发明名称 |
Air intake structure of a turbojet engine nacelle with pneumatic anti-icing |
摘要 |
<p>This assembly comprises a first component (9), a second component (3), and a connecting device (19) for connecting these two components together, this device (19) being of the type that maintains the integrity of the surface of said second component (3), and the assembly being noteworthy in that said connecting device (19) comprises a structural skin (21) fixed to said first component (9) and a porous material (23) attached to this structural skin and fixed by contact to said second component (3).</p> |
申请公布号 |
EP2321510(A2) |
申请公布日期 |
2011.05.18 |
申请号 |
EP20090784308 |
申请日期 |
2009.07.28 |
申请人 |
AIRCELLE |
发明人 |
VAUCHEL, GUY, BERNARD;RUCKERT, GUILLAUME |
分类号 |
F02C7/045;B64D33/02;F02C7/047 |
主分类号 |
F02C7/045 |
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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