发明名称 |
Lateral control system |
摘要 |
Apparatus including a spoiler quadrant coupled to the aileron cable control system of the aircraft, rotation of which spoiler quadrant in either direction causes a bell crank to rotate about its pivot point in one direction only from its inactive position. A plurality of links transfer this motion to operate inboard spoilers simultaneously on both sides of the aircraft in response to and proportional to the degree of aileron deflection.
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申请公布号 |
US4142699(A) |
申请公布日期 |
1979.03.06 |
申请号 |
US19770765519 |
申请日期 |
1977.02.04 |
申请人 |
BOEING COMMERCIAL AIRPLANE COMPANY |
发明人 |
ARNQUIST, WILLARD D.;FOSTER, THOMAS G.;ROALSVIG, MELVIN J. |
分类号 |
B64C13/30;(IPC1-7):B64C13/30 |
主分类号 |
B64C13/30 |
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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