Aircraft attitude control configuration
Number of patents in Portfolio can not be more than 2000
United States of America Patent
Stats
-
Dec 13, 2011
Grant Date -
Nov 19, 2009
app pub date -
Jul 22, 2009
filing date -
Nov 9, 2005
priority date (Note) -
In Force
status (Latency Note)
Importance
Abstract
An aircraft attitude control configuration enables control surfaces to provide attitude control for an aircraft at hover or low air speed conditions. The aircraft attitude control configuration includes a plurality of thrusters mounted to an aircraft for thrusting air, a first control surface kinematically coupled to the aircraft at a position downstream of a first thruster to enable a first vector force to be generated by a portion of the thrusted air from the first thruster on the first control surface, and a second control surface kinematically coupled to the aircraft at a position downstream of a second thruster, the first and the second control surfaces being displaced symmetrically on opposite sides of a longitudinal axis of the aircraft, the second control surface being configured to be independently and differentially movable with respect to the first control surface to enable a second vector force to be generated by a portion of the thrusted air from the second thruster on the second control surface.
First Claim
Family
International Classification(s)
Cited Art Landscape
| Patent Info | (Count) | # Cites | Year |
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| 4449703 Apparatus for bonding main rotor blades | 10 | 1982 | |
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| 2007/0271,008 MANUAL AND COMPUTERIZED FLIGHT CONTROL SYSTEM WITH NATURAL FEEDBACK | 9 | 2006 | |
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| 6431494 Flight control system for a hybrid aircraft in the roll axis | 29 | 2001 | |
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| * 2003/0061,168 Method for generating customer secure card numbers | 41 | 2001 | |
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| 6896221 Vertical takeoff and landing aircraft | 15 | 2003 | |
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