby it is possible to reduce rotational flow and hub vortex cavitation that
are generated behind a propeller, to easily manufacture the propeller cap at a low
cost in a simple configuration, as compared with the existing PBCF, to reduce noise
and vibration in a vessel and prevent erosion and corrosion of a rudder, and to save
fuel by improving propulsive efficiency.
[0051] Hereinafter, detailed embodiments of a combined propeller cap for reducing rotational
flow and hub vortex and improving propulsive efficiency according to the present invention
are described with reference to accompanying drawings.
[0052] First, referring to FIG. 1, FIG. 1 is a view schematically showing the structure
of a propeller cap of the related art.
[0053] As shown in FIG. 1, generally, a propeller cap of the related art can be largely
classified into three types: a contraction type propeller cap shown in FIG. 1a, a
straight type propeller cap shown in FIG. 1b, and a diffusion type propeller cap shown
in FIG. 1c.
[0054] In detail, the contraction type propeller cap has high propulsive efficiency, but
large hub vortex cavitation is caused by concentration of motion of the hub in the
cap, so noise and vibration are increased and erosion and corrosion of a rudder may
become severe.
[0055] On the other hand, the diffusion type propeller cap has low propulsive efficiency,
but hub vortex cavitation is weakened, so noise and vibration can be reduced and erosion
and corrosion of a rudder can be attenuated.
[0056] Accordingly, in general, vessels that sail at high speeds such as a container ship
are usually equipped with the diffusion type propeller cap due to the problem of corrosion
of a rudder due to hub vortex cavitation and are additionally equipped with an additional
device such as a PBCF to overcome reduction of propulsive efficiency, thereby improving
the propulsive efficiency and coping with hub vortex cavitation.
[0057] On the contrary, tank ships that sail low speeds are usually equipped with the contraction
type propeller cap because they generate weak hub vortex cavitation.
[0058] When a container ship using a diffusion type propeller is equipped with a PBCF that
is a device for saving fuel to prevent reduction of propulsive efficiency, the fins
of the PBCF are designed and manufactured in the same way as the existing propellers,
so the manufacturing cost is high relative to the size.
[0059] Therefore, the inventor(s) has proposed a new propeller cap structure that can improve
propulsive efficiency with low hub vortex cavitation, similar to the PBCF, and can
achieve an effect similar to the PBCF even at a very low manufacturing cost in comparison
to the manufacturing cost of the PBCF by simplifying the configuration.
[0060] Further, referring to FIG. 2, shown is a view schematically showing the entire configuration
of a combined propeller cap 20 according to a first embodiment of the present invention.
[0061] In detail, as shown in FIG. 2, the combined propeller cap 20 according to the first
embodiment of the present invention includes a contraction section 21 of which the
diameter decreases as it goes away from a propeller and a diffusive section 22 that
extends from the contractive section and of which the diameter increases as it goes
away from the propeller.
[0062] That is, the combined propeller cap 20 according to the first embodiment of the present
invention, as shown in FIG. 2, has a shape of which the diameter gradually decreases
from the end of a propeller and increases at the end portion of the propeller cap.
[0063] The inclination angle α of the contractive section 21 may be set, for example, to
0 ∼ 40°.
[0064] When the inclination angle of the contractive section 21 exceeds 40 degrees, the
performance rapidly drops due to flow separation, that is, when flow separation is
generated, pressure is not recovered on the propeller cap, so resistance increases.
[0065] In more detail, referring to the following Table 1, Table 1 shows changes in performance
due to changes in the inclination angle α of the contractive section 22.
[Table 1]
Angle (α) |
10 |
20 |
30 |
40 |
50 |
60 |
Performance change (%) |
+1.0 |
+1.0 |
+0.9 |
+0.7 |
+0.2 |
+0.2 |
[0066] The result in Table 1 shows estimated values of propulsive performance according
to changes in the inclination angle α of the contractive section 22, as compared with
a propeller equipped with a diffusion type propeller cap of the related art.
[0067] Further, referring to FIG. 3, FIG. 3 is a view schematically showing the entire configuration
of a combined propeller cap 30 according to a second embodiment of the present invention.
[0068] In the following description of the second embodiment of the present invention, the
same or similar components as in the first embodiment are not described and only other
different components are described for simple description.
[0069] That is, as shown in FIG. 3, the combined propeller cap 30 according to the second
embodiment of the present invention has a contractive section 31 of which the diameter
decreases as it goes away from a propeller and a diffusive section 32 that extends
from the contractive section 31 and of which the diameter increases as it goes away
from the propeller, which is the same as the first embodiment shown in FIG. 2. However,
the propeller cap 30 according to the second embodiment of the present invention is
characterized in that the contractive section 31 is not formed straight, as in the
first embodiment, but curved with a predetermined curvature.
[0070] That is, the combined propeller cap 30 according to the second embodiment of the
present invention is characterized in that the contractive section 31 is curved to
be convex outwardly with a predetermined curvature, as shown in FIG. 3a, or is curved
to be convex inwardly with a predetermined curvature, as shown in FIG. 3b.
[0071] The curvature of the contractive section 31 can be appropriately determined, depending
on the type or the use of a propeller or a ship, and other parts are the same as those
in the first embodiment, so they are not described in detail.
[0072] Accordingly, as the propeller cap is formed in a shape of which the diameter decreases
and increases again, when a propeller is operated, pressure is recovered and propulsive
efficiency is improved by the shape of which the diameter decreases to the contractive
sections 21 and 31 at the middle portion of the propeller caps 20 and 30 and a strong
rotational flow (vortex) is weakened by the shape of which the diameter increases
over the diffusive sections 22 and 32 at the end of the propeller caps 20 and 30,
whereby it is possible to reduce hub vortex cavitation.
[0073] Further, energy loss due to hub vortex and a cap shape is prevented accordingly,
so the propulsive efficiency can be improved in comparison to the existing diffusion
type propellers (1 ∼ 3%), vibration and noise due to hub vortex can be reduced, and
erosion and corrosion of a rudder can be prevented in comparison to the existing contraction
type propeller caps.
[0074] In more detail, referring to FIG. 4, shown is a view comparing propulsive efficiency
of a propeller equipped with a propeller cap of the related art and a propeller equipped
with the combined propeller cap 20 according to the first embodiment of the present
invention shown in FIG. 2.
[0075] That is, it can be seen from FIG. 4 that the propeller equipped with the combined
propeller cap 20 according to the first embodiment of the present invention had propulsive
efficiency similar to that of the contraction type propeller cap of the related art,
but side effects due to hub vortex cavitation can be greatly reduced and the propulsive
efficiency was considerably improved as compared with the diffusion type propeller
cap.
