[0001] . The present invention relates to a marine contra-rotating propeller apparatus which
includes a stern-side propeller for propelling a ship and a bow-side propeller which
is rotated in the opposite direction to that of the stern-side propeller at the same
revolution speed as that of the stern-side propeller.
[0002] . A conventional marine contra-rotating propeller apparatus is now described, by
way of example, with reference to Fig. 1. The marine contra-rotating propellers are
composed of the combination of a stern-side propeller 1 and a bow-side propeller 2.
The torque delivered by a main diesel engine 7 is transmitted to a planetary gear
mechanism 5 through an elastic coupling 6 which eliminates any variation component
or vibration component of the torque. The torque transmitted to the planetary gear
mechanism 5 rotates an inner shaft 4 through a spur gear meshing with a planet gear
and the revolution of the planet gear is taken out from an outer shaft 3 so that the
outer shaft 3 is rotated in the opposite direction to that of the inner shaft 4 and
a substantially equal torque is transmitted to both the shafts 3 and 4. The propellers
1 and 2 are rotated in the opposite directions to each other at the substantially
same revolution speed depending on the design of a shape of the propellers. In other
words, the contra-rotating propellers are designed to be rotated in the opposite directions
to each other with the torque and the revolution speed being substantially equal and
with the high efficiency of propulsion.
[0003] . The thrust developed by the stern-side propeller 1 and the bow-side propeller 2
is transmitted through the inner shaft 4 and the outer shaft 3 to a ship body by means
of a thrust bearing 8. The elastic coupling 6 smooths the variation component of the
torque and serves to protect the gears of the planetary gear mechanism 5 for reversing
the revolution direction.
[0004] . However, while the conventional marine contra-rotating propeller apparatus is designed
so that the revolution directions of both the propellers are opposite and the revolution
speed and the torque are substantially equal in order to optimize the efficiency of
propulsion, the adoption of the planetary gear mechanism shown in the figure produces
the following drawbacks:
[0005] . I) If both the propellers 1 and 2 of the contra-rotating propeller apparatus are
rotated in the opposite directions to each other at the same revolution speed using
the planetary gear mechanism 5, the number of revolutions of the main diesel engine
is reduced (the reduction ratio is 3 or more) to be transmitted to the propellers.
Accordingly, if a low-speed diesel engine having an output shaft rotated at a low
revolution speed (for example, 70 revolutions/minute) is used, the revolution of the
propellers is reduced below a desired optimum revolution speed and the efficiency
of propulsion is deteriorated. If a middle-speed diesel engine having an output shaft
rotated at a relatively high revolution speed (for example, 450 revolutions/minute)
is used, it can not obtain the advantages of the low-speed diesel engine such as good
fuel consumption rate, easiness in maintenance and usability of bad quality fuel although
the revolution of the propellers can be set near a disired maximum revolution speed
and the improved efficiency of propulsion can be expected.
[0006] . Further, since the speed reduction ratio of the input side and the output side,
that is, the outer shaft 3 and the inner shaft 3 and the torque ratio of the outer
shaft 3 and the inner shaft 4 in the planetary gear mechanism 5 are related to each
other, it is necessary that the main diesel engine is provided at its output shaft
with a separate speed reduction or increase device to adjust the revolution of the
planetary gear mechanism at its input side so that the torque ratio is optimized.
(Since the main diesel engine possesses a rated output power and revolution speed,
a continuous revolution speed can not be selected.)
[0007] . II) Recently, a main engine in a large ship mainly uses a low-speed diesel engine
due to the above advantages. Since the low-speed engine is directly coupled to the
propeller through a shaft generally, the main engine contains a thrust bearing therein
in a standard configuration. If the planet gear is disposed between the main diesel
engine and the propeller, the thrust bearing is required to be provided between the
propeller and the planet gear. Consequently, the thrust bearing in the main engine
merely serves to stop the movement of a crank shaft of the main diesel engine and
the capacity thereof is vainly too large. (In Fig. 1, the thrust bearing 8 receives
the thrust of the propellers 1 and 2 while the thrust bearing (not shown) in the main
engine does not receive the thrust of the propellers.)
