发明名称 |
AIR INTAKE FOR AIRCRAFT NACELLE, AND PROPULSION ASSEMBLY INCLUDING SUCH AIR INTAKE |
摘要 |
<p>The invention relates to an air intake for an aircraft nacelle that comprises a shroud (19) that can be mounted on the fan casing (15) of a turbojet engine (1). The shroud (19) is sized so as to define a circumferential gap (J) relative to the casing (15). Punctual linking means (27, 33) between the shroud (19) and the casing (15) are discretely distributed at the periphery of said shroud (19).</p> |
申请公布号 |
EP2238031(A1) |
申请公布日期 |
2010.10.13 |
申请号 |
EP20090716599 |
申请日期 |
2009.01.21 |
申请人 |
AIRCELLE |
发明人 |
VAUCHEL, GUY, BERNARD;BEILLIARD, STEPHANE;BRAVIN, FABIEN;VALLEROY, LAURENT, GEORGES |
分类号 |
B64D29/00;B64D33/02 |
主分类号 |
B64D29/00 |
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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