The present invention relates to a steering actuator for a steer-by-wire ship's control system. Furthermore, the invention relates to methods for operating the steering actuator.
From the prior art, steer-by-wire systems are known, which are also used in ship control technology. In such systems the steering commands given by a steering unit are detected by a sensor and transmitted by a control unit to a steering actuator which carries out the steering command. Advantageously, there is no mechanical connection between the helm and the rudder, or in the case of a motor vehicle, between the steering-wheel and the steered wheels.
In ship control technology the steering units connected to the rudder are usually hydraulically actuated, which results disadvantageously in poor dynamics and high maintenance costs. In addition steer-by-wire ship's control systems are known, in which the steering actuator is an electro-mechanical actuator in the form of a ball-screw spindle by means of which rotational movement of the one electric motor is converted by the ball-screw spindle into a translational movement for actuating the rudder.
This use of an electric motor driven ball-screw spindle as the steering actuator has the drawback that the adjustment speed and dynamics of the actuator are low; furthermore, ball-screw spindles are not self-locking, especially when the forces acting are large.
For example, a steer-by-wire ship's control system is known from U.S. Pat. No. 6,431,928 B1. In this known system an electric motor is provided for rotating the entire propeller-drive unit by means of a mechanical energy transfer chain, the electric motor being controlled by a control unit connected on the one hand to the steering device to obtain steering command information, and on the other hand to a sensor which detects the steering setting information.
From EP 1770008 A2 a steer-by-wire ship's control system is known, which comprises at least two steering units. In this case the rudder is actuated by means of an actuator which can be operated hydraulically with reference to the steering signals generated by whichever steering unit demands the more rapid movement of the rudder. In the known system the steering units each have a rudder, each of which is connected to a control device which, in turn, is connected to the control network.
The purpose of the present invention is to provide a steering actuator for a steer-by-wire ship's control system, which is of compact structure and can be produced in a favorable manner. Furthermore, the steering actuator must be largely self-locking and must have a good dynamic performance. In addition, a method for operating the steering actuator is indicated.
Accordingly, a steering actuator for a steer-by-wire ship's control system is proposed, which is designed as a linear electro-mechanical actuator comprising an electric motor designed as a vector-controlled brushless motor.
The design of the electric motor as a vector-controlled brushless motor enables sinusoidal or trapezium-shaped signal conversion whereby direct-current or alternating-current motors can be used. Furthermore, owing to the vector control the motor power can be doubled for approximately 5 seconds, corresponding to a 100% overload. The dynamics are also optimized since the vector control enables very high accelerations compared with a conventional electric motor.
In a first preferred embodiment of the invention the steering actuator is designed as an electric motor powered geared spindle drive whose threaded spindle, which is articulated to the tiller or to a suitable part of the rudder mechanism, has an outer thread which engages with the inner thread of a screw nut driven by the electric motor.
Alternatively, the threaded spindle can be hollow-bored and have an inner thread, in which the outer thread of a screw driven by the electric motor engages.
In a particularly advantageous further development of the invention the screw nut is formed by the rotor of the electric motor.
Thanks to the conversion, according to the invention, of the rotary movement of the electric motor into a translational movement of the threaded spindle by virtue of the cooperation of an inner thread with an outer thread, desired self-locking is achieved in an advantageous manner, so that when the rudder is not actuated the electric motor consumes very little current.
To enable maneuverability in the event that the electric motor should fail, it is also proposed to fix one end of a Bowden cable detachable to the end of the steering actuator remote from the threaded spindle, to the screw nut or to the rotor of the electric motor, so that by actuating (rotating) the Bowden cable by means of a suitable device, for example by means of a crank, the threaded spindle can be moved.
Advantageously, the end of the Bowden cable remote from the rotor can be connected in a rotationally fixed manner by means of an adaptor device to the shaft connected in a rotationally fixed manner to the rudder, so that the Bowden cable can be actuated by actuating the rudder.
According to the invention, to control the steering actuator a controller is provided, which is connected via the CAN bus to the electronic control unit of the ship's control system ECU; to determine the angular position of the rudder an angle sensor is provided, which is preferably designed as an incremental emitter and determines the rotation of the rotor of the electric motor or that of the threaded spindle. The ECU processes the signals of the steering unit actuated by the user or of an auto-pilot device and passes them on to the steering actuator. In this way the steering actuator is operated in accordance with the specifications of the steering unit and the ECU in relation to the steering angle and the turning speed of the rudder.
According to the invention, two rudders can be actuated by one steering actuator and for that purpose the spindle is connected to both tillers via an intermediate component. According to the invention a steering actuator can also be provided for each rudder, so that the rudders can be actuated independently of one another with reference to commands from the ECU. This can be an advantage, for example, when carrying out complex maneuvers.