[0008] . Figs. 2 to 4 illustrate a propeller driving system of a ship equipped with a conventional
contra-rotating propeller apparatus using by way of example a parallel shaft gear
system.
[0009] . In Figs. 2 to 4, numeral 01 denotes a stern-side propeller, 02 a bow-side propeller,
03 an inner shaft for driving the stern-side propeller, 04 an outer shaft for driving
the bow-side propeller, 05 a parallel shaft gear device for driving the bow-side propeller,
06 a parallel shaft gear device for driving the stern-side propeller, and 07 a main
engine. One or more main engines 07 are used to transmit the torque to the inner shaft
03 and the outer shaft 04 to rotate them in the opposite directions through the parallel
shaft gear device. In Fig. 2, an idle gear 5a produces the inverse revolution. In
Figs. 3 and 4, the revolution direction of each main engine 07 which transmits the
torque to the inner shaft 03 and the onter shaft 04 is changed to rotate the inner
shaft 03 and the outer shaft 04 in the opposite directions.
[0010] . However, the above conventional driving system possesses the following drawbacks.
Since the main engine 07 is not in alignment with the inner shaft 03 and the outer
shaft 04, a wide space is required for the arrangement of the main engine 07 and the
driving devices 03, 04, 05 and 06. If a plurality of main engines 07 are used, a cost
thereof is high, and a merit of the contra-rotating propeller apparatus which intends
to reduce a running cost due to the improved propulsion performance can not be effected.
[0011] . The first invention concerns a marine contra-rotating propeller apparatus for propelling
a ship attained in view of the above facts. The invention is characterized in that
an output shaft of a main diesel engine is directly coupled to a stern-side propeller
through an intermediate inner shaft and an inner shaft, and an output from the engine
is derived through a flanged friction sleeve coupling mounted on the intermediate
inner shaft and which is coupled to a bow-side propeller through an elastic coupling,
a reversing transmission mechanism and an outer shaft so that the thrust of the outer
shaft produced by the bow-side propeller is transmitted to a thrust bearing on the
intermediate inner shaft and the thrust of the inner and outer shafts are transmitted
to a thrust bearing contained within the main diesel engine. It is an object of the
invention to provide a marine contra-rotating propeller apparatus for propelling a
ship using a low-speed main diesel engine for eliminating the above drawbacks and
in which the revolution performance for driving the contra-rotating propellers and
the thrust supporting performance are enhanced with simple structure.
[0012] . In the first invention, since the stern-side propeller is directly coupled through
the intermediate inner shaft and the inner shaft to the main diesel engine to be driven
by means of the engine of which the output is derived through the flanged friction
sleeve coupling on the intermediate inner shaft and the outer shaft is inversely rotated
through the elastic coupling and the reversing transmission mechanism to rotate the
bow-side propeller, the reverse revolution, the revolution speed and the torque distribution
between the inner shaft for the stern-side propeller and the outer shaft for the bow-side
propeller can be freely obtained and the revolution performance for driving the contra-rotating
propellers is remarkably improved. A low-speed main diesel engine is adopted so that
it can be effectively utilized and the characteristics thereof can be exhibited. Further,
since the thrust acting on the outer shaft from the bow-side propeller is transmitted
to the thrust bearing on the intermediate inner shaft and transmitted to the thrust
bearing contained in the main diesel engine together with the thrust acting on the
inner shaft from the stern-side propeller, the revolution performance for driving
the contra-rotating propellers is remarkably improved. In addition, the reversing
transmission mechanism and the gears are protected by the output transmission performance
exhibited by means of the flanged friction coupling and the elastic coupling so that
the revolution performance for driving the contra-rotating propellers is further improved
and reliability of the apparatus is extremely improved.
[0013] . The second invention concerns a marine contra-rotating propeller apparatus eliminating
the above drawbacks in the conventional apparatus. The marine contra-rotating propeller
apparatus in which a stern-side propeller is directly connected to an inner shaft
coupled to a main diesel engine and a bow-side propeller is coupled to an outer shaft
coupled to the intermediate portion of the inner shaft through an elastic coupling,
an input outer shaft and a reversing transmission mechanism, is characterized in that
the reversing transmission mechanism is formed of a planetary gear mechanism comprising
a sun gear interposed between the input outer shaft and the outer shaft, a small planet
gear meshed with the sun gear, a large planet gear coupled to the small planet gear
and an inner gear meshed with the large planet gear. It is an object of the invention
to provide the marine contra-rotating propeller apparatus eliminating the above drawbacks
in which the reversing transmission mechanism interposed between the input outer shaft
and the outer shaft forming a bow-side propeller driving mechanism is formed of a
special planetary gear mechanism which can allow the movement in the thrust direction
of the outer shaft and rotate the input outer shaft and the outer shaft at the same
revolution speed.
