发明名称 |
Method and apparatus for rolling control of airplanes by means of spoilers |
摘要 |
This invention relates to a method for rolling control of an airplane by means of spoilers mounted at lift surfaces, which comprises subdividing the entire control range into a plurality of firmly graduated and successively adjustable control steps, and adjusting the individual control steps by means of a series of different partial spoiler surfaces actuatable in dependence upon each other either individually or in combination. The invention also relates to an apparatus for performing the method.
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申请公布号 |
US4270712(A) |
申请公布日期 |
1981.06.02 |
申请号 |
US19790057447 |
申请日期 |
1979.07.13 |
申请人 |
DORNIER GMBH |
发明人 |
VON DER DECKEN, JAN;MAX, HEINZ |
分类号 |
B64C9/00;(IPC1-7):B64C9/32;B64C13/32 |
主分类号 |
B64C9/00 |
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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