A method for decelerating a watercraft is disclosed. The watercraft has a reverse gate and a reverse gate actuator operatively connected to the reverse gate for moving the reverse gate between at least a stowed position and a deceleration position. The method includes: receiving, in a control unit,
A method for decelerating a watercraft is disclosed. The watercraft has a reverse gate and a reverse gate actuator operatively connected to the reverse gate for moving the reverse gate between at least a stowed position and a deceleration position. The method includes: receiving, in a control unit, a deceleration signal from a deceleration device position sensor, the deceleration signal being indicative of an actuated position of a deceleration device; controlling, by the control unit, an operation of the reverse gate actuator based at least in part on the actuated position of the deceleration device; and moving the reverse gate from the stowed position to the deceleration position with the reverse gate actuator, the reverse gate actuator being controlled such that a speed of rotation of the reverse gate depends at least in part on the actuated position of the deceleration device.
대표청구항▼
1. A method for decelerating a watercraft, the watercraft having a hull, a deck disposed on the hull, a seat disposed on the deck, a motor connected to at least one of the hull and the deck, a jet propulsion system operatively connected to the motor, a reverse gate connected to at least one of the h
1. A method for decelerating a watercraft, the watercraft having a hull, a deck disposed on the hull, a seat disposed on the deck, a motor connected to at least one of the hull and the deck, a jet propulsion system operatively connected to the motor, a reverse gate connected to at least one of the hull and the jet propulsion system, the reverse gate being movable between at least a stowed position and a deceleration position, and a reverse gate actuator operatively connected to the reverse gate for moving the reverse gate between at least the stowed position and the deceleration position, the method comprising: receiving, in a control unit, a deceleration signal from a deceleration device position sensor, the deceleration signal being indicative of an actuated position of a deceleration device, the deceleration device having multiple actuated positions;controlling, by the control unit, an operation of the reverse gate actuator based at least in part on the actuated position of the deceleration device; andmoving the reverse gate from the stowed position to the deceleration position with the reverse gate actuator, the reverse gate actuator being controlled such that a speed of rotation of the reverse gate varies based at least in part on the actuated position of the deceleration device. 2. The method of claim 1, wherein: controlling the operation of the reverse gate actuator includes: controlling the reverse gate actuator to operate according to a first operation mode as the reverse gate moves from the stowed position to an intermediate position of the reverse gate, the intermediate position being intermediate the stowed and deceleration positions; andcontrolling the reverse gate actuator to operate according to a second operation mode as the reverse gate moves from the intermediate position to the deceleration position; andthe speed of rotation of the reverse gate varies based at least in part on the one of the first and second operation modes according to which the reverse gate actuator is being controlled. 3. The method of claim 2, wherein the reverse gate actuator moves the reverse gate faster in the first operation mode than in the second operation mode. 4. The method of claim 3, wherein: the first operation mode is independent of the actuated position of the deceleration device; andthe second operation mode is dependent on the actuated position of the deceleration device. 5. The method of claim 4, wherein, in the second operation mode, the reverse gate actuator moves the reverse gate slower as the actuated position of the deceleration device is smaller. 6. The method of claim 3, wherein moving the reverse gate toward the deceleration position with the reverse gate actuator includes: moving the reverse gate from the stowed position to the intermediate position with the reverse gate actuator operating according to the first operation mode;stopping the reverse gate at the intermediate position for a time delay; andonce the time delay has expired, moving the reverse gate from the intermediate position to the deceleration position with the reverse gate actuator operating according to the second operation mode. 7. The method of claim 6, wherein the time delay is constant. 8. The method of claim 3, wherein the intermediate position is a neutral position of the reverse gate. 9. The method of claim 1, wherein: when the actuated position of the reverse gate actuator is less than a predetermined position, controlling the operation of the reverse gate actuator includes: controlling the reverse gate actuator to operate according to a first operation mode as the reverse gate moves from the stowed position to an intermediate position of the reverse gate, the intermediate position being intermediate the stowed and decelerations positions; andcontrolling the reverse gate actuator to operate according to a second operation mode as the reverse gate moves from the intermediate position to the deceleration position;when the actuated position of the reverse gate actuator is greater than the predetermined position, controlling the operation of the reverse gate actuator includes: controlling the reverse gate actuator to operate according to a third operation mode as the reverse gate moves from the stowed position to the deceleration position; andthe speed of rotation of the reverse gate varies based at least in part on the one of the first, second and third operation modes according to which the reverse gate actuator is being controlled. 10. The method of claim 9, wherein the reverse gate actuator moves the reverse gate faster in the first and third operation modes than in the second operation mode. 11. The method of claim 10, wherein: the first and third operation modes are independent of the actuated position of the deceleration device; andthe second operation mode is dependent on the actuated position of the deceleration device. 