[0014] . The second invention is constructed as described above, and since the stern-side
propeller is directly connected to the inner shaft coupled to the main diesel engine
and the bow-side propeller is connected to the outer shaft coupled to the intermediate
portion of the inner shaft through the elastic coupling, the input outer shaft and
the reversing transmission mechanism which is formed of the planetary gear mechanism
including the sun gear interposed between the input outer shaft and the outer shaft,
the small planet gear meshed with the sun gear, a large planet gear coupled to the
small planet gear, and the inner gear on the side of the outer shaft meshed with the
large planet gear, the torque of which variation is smoothed through the elastic coupling
connected to the intermediate portion of the inner shaft is transmitted to the input
outer shaft and the construction of the large planet gear coupled to the small planet
gear in the planetary gear mechanism allows each gear to be formed of a spur gear
and forms the reversing function. The revolution speed and the torque distribution
for the input outer shaft and the outer shaft can be remarkably freely set up and
the special planetary gear mechanism sufficiently absorbs the movement in the thrust
direction of the outer shaft to protect the gears. The inverse revolution, the revolution
speed and the torque distribution of the bow-side propeller for the stern-side propeller
are extremely enhanced, and the revolution performance and the reliability of the
contra-rotating propellers are remarkably improved.
[0015] . Further, the planetary gear mechanism can be formed to relatively simple and small
structure and be provided to be inexpensive since the large planet gear is merely
provided. The excellent propeller revolution performance as described above allows
the low-speed main diesel engine possessing various characteristics to be adopted
and be effectively utilized, and further the characteristics of a conventional bevel
gear group is exhibited.
[0016] . The third invention eliminates the drawbacks of the conventional marine contra-rotating
propeller apparatus and an object of the invention is to simplify the contra-rotating
propeller driving mechanism using a low-speed main diesel engine with excellent fuel
consumption ratio. In the invention, the contra-rotating propeller driving mechanism
is formed of a parallel shaft gear device coupled to the main engine disposed on the
aligned line with the propeller shaft. In other words, the marine contra-rotating
propeller apparatus of the invention in which a ship is propelled by the contra-rotating
propellers is characterized by comprising an inner shaft having one end to which a
stern-side propeller is mounted and the other end coupled to the main engine, an elastic
coupling having an inner periphery being in contact with the inner shaft and an outer
periphery being in contact with an inner periphery of the outer shaft, and a bow-side
propeller mounted through a reversing mechanism on the outer shaft at the side of
the bow rather than the position where the stern-side propeller is mounted.
[0017] . Other objects and advantages of the present invention will be apparent from the
following description in connection with drawings, in which:
. Fig. 1 is a longitudinal sectional view of a construction showing a prior art marine
contra-rotating propeller apparatus;
. Figs. 2 to 4 illustrate constructions of the parallel shaft gear device of the prior
art contra-rotating propellers;
. Fig. 5 is a longitudinal sectional view of an overall construction showing a first
embodiment of the present invention;
. Fig. 6 is an enlarged longitudinal sectional view of a reversing transmission mechanism
in Fig. 5;
. Fig. 7 is a sectional view of a portion taken along line VII - VII in Fig. 6;
. Fig. 8 illustrates an overall construction according to a second embodiment of the
present invention;
. Fig. 9 is an enlarged longitudinal sectional view of a reversing transmission mechanism
in Fig. 8;
. Fig. 10 illustrates an arrangement of each gear taken along line X - X in Fig.9;
. Fig. 11 is a longitudinal sectional view showing a third embodiment of the present
invention;
. Fig. 12 is a sectional view taken along line XII - XII in Fig. 11; and
. Fig. 13 is a sectional view taken along line XIII - XIII in Fig. 11.