[0076] That is, as described above, according to the configuration of the combined propeller
caps 20 and 30 of the first and second embodiments of the present invention, the propulsive
efficiency is improved by pressure recovery due to the shape from a propeller to the
contractive sections 21 and 31 and a strong rotational flow (vortex) is weakened by
the diffusive sections 22 and 32 while the flow from the propeller passes over the
ends of the caps, whereby hub vortex cavitation can be suppressed. Accordingly, energy
loss due to hub vortex and a cap shape is prevented, so the propulsive efficiency
of a vessel can be improved by about 1 ∼ 3% in comparison to the existing diffusion
type propeller. Further, vibration and noise due to hub vortex cavitation can be reduced,
and erosion and corrosion of a rudder can be prevented, as compared with the contraction
type propeller caps.
[0077] Further, according to the configuration of the combined propeller caps 20 and 30
of the first and second embodiments of the present invention described above, there
is an advantage that it is possible to reduce hub vortex cavitation, similar to the
existing diffusion type propeller caps used for container ships, and it is possible
to improve propulsive efficiency in comparison to the existing diffusion type propeller
cap. Further, there is another advantage that it is possible to obtain propulsive
efficiency similar to the contraction type propeller caps when it is applied to tank
ships, but it is possible to greatly reduce hub vortex cavitation.
[0078] Further, since the shapes of the combined propeller caps 20 and 30 of the first and
second embodiments of the present invention described above are simple in structure,
they can be easily manufactured, so there is also an advantage that it is possible
to remarkably decrease the manufacturing cost, which was over one hundred million
South Korean won due to precise machining of the fins of the PBCF in the related art,
to within thirty million South Korean won similar to the existing propeller caps.
[0079] Further, referring to FIG. 5, FIG. 5 is a view schematically showing the entire configuration
of a combined propeller cap 50 according to a third embodiment of the present invention.
[0080] In detail, the combined propeller cap 50 according to the third embodiment of the
present invention has a first diffusive section 51 of which the diameter increases
from the end of a propeller, a straight section 52 that horizontally extends from
the first diffusive section 51, a contractive section 53 that extends from the straight
section 52 and of which the diameter decreases as it goes away from the propeller,
and a second diffusive section 54 that extends from the contractive section 53 and
of which the diameter increases again as it goes away from the propeller.
[0081] That is, the combined propeller cap 50 according to the third embodiment of the present
invention, as shown in FIG. 5, has a shape of which the diameter gradually decreases
from the end of a propeller to a predetermined portion, but increases at the end portion
of the propeller cap.
[0082] In more detail, since the combined propeller cap 50 according to the third embodiment
of the present invention is convexly formed at the front portion by the first diffusive
section 51, a shown in FIG. 5, the pressure at the pressure side of the propeller
increases, thereby improving the propulsive efficiency.
[0083] That is, the propeller cap 50 according to the third embodiment of the present invention
for reducing hub vortex cavitation and improving propulsive efficiency is additionally
improved in propulsive efficiency by pressure recovery due to the shape from the propeller
to the contractive section 53 at the middle portion, as shown in FIG. 5, and can reduce
hub vortex cavitation by decreasing a strong rotational flow (vortex) through the
second diffusive section 54 while the flow from the propeller passes over the end
of the diffusive cap.
[0084] Further, as hub vortex cavitation is reduced, as described above, it is possible
to improve propulsive efficiency in comparison to the existing diffusion type propeller
caps and it is also possible to prevent vibration and noise due to hub vortex cavitation
and erosion and corrosion of a rudder. Further, it is possible to more efficiently
prevent vibration and noise and, erosion and corrosion of a rudder and to improve
propulsive efficiency, as compared with the existing contraction type propeller caps.
[0085] The inclination angles α and β of the contractive section 1 and the second diffusive
section 54, respectively, may be set, for example, to 0 ∼ 40°.
[0086] When α and β exceed 40 degrees, the performance rapidly drops due to flow separation,
that is, when flow separation is generated, pressure is not recovered on the propeller
cap, so resistance increases.
[0087] In more detail, referring to the following Table 2, Table 2 shows changes in performance
due to changes in the inclination angles α and β of the second diffusive section 54.
[Table 2]
Angle (α) |
10 |
20 |
30 |
40 |
50 |
60 |
Performance change (%) |
+1.1 |
+1.1 |
+1.1 |
+1.0 |
+0.7 |
+0.7 |
Angle (β) |
10 |
20 |
30 |
40 |
50 |
60 |
Performance change (%) |
+1.1 |
+1.1 |
+1.1 |
+0.8 |
+0.3 |
+0.2 |
[0088] In Table 1, when α was changed, β was fixed at 30 degrees, while when β was changed,
α was fixed at 30 degrees. Further, the result in Table 2 shows estimated values of
propulsive performance according to angle changes, as compared with a propeller equipped
with an existing diffusion type propeller cap.
[0089] Further, referring to FIG. 6, FIG. 6 is a view schematically showing the entire configuration
of a combined propeller cap 60 according to a fourth embodiment of the present invention.
[0090] In the following description of the fourth embodiment of the present invention, the
same or similar components as in the third embodiment are not described and only other
different components are described for simple description.
[0091] That is, as shown in FIG. 6, the combined propeller cap 60 according to the fourth
embodiment of the present invention has a first diffusive section 61 of which the
diameter increases from the end of a propeller, a straight section 62 that horizontally
extends from the first diffusive section 61, a contractive section 63 that extends
from the straight section 62 and of which the diameter decreases as it goes away from
the propeller, and a second diffusive section 64 that extends from the contractive
section 63 and of which the diameter increases again as it goes away from the propeller,
so the diameter increases from the end of the propeller to a predetermined portion,
but increases again at the rear end portion of the propeller cap, which is the same
as the third embodiment shown in FIG. 5.
[0092] However, in the combined propeller cap 60 according to the fourth embodiment of the
present invention, the contractive section 63 is not straight as in the third embodiment
shown in FIG. 5, but is curved with a predetermined curvature.
[0093] That is, the combined propeller cap 60 according to the fourth embodiment of the
present invention is characterized in that the contractive section 63 is curved to
be convex outwardly with a predetermined curvature, as shown in FIG. 6a, or is curved
to be convex inwardly with a predetermined curvature, as shown in FIG. 6b.
[0094] The curvature of the contractive section 63 can be appropriately determined, depending
on the type or the use of a propeller or a ship, and other parts are the same as those
in the third embodiment, so they are not described in detail.
