The present application claims priority to United Kingdom Application 0920249.0 filed on 19 Nov. 2009, the contents of which are incorporated herein by reference.
This invention relates to an actuator and, in particular, but not exclusively, to a linear actuator for use in manipulating a control surface of a seagoing vessel.
Actuators are used for a variety of functions on seagoing vessels. For example, actuators are used to control the position and/or attitude of a seagoing vessel by manipulation of the vessels control surfaces, including, for example, rudders, tail planes, fore planes, stabilisers and the like. Typically, mechanical or hydraulic actuators are used to manipulate the control surfaces of larger vessels; hydraulic actuators being used, for example, due to their flexibility and the ability to remotely operate the relevant control surface.
Control surfaces in larger vessels may be of significant mass and the actuators must be capable of providing significant force in order to provide precise control over the movement of the control surface, for example, to overcome hydrodynamic forces in moving the control surface against a water flow, wave or the like.
In addition to manipulation of control surfaces, actuators may also be used to deploy and retrieve sensor arrays, telecommunication antennae, mast assemblies or other components or assemblies.
A control surface, component or assembly to be manipulated is often provided in a relatively exposed location on the vessel and it is common that the component will be subject to impacts, for example, from fluid forces or from physical impact of an object.
Furthermore, during operation the control surface, component or assembly may be submerged, or located in another inaccessible location on the vessel, such that damage to a respective component or assembly may severely limit the operational effectiveness of the vessel.
According to a first aspect of the present invention, there is provided an actuator for use in controlling the movement of a component of a seagoing vessel, the actuator comprising:
an actuation member adapted to be coupled to a component, the movement of which is to be controlled; and
a force-generating arrangement for applying a control force to the actuation member, wherein the actuation member is compliant when the component is subject to an opposing force.
Traditionally, actuators provide a mechanical or hydraulic lock such that an opposing force, for example resulting from an impact, is more likely to cause damage to the actuator and/or component such as a control surface. An actuator according to embodiments of the present invention may be adapted to be compliant, that is, to render or yield to the opposing force, thereby substantially eliminating, or at least mitigating, damage to the component and/or the actuator resulting from the opposing force.
The control force may be adapted to move the component, for example, at a desired velocity, distance/stroke or with the required acceleration. Alternatively, the control force may be comprise a holding, or securing, force for controlling movement of the component. For example, where the component to be controlled comprises a control surface of a vessel, the control force may be adapted to move the surface to facilitate control over the direction and/or speed of the vessel.
The opposing force may comprise any force acting against the actuator and may, for example, comprise an impact force. The actuation member may be compliant when it is subject to a predetermined opposing force or where the opposing force exceeds a selected threshold. For example, the threshold may be selected according to the operational requirements of the component, the actuator being configured to overcome or resist a degree of opposing forces, for example, hydrodynamic forces and the like that might be expected during operation. In particular embodiments, the opposing force may result from hydrodynamic forces generated by the passage of fluid over the component, aerodynamic forces such as wind sheer, or from a physical impact, shock load or other engagement.
The actuator may be adapted to apply the control force to the component irrespective of the opposing force. Thus, where the opposing force exceeds the selected force threshold, the actuation member will retreat while still applying the control force. Beneficially, acceleration of the component and actuator may be reduced due to the reduced unbalanced force acting between the opposing forces across the component, thereby further reducing the risk of damage to the component and/or the actuator.
The actuator may be of any suitable form and may, for example, comprise a linear actuator. The actuator may comprise an electric linear actuator, although other forms of actuator may be used, where appropriate. In particular embodiments, the actuation member may be at least partially surrounded by a coil or stator. The actuation member may define or provide mounting for a magnet and may be adapted for linear movement in response to an electro-motive force resulting from current flow in the stator, thereby providing the control force for manipulating the component.
The stator may be coupled to the vessel hull and the actuation member may be configured to define a first, retracted, position relative to the stator/vessel and a second, extended, position. The actuation member may be adapted to move from the first position to the second position under the influence of the control force.
The component to be controlled may comprise any suitable component, including, for example, a vessel control surface, sensor array, telecommunication antenna, mast assembly or any other component or assembly.
The actuator may further comprise a sensor for detecting the forces on the actuation member.
The actuator may further comprise a transmission system for transmitting sensor information to and from a control system. For example, the control system may be adapted to control the current to the stator to assist in mitigating damage to the actuator and the component.
These and other aspects of the present invention will now be described, by way of example only, with reference to the accompanying drawings, in which:
Referring initially to
As shown in
In use, the control force “Fc” will overcome opposing forces up to and including a selected threshold, for example, resulting from hydro-dynamic resistance and the like.
Referring now to
Referring now to
By reversing the direction of current flow, the control force “Fc” is reversed to return the actuator 10 to the first position.
It should be understood that the embodiments described are merely exemplary of the present invention and that various modifications may be made without departing from the scope of the invention.
For example, as an alternative or in addition to reversing the direction of current flow, the actuator may comprise a return mechanism, such as a spring biasing mechanism to return the shaft to the retracted or parked position. This may function as a fail safe in the event of loss of power to the actuator to prevent damage to the control surface. Alternatively, the actuator may be capable of returning to the first position by gravity or under the under the mass of the control surface and shaft or by any other suitable means
Number | Date | Country | Kind |
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0920249.0 | Nov 2009 | GB | national |