[0018] . An embodiment of the present invention is now described with reference to the drawings.
[0019] . Figs. 5 to 7 show a first embodiment of the present invention. In the drawings,
numeral 1 denotes a stern-side propeller, 2 a bow-side propeller, 3 an outer shaft
to which the bow-side propeller 2 is coupled, and 4 an inner shaft to which the stern-side
propeller 2 is coupled. An output shaft 9 of a low-speed main diesel engine 7 is directly
coupled to the stern-side propeller 1 through a flanged friction sleeve coupling 14,
an intermediate inner shaft 4a, a friction sleeve coupling 11 and the inner shaft
4. Further, the output shaft 9 is coupled to the bow-side propeller 2 through an elastic
coupling 6, a reversing transmission mechanism 20, an intermediate outer shaft 3a
and the outer shaft 3.
[0020] . More particularly, the low-speed main diesel engine 7 and the reversing transmission
mechanism 20 are installed on a tank top b forming a double bottom which is part of
a ship body a. The inner shaft 4 and the outer shaft 3 for rotating the contra-rotating
propellers, that is, the stern-side propeller 1 and the bow-side propeller 2, respectively,
penerate a rear partition wall c forming part of the ship body a.
[0021] . The output shaft 9 of the main diesel engine 7 is coupled through the friction
sleeve coupling 14 to the intermediate inner shaft 4a which is coupled through the
friction sleeve coupling 11 to the inner shaft 4, so that the torque and the thrust
are transmitted through friction.
[0022] . The torque is transmitted to the bow-side propeller 2 through the friction sleeve
coupling 14, the elastic coupling 6, the reversing transmission mechanism 20, the
intermediate outer shaft 3a, a sleeve 10 and the outer shaft 3. Flanged friction couplings
15 and 16 are interposed between the intermediate outer shaft 3a and the sleeve 10
and the sleeve 10 and the outer shaft 3, respectively, so that the torque and the
thrust are transmitted through friction.
[0023] . The friction couplings 11, 14, 15 and 16 are of a known oil injection type to which
oil pressure is loaded and which can be fitted up and opened.
[0024] . The thrust developed by the bow-side propeller 2 is transmitted to the intermediate
inner shaft 4a through the outer shaft 3, the sleeve 10, the intermediate outer shaft
3a, and a thrust bearing 8a of the intermediate inner shaft 4a. On the other hand,
the thrust developed by the stern-side propeller 1 is transmitted to the inner shaft
4 and the intermediate inner shaft 4a and is applied to the thrust bearing 8b contained
in the main diesel engine 7 together with the thrust of the bow-side propeller 2,
whereby both the thrusts are transmitted to the ship body.
[0025] As shown in Figs. 6 and 7, the reversing transmission mechanism 20 includes a casing
20-1, a substrate 20-2, an input bevel gear 20-3, an output bevel gear 20-4, a reversing
bevel gear 20-5, a fit gear 20-6, a ring 20-7, an intermediate inner shaft bearing
20-8, a bevel gear bearing 20-9, a bevel gear (with fit teeth) bearing 20-10, an oil
seal ring 20-11, an oil stop cover 20-12 and a reversing bevel gear bearing 20-13.
[0026] . The reversing bevel gears 20-5 are mounted to be capable of rotating on inner surface
of the casing 20-1 and the number of the gears 20-5 are sufficient to cause the torque
of the main diesel engine 7 to be transmitted to the bow-side propeller 2.
[0027] . The torque transmitted to the flanged friction sleeve coupling 14 from the output
shaft 9 of the main engine is transmitted to the intermediate inner shaft 4a and also
is transmitted to the elastic coupling 6 to be transmitted to the input bevel gear
20-3 so that the variation component or the vibration component thereof is smoothed.
[0028] . The output bevel gear 20-4 is provided with fit teeth 21-4 as its inner teeth and
the inner teeth are meshed with outer teeth of the fit gear 20-6 slidably in the axial
direction thereof ( refer to the sectional view shown in Fig.7). With the arrangement,
even if the fit gear 20-6 moves within clearance of the thrust bearing 8a at the side
of the intermediate inner shaft upon forward and backward movement of the ship, it
is designed so that the fit operation between the bevel gear group 20-3, 20-4 and
20-5 does not fail.