[0095] Therefore, according to this configuration, it is possible to not only reduce hub
vortex cavitation with a simple configuration, but further improve propulsive efficiency
in comparison to propeller caps in the related art.
[0096] In more detail, referring to FIG. 7, shown is a view comparing efficiency of a propeller
equipped with a propeller cap of the related art and a propeller equipped with the
combined propeller caps 50 and 60 according to the third and fourth embodiments of
the present invention shown in FIGS. 5 and 6.
[0097] That is, it can be seen from FIG. 7 that the efficiency of the propellers equipped
with the propeller caps 50 and 60 according to embodiments of the present invention
was improved, as compared with the existing contraction type propeller cap and the
diffusion type propeller cap.
[0098] As described above, according to the combined propeller caps 50 and 60 of the third
and fourth embodiments of the present invention, since the first diffusive sections
51 and 61 are formed such that the front potions of the propeller caps are convexly
formed, the pressure at the pressure side of a propeller increases and the propulsive
efficiency is improved. Further, the propulsive efficiency is further improved by
pressure recovery due to the shapes of the contractive sections 53 and 63 at the middle
portions.
[0099] Further, as a strong rotational flow (vortex) is weakened by the second diffusive
sections 54 and 64 while the flow from the propeller passes over the diffusive cap
end, hub vortex cavitation can be reduced, the propulsive efficiency of a vessel can
be improved about 1 ∼ 3% in comparison to the existing diffusion type propeller, vibration
and noise due to hub vortex cavitation can be reduced, and erosion and corrosion of
a rudder can be prevented in comparison to the existing contraction type propeller
caps.
[0100] That is, according to the configuration of the combined propeller caps 50 and 60
of the third and fourth embodiments of the present invention described above, there
is an advantage that it is possible to reduce hub vortex cavitation, similar to the
existing diffusion type propeller caps used for container ships, and it is possible
to improve propulsive efficiency in comparison to the existing diffusion type propeller
cap. Further, there is another advantage that it is possible to obtain propulsive
efficiency similar to the contraction type propeller caps when it is applied to tank
ships, but it is possible to greatly reduce hub vortex cavitation.
[0101] Further, since the shapes of the combined propeller caps 50 and 60 of the third and
fourth embodiments of the present invention described above are simple in structure,
they can be easily manufactured, so there is also an advantage that it is possible
to remarkably decrease the manufacturing cost, which was over one hundred million
South Korean won due to precise machining of the fins of the PBCF in the related art,
to within thirty million South Korean won similar to the existing propeller caps.
[0102] Further, referring to FIG. 8, FIG. 8 is a view schematically showing the entire configuration
of a combined propeller cap 80 according to a fifth embodiment of the present invention.
[0103] In more detail, as shown in FIG. 8, the combined propeller cap 80 according to the
fifth embodiment of the present invention has a contractive section 81 of which the
diameter decreases as it goes away from a propeller, a diffusive section 82 that extends
from the contractive section 81 and of which the diameter increases as it goes away
from the propeller, and a plurality of guide fins 83 that is formed in a thin plate
shape having a rectangular or curved cross-section with a predetermined uniform thickness
and is disposed with regular intervals between the contractive section 81 and the
diffusive section 82.
[0104] That is, in the combined propeller cap 80 according to the fifth embodiment of the
present invention, as shown in FIG. 8, the diameter gradually decreases from the end
of a propeller and increases again at the rear end portion, in which the guide fins
83 having a triangular plate shape are added at the contractive section 81 or between
the contractive section 81 and the diffusive section 82 of the propeller cap 80.
[0105] In this configuration, the inclination angle α of the contractive section 81 may
be, for example, set to 0 ∼40°, and when the inclination angle of the contractive
section 81 exceeds 40 degrees, the performance rapidly drops due to flow separation.
Further, when flow separation is generated, pressure is not recovered on the propeller
cap, so resistance increases.
[0106] In more detail, referring to the following Table 3, Table 3 shows changes in performance
due to changes in the inclination angle α of the contractive section 82.
[Table 3]
Angle (α) |
10 |
20 |
30 |
40 |
50 |
60 |
Performance change (%) |
+1.2 |
+1.2 |
+1.1 |
+0.9 |
+0.3 |
+0.2 |
[0107] The result in Table 3 shows estimated values of propulsive performance according
to changes in the inclination angle α of the contractive section 82, as compared with
a propeller equipped with a diffusion type propeller cap of the related art.
[0108] Accordingly, as the propeller cap is formed in a shape of which the diameter decreases
and increases again, when a propeller is operated, pressure is recovered and propulsive
efficiency is improved by the shape of which the diameter decreases to the contractive
section 81 at the middle portion of the propeller cap 80 and a strong rotational flow
(vortex) is weakened by the shape of which the diameter increases over the diffusive
section 82 at the end of the propeller cap 80, whereby it is possible to reduce hub
vortex cavitation.
[0109] Further, energy loss due to hub vortex is prevented accordingly, so the propulsive
efficiency can be improved in comparison to the existing diffusion type propellers,
vibration and noise due to hub vortex cavitation can be reduced, and erosion and corrosion
of a rudder can be prevented in comparison to the existing contraction type propeller
cap.
[0110] Further, the guide fins 83, as shown in FIG. 8, for example, are formed in a thin
triangular plate shape to be fitted in the recession between the contractive section
81 and the diffusive section 82 of the propeller cap 80 and attached with regular
intervals simply by welding. Accordingly, a vortex induced by rotation of a propeller
not only weakens over the diffusive section 82, but weakens in advance before the
diffusive section 82 of the propeller cap 30, so the vortex due to the rotation of
the propeller changes into a straight flow in the rotational axial direction, whereby
hub vortex cavitation can be additionally reduced.
[0111] The number of the guide fins 83 may be appropriately changed, for example, within
2 ∼ 8 and the size of the guide fins may be determined in accordance with the diameter
of the diffusive section 82 to avoid an increase in resistance due to the guide fins.
[0112] Further, the guide fins 83 are attached with a manufacturing tolerance of +20 ∼ -20
degrees, preferably +10 ∼ -10 degrees with respect to 0 degree when seen from vertically
above.