12. The method of claim 10, wherein: when the actuated position of the reverse gate actuator is less than the predetermined position, moving the reverse gate toward the deceleration position with the reverse gate actuator includes: moving the reverse gate from the stowed position to the intermediate position with the reverse gate actuator operating according to the first operation mode;stopping the reverse gate at the intermediate position for a time delay; andonce the time delay has expired, moving the reverse gate from the intermediate position to the deceleration position with the reverse gate actuator operating according to the second operation mode; andwhen the actuated position of the reverse gate actuator is greater than the predetermined position, moving the reverse gate toward the deceleration position with the reverse gate actuator includes: moving the reverse gate uninterruptedly from the stowed position to the deceleration position with the reverse gate actuator operating according to the third operation mode. 13. The method of claim 1, further comprising: reducing a thrust request upon receiving the deceleration signal prior to moving the reverse gate toward the deceleration position;reducing a speed of the motor in response to the reduction of the thrust request;continuing to reduce the speed of the motor as the reverse gate moves toward an intermediate position of the reverse gate, the intermediate position being intermediate the stowed and decelerations positions;increasing the thrust request at the intermediate position of the reverse gate; andincreasing the speed of the motor in response to increasing the thrust request. 14. A watercraft comprising: a hull;a deck disposed on the hull;a seat disposed on the deck;a motor connected to one of the hull and the deck;a jet propulsion system operatively connected to the motor;an electronic control unit (ECU) communicating with the motor for controlling an operation of the motor;a reverse gate operatively connected to at least one of the hull and the jet propulsion system, the reverse gate being movable between at least a stowed position and a deceleration position;a reverse gate actuator operatively connected to the reverse gate for moving the reverse gate between at least the stowed position and the deceleration position, and being in communication with the ECU;a deceleration device position sensor in communication with the ECU; anda deceleration device connected to the deceleration device position sensor, the deceleration device position sensor sensing a position of the deceleration device,the ECU being configured to, upon receiving a deceleration signal indicative of an actuation of the deceleration device from the deceleration device position sensor, send an actuation signal to the reverse gate actuator to move the reverse gate toward the deceleration position,the actuation signal being based at least in part on an actuated position of the deceleration device, the deceleration device having multiple actuated positions, anda speed of rotation of the reverse gate varying based at least in part on the actuated position of the deceleration device. 15. The watercraft of claim 14, wherein: the actuation signal includes a first actuation signal and a second actuation signal;the ECU is configured to, upon receiving the deceleration signal indicative of the actuation of the deceleration device from the deceleration device position sensor: send the first actuation signal to the reverse gate actuator to move the reverse gate from the stowed position to an intermediate position of the reverse gate, the intermediate position being intermediate the stowed and decelerations positions; andsend the second actuation signal to the reverse gate actuator to move the reverse gate from the intermediate position to the deceleration position; andthe reverse gate actuator moves the reverse gate faster when the ECU sends the first actuation signal than when the ECU sends the second actuation signal. 16. The watercraft of claim 14, wherein the reverse gate actuator is an electric motor. 17. A method for decelerating a watercraft, the watercraft having a hull, a deck disposed on the hull, a seat disposed on the deck, a motor connected to at least one of the hull and the deck, a jet propulsion system operatively connected to the motor, a reverse gate connected to at least one of the hull and the jet propulsion system, the reverse gate being movable between at least a stowed position and a deceleration position, and a reverse gate actuator operatively connected to the reverse gate for moving the reverse gate between at least the stowed position and the deceleration position, the method comprising: receiving, in a control unit, a deceleration signal from a deceleration device position sensor, the deceleration signal being indicative of an actuated position of a deceleration device;controlling, by the control unit, an operation of the reverse gate actuator based at least in part on the actuated position of the deceleration device; andmoving the reverse gate from the stowed position to the deceleration position with the reverse gate actuator, the reverse actuator being controlled such that a time taken for moving the reverse gate from the stowed position to the deceleration position varies depending at least in part on the actuated position of the deceleration device, the time starting from the reception of the deceleration signal by control unit. 18. The method of claim 17, wherein the operation of the reverse gate actuator is controlled such that an average speed of rotation of the reverse gate over the time is based at least in part on the actuated position of the deceleration device. 19. The method of claim 18, wherein the operation of the reverse gate actuator is controlled such that an instantaneous speed of rotation of the reverse gate varies from the stowed position to the deceleration position. 20. The method of claim 18, wherein the reverse gate actuator is controlled to: rotate the reverse gate at a first speed of rotation from the stowed position to an intermediate position, the intermediate position being intermediate the stowed and deceleration positions; androtate the reverse gate at a second speed of rotation from the intermediate position to the deceleration position, the second speed of rotation being less than the first speed of rotation.
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이 특허에 인용된 특허 (14)
St-Pierre, Luc; Gaudet, Pierre; Laing, Christian, Automatic trim system for a jet propulsion watercraft.
St-Pierre, Luc; Gaudet, Pierre; Laing, Christian; Leclerc, Alexandre; Mailloux-Leclerc, legal representative, Louise, Commonly actuated trim and reverse system for a jet propulsion watercraft.
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