发明名称 |
SELF-ALIGNING INLET PLENUM SYSTEM FOR ROTORCRAFT |
摘要 |
<p>An inlet system for a rotorcraft includes a cowl door assembly and a plenum assembly. The cowl door assembly includes a door member, a cowl inlet opening, and a cowl inlet duct. The plenum assembly is configured to free float in relation to the cowl door. The plenum assembly includes a plenum duct with a plenum band configured to attach the plenum assembly to an inlet opening. An aft seal is located between the aft plenum flange and a firewall, the aft seal being configured to provide a compressive contact between the plenum assembly and the firewall.</p> |
申请公布号 |
EP2678226(B1) |
申请公布日期 |
2015.01.21 |
申请号 |
EP20110864163 |
申请日期 |
2011.04.28 |
申请人 |
BELL HELICOPTER TEXTRON INC. |
发明人 |
DAILEY, ZACHARY, E.;MAST, THOMAS, M. |
分类号 |
B64D33/02 |
主分类号 |
B64D33/02 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|