发明名称 |
Three axis flap control system |
摘要 |
A three axis control system employing four flaps is disclosed. The flaps are of uniform design, which decreases machining and manufacturing costs. The flaps are positioned on a vehicle orthogonally, but offset from a vehicle centerline. The system provides not only pitch and yaw control, but also bi-directional roll control with a minimum number of parts and minimal infringement of packaging envelope. The system provides quick response and increased capability for difficult maneuvers and is useable for hypersonic/supersonic applications.
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申请公布号 |
US6502785(B1) |
申请公布日期 |
2003.01.07 |
申请号 |
US20000714455 |
申请日期 |
2000.11.17 |
申请人 |
LOCKHEED MARTIN CORPORATION |
发明人 |
TETER ROGER D.;KUDLICK DEAN A.;WILLIAMS RICHARD M. |
分类号 |
F42B10/64;(IPC1-7):G06E19/00;F42B10/00 |
主分类号 |
F42B10/64 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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