[0113] In more detail, according to the propeller cap 80 of the fifth embodiment of the
present invention, the propulsive efficiency is improved by pressure recovery due
to the shape from the propeller to the contractive section 81 at the middle portion
and a strong rotational flow (vortex) is weakened by the diffusive section 82 while
a flow from the propeller passes over the diffusive cap end, so hub vortex cavitation
can be reduced. Further, since the guide fins 83 having a triangular plate shape are
attached between the contractive section 81 and the diffusive section 82 of the propeller
cap 80, as described above, a vortex induced by rotation of the propeller is weakened
by the guide fins 83 before it reaches the diffusive section 82 of the propeller cap
80, so the vortex by the rotation of the propeller is changed into a straight flow
in the rotational axial direction, whereby hub vortex cavitation can be further reduced,
thus rotational flow and hub vortex cavitation by rotation of the propeller both can
be reduced. Accordingly, energy loss due to hub vortex is prevented, so the propulsive
efficiency of a vessel can be improved about 1 ∼ 3% in comparison to the existing
diffusion type propellers, vibration and noise due to hub vortex cavitation can be
reduced, and erosion and corrosion of a rudder can be prevented in comparison to the
existing contraction type propeller caps.
[0114] That is, according to the principle of the combined propeller cap 80 of the fifth
embodiment of the present invention having the configuration described above, the
propulsive efficiency is improved by pressure recovery from the propeller to the contractive
section 81 at the middle portion by the shape and a strong rotational flow (vortex)
is weakened by the diffusive section 82 while the flow generated by the propeller
flows over the end of the cap, so hub vortex cavitation is reduced. Further, since
the guide fins 83 having a plate shape are attached between the contractive section
81 and the diffusive section 82 of the propeller cap 80, the vortex induced by rotation
of the propeller is weakened by the guide fins 83 before reaching the diffusive section
82 of the propeller cap 80, so the vortex by the rotation of the propeller is changed
into a straight flow in the rotational axial direction, thus rotational flow and hub
vortex cavitation can be reduced.
[0115] Therefore, according to the combined propeller cap 80 of the fifth embodiment of
the present invention having the configuration described above, not only hub vortex
cavitation is reduced by the diffusive section 82 of the propeller cap 80, but the
vortex induced by rotation of a propeller is slightly weakened by the guide fins 83
before reaching the diffusive section 82 of the propeller cap 80, thereby changing
the vortex by the rotation of the propeller into a straight flow in the rotational
axial direction, so hub vortex cavitation can be additionally reduced. Accordingly,
it is possible to improve propulsive efficiency by preventing energy loss due to hub
vortex, reduce vibration and noise due to hub vortex cavitation, and prevent erosion
and corrosion of a rudder.
[0116] Further, since the combined propeller cap 80 according to the fifth embodiment of
the present invention having the configuration described above has a very simple shape
and structure and, the guide fins 83 are formed in a simple plate shape, so they can
be easily manufactured and attached by simple welding, it is possible to considerably
decrease the high manufacturing cost due to precise machining of the fins of a PBCF
in the related art.
[0117] In more detail, referring to FIG. 9, shown is a view comparing propulsive efficiency
of a propeller equipped with a propeller cap of the related art and a propeller equipped
with the combined propeller cap 80 according to the fifth embodiment of the present
invention shown in FIG. 8.
[0118] That is, it can be seen from FIG. 9 that the propeller equipped with the propeller
cap 80 according to the fifth embodiment of the present invention had propulsive efficiency
higher than that of the contraction type propeller of the related art and side effects
due to hub vortex can be greatly reduced and, the propulsive efficiency was considerably
improved as compared with the diffusion type propeller cap.
[0119] That is, according to the propeller cap 80 of the fifth embodiment of the present
invention, the propulsive efficiency is improved by pressure recovery due to the shape
from the propeller to the contractive section 81 at the middle portion and a strong
rotational flow (vortex) is weakened by the diffusive section 82 while a flow from
the propeller flows over the diffusive cap end, so hub vortex cavitation can be reduced.
Further, since the guide fins 83 having a triangular plate shape are attached between
the contractive section 81 and the diffusive section 82 of the propeller cap 80, as
described above, a vortex induced by rotation of the propeller is weakened by the
guide fins 23 before it reaches the diffusive section 82 of the propeller cap 80,
so the vortex by the rotation of the propeller is changed into a straight flow in
the rotational axial direction, whereby hub vortex cavitation can be further reduced,
thus rotational flow and hub vortex cavitation by rotation of the propeller both can
be reduced. Accordingly, energy loss due to hub vortex is prevented, so the propulsive
efficiency of a vessel can be improved about 1 ∼ 3% in comparison to the existing
diffusion type propellers, vibration and noise due to hub vortex cavitation can be
reduced, and erosion and corrosion of a rudder can be prevented in comparison to the
existing contraction type propeller caps.
[0120] That is, according to the configuration of the propeller cap 80 of the fifth embodiment
of the present invention, similar to diffusion type propeller caps that are used container
ships in the related art, hub vortex cavitation can be reduced and the propulsive
efficiency is greatly improved as compared with the diffusion type propeller caps
of the related art. Further, the propulsive efficiency is high and hub vortex cavitation
can be remarkably reduced in comparison to the existing contraction type propeller
caps when the propeller cap 80 is applied to tank ships. Further, as described above,
since the guide fins 83 having a triangular plate shape are attached between the contractive
section 81 and the diffusive section 82 of the propeller cap 80, rotational flow and
hub vortex cavitation are additionally reduced, so vibration and noise due to hub
vortex cavitation can be reduced and erosion and corrosion of a rudder can be prevented.
[0121] Further, precise machining for manufacturing the fins of a PBCF was a problem because
it increased the manufacturing cost, but the propeller cap 80 according to the fifth
embodiment of the present invention can be easily manufactured in simple shape and
structure, so there is also an advantage that it is possible to remarkably decrease
the manufacturing cost, which was over one hundred million South Korean won due to
precise machining of the fins of the PBCF in the related art, to within thirty million
South Korean won similar to the existing propeller caps.
[0122] Further, referring to FIG. 10, shown is a view schematically showing the entire configuration
of a combined propeller cap 100 according to a sixth embodiment of the present invention.
[0123] In the following description of the sixth embodiment of the present invention, the
same or similar components as in the fifth embodiment are not described and only other
different components are described for simple description.
[0124] That is, as shown in FIG. 10, the combined propeller cap 100 according to the sixth
embodiment of the present invention has a contractive section 101 of which the diameter
decreases as it goes away from a propeller, a diffusive section 102 that extends from
the contractive section 101 and of which the diameter increases as it goes away from
the propeller, and guide fins 103 that are attached between the contractive section
101 and the diffusive section 102, which is the same as the fifth embodiment shown
in FIG. 8.
[0125] However, in the combined propeller cap 100 according to the sixth embodiment of the
present invention, the contractive section 101 is not straight as in the fifth embodiment
shown in FIG. 8, but is curved with a predetermined curvature.
