发明名称 |
MULTI-MODE TILTROTOR NACELLE CONTROL SYSTEM |
