发明名称 |
Thrust reverser system for an aircraft |
摘要 |
<p>Aircraft systems including cascade thrust reversers are disclosed herein. An aircraft system in accordance with one embodiment includes a cascade thrust reverser having a fixed reverser ramp and a nozzle outer wall section at least partially aft of the fixed reverser ramp. The nozzle outer wall section is movable between a deployed position and a stowed position. The nozzle outer wall section includes a forward portion with a leading edge section. The fixed reverser ramp has a portion forward of and adjacent to the nozzle outer wall section when the nozzle outer wall section is in the stowed position. The portion of the fixed reverser ramp has a first slope. The forward portion of the nozzle outer wall section that is aft of the leading edge section has a second slope different than the first slope.</p> |
申请公布号 |
EP1726812(B1) |
申请公布日期 |
2014.09.24 |
申请号 |
EP20060008143 |
申请日期 |
2006.04.20 |
申请人 |
THE BOEING COMPANY |
发明人 |
THORNOCK, RUSSEL L.;SANGWIN, MICHAEL L.;HSIAO, ENTSUNG |
分类号 |
F02K1/64;F02K1/72 |
主分类号 |
F02K1/64 |
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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