[0126] That is, the combined propeller cap 100 according to the sixth embodiment of the
present invention is characterized in that the contractive section 101 is curved to
be convex outwardly with a predetermined curvature, as shown in FIG.10a, or the contractive
section 101 is curved to be convex inwardly with a predetermined curvature, as shown
in FIG. 10b.
[0127] The curvature of the contractive section 101 can be appropriately determined, depending
on the type or the use of a propeller or a ship, and other parts are the same as those
in the fifth embodiment, so they are not described in detail.
[0128] Further, a combined propeller cap according to a seventh embodiment of the present
invention is described with reference to FIG. 11.
[0129] That is, referring to FIG. 11, shown is a view schematically showing the entire configuration
of a combined propeller cap 110 according to the seventh embodiment of the present
invention.
[0130] In detail, as shown in FIG. 11, the combined propeller cap 110 according to the seventh
embodiment of the present invention has a first diffusive section 111 of which the
diameter increases from the end of a propeller, a straight section 112 that horizontally
extends from the first diffusive section 111, a contractive section 113 that extends
from the straight section 112 and of which the diameter decreases as it goes away
from the propeller, a second diffusive section 114 that extends from the contractive
section 113 and of which the diameter increases again as it goes away from the propeller,
and a plurality of guide fins 115 that is formed in a thin plate shape and disposed
with regular intervals between the contractive section 113 and the second diffusive
section 114.
[0131] That is, in the combined propeller cap 110 according to the seventh embodiment of
the present invention, as shown in FIG. 11, the diameter first gradually increases
and decreases from the end of a propeller to a predetermined portion and then increases
again at the rear end portion, in which the guide fins 115 having a triangular plate
shape are added between the contractive section 113 and the second diffusive section
114 of the propeller cap 110.
[0132] The inclination angle α and β of the first diffusive section 111 and the contractive
section 113 respectively, may be set, for example, to 0 ∼ 40°.
[0133] When α and β exceed 40 degrees, the performance rapidly drops due to flow separation,
that is, when flow separation is generated, pressure is not recovered on the propeller
cap, so resistance increases.
[0134] In more detail, referring to the following Table 4, Table 4 shows changes in performance
due to changes in the inclination angles α and β of the first diffusive section 111
and the contractive section 113.
[Table 4]
Angle (α) |
10 |
20 |
30 |
40 |
50 |
60 |
Performance change (%) |
+1.3 |
+1.3 |
+1.3 |
+1.2 |
+0.9 |
+0.9 |
Angle (β) |
10 |
20 |
30 |
40 |
50 |
60 |
Performance change (%) |
+1.3 |
+1.3 |
+1.3 |
+1.0 |
+0.4 |
+0.4 |
[0135] In Table 4, when α was changed, β was fixed at 30 degrees, while when β was changed,
α was fixed at 30 degrees. Further, the result in Table 4 shows estimated values of
propulsive performance according to angle changes, as compared with a propeller equipped
with an existing diffusion type propeller cap.
[0136] Therefore, according to the combined propeller cap 110 of the seventh embodiment
of the present invention, as shown in FIG. 11, since the front potion of the propeller
cap is convexly formed by the first diffusive section 111, the pressure at the pressure
side of a propeller increases and the propulsive efficiency is improved. Further,
the propulsive efficiency is further improved by pressure recovery due to the shape
of the contractive sections113 at the middle portion.
[0137] Further, the combined propeller cap 110 according to the seventh embodiment of the
present invention is additionally improved in propulsive efficiency by pressure recovery
due to the shape from the propeller to the contractive section 113 at the middle portion,
as shown in FIG. 11, and can reduce hub vortex cavitation by decreasing a strong rotational
flow (vortex) through the second diffusive section 114 while the flow from the propeller
passes over the end of the diffusive cap.
[0138] Further, energy loss due to hub vortex is prevented accordingly, so the propulsive
efficiency of a vessel can be improved about 1 ∼ 3% in comparison to existing diffusion
type propellers, vibration and noise due to hub vortex cavitation can be reduced,
and erosion and corrosion of a rudder can be prevented in comparison to the existing
contraction type propeller caps.
[0139] Further, the guide fins 115, as shown in FIG. 11, for example, are formed in a thin
triangular plate shape to be fitted in the recession between the contractive section
113 and the second diffusive section 2 of the propeller cap 110 and attached with
regular intervals simply by welding. Accordingly, a vortex induced by rotation of
a propeller not only weakens over the second diffusive section 114, but weakens in
advance before the second diffusive section 114 of the propeller cap 110, so the vortex
due to the rotation of the propeller changes into a straight flow in the rotational
axial direction, whereby hub vortex cavitation can be additionally reduced.
[0140] The number of the guide fins 115 may be appropriately changed, for example, within
2 ∼ 8 and the size of the guide fins may be determined in accordance with the diameter
of the second diffusive section 114 to avoid an increase in resistance due to the
guide fins.
[0141] Further, the guide fins 115 are attached with a manufacturing tolerance of +20 ∼
-20 degrees, preferably +10 ∼ -10 degrees with respect to 0 degree when seen from
vertically above.
[0142] In more detail, according to the principle of the propeller cap 110 for reducing
a rotational flow and hub vortex and improving propulsive efficiency of the seventh
embodiment of the present invention, the propulsive efficiency is improved by pressure
recovery due to the shape from the propeller to the contractive section 113 at the
middle portion and a strong rotational flow (vortex) is weakened by the second diffusive
section 114 while a flow from the propeller passes over the diffusive cap end, so
hub vortex can be reduced. Further, since the guide fins 115 having a triangular plate
shape are attached between the contractive section 113 and the second diffusive section
114 of the propeller cap 110, as described above, a vortex induced by rotation of
the propeller is weakened by the guide fins 115 before it reaches the second diffusive
section 114 of the propeller cap 110, so the vortex by the rotation of the propeller
is changed into a straight flow in the rotational axial direction, whereby hub vortex
cavitation can be further reduced, thus rotational flow and hub vortex cavitation
by rotation of the propeller both can be reduced. Accordingly, energy loss due to
hub vortex is prevented, so the propulsive efficiency of a vessel can be improved
about 1 ∼ 3% in comparison to the existing diffusion type propellers, vibration and
noise due to hub vortex cavitation can be reduced, and erosion and corrosion of a
rudder can be prevented in comparison to the existing contraction type propeller caps.
