JP2014031170A - Electric propulsion system of electric propulsion ship - Google Patents

Abstract

PROBLEM TO BE SOLVED: To provide an electric propulsion system of an electric propulsion ship which sufficiently inhibits a start current of a propulsion electric motor and achieves low costs.SOLUTION: An electric propulsion system of an electric propulsion ship includes: a propulsion electric motor 5 which drives a propeller 3; and an electric power supply device 6 which supplies electric power to the propulsion electric motor 5. In the electric propulsion system of the electric propulsion ship, an actuator 21 which provides startup power to the propulsion electric motor 5 is provided, and the actuator 21 is formed so as to have the same power source as an actuator 18 of a starter of the electric power supply device 6.

Description

  The present invention relates to an electric propulsion system for an electric propulsion ship.

  Conventionally, as an electric propulsion system for an electric propulsion ship, electric power generated by a generator is supplied to a propulsion motor such as an induction motor, and a propulsion device (such as a propeller and a gear box) is rotated by the propulsion motor rotated by the supplied electric power. What is driven is known. In such an induction motor for an electric propulsion ship, a starting device is configured by a reduced voltage starting method such as a condorfa starting method in order to suppress the starting current. Moreover, it is set as the structure which provides power converters, such as an inverter and a soft starter, and controls this power converter and suppresses starting current (for example, refer patent document 1).

JP 2006-155503 A

  However, when the induction motor is started by the condorfa starting method, the starting device is inexpensive, but the starting current (starting power) cannot be sufficiently suppressed, and a large amount of power corresponding to this starting current is obtained. A supply device (generator) was required. And since this electric power supply apparatus was expensive, there existed a problem that the whole electric propulsion system became high cost. In addition, when controlling the power supplied to the induction motor using an inverter or soft starter, it is difficult to use a general-purpose power converter because the induction motor of the electric propulsion ship has a large capacity, and the dedicated expensive power There was a problem that a converter was necessary and the entire electric propulsion system was similarly expensive.

  The present invention has been made in view of the above problems, and an object of the present invention is to provide a low-cost electric propulsion system for an electric propulsion ship by sufficiently suppressing the starting current of the propulsion motor.

  The problem to be solved by the present invention is as described above. Next, means for solving the problem will be described.

  The electric propulsion system for an electric propulsion ship comprising: a propulsion motor that drives a propeller; and a power supply device that supplies electric power to the propulsion motor, wherein an actuator that applies starting power to the propulsion motor is provided. The actuator is an actuator having the same power source as the actuator of the starting device of the power supply device.

  According to a second aspect of the present invention, at the time of starting, the propulsion motor is rotated to the starting rotational speed set by the power of the actuator, and then the electric power is supplied from the power supply device.

  According to a third aspect of the present invention, the actuator applies power from the output shaft side of the propulsion motor.

  According to a fourth aspect of the present invention, the actuator is an air motor or a cell motor.

  The electric propulsion system for an electric propulsion ship comprising: a propulsion motor that drives a propeller; and a power supply device that supplies electric power to the propulsion motor, wherein an actuator that applies starting power to the propulsion motor is provided. Since the actuator is an actuator having the same power source as the actuator of the starter of the power supply device, the propulsion motor is started with the power from the actuator. There is no need to supply starting power to the motor, the power supply capacity of the power supply device can be reduced, the cost of the power supply device can be reduced, and an actuator for applying starting power to the propulsion motor; To share the power source with the actuator of the starting device of the power supply device Runode, it is possible to reduce the cost of the electric propulsion system for an electric propulsion ships.

  According to a second aspect of the present invention, at the time of starting the propulsion motor, the electric power is supplied from the power supply device after rotating to the starting rotational speed set by the power of the actuator, so that the starting current of the propulsion motor is sufficiently increased It can suppress and can provide the electric propulsion system of an electric propulsion ship of low cost.

  According to the third aspect of the present invention, since the power from the actuator is applied from the output shaft side of the propulsion motor, the starting torque of the actuator that applies the starting power to the propulsion motor can be small, and the actuator can be downsized.

  According to claim 4, when the actuator is an air motor or a cell motor, when the power generation engine is started by the air motor or the cell motor, the engine starting facility is used as the propulsion motor starting facility. Therefore, it is possible to drive an air motor or a cell motor that applies starting power to the propulsion motor using existing equipment, and to reduce the cost of the electric propulsion system of the electric propulsion ship.

