[0001] The subject matter of this invention is a stern mounting structure for rudder, screw
propeller , and shafting, suitable for ship of any kind and use .This structure
is arranged abaft the screw propeller and substantially comprises an integral to
the hull, foil-shaped post which sustains the rudderstock and an integral to the post
boss which sustains the rudder heel and houses the last shafting bearing. Where a
controllable pitch propeller (CPP ) is used, the post houses the most of the pitch
control hydraulic devices in order to provide an apparatus wherein there are no rotating
members under hydraulic pressure .
[0002] The preliminary search results show that six patents could be considered in the discussion
of the present application. Comments showing the differences between them and the
present application can be made as following: Pat. n. US-A-2317196 is applicable only
to very small boats for the presence of a pivoted bearing at the rear end of the shaft,
and does not consider the possibility of disassembling the screw propeller without
moving all the shaft-line. Furthermore it does not consider controllable pitch propellers.
[0003] Pat. n. GB-A-446838 has the feature of varying the length of the cross section of
the stationary rudder member in order to approach the contour of the after edges of
the propeller blades; it does not take into account the disassembling of the screw
propeller and the possible installation of a controllable pitch propeller.
[0004] Pat. n. US-A-2931443 has a completely different structure of the rudder, it has under
pressure rotating members and does not consider the disassembling of the screw propeller.
[0005] Pat. n. FR-A-2044651 does not support the shaft with a bearing in its rear end, it
has under pressure rotating members, the rudder has a completely different hydraulic
motor, it does not consider the screw propeller disassembling.
[0006] Pat. n. WO-A-80/01373 has under pressure rotating members, it does not consider a
bearing at the rear end of the shaft, it does not consider the screw propeller disassembling.
[0007] Pat. n. FR-A-844151 has the main purpose to allow the rear bearing maintenance and
control from the inside of the hull and thus is not comparable with the present patent
application.
[0008] As it is well known to the naval architects, a great care must be taken in the propulsive
system design to the problem of the screw propeller-ship hull interaction in order
to match the screw characteristics to the hull form, particularly the stern body.
[0009] As regard as this problem , and in order to avoid large changes in the hydrodynamic
angle of attack on the blades sections, it is of paramount importance to achieve a
flow uniformity as high as possible in the propeller disk region. The flow uniformity
problem, and therefore the problem of achieving the higher propulsive system efficiency,related
thereto which is already present in the twin screw ships is of bigger importance in
the mono screw ships . This is due to the fact that the flow uniformity mainly depends
upon the presence of appendages protruding from the hull before the propeller disk
, and that the twin screw ships can be fitted either with simple strut, or strut and
brackets, etc., and generally they do not have the hull skeg before the propellers
. By using the traditional stern structures it is impossible to eliminate the flow
disuniformity due to the appendages, consequently, the main object of the invention
is to provide a new stern structure which allows to optimize the propeller disk in-flow
.
[0010] It is another object of the invention to provide such a structure which houses a
CPP pitch control device wherein no rotating members are under hydraulic pressure
.
[0011] Furthermore, it is another object of the invention to provide such a structure which
allows to reduce in size or eliminate the skeg, and thus obtaining a bigger net volume
in the aftbody.
[0012] These objects can be achieved by using this invention which :
- carries the screw propeller , therefore eliminating any shaft overhang ;
- sustains the rudderstock bending stress ;
- houses the devices and members of the CPP pitch control system,which accordingly
is simpler and more reliable .
[0013] Furthermore this invention is particularly suitable to reduce the cavitation phenomena
related to the flow disuniformity.
[0014] The applicant has also studied a non-symmetrical shaped post suitable for those special
cases wherein the cavitation phenomenon can occur over the post .
[0015] The invention will now be more particularly described with an embodiment thereaf
with an exclusively exemplifying and not limiting aim . This embodiment is suitable
for a mono screw ship fitted with an hydraulic CPP plant .
[0016] In the drawings :
Fig.1 shows a partial lateral view of a stern mounting structure according to the
invention .
Fig.2 is a section fragmentary showing in a larger scale, the stern mounting structure
of fig.1 with the rudderstock ,last shaft bearing, and a fixed pitch propeller (
FPP ) arrangement .
Fig.3 is a cutaway section on line III-III of fig .2.
Fig.4 shows perspective view of an alternative embodiment of the post which is suitable
to eliminate the cavitation phenomenon over it .
Fig.5 is a front view of the post of fig.4 .
Fig.6 is a detailed section showing the invention when applied to an hydraulically
operated CPP propulsive plant.
Fig.7 is a perspective view showing the blade position control plate of fig.6 .
Fig.8 is a fragmentary section along line VIII-VIII of fig.6 .