[0029] . Thus, the half of the torque of the main diesel engine 7 is transmitted to the
bow-side propeller 2.
[0030] . The bevel gear group 20-3, 20-4 and 20-5 and the fit gear 20-6 are properly supported
by the bearings 20-9, 20-10 and 20-13. The intermediate inner shaft 4a is supported
by the bearing 20-8 which has not relative speed except the vibration component when
the shaft is rotated at a constant speed.
[0031] . The inside of the reversing transmission mechanism 20 is sealed by the oil seal
ring 20-11 and the oil stop cover 20-12, and the gear and the bearing are properly
lubricated with oil. The oil falls into a sump 30 without leakage to outside and is
recirculated by a pump.
[0032] . The inner and outer shafts 4 and 3 are supported by bearings which are properly
lubricated with oil or seawater.
[0033] . The friction coupling 15 can be opened so that the sleeve 10 can be slidably moved
to the bow side in the axial direction and the inner friction sleeve coupling 11 can
be opened.
[0034] . The friction coupling 16 can be opened so that the inner and outer shaft 4 and
3 can be extracted from the outside of the ship a. Further, if the flanged friction
sleeve coupling 14 is opened to be move toward the bow side in a slide manner and
the casing 20-1 divided into two upper and lower portions in the axial direction and
the bearings 20-9 and 20-10 are opened, the intermediate inner and outer shafts 4a
and 3a can be inspected for maintenace.
[0035] . If the intermediate inner shaft 4a is long, the output shaft 9 and the intermediate
inner shaft 4a can be coupled by another friction sleeve coupling instead of the coupling
14. In this case, the coupling 14 may be used as a friction coupling for the intermediate
outer shaft 3.
[0036] . The reversing bevel gear 20-5 mounted on the inner surface of the casing 20-1 is
coupled at its end to the ring 20-7 for reinforcement. However, if the supporting
reinforcement for the reversing bevel gear 20-5 is insufficient, the ring 20-7 may
be coupled to the casing 20-1 to further reinforce the support of the bevel gear.
[0037] . Since the embodiment of the present invention comprises the reversing transmission
mechanism 20 i.e. the bevel gear mechanism as shown in Figs. 6 and 7, the revolution
transmission performance such as the inverse revolution, the revolution speed and
the torque distribution is improved, the fuel consumption ratio is good and the maintenance
control is easy. The low-speed diesel engine which can use a bad quality fuel oil
can be effectively utilized and its merit is sufficiently obtained.
[0038] . The stern-side propeller 1 is directly coupled to the output shaft 9 of the low-speed
main diesel engine 7 through the intermediate inner shaft 4a and the inner shaft 4.
On the other hand, since the torque or the output is derived from the intermediate
inner shaft having less twisted vibration and the output shaft 9 of the main engine
through the flanged friction sleeve coupling 14 to the bow-side propeller 2 which
is coupled through the elastic coupling 6 and the bevel gear group of the reversing
transmission mechanism 20 to the main engine 7, the respective contra-rotating propellers
are rotated in the opposite directions to each other at the same revolution speed
with the same torque distribution independently of the load of the propeller, so that
the optimum design of the contra-rotating propellers can be made freely.
[0039] . Further, the capacity of the elastic coupling 6 and the reversing transmission
mechanism 20 may be about half of the capacity of driving the bow-side propeller or
the output of the main diesel engine. Since the stern-side propeller is directly coupled
through the inner shaft and the intermediate inner shaft to the main diesel engine,
the elastic coupling and the bevel gear are not required in these shafts and hence
its structure can be simple.
[0040] . In addition, since the intermediate inner shaft 4a is directly coupled to the main
diesel engine 7 and the thrusts of the inner and outer shaft are received by the thrust
bearing 8b contained in the low-speed main diesel engine through slide bearing 8a
to be received by the ship body, the support performance of the thrust can be remarkably
improved and the bevel gear group of the reversing transmission mechanism 20 can be
protected together with the elastic coupling 6.