1 is a block diagram showing an electric propulsion system according to a first embodiment of the present invention. The block diagram which shows the flow at the time of start-up of the propulsion electric device which concerns on 1st embodiment. The block diagram which shows the electric propulsion system which concerns on 2nd embodiment of this invention. The block diagram which shows the flow at the time of starting of the propulsion electric device which concerns on 2nd embodiment. The block diagram which shows the electric propulsion system which concerns on another embodiment of this invention. The block diagram which shows the electric propulsion system which concerns on another embodiment of this invention.

  An overall configuration of an electric propulsion system 1 according to an embodiment of the present invention will be described. The electric propulsion system 1 is used to sail an electric propulsion ship. The electric propulsion system 1 is a system in which an AC generator is driven by a diesel engine and a propeller is driven via a propulsion motor without performing frequency conversion. As shown in FIG. 1, the electric propulsion system 1 has two propulsion devices 2, 2, two propellers 3, 3, two speed reducers 4, 4, two propulsion motors 5, 5, A power supply device 6, a switchboard 7, and an operation panel 8 are provided.

  The propellers 3 and 3 are devices for converting power into propulsion power of an electric propulsion ship. The propellers 3 and 3 are variable pitch propellers (CPP), and can control the blade angle while changing the rotation speed of the propeller shaft 3a to change the thrust and the traveling direction of the electric propulsion ship.

  The speed reducers 4 and 4 reduce the rotational speed of the output shafts 5a and 5a of the propulsion motors 5 and 5, and transmit or block the power transmitted from the propulsion motors 5 and 5 to the propellers 3 and 3. . Each speed reducer 4 includes a speed change mechanism 14 and a clutch mechanism 15. The speed change mechanism 14 is provided on the downstream side (propeller 3 side) of the power transmission path, and the clutch mechanism 15 is located on the upstream side of the power transmission path ( Provided on the propulsion motor 5 side).

  The speed change mechanism 14 is constituted by a plurality of reduction gears, and can be changed in a plurality of stages. When the clutch mechanism 15 is operated to “ON”, the output shaft 5 a of the propulsion motor 5 and the propeller shaft 3 a of the propeller 3 are interlocked and connected, and power is transmitted from the propulsion motor 5 to the propeller 3. When the clutch mechanism 15 is operated to “OFF”, the connection between the output shaft 5a of the propulsion motor 5 and the propeller shaft 3a of the propeller 3 is released, and the power is not transmitted from the propulsion motor 5 to the propeller 3. Blocked. The transmission mechanism 14 and the clutch mechanism 15 can be operated by a hydraulic actuator 16 driven by hydraulic pressure or the like.

  The propulsion motors 5 and 5 drive the propellers 3 and 3. The propulsion motors 5 and 5 are induction motors that are applied with a constant rated voltage and are driven at a constant rotational speed. In the propulsion motors 5 and 5 including such an induction motor, when starting, a starting current several times that in steady operation flows. Therefore, in this embodiment, the propulsion motor 5 is controlled in order to suppress the starting current. A starter 20 is provided for 5. In the propulsion motors 5 and 5, the output shafts 5a and 5a, which are the rotor shafts, are interlocked with the speed reducers 4 and 4. In addition to the induction motor, the propulsion motors 5 and 5 may be, for example, a synchronous motor or the like.

  The power supply device 6 supplies power to the propulsion motors 5 and 5. The power supply device 6 is connected to the propulsion motors 5 and 5 via the switchboard 7 and the starting circuit 26 of the starting device 20. In the present embodiment, the power supply device 6 includes three power generation engines. However, the number of power generation engines is not limited. Each power generation engine is provided with a synchronous generator 11 and a diesel engine 12 that drives the synchronous generator 11. The diesel engine 12 is a constant speed rotation engine, and is easier to control and maintain than a variable rotation engine. The rotor shaft of the synchronous generator 11 and the crankshaft of the diesel engine 12 are linked together. In addition, the power supply device 6 is configured to supply power to inboard loads such as lighting and auxiliary machines used in the ship.

  The switchboard 7 supplies or cuts off power generated by the power supply device 6 with respect to each load. The switchboard 7 is provided with a circuit breaker 13 such as an ACB (Air Circuit Breaker) on the output side of each generator and the input side of each propulsion motor 5.