Below, the steering actuator according to the invention and methods for its operation are described in more detail as examples with reference to the attached figures, which show:
In the example shown in
By virtue of the active connection between the outer and inner threads and the multiple points of contact between the two components, the advantage is obtained that high torques can be transferred even with a compact structure and high accelerations and speed values can be achieved. For example, with the actuator according to the invention up to 7000 r/min are possible, whereas with an actuator having a conventional ball-screw spindle up to 2500 r/min can be obtained. The number of contact points between the two components, the spindle and the screw nut (see
To control the steering actuator 1 a controller 11 is provided, which is connected via the CAN bus to the electronic control unit of the ship's control system ECU. In addition, to determine the angular position of the rudder an angle sensor 12 is connected to the controller 11, which is preferably designed as an incremental emitter and which determines the angular position of the rotor 9 of the electric motor 2 or that of the threaded spindle 5.
As indicated in
However, it is also possible for the sensor 12 to be arranged on the side of the electric motor facing toward the rudder 13. In the example shown in
To enable maneuverability in the event that the electric motor should fail, in any embodiment a Bowden cable 16 can optionally be provided, which can be connected detachably at the end of the steering actuator 1 remote from the rudder 13 to the screw nut or to the rotor 9 of the electric motor, so that the threaded spindle 5 can be moved by turning the Bowden cable by means of a crank 17. To enable the Bowden cable 16 to be connected to the rotor 9, an opening 18 is provided in the housing 14, which can preferably be closed when not in use.
In the example shown in
The sensor 12 for detecting the angular position of the rudder is advantageously designed as an incremental emitter, which results in lower cost. Since an incremental emitter does not deliver an absolute value, each time the ship's control system is started up the null position (the straight-ahead position) has to be determined and the rudder brought to that position.
According to the invention, the null position is determined, when the ship's control system is started up, by operating the electric motor at a specified constant speed in one direction until the end position corresponding to that steering direction has been reached, and then storing the sensor value for that position in the controller 11.
Then, the electric motor 2 of the steering actuator is operated at a specified speed in the opposite direction until the second end position of the rudder has been reached, and the sensor value corresponding to this second end position is used in order to determine the null position with reference to the number of increments between the two end positions (it will correspond to half the incremental difference), and the rudder is finally brought to that position by actuating the electric motor is the appropriate direction. If the two end positions do not have the same angular separation from the null position, this is taken into account when determining the null position from the increments.
The end positions can preferably be determined by recognizing as an end position a point where the current taken up by the electric motor exceeds a specified threshold value. At such points the current needed by the motor operated at constant speed increases in order to overcome the “obstacle”.
According to the invention, before determining the null position it is optionally checked whether the connection between the incremental emitter and the controller is functioning properly and whether the CAN is ready to operate. If this is not the case, the rudder is locked and an error message is emitted.
In addition, during the operation of the ship's control system, at specified time intervals the functionality of the CAN is checked, and for this purpose a defined signal is sent by the electronic control unit of the ship's control system ECU to the controller 11. If this signal is received without error by the controller within a specified time interval the operation of the steering actuator is continued, but if the signal is not received, or contains an error, then the controller 11 brings the rudder to the null position and holds it in that position, and an error message is emitted.
According to a variant of the method, if the signal is not received within the specified time interval or contains an error, the electronic control unit of the ship's control system ECU is requested again by the controller 11 to transmit the signal, and this can be repeated up to n times (n is a specified whole number with a value between 2 and 50). If the signal has not been received within the specified time interval or is received erroneously after the n-th repetition, then the controller 11 brings the rudder to the null position and holds it in that position, and an error message is emitted.
1 Steering actuator
2 Electric motor
3 Tiller
4 Articulation
5 Threaded spindle
6 Outer thread
7 Inner thread
8 Screw nut
9 Rotor
10 Stator
11 Controller
12 Sensor
13 Rudder
14 Housing
15 Ship's hull
16 Bowden cable
17 Crank
18 Opening
19 Planetary transmission
20 Outer thread
21 Inner thread
22 Screw
23 Housing
24 Belt drive
Number | Date | Country | Kind |
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10 2007 048 061.1 | Oct 2007 | DE | national |
This application is a National Stage completion of PCT/EP2008/062894 filed Sep. 26, 2008, which claims priority from German patent application serial no. 10 2007 048 061.1 filed Oct. 5, 2007.
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/EP2008/062894 | 9/26/2008 | WO | 00 | 3/29/2010 |