发明名称 |
HOT GAS EXHAUST NOZZLE FOR A TURBOJET COMPRISING A DEFLECTOR OF SAID GASES ON THE OUTSIDE THEREOF |
摘要 |
<p>The invention relates to a hot gas exhaust nozzle for an aircraft turbojet, provided such as to be placed in a pod supported by a pylon including a fairing (8) placed near the outer surface of said nozzle (12). The space between said fairing and said nozzle forms a substantially longitudinal channel (10). Said nozzle comprises, on the outer wall (12) thereof, a deflector (20) placed in a transverse plane covering an angular sector located in the channel (10), that is provided such as to come near the fairing (8) without touching same.</p> |
申请公布号 |
WO2014184497(A1) |
申请公布日期 |
2014.11.20 |
申请号 |
WO2014FR51134 |
申请日期 |
2014.05.15 |
申请人 |
AIRCELLE |
发明人 |
ANDRE, VIJAY;GUILLET, ARNAUD;MARIE, NICOLAS |
分类号 |
F02K1/52;B64D27/00;F02C7/25 |
主分类号 |
F02K1/52 |
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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