Vehicle control system and method employing control surface and geared tab
AssigneeThe Boeing Company
InventorMark G. Brislawn
Life of this patent
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AssigneeThe Boeing Company
InventorMark G. Brislawn
Estimating the term…
Control systems and methods for a vehicle such as an aircraft or watercraft employ a trailing edge control surface that is pivotal about a pivot axis fixed relative to the vehicle and is deflected to create control forces, and a tab pivotally mounted to an aft end of the control surface. An aft end of a linkage is connected to the tab spaced from the tab pivot axis, and the linkage extends forward to a forward end that is coupled to fixed vehicle structure, such that deflection of the control surface causes a deflection of the tab as long as the forward end of the linkage does not lie in line with the control surface pivot axis, the in-line position defining a neutral position of the linkage. A gearing control actuator is coupled to the linkage and is operable to position the forward end of the linkage at selectively variable distances on one or the other side of the neutral position, thus providing variable gearing ratios between the control surface and the tab. Tab gearing ratio can be varied as a function of vehicle operating condition. An alternative control system includes a backup tab actuator for providing tab deflection upon failure of the actuator system that deflects the control surface. The tab can be used as a control tab for providing the motive force for moving the control surface, or the tab can be used as a mini control surface by locking the control surface in a fixed position.
A control system for a vehicle having a trailing edge control surface mounted for pivotal movement about a control surface pivot axis fixed relative to the vehicle, and a control surface actuator connected between the vehicle and the control surface and operable to pivotally move the control surface, the control system comprising:
A control system for a vehicle having a trailing edge control surface mounted for pivotal movement about a control surface pivot axis fixed relative to the vehicle, and a control surface actuator connected between the vehicle and the control surface and operable to pivotally move the control surface about the control surface pivot axis, the control system comprising:
A method for controlling an aircraft having a trailing edge control surface mounted to the aircraft such that the control surface is pivotally movable relative to the aircraft about a control surface pivot axis, and having a tab connected to the control surface such that the tab is pivotally movable relative to the control surface about a tab pivot axis, the method comprising:
Dependencies are inferred from the claim text.