[0143] That is, according to the principle of the combined propeller cap 110 of the seventh
embodiment of the present invention having the configuration described above, the
propulsive efficiency is improved by pressure recovery from the propeller to the contractive
section 113 at the middle portion by the shape and a strong rotational flow (vortex)
is weakened by the second diffusive section 114 while the flow generated by the propeller
flows over the end of the cap, so hub vortex is reduced. Further, since the guide
fins 115 having a triangular plate shape are attached between the contractive section
113 and the second diffusive section 114 of the propeller cap 110, the vortex induced
by rotation of the propeller is weakened by the guide fins 115 before reaching the
second diffusive section 114 of the propeller cap 110, so the vortex by the rotation
of the propeller is changed into a straight flow in the rotational axial direction,
thus rotational flow and hub vortex cavitation can be reduced.
[0144] Therefore, according to the combined propeller cap 110 of the seventh embodiment
of the present invention having the configuration described above, not only hub vortex
cavitation is reduced by the second diffusive section 114 of the propeller cap 110,
but the vortex induced by rotation of a propeller is slightly weakened by the guide
fins 115 before reaching the second diffusive section 114 of the propeller cap 110,
thereby changing the vortex by the rotation of the propeller into a straight flow
in the rotational axial direction, so hub vortex cavitation can be additionally reduced.
Accordingly, it is possible to improve propulsive efficiency by preventing energy
loss due to hub vortex, reduce vibration and noise due to hub vortex cavitation, and
prevent erosion and corrosion of a rudder.
[0145] Further, since the combined propeller cap 110 according to the seventh embodiment
of the present invention having the configuration described above has a very simple
shape and structure and, the guide fins 115 are formed in a simple plate shape, so
they can be easily manufactured and attached by simple welding, it is possible to
considerably decrease the high manufacturing cost due to precise machining of the
fins of a PBCF in the related art.
[0146] Further, referring to FIG. 12, shown is a view comparing efficiency of a propeller
equipped with a propeller cap of the related art and a propeller equipped with the
combined propeller cap according to the seventh embodiment of the present invention
shown in FIG. 11.
[0147] That is, it can be seen from FIG. 12 that the propeller equipped with the propeller
cap 110 according to the seventh embodiment of the present invention had propulsive
efficiency higher than that of the contraction type propeller cap of the related art
and side effects due to hub vortex can be greatly reduced and, the propulsive efficiency
was considerably improved as compared with the diffusion type propeller cap.
[0148] That is, according to the combined propeller cap 110 of the seventh embodiment of
the present invention, since the first diffusive section 111 is formed such that the
front potion of the propeller cap is convexly formed, the pressure at the pressure
side of a propeller increases and the propulsive efficiency is improved. Further,
the propulsive efficiency is further improved by pressure recovery due to the shapes
of the contractive section 113 at the middle portion.
[0149] Further, since the strong rotational flow (vortex) is weakened by the second diffusive
section 114 while the flow from the propeller passes the diffusive cap end, hub vortex
cavitation can be reduced. Further, as described above, since the guide fins 115 having
a triangular plate shape are attached between the contractive section 113 and the
second diffusive section 114 of the propeller cap 110, as described above, rotational
flow and hub vortex cavitation can be additionally reduced. Accordingly, energy loss
due to hub vortex is prevented, the propulsive efficiency can be improved about 1
∼ 3% in comparison to the existing diffusion type propellers, vibration and noise
due to hub vortex cavitation can be reduced, and erosion and corrosion of a rudder
can be prevented in comparison to the existing contraction type propeller caps.
[0150] That is, according to the configuration of the combined propeller cap 110 of the
seventh embodiment of the present invention, similar to diffusion type propeller caps
that are used container ships in the related art, hub vortex cavitation can be reduced
and the propulsive efficiency can be improved as compared with the diffusion type
propeller caps of the related art. Further, the propulsive efficiency is similar and
hub vortex cavitation can be remarkably reduced in comparison to the existing contraction
type propeller caps when the propeller cap 110 is applied to tank ships. Further,
as described above, since the guide fins 115 having a triangular plate shape are attached
between the contractive section 113 and the second diffusive section 114 of the propeller
cap 110, rotational flow and hub vortex cavitation are additionally reduced, so vibration
and noise due to hub vortex cavitation can be reduced and erosion and corrosion of
a rudder can be prevented.
[0151] Further, precise machining for manufacturing the fins of a PBCF was a problem because
it increased the manufacturing cost, but the combined propeller cap 110 according
to the seventh embodiment of the present invention can be easily manufactured in simple
shape and structure, so there is also an advantage that it is possible to remarkably
decrease the manufacturing cost, which was over one hundred million South Korean won
due to precise machining of the fins of the PBCF in the related art, to within thirty
million South Korean won similar to the existing propeller caps.
[0152] Further, referring to FIG. 13, shown is a view schematically showing the entire configuration
of a combined propeller cap 130 according to an eighth embodiment of the present invention.
[0153] That is, as shown in FIG. 13, the combined propeller cap 130 according to the eighth
embodiment of the present invention has a first diffusive section 131 of which the
diameter increases from the end of a propeller, a straight section 132 that horizontally
extends from the first diffusive section 131, a contractive section 133 that extends
from the straight section 132 and of which the diameter decreases as it goes away
from the propeller, a second diffusive section 134 that extends from the contractive
section 133 and of which the diameter increases again as it goes away from the propeller,
and guide fins 135 that are coupled to an end of the second diffusive section 134,
which is the same as the seventh embodiment shown in FIG. 11.
[0154] However, in the combined propeller cap 130 according to the eighth embodiment of
the present invention, the contractive section 133 is not straight as in the seventh
embodiment shown in FIG. 11, but is curved with a predetermined curvature.
[0155] That is, the combined propeller cap 130 according to the eight embodiment of the
present invention is characterized in that the contractive section 133 is curved to
be convex outwardly with a predetermined curvature, as shown in FIG. 13a, or the contractive
section 133 is curved to be convex inwardly with a predetermined curvature, as shown
in FIG. 13b.
[0156] The curvature of the contractive section 133 can be appropriately determined, depending
on the type or the use of a propeller or a ship, and other parts are the same as those
in the seventh embodiment, so they are not described in detail.
[0157] Further, referring to FIGS. 14 and 15, FIG. 14 is a view schematically showing the
entire configuration of a combined propeller cap according to a ninth embodiment of
the present invention and FIG. 15 is a view schematically showing the entire configuration
of a combined propeller cap according to a tenth embodiment of the present invention.