  The operation panel 8 is for an operator to operate the electric propulsion ship. The operation panel 8 is connected to a control device 100 that performs starting and operation control, and the control device 100 controls the entire electric propulsion system 1 including the diesel engine 12. The control device 100 is actually composed of a CPU, ROM, RAM, interface, bus, and the like.

  In such an electric propulsion system 1, an operator operates the operation panel 8 to drive the diesel engines 12, 12, 12 of the power supply device 6 by the control device 100, and the synchronous generators 11, 11, 11 Electric power is generated, and the generated electric power is supplied to the propulsion motors 5 and 5 via the switchboard 7. The propulsion motors 5 and 5 are driven by the supplied electric power, and after the rotational speed of the output shafts 5a and 5a is decelerated by the speed change mechanisms 14 and 14 of the speed reducers 4 and 4, the power is propeller shaft 3a. • Transmitted to 3a. In this way, the propellers 3 and 3 are driven and the electric propulsion ship sails.

  Next, the starter 20A that is the first embodiment of the starter 20 will be described in detail. However, since the starting devices 20A and 20A for starting the propulsion motors 5 and 5 have the same configuration in the two propulsion devices 2 and 2, only the starting device 20A in one propulsion device 2 will be described.

  The starting device 20 </ b> A suppresses a starting current that flows when electric power is supplied to the propulsion motor 5. The starter 20 </ b> A includes an actuator, an air compressor 22, an air tank 23, an electromagnetic valve 24, a coupling mechanism 25, a starter circuit 26, and a rotation speed detection means 27.

  The actuator applies power to the propulsion motor 5, more specifically, to the output shaft 5a of the propulsion motor. In this embodiment, since the motor which starts diesel engine 12,12,12 is air motor 18,18,18, an actuator is used as an air motor. That is, the actuator is the air motor 21 so that these motors can be used as facilities such as the air compressor 22 and the air tank 23. In this way, the cost for the starting device 20A of the propulsion motor 5 can be reduced.

  The air motor 21 is disposed in the vicinity of the propulsion motor 5. The air motor 21 is configured such that its output shaft 21 a can be connected to the output shaft 5 a of the propulsion motor 5 via a connection mechanism 25. The air motor 21 is connected to the air tank 23 via an oiler, a solenoid valve 24, a filter, a pressure reducing valve, and the like in order to obtain air as power. The air tank 23 is connected to the air compressor 22 via a drain separator or an air pipe.

  The air tank 23 is connected to the air motor 18 for starting the diesel engine 12 via the electromagnetic valve 17. In the present embodiment, one air tank 23 includes a total of five air motors 18, 18, 18, including three air motors 18, 18, 18 for the diesel engine 12 and two air motors 21, 21 for the starter 20 </ b> A. Cost reduction of the electric propulsion system 1 can be achieved by sharing the equipment as a configuration for supplying air to 21 and 21.

  The solenoid valve 24 is connected to the control device 100. When the solenoid valve 24 is operated to “open”, air is supplied from the air tank 23 to the air motor 21 and the air motor 21 is driven. When the solenoid valve 24 is operated to “close”, air is not supplied from the air tank 23 to the air motor 21 and the air motor 21 stops.

  The connection mechanism 25 is for connecting the output shaft 21a of the air motor 21 and the output shaft 5a of the propulsion motor 5 or releasing the connected state. The coupling mechanism 25 is composed of, for example, an electromagnetic clutch, a transmission shaft, a gear, and the like. The coupling mechanism 25 is connected to the control device 100 and operated by the control device 100 to “ON” or “OFF”. When the coupling mechanism 25 is operated to “ON”, the output shaft 21a of the air motor 21 and the output shaft 5a of the propulsion motor 5 are coupled, and power is transmitted from the output shaft 21a to the output shaft 5a. Power is applied to the propulsion motor 5. On the other hand, when the connection mechanism 25 is operated to “OFF” by the control device 100, the connection state between the output shaft 21a of the air motor 21 and the output shaft 5a of the propulsion motor 5 is released, and the output shaft 21a is connected to the output shaft 21a. Transmission of power to 5a is interrupted, and power is not applied from the air motor 21 to the propulsion motor 5.

