发明名称 |
Integrated divergent exhaust nozzle thrust reverser |
摘要 |
A relatively simple variable area divergent exhaust nozzle and low drag afterbody integrated with a target-type thrust reverser and used in conjunction with a convergent nozzle for application to the propulsion system of a high performance jet powered aircraft. Two or more aerodynamically shaped afterbody surfaces may be pivoted with a common actuation system to form: first an efficient nozzle-afterbody suitable for subsonic operation; second, a divergent nozzle-afterbody for efficient supersonic operation and; third, a target-type thrust reverser for in-flight or ground roll deceleration.
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申请公布号 |
US4093122(A) |
申请公布日期 |
1978.06.06 |
申请号 |
US19760738578 |
申请日期 |
1976.11.03 |
申请人 |
ROHR INDUSTRIES, INC. |
发明人 |
LINDERMAN, DUANE L.;HOM, FELIX |
分类号 |
F02K1/11;F02K1/60;(IPC1-7):B64C15/06;B64D33/04 |
主分类号 |
F02K1/11 |
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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