Fig.9 is a schematic view showing various positions of the blade eccentric-holder
slide .
Fig.10 is a sketch of the blade control equipment; which in this case is of the hydraulic
type .
[0017] Looking now at figures 1-3 they show the stern mounting structure comprising : a
foil shaped post 10, which is integral to the stern PP of the ship NV. This post has
a sikle-shaped outline to house the rudder blade and presents a boss 11 having an
overhanged aftbody 12 and an ogive-shaped fore body 13.
[0018] As it is clearly shown post 10 supports the rudderstock 14, the rudder heel 16 of
which is pivoted in the overhanged aft body 12 ; rudderstock 14 is partially housed
in the vertical groove 18 of post 10 .
[0019] The forebody 13 of boss 11 houses the last bearing 19 of the shafting 20. The boss
forebody 13 and the screw propeller hub 22 are sized and shaped in such a way to avoid
flow separation or vortices ; the same concept is valid for rudder 15 and post 10
.
[0020] Figures 4 and 5 show a variant stern mounting structure of the invention thus it
is suitable to eliminate cavitation phenomenon over the post. This structure also
allows mono screw ships to keep the course, eliminating the need of steering, thus
giving a further advantage to the overall efficiency of the ship.
[0021] In this second embodiment the side surfaces of the post, indicated by reference 10A
, are not symmetrically layed with respect to the ship symmetry plane, since they
have both a curved surface while boss 11A and the rudderstock maintain their central
position and rectilinear shape, respectively .
[0022] It can be useful to note that the arrangement shown is suitable for a counter clockwise
screw propeller .
[0023] Figures 6-10 show the invention as applied to a CPP plant for a monoscrew ship .
[0024] At present the hydraulic oil pipes for the CPP are housed inside the shaft line and
reach the hub from the main gear box. This arrangement makes it necessary to perform
very costly fine workings of the shaft line and involves the use of heavy and complicated
members under pressure which are in rotation.
[0025] This invention eliminates all the above mentioned draw backs as it allows to control
the blade position making use of devices which are all housed either in the propeller
hub or boss . The oil pipes , in the case of an hydraulic operated plant, arrive
to the screw boss through the post of the invention .
[0026] As it is shown, the pitch control device comprises substantially three sections
:
- a first section housed in the ship hull ; comprising the auxiliaries ;
- the second section, which is partially fitted inside post 110 and boss 111 and partially
fitted inside the hub ; this section comprising non-rotating members ;
- the third section, which is totally fitted inside hub 25 and comprises rotating
members .
[0027] The first section comprises :
- a high pressure oil pump 30,
- a high pressure oil storage chamber 31 ,
- a hydraulic circuit including a distributing valve 32 and remote controlled valves
33,
- an oil pressure regulating valve 34 ,
- a low pressure hydraulic circuit 37 .
[0028] The non-rotating section comprises :
- a double-acting hydraulic unit consisting of a cylinder 40 and a piston 41 ,
- a first operating disk 42 , that is fixed ,
- a second movable-operating disk 43 ,
- a low pressure hydraulic actuator, includind a first chamber 44, which is internal
to the piston 41, and a second chamber 45 which houses the forebody 46 of movable-operating
disk 43 .
[0029] Finally the rotating section comprises :
- a slidable plate 60 ( fig.8 ),
- eccentric-holder slides 61 ,
- rotating disk 62 .
[0030] Furthermore, two groves 64 are machined on the opposite sides of slidable plate 60,
which engage the slide-guides 75 machined on the hub .
[0031] From the foregoing it is easy to understand that all the pitch control system of
screw blades 70 does not rotate with the exception of slidable plate 60 , which is
positioned between the fixed operating disk 42 and movable operating disk 43. Between
slidable plate 60 and disks 42 and 43 , antifriction plain bearings 65 and 66 are
interposed .
[0032] Making use of the described arrangement it will happen that the position of piston
41 inside cylinder 40 will set the axial position of the slidable plate 60 trough
fixed disk 42 and movable disk 43 .
[0033] Furthermore an axial passage 47 is machined in piston 41 .This passage allows chamber
45 , at the end 48 of piston 41, to communicate the oil pressure to chamber 44 . That
is located between the end of drilled stem 49 and the housing thereaf which is in
the head 50 of the axial hole 47 .
[0034] Drilled stem 49 is integral to the bottom 53 of cylinder 40. With such arrangement
end chamber 45 communicates with chamber 44 trough passage 47 and then with low pressure
circuit 37 trough axial passage 54 of stem 49 .