  The starting circuit 26 supplies or blocks the electric power supplied from the power supply device 6 to the propulsion motor 5. The starting circuit 26 is provided with a switch such as an electromagnetic switch or an electromagnetic contactor, and a holding circuit that keeps the switch “closed”. The primary side (input side) of the switch is connected to the wiring breaker 13 of the switchboard 7. The secondary side (output side) of the switch is connected to the propulsion motor 5. The starting circuit 26 is connected to the control device 100 and is operated to be “closed” or “open” by the control device 100. When the switch is operated to “close”, the power supply device 6 and the propulsion motor 5 are connected, and power is supplied from the power supply device 6 to the propulsion motor 5. On the other hand, when the switch of the starting circuit 26 is operated to “open”, the connection between the power supply device 6 and the propulsion motor 5 is released, and power is not supplied from the power supply device 6 to the propulsion motor 5.

  The rotation speed detecting means 27 detects the rotation speed N of the output shaft 5a of the propulsion motor 5. The rotation speed detection means 27 is, for example, a non-contact type optical sensor, and detects the rotation speed by projecting light onto the output shaft 5a of the propulsion motor 5 and receiving light reflected by the output shaft 5a. Configured as follows. The rotational speed detection means 27 is connected to the control device 100 and transmits a waveform corresponding to the detected rotational speed N to the control device 100.

  In such a starter 20A, as shown in FIG. 2, in the initial state (stop state) before the propulsion motor 5 is driven, the starter circuit 26 is stopped, and the switch is “open”. The clutch mechanism 15 of the speed reducer 4 is “disengaged”. That is, the propulsion motor 5 is not supplied with power from the power supply device 6 and is not interlocked with the propeller 3. Further, the coupling mechanism 25 is “ON”, and the output shaft 5 a of the propulsion motor 5 and the air motor 21 are coupled.

  When starting the propulsion motor 5 from this state, the operator starts the operation panel 8 (S1), and a start command is transmitted from the control device 100 to the actuator based on the start operation. That is, in the present embodiment, an “open” command is transmitted to the electromagnetic valve 24 that controls the driving of the air motor 21 that is an actuator (S2). As a result, the electromagnetic valve 24 is opened, the air motor 21 is driven (S3), and the output shaft 5a of the propulsion motor 5 is powered by the air motor 21 and starts rotating (S4).

  Next, when the rotational speed N of the output shaft 5a of the propulsion motor 5 detected by the rotational speed detection means 27 becomes equal to or higher than a first preset rotational speed (starting rotational speed) N1 (S5), control is performed. A stop command is transmitted from the apparatus 100 to the actuator. That is, in this embodiment, a “close” command is transmitted to the electromagnetic valve 24 that controls the driving of the air motor 21 that is an actuator (S6). Thereby, the electromagnetic valve 24 is “closed” and the air motor 21 is stopped (S7). In step S <b> 7, a command “OFF” is transmitted from the control device 100 to the coupling mechanism 25. As a result, the coupling mechanism 25 is turned off, and the coupling state between the output shaft 21a of the air motor 21 and the output shaft 5a of the propulsion motor 5 is released.

  Then, an operation command is transmitted from the control device 100 to the starting circuit 26 (S8). As a result, the starting circuit 26 is activated, the switch is “closed”, and the supply of electric power to the propulsion motor 5 is started (S9). That is, power is supplied from the power supply device 6 to the propulsion motor 5. As a result, the propulsion motor 5 is driven, and the rotational speed N of the output shaft 5a further increases from the first set rotational speed N1 (S10).

  At the start of power supply, in the propulsion motor 5, the output shaft 5 a is rotated by the power applied by the air motor 21, so that an electromotive force is induced in the stator coil of the propulsion motor 5 by this rotation. As a result, even when a constant voltage (rated voltage) is applied from the power supply device 6, the voltage applied to the propulsion motor 5 is equivalently reduced by the potential generated in the stator coil. That is, even when a rated voltage is applied to the propulsion motor 5 from the power supply device 6, the current flowing through the propulsion motor 5 can be reduced.

  After that, when the rotational speed N of the output shaft 5a of the propulsion motor 5 detected by the rotational speed detection means 27 reaches a preset second set rotational speed (rated rotational speed) N2 or settles to N2 ( S11), the control device 100 transmits a start control stop command to the start circuit 26 (S12). As a result, the starting circuit 26 stops, but the “ON” of the switch is held by the holding circuit, and the power supply of the propulsion motor 5 is maintained (S13). That is, the rotational speed N of the propulsion motor 5 maintains the rated rotational speed. The first set rotational speed (starting rotational speed) N1 is slightly lower than the second set rotational speed (rated rotational speed) N2.