[0158] In detail, although the guide fins are formed in a triangular shape and attached
in the recession between the contractive section and the diffusive section, and have
a size corresponding to the diameter of the diffusive section in order not to protrude
at the end of the diffusive section in the fifth to eighth embodiments of the present
invention, the present invention is not limited to this configuration, that is, the
present invention may be configured, as shown in FIG. 14, such that guide fins 143
are formed in a not triangular, but thin pentagonal plate shape are attached by simple
welding between the contractive section 141 and the diffusive section 143 of the propeller
cap 140 to extend from an end of the diffusive section 142.
[0159] In this configuration, the size of the guide fins 143 may be determined such that
the length L of the portion extending from the end of the diffusive section 142 is
within two times the diameter D of the diffusive section (that is, L ≤ 2D).
[0160] Alternatively, the present invention may be configured, as shown in FIG. 15, such
that guide fins 153 are formed in a thin trapezoidal shape and attached to a contractive
section 151 of a propeller cap 150 by simple welding.
[0161] In this configuration, the size of the guide fins 153 may be determined such that
the length L2 of a shorter portion of the portions extending from the side of the
contractive section 151 is within two times the diameter of the diffusive section
152 (that is, L2 ≤ 2D), but other factors L1 and W are not specifically limited.
[0162] Further, the other configurations except the guide fins 143 and 153 can be achieved
in the same way as the fifth to eighth embodiments, so they are not described in detail.
[0163] Examples of applying the guide fins 143 and 153 to the propeller cap according to
the first embodiment shown in FIG. 2 are shown in FIGS. 14 and 15, but the present
invention is not limited thereto, that is, it should be noted that the guide fins
143 and 153 shown in FIGS. 14 and 15 can be applied in the same way not only to the
first embodiment shown in FIG. 2, but to the second to fourth embodiments.
[0164] Further, referring to FIG. 16, shown is a view comparing propulsion, torque, and
efficiency of a propeller equipped with a propeller cap of the related art and a propeller
equipped with the combined propeller cap 140 according to the ninth embodiment of
the present invention shown in FIG. 14.
[0165] That is, it can be seen from FIG. 16 that the propeller equipped with the propeller
cap 140 according to the ninth embodiment of the present invention had propulsive
efficiency higher than that of the contraction type propeller cap of the related art
and side effects due to hub vortex can be greatly reduced and, the propulsive efficiency
was considerably improved as compared with the diffusion type propeller cap. Further,
it can be seen that the propulsive efficiency was improve as compared with the first,
fifth, and seventh embodiments too.
[0166] Therefore, according to the configuration, it is possible to achieve a combined propeller
cap for reducing rotational flow and hub vortex and improving propulsive efficiency
according to the present invention.
[0167] Further, according to the present invention, as a combined propeller cap for reducing
rotational flow and hub vortex and improving propulsive efficiency according to the
present invention is achieved, it is possible to reduce hub vortex cavitation that
is generated behind a propeller through a combined propeller cap structure in which
a diffusion type propeller cap is coupled to the end of a contraction type propeller
cap, so a combined propeller cap that can be easily manufactured at a low cost in
a simple configuration, as compared with the existing PBCF, for reducing rotational
flow and hub vortex and improving propulsive efficiency. Further, a plurality of small
fins is attached to the propeller cap to reduce hub vortex cavitation, so it is possible
to solve the problem with the existing PBCF (Propeller Boss Cap Fin) in that manufacturing
is difficult and the manufacturing cost is high due to precise machining for designing
and manufacturing fins.
[0168] Further, according to the present invention, as described above, there is provided
a combined propeller cap for reducing rotational flow and hub vortex and improving
propulsive efficiency that is configured not only to reduce hub vortex cavitation
that is generated behind a propeller through a combined propeller cap structure in
which a diffusion type propeller cap is coupled to the end of a contraction type propeller
cap, but also to additionally reduce hub vortex cavitation by attaching plate-shaped
guide fins to the contractive section or between the contractive section and the diffusive
section of the propeller cap. Accordingly, it is possible to reduce rotational flow
and hub vortex cavitation that are generated behind a propeller, to easily manufacture
the propeller cap at a low cost in a simple configuration, as compared with the existing
PBCF, to reduce noise and vibration in a vessel and prevent erosion and corrosion
of a rudder, and to save fuel by improving propulsive efficiency
[0169] Although combined propeller caps for reducing rotational flow and hub vortex and
improving propulsive efficiency according to embodiments of the present invention
were described above, the present invention is not limited to the embodiments and
may be changed, modified, combined, and replaced in various ways, depending on necessities
in design and other various factors by those skilled in the art.
<Description of the Reference Numerals in the Drawings>
20: Propeller cap |
21: Contractive section |
22: Diffusive section |
30: Propeller cap |
31: Contractive section |
32: Diffusive section |
50: Propeller cap |
51: First diffusive section |
52: Straight section |
53: Contractive section |
54: Second diffusive section |
60: Propeller cap |
61: First diffusive section |
62: Straight section |
63: Contractive section |
64: Second diffusive section |
80: Propeller cap |
81: Contractive section |
82: Diffusive section |
83: Guide fin |
100: Propeller cap |
101: Contractive section |
102: Diffusive section |
103: Guide fin |
110: Propeller cap |
111: First diffusive section |
112: Straight section |
113: Contractive section |
114: Second diffusive section |
115: Guide fin |
130: Propeller cap |
131: First diffusive section |
132: Straight section |
133: Contractive section |
134: Second diffusive section |
135: Guide fin |
140: Propeller cap |
141: Contractive section |
142: Diffusive section |
143: Guide fin |
150: Propeller cap |
151: Contractive section |
152: Diffusive section |
153: Guide fin |
1. A combined propeller cap for reducing rotational flow and hub vortex and improving
propulsive efficiency, the combined propeller cap having:
a contractive section having a diameter that decreases as it goes away from a propeller;
and
a diffusive section extending from the contractive section and having a diameter that
increases as it goes away from the propeller,
wherein pressure of a flow from the propeller is recovered by the shape of the contractive
section having the decreasing diameter, so propulsive efficiency is improved, and
rotational flow (vortex) is weakened by the shape of the diffusive section having
the increasing diameter at an end of the propeller cap.
2. The combined propeller cap of claim 1, wherein an inclination angle of the contractive
section is set to 0 ~ 40°.
3. The combined propeller cap of claim 1, wherein a side of the contractive section is
formed straight, or
the side of the contractive section is curved to be convex outwardly with a predetermined
curvature, or
the side of the contractive section is curved to be convex inwardly with a predetermined
curvature.
