发明名称 |
Thrust vector control for aircraft |
摘要 |
The invention is directed to a thrust vector control for aircraft with one or more jet engines whose thrust nozzles have an adjustable size exist cross-section, each of the jet engines having a ring rudder axially spaced behind the engine and movable about at least one pivot axis extending substantially perpendicular to the engine's longitudinal axis. A substantially planar rudder plate is secured diagonally in the inside cross-section of the ring rudder for each plane defined by each pivot axis and the longitudinal axis of the engine. The rudder plate or plates each consist of a material which is stable at high temperatures without supplementary cooling and which is mechanically loadable, and the connection between the rudder plate or plates and the ring rudder each include a layer of elastic and thermo-insulating material.
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申请公布号 |
US4809932(A) |
申请公布日期 |
1989.03.07 |
申请号 |
US19870134364 |
申请日期 |
1987.12.17 |
申请人 |
MESSERSCHMITT-BOEKOW-BLOHM GMBH |
发明人 |
MUELLER, WERNER |
分类号 |
B64C15/02;F02K1/00;(IPC1-7):B64C15/00 |
主分类号 |
B64C15/02 |
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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