[0035] Operation of the blades rotation is made in the following way :
the high pressure circuit, through distributing valve 32 and valves 33, controls the
position of piston 41 by means of oil chambers 55 and 56,located on the sides of head
50. The fixed-operating disk 42, which is integral to the piston 41, sets up the position
of slidable plate 60. This plate, through eccentric-holder slides 61 and eccentrics
67, which are integral to the rotating disk 62 ,ultimately controls the blade pitch,being
disk 62 bolted to the root 68 of screw blade 70 .(See figures 7,8,9) .The position
of fixed operating disk 42 is directly related to the position of piston 41 ; the
position of movable-operating disk 43, that can slide axially to piston 41 ,is set
up by the low pressure circuit action . This circuit comprises :
- oil storage chamber 35 ,
- pipe 37 ,
- passage 54 ,
- chamber 44 ,
- passage 47 ,
and chamber 45 .
[0036] With this arrangement disk 43 engages the plate 60 owing to the pressure in end chamber
45 .
[0037] The aims of the capability of sliding disk 43 are :
- to take up automatically the slack due to the wear of antifriction bearings 65 and
66 ,
- to maintain a low pressure engagement between antifriction bearing 66 and the slidable
plate 60. Bearings 77 and 78 are provided for guiding and supporting piston 41 . Stop
ring 80 , which slides in groove 81 , is mounted, at the end 79 of cylinder 40 , for
preventing piston 41 to rotate.
[0038] The embodiment shown and illustrated is designed for a four-bladed propeller having
the capability of the three positions :
- ahead ,
- astern ,
- feathering
and the intermediates ones of course .
[0039] In fig.9 are schematically shown the positions of one eccentric-holder slide 61 and
its eccentric 67 .
[0040] The positions are represented:
- ahead, with solid lines
- astern , with dashed lines
- feathering , with chain lines .
[0041] The shafting disassembly will be made by taking down the sections of the shaft line
from the stern , being the length TR of the shaft sections less than the clearance
between stern boss 73 and end 74 of the forebody 13 of boss 11 .
[0042] It has been shown how the invention provides a stern mounting structure which , by
using a new concept , allows the designer to achieve the target of increased efficiency
, lower cavitation ,simpler and cheaper construction .
[0043] It is intended that it is possible to modify and change in some way what has been
herein illustrated and described without altering the concepts and scope of the invention
.
[0044] Instead of the hydraulic type which has been thoroughly described , for example ,
it will be possible to install inside port 110 and boss 111 either a pneumatic or
a mechanic device to control the blades position .
1. A stern mounting structure located abaft the screw propeller ,for ship of any
kind and use ,characterized in that it comprises an integral to the hull foil-shaped
post and a boss ,integral to the post , which houses the last shafting bearing ,thus
eliminating any shaft overhang .
2. The stern mounting structure , of claim 1 , wherin said post houses the rudderstock
and supports the rudder heel.
3. The stern mounting structure of claim 2 , wherin said post has curved lateral surfaces
, while boss and rudderstock maintain their central position and rectilinear shape,
respectively.
4. The stern mounting structure ,of claim 1, particularly adapted to controllable
pitch propeller ships , wherin said post and boss house the devices and members of
the blades position control system, so that said devices and members have not to be
housed inside the shafting .
5.The stern mounting structure ,of claim 4, wherin the control system comprises :a
first section housed in the ship hull; a second non rotating section partially housed
in said propeller boss and partially in said hub, and a third rotating section which
is totally housed in said propeller hub .
6.The stern mounting structure , of claim 5,wherein control system is hydraulically
operated and wherein said first section comprises : a high pressure oil pump , a high
pressure oil storage chamber,a hydraulic circuit including a distributing valve and
remote-controlled valves, an oil pressure regulating valve ,an oil tank, a low pressure
oil storage chamber, a low pressure hydraulic circuit ;said second non rotating section
includes : a double acting hydraulic cylinder and piston unit ;a fixed-operating disk
and a movable-operating disk, a low pressure hydraulic actuator which includes a first
and a second chamber , said first chamber being internal to said piston, and said
second chamber being external thereto, and housing the end of said movable-operating
disk ;
said third rotating section comprises :
a squared sliding plate which rotates with the shaft and is positioned between said
operating disks ; more eccentric-holder slides,and pivotally mounted disks ,one for
each blade ,each mounting eccentric pin ;and wherein each of said pivotally mounted
disks is suitably connected to the respective blade root that is compelled to rotate
therewith.
7.The stern mounting structure , of claim 6 , wherein said fixed-operating disk is
integral to the piston , and said sliding-operating disk is allowed to slide axially
when operated by said low pressure oil circuit , so that the slack due to the wear
of the antifriction bearings is continously taken up.
8.The stern mounting structure ,of claim 1 , wherein said sliding plate presents a
pair of grooves machined therein which cooperate with slide-guides machined in said
hub ,in order to easily move axially thereto.