Asymmetrical control surface system for tube-launched air vehicles
First Claim
1. Asymmetrical control surface system for an air vehicle, the air vehicle having a horizontal midplane axis, a controlling computer, vertical tails and further being stowable in and launchable from a tube, said asymmetrical control surface system comprising:
- a plurality of stowable wings, said wings being deployable upon launch of the air vehicle from the tube, at least one of said wings being movably attached to the vehicle above said midplane axis and at least one of said wings being movably attached to the vehicle below said midplane axis;
a plurality of horizontal tails, at least one of said horizontal tails being movably attached to the vehicle above said midplane axis and at least one of said horizontal tails being movably attached to the vehicle below said midplane axis; and
a means to deploy said wings and horizontal tails in response to the controlling computer.
1 Assignment
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Accused Products
Abstract
Asymmetrical Control Surface System for Tube-Launched Air Vehicles places one control surface, such as a wing or a horizontal tail, above horizontal midplane axis of an air vehicle, such as a tube-launched missile, and the opposing control surface below the midplane axis. Such asymmetrical arrangement of the control surfaces increases the lift and maneuverability of the air vehicle during flight. For stowage inside the tube prior to launch, each control surface slides into its corresponding slot in the body of the vehicle, making the entire control system compact.
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Citations
7 Claims
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1. Asymmetrical control surface system for an air vehicle, the air vehicle having a horizontal midplane axis, a controlling computer, vertical tails and further being stowable in and launchable from a tube, said asymmetrical control surface system comprising:
- a plurality of stowable wings, said wings being deployable upon launch of the air vehicle from the tube, at least one of said wings being movably attached to the vehicle above said midplane axis and at least one of said wings being movably attached to the vehicle below said midplane axis;
a plurality of horizontal tails, at least one of said horizontal tails being movably attached to the vehicle above said midplane axis and at least one of said horizontal tails being movably attached to the vehicle below said midplane axis; and
a means to deploy said wings and horizontal tails in response to the controlling computer. - View Dependent Claims (2, 3, 4, 5, 6, 7)
- a plurality of stowable wings, said wings being deployable upon launch of the air vehicle from the tube, at least one of said wings being movably attached to the vehicle above said midplane axis and at least one of said wings being movably attached to the vehicle below said midplane axis;
Specification