  Then, a command for “ON” is transmitted from the control device 100 to the clutch mechanism 15. That is, a command to turn on the clutch mechanism 15 is transmitted to the hydraulic actuator 16 of the speed reducer 4 (S14). As a result, the hydraulic actuator 16 is driven and the clutch mechanism 15 is operated to “ON” (S15). As a result, power is transmitted to the propeller shaft 3a, and the propeller 3 is driven.

  Next, the starter 20B that is the second embodiment of the starter 20 will be described in detail. However, it demonstrates centering on a different part from the starting device 20A of 1st embodiment.

  As shown in FIG. 3, in the starter 20 </ b> B, the actuator is a cell motor 28 when the motor for starting the diesel engine 12, 12, 12 is the cell motor 19, 19, 19. The starter 20 </ b> B mainly includes a cell motor 28, a battery 29, a coupling mechanism 25, a starter circuit 26, and a rotation speed detection means 27.

  The cell motor 28 applies power to the propulsion motor 5, more specifically to the output shaft 5a of the propulsion motor. The cell motor 28 is disposed in the vicinity of the propulsion motor 5. The cell motor 28 is configured such that its output shaft 28 a can be connected to the output shaft 5 a of the propulsion motor 5 via the connection mechanism 25. Note that the timing for operating and stopping the cell motor 28 at the time of starting is controlled in the same manner as the air motor 21.

  The battery 29 is connected to the cell motors 19, 19, 19. That is, the battery 29 is configured to supply electric power to each cell motor 19 used to start each diesel engine 12, and includes equipment for driving the cell motors 28 and 28, equipment for driving the cell motors 19, 19, and 19. It is comprised so that it can be combined. The battery 29 is configured to be charged by the synchronous generator 11 connected to the diesel engine 12.

  In such a starting device 20B, as shown in FIG. 4, in the initial state (stopped state) before the propulsion motor 5 is driven, the starting circuit 26 is stopped and the switch is "open", and the speed reducer The fourth clutch mechanism 15 is “disengaged”. That is, the propulsion motor 5 is not supplied with power from the power supply device 6 and is not linked to the propeller 3. Further, the connecting mechanism 25 is “ON”, and the output shaft 5 a of the propulsion motor 5 and the cell motor 28 are connected.

  When starting the propulsion motor 5 from this state, the operator starts the operation panel 8 (S1), and a start command is transmitted from the control device 100 to the actuator based on the start operation (S2). ). That is, in this embodiment, a start command is transmitted to the cell motor 28 (S2). As a result, the cell motor 28 is driven (S3), and the output shaft 5a of the propulsion motor 5 is powered by the cell motor 28 and starts rotating (S4).

  Next, when the rotational speed N of the output shaft 5a of the propulsion motor 5 detected by the rotational speed detection means 27 becomes equal to or higher than a first preset rotational speed (starting rotational speed) N1 (S5), control is performed. A stop command is transmitted from the apparatus 100 to the actuator (S6). That is, in this embodiment, a stop command is transmitted to the cell motor 28 that is an actuator (S6). Thereby, the cell motor 28 stops (S7). In step S <b> 7, a command “OFF” is transmitted from the control device 100 to the coupling mechanism 25. As a result, the coupling mechanism becomes “OFF”, and the coupling state between the output shaft 28a of the cell motor 28 and the output shaft 5a of the propulsion motor 5 is released. Thereafter, control is performed in the same manner as the starting device 20A of the first embodiment.

  The actuator (air motor 21 or cell motor 28) can also apply power from the input shaft side of the speed reducer 4. For example, as in the starter 20C shown in FIG. 5, the air motor 21 is attached to the speed reducer 4, and the output shaft 21 a of the air motor 21 and the input shaft 4 a of the speed reducer 4 are connected or connected by the connecting mechanism 25. It is configured to be releasable, and power is applied from the input shaft side of the speed reducer 4. 6, the cell motor 28 is attached to the speed reducer 4, and the output shaft 28 a of the cell motor 28 and the input shaft 4 a of the speed reducer 4 are connected or connected by the connecting mechanism 25. It is configured to be releasable, and power is applied from the input shaft side of the speed reducer 4.

