Control surface actuation system
AssigneeHer Majesty in Right of Canada as Represented by the Minister of National Defence
InventorsFrank Wong, Camille Alain Rabbath, Nicholas Lechevin, Olivier Boissonneault
Life of this patent
Estimating the term…
Abstract
Systems for controlling flow effector control surfaces. The system comprises a flow effector control coupled to an elongated bar at one end of the bar. The elongated bar is coupled at the other end to the middle of a T-shaped member. A compliant link is coupled to the bar between the control surface and the T-shaped member. At each end of the T-shaped member is coupled a shape memory alloy wire which acts as an actuating means. When one of the shape memory alloy wire contracts, the elongated bar pivots about the compliant link and activates or retracts the flow effector control surface.
Claims5
A system for controlling a control surface on a missile, the system comprising:
- a control surface;
- an elongated member coupled to said control surface of said missile, said elongated member having a first member end and a second member end;
- a T-shaped bar coupled to said elongated member, said bar having a first bar end and a second bar end;
- a pivotable link coupled to said elongated member;
- first actuator means coupled to said T-shaped bar at said first bar end;
- second actuator means coupled to said T-shaped bar at said second bar end;
- wherein
- said control surface is coupled to said elongated member at said first member end of said elongated member;
- said T-shaped bar is coupled to said elongated member at said second member end of said elongated member, said second member end being coupled to said T-shaped bar at a point between said first bar end and said second bar end;
- when either said first or second actuator means is actuated, said elongated member pivots about said pivotable link to deploy or retract said control surface.
Dependencies are inferred from the claim text.