[0041] . In the conventional planetary gear system, the unbalance of torque occurs in each
propeller and the revolution speed for each propeller is different. At an extreme,
both propellers may be rotated in the same direction. In the revolution transmission
driving mechanism of the present embodiment, each contra-rotating propeller is always
rotated in the opposite direction at the same revolution speed and the transient characteristic
upon the increase and reduction of the speed and the backward movement is extremely
improved. The driving mechanism is relatively inexpensive as a whole and the revolution
driving performance and the reliability of the contra-rotating propellers are remarkably
improved.
[0042] . A second embodiment of the present invention is now described.
[0043] . Figs. 8 to 10 show the second embodiment of the present invention. In the drawings,
reference letter a denotes a ship body, reference numeral 101 denotes a stern-side
propeller, 102 a bow-side propeller, 103a an input outer shaft supplied with the torque
derived through an elastic coupling 106 disposed on the intermediate portion of an
inner shaft 104, 103b an outer shaft coupled through a reversing transmission mechanism
110 to the input outer shaft 103a and to which the bow-side propeller 102 is coupled,
104 an inner shaft coupled directly to the output shaft of a low-speed main diesel
engine 107 and to which the stern-side propeller 101 is directly coupled, 108a a thrust
bearing of the output shaft coupled to one end of the inner shaft 104 contained in
the engine 107, and 108b a thrust bearing of the inner shaft 104, the thrust bearing
108b having a function of transmitting the thrust of the outer shaft 103b to the inner
shaft 104.
[0044] . The reversing transmission mechanism 110 comprises a planetary gear mechanism composed
of a sun gear 110a which is fixedly mounted on an end of the input outer shaft 103a,
a small planet gear 110b meshed with the sun gear 110a, a large planet gear 110c mounted
on the same shaft as that of the small planet gear 110b, and a spur gear 110d fixedly
mounted on the basal portion of the outer shaft 103b and meshed with the large planet
gear 110c as shown in Fig. 9. A planetary shaft 115 common to the small planet gear
110b and the large planet gear 110c is supported on a fixed stand 111 and a disc 112
as shown in the drawing. The necessary number of pairs of the large and small planet
gears are provided to transmit the torque to the bow-side propeller 102.
[0045] . In this manner, the torque transmitted to the input outer shaft 103a through the
elastic coupling 106 from the intermediate portion of the inner shaft 104 is smoothed
in its variation component by the action of the elastic coupling 106 and is transmitted
to the sun gear 110a through the input outer shaft 103a. The sun gear 110a rotates
the large planet gear 110c as well as the small planet gear 110b, and the large planet
gear 110c rotates the spur gear 110d and the outer shaft 103b, so that the outer shaft
103b is rotated in the opposite direction to that of the input outer shaft 103a.
[0046] . Each of the above gears is formed of a spur gear, and the sun gear 110a and the
inner gear 110d are rotated in the opposite directions to each other at the same revolution
speed by varying the magnitude or the gear ratio of the large planet gear 110c and
the small planetary gear 110b. As shown in Fig. 10, when the radii of the sun gear
110a, the inner gear 110d, the small planet gear 110b and the large planet gear 110c
are r, R, a and b, respectively, the sun gear 110a and the inner gear 110d i.e. the
input outer shaft 103a and the outer shaft 103b are rotated in the opposite directions
to each other at the same revolution direction if the radii of the respective gears
are made to safisfy the following equation (1).

[0047] In the prior art planetary gear mechanism, the revolution speeds of the input shaft
and the output shaft can not be equal to each other.
[0048] . For example, if a:b:r:R = 1:2:3:6, the above equation can be satisfied. Further,
the ratio can be freely set to the best condition in connection with the structure
of both the propellers.
[0049] . With the above structure of the embodiment, the stern-side propeller 101 is directly
driven through the inner shaft 104 from the low-speed main diesel engine 107 and the
output torque is derived to the input outer shaft 103a while smoothing the variation
component through the elastic coupling 106 from the intermediate portion of the inner
shaft 104. With the structure that the large planet gear 110c is coupled to the same
shaft as that of the small planet gear 110b in the reversing transmission mechanism
110, the input outer shaft 103a and the outer shaft 103b are rotated in the opposite
directions to each other, and the same revolution speed and the same torque distribution
of the outer shaft 103b for the inner shaft 103a, that is, the bow-side propeller
102 for the stern-side propeller 101 can be freely established and hence the revolution
propulsion performance and reliability of the contra-rotating propellers are improved
remarkably.