  As described above, in the electric propulsion system 1 according to the first and second embodiments of the present invention, the propulsion motor 5 that drives the propeller 3, and the power supply device 6 that supplies electric power to the propulsion motor 5. The electric propulsion system 1 of the electric propulsion ship is provided with an actuator for applying power to the propulsion motor 5, and the propulsion motor 5 rotates to the starting rotational speed N1 set by the power of the actuator at the time of starting. Then, power is supplied from the power supply device.

  Accordingly, the starting power can be reduced by rotating the output shaft 5a by the actuator at the time of starting. That is, when the propulsion motor 5 is started, if power is supplied from the power supply device 6 and started, the starting current is large, and the power supply device 6 needs a capacity corresponding to the starting power and becomes large. The power supply capacity of the power supply device 6 can be reduced, and the cost for the power supply device 6 can be reduced. Further, the starting current of the propulsion motor 5 can be suppressed without separately controlling the diesel engine 12 and the synchronous generator 11 of the power supply device 6.

  In the electric propulsion system 1 according to the first embodiment and the second embodiment of the present invention, the actuator applies power from the output shaft 5 a of the propulsion motor 5. Thereby, the starting torque of the actuator can be small, and the actuator can be miniaturized. Moreover, it can arrange | position near the starting equipment of an engine, and can perform a connection easily.

  In the electric propulsion system 1 according to the first embodiment of the present invention, the actuator is an air motor 21. Thereby, in the case of the specification for starting the diesel engine 12, 12, 12 for power generation with the air motor 18, the facility of the air motor 18 for starting the engine can be used as the facility of the air motor 21 for starting the propulsion motor. Thereby, the actuator can be driven by diverting existing equipment, and the cost of the starting device 20A of the propulsion motor 5 can be reduced.

  In the electric propulsion system 1 according to the second embodiment of the present invention, the actuator is a cell motor 28. Thus, in the case of the specification for starting the diesel engine 12, 12, 12 for power generation by the cell motor 19, the facility of the cell motor 19 for starting the engine can be used as the facility of the cell motor 28 for starting the propulsion motor. Moreover, the starter 20B can be a simple facility, and the cost of the starter 20B of the propulsion motor 5 can be reduced. Further, the cell motor 28 is small and has a large starting torque, and can easily rotate the output shaft 5a of the propulsion motor 5.

  In the electric propulsion system 1 according to another embodiment of the present invention, a speed reducer 4 is provided between the propeller 3 and the propulsion motor 5, and the actuator receives power from the input shaft side of the speed reducer 4. It is given. Thereby, an actuator can be easily arranged in a vacant space on the input shaft side of the speed reducer 4.

DESCRIPTION OF SYMBOLS 1 Electric propulsion system 3 Propeller 4 Reduction gear 6 Electric power supply device 7 Distribution board 8 Operation panel 11 Synchronous generator 12 Diesel engine 13 Circuit breaker 14 Transmission mechanism 15 Clutch mechanism 16 Hydraulic actuator 20 Starter 20A Start according to the first embodiment Device 20B Start device according to second embodiment 21 Air motor 24 Solenoid valve 25 Connection mechanism 26 Start circuit 27 Rotational speed detection means 28 Cell motor 100 Controller N Rotational speed N1 First set rotational speed (starting rotational speed)
N2 Second set speed (rated speed)

Claims (4)

In an electric propulsion system for an electric propulsion ship comprising: a propulsion motor that drives a propeller; and a power supply device that supplies electric power to the propulsion motor.
An electric propulsion system for an electric propulsion ship, characterized in that an actuator for applying starting power to the propulsion motor is provided, and the actuator is an actuator having the same power source as the actuator of the starting device of the power supply device. The electric propulsion system for an electric propulsion ship according to claim 1,
An electric propulsion system for an electric propulsion ship, wherein the propulsion motor is rotated to a starting rotational speed set by the power of the actuator, and then electric power is supplied from the power supply device. The electric propulsion system for an electric propulsion ship according to claim 1 or 2,
The electric propulsion system for an electric propulsion ship, wherein the actuator applies power from an output shaft side of the propulsion motor. In the electric propulsion system of the electric propulsion ship according to claim 1, 2, or 3,
An electric propulsion system for an electric propulsion ship, wherein the actuator is an air motor or a cell motor.

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