4. A combined propeller cap for reducing rotational flow and hub vortex and improving
propulsive efficiency, the combined propeller cap has:
a first diffusive section having a diameter that increases from an end of a propeller
as it goes toward the propeller;
a straight section horizontally extending from the first diffusive section;
a contractive section extending from the straight section and having a diameter that
decreases as it goes away from the propeller; and
a second diffusive section extending from the contractive section and having a diameter
that increases as it goes away from the propeller,
wherein the combined propeller cap is convexly formed at a front portion by the first
diffusive section, so pressure at a pressure side of the propeller increases and propulsive
efficiency is improved,
pressure of a flow passing the propeller cap from the propeller is recovered by the
contractive section, so the propulsive efficiency is improved, and
rotational flow (vortex) of a flow from the propeller is weakened by the second diffusive
section, so hub vortex cavitation is reduced.
5. The combined propeller cap of claim 4, wherein inclination angles of the first diffusive
section and the second diffusive section are set to 0 ~ 40°.
6. The combined propeller cap of claim 4, wherein a side of the contractive section is
formed straight, or
the side of the contractive section is curved to be convex outwardly with a predetermined
curvature, or
the side of the contractive section is curved to be convex inwardly with a predetermined
curvature.
7. A combined propeller cap for reducing rotational flow and hub vortex and improving
propulsive efficiency, the combined propeller cap having:
a contractive section having a diameter that decreases as it goes away from a propeller;
a diffusive section extending from the contractive section and having a diameter that
increases as it goes away from the propeller; and
a plurality of guide fins formed in a thin plate shape having a rectangular or curved
cross-section with a predetermined uniform thickness and, disposed with regular intervals
at the contractive section or between the contractive section and the diffusive section,
wherein pressure of a flow from the propeller is recovered by the shape of the contractive
section having the decreasing diameter, so propulsive efficiency is improved,
rotational flow (vortex) is weakened by the shape of the diffusive section having
the increasing diameter at an end of the propeller cap, and
rotational flow by rotation of the propeller is changed into a straight flow in a
rotational axial direction, so the hub vortex cavitation is further reduced.
8. The propeller cap of claim 7, wherein an inclination angle of the contractive section
is set to 0 ~ 40°.
9. The combined propeller cap of claim 8, wherein a side of the contractive section is
formed straight, or
the side of the contractive section is curved to be convex outwardly with a predetermined
curvature, or
the side of the contractive section is curved to be convex inwardly with a predetermined
curvature.
10. The combined propeller cap of claim 9, wherein the guide fins are formed in a thin
rectangular plate shape and attached between the contractive section and the diffusive
section of the propeller cap by simple welding, and
a size of the guide fins is determined to correspond to the diameter of the diffusive
section in order to avoid an increase in resistance due to the guide fins.
11. The combined propeller cap of claim 9, wherein the guide fins are formed in a thin
pentagonal plate shape and attached between the contractive section and the diffusive
section of the propeller cap by simple welding, and
a length of a portion extending from an end of the diffusive section is within two
times the diameter of the diffusive section.
12. The combined propeller cap of claim 9, wherein the guide fins are formed in a thin
trapezoidal plate shape and attached between the contractive section and the diffusive
section of the propeller cap by simple welding, and
a length of a shorter portion of portions extending from a side of the contractive
section is within two times the diameter of the diffusive section.
13. The combined propeller cap of claim 9, wherein two to eight guide fins are disposed
at the contractive section or between the contractive section and the diffusive section
of the propeller cap, and
the guide fins are attached with a tolerance of +10 ~ - 10 degrees or +20 ~ -20 degrees
with respect to 0 degree when seen from vertically above.
14. A combined propeller cap for reducing rotational flow and hub vortex and improving
propulsive efficiency, the combined propeller cap having:
a first diffusive section having a diameter that increases from an end of a propeller
as it goes toward the propeller;
a straight section horizontally extending from the first diffusive section;
a contractive section extending from the straight section and having a diameter that
decreases as it goes away from the propeller;
a second diffusive section extending from the contractive section and having a diameter
that increases as it goes away from the propeller; and
a plurality of guide fins formed in a thin plate shape having a rectangular or curved
cross-section with a predetermined uniform thickness and, disposed with regular intervals
at the contractive section or between the contractive section and the diffusive section,
wherein the combined propeller cap is convexly formed at a front portion by the first
diffusive section, so pressure at a pressure side of the propeller increases and propulsive
efficiency is improved,
pressure of a flow passing the propeller cap from the propeller is recovered by the
contractive section, so the propulsive efficiency is improved,
rotational flow (vortex) of a flow from the propeller is weakened by the second diffusive
section, so hub vortex cavitation is reduced, and
rotational flow by rotation of the propeller is changed into a straight flow in a
rotational axial direction, so the hub vortex cavitation is further reduced.
15. The combined propeller cap of claim 14, wherein inclination angles of the first diffusive
section and the contractive section are set to 0 ~ 40°.
16. The combined propeller cap of claim 15, wherein a side of the contractive section
is formed straight, or
the side of the contractive section is curved to be convex outwardly with a predetermined
curvature, or
the side of the contractive section is curved to be convex inwardly with a predetermined
curvature.
17. The combined propeller cap of claim 16, wherein the guide fins are formed in a thin
rectangular plate shape and attached between the contractive section and the second
diffusive section of the propeller cap by simple welding, and
a size of the guide fins are determined to correspond to the diameter of the diffusive
section in order to avoid an increase in resistance due to the guide fins.
18. The combined propeller cap of claim 16, wherein the guide fins are formed in a thin
pentagonal plate shape and attached between the contractive section and the second
diffusive section of the propeller cap by simple welding, and
a length of a portion extending from an end of the second diffusive section is within
two times the diameter of the second diffusive section.
19. The combined propeller cap of claim 16, wherein the guide fins are formed in a thin
trapezoidal plate shape and attached between the contractive section and the diffusive
section of the propeller cap by simple welding, and
a length of a shorter portion of portions extending from a side of the contractive
section is within two times the diameter of the second diffusive section.
20. The combined propeller cap of claim 16, wherein two to eight guide fins are disposed
at the contractive section or between the contractive section and the second diffusive
section of the propeller cap, and
the guide fins are attached with a tolerance of +10 ~ - 10 degrees or +20 ~ -20 degrees
with respect to 0 degree when seen from vertically above.
21. A propeller for a vessel, which uses the combined propeller cap of any one of claims
1 to 20, wherein as compared with existing propellers, energy loss due to hub vortex
cavitation and a propeller cap shape is prevented and propulsive efficiency is improved,
vibration and noise are reduced, and erosion and corrosion of a rudder by the hub
vortex cavitation are prevented, and
in comparison to existing PBCFs, manufacturing cost is reduced.