[0050] . Since tne inner gear 110d and the large planet gear 110c are meshed with each other
as in spur gears and can move freely in the thrust direction of the outer shaft 103b
to absorb the thrust, the gears of the planetary gear mechanism 110 are protected
and the function of the thrust bearings 108b and 108a which receive the thrust from
the outer shaft 103b and the inner shaft 104 are sufficiently exhibited.
[0051] . The function of the large planet gear is added to the function of the prior art
planet gear which has been mainly used as a propulsion apparatus for a large ship
and consequently the contra-rotating propeller apparatus which has the features in
the prior art and completely eliminates the drawbacks in the prior art is attained
with a extremely simple and small structure. Further, a low-speed main diesel engine
which is superior in the fuel consumption and the maintenance control and can use
a bad quality fuel oil can be used and effectively utilized.
[0052] . While the sun gear 110a is used at the input side and the inner gear 110d is used
at the output side in the above embodiment, it is not limited to such an arrangement
but the same effect can be obtained even if the arrangement is reversed. Although
the planetary shaft 115 for a plurality of the large planet gears 110c and the small
planetary gears 110b is coupled at its end to the disc 112 for reinforcement, the
disc 112 can be designed to be coupled to the fixed stand 111 in order to increase
the reinforcement.
[0053] . A third embodiment of the present invention is now described with reference to
Figs. 11 to 13. In Figs. 11 to 13, numeral 201 denotes a stern-side propeller, 202
a bow-side propeller, 203 an inner shaft for driving the stern-side propeller, 204
an outer shaft for driving the bow-side propeller, 205 an output-side gear device
for driving the bow-side propeller, 205a a small gear, 205b a large gear, 206 an input-side
gear device for driving the bow-side propeller, 206a a small gear, 206b an idle gear,
206c a large gear, 207 an elastic coupling, 208 a thrust bearing for the outer shaft,
209 a thrust bearing for the inner shaft, and 210 an main engine. The inner shaft
203, the outer shaft 204 and the gears 205a, 205b, 206a, 206b and 206c are supported
by bearings not shown.
[0054] . In the marine contra-rotating propeller apparatus constructed above, the stern-side
propeller 201 is directly coupled to the main engine 210 through the inner shaft 203
and the propeller 201 is driven by the engine. The torque is transmitted to the bow-side
propeller 202 from the main engine 210 as follows. The torque from the engine which
is smoothed in its variation by means of the elastic coupling 207 mounted on the intermediate
portion of the inner shaft 203 directly coupled to the engine 210 is transmitted to
the large gear 206c of the input-side gear device 206, and the small gear 206a is
rotated in the opposite direction to that of the large gear 206c through the idle
gear 206b.
[0055] . On the other hand, the revolution is transmitted to the output-side gear device
205 through a small gear 205a mounted on the same shaft as that of the small gear
206a of the input-side gear device 206, and the large gear 205b meshing with the small
gear 205a is rotated in the opposite direction to that of the large gear 206c of the
input-side gear device 206. Accordingly, the bow-side propeller 202 is rotated in
the opposite direction to that of the stern-side propeller 201 which is directly coupled
to the engine 210.
[0056] The speed increase ratio of the input-side gear device 206 and the speed reduction
ratio of the output-side gear device 205 may be selected to be the speed increase
ratio / the speed reduction ratio - 1.0.
[0057] . As described above in detail with reference to the embodiment of the present invention,
according to the present invention, the following effects can be obtained.
[0058]
(1) The main engine is disposed on the propeller shaft and the overall structure is
compact.
(2) The gear device which is easily manufactured and assembled and has high reliability
can be provided.
(3) The capacity of the elastic coupling may be about half of that of the main engine
output since the stern-side propeller is directly coupled to the main engine.
(4) By adopting the contra-rotating propellers which can provide the gear device which
is compact as a whole, is inexpensive in the manufacture cost and has high reliability,
a merit in reduction of the running cost effected by the improvement of the propulsion
performance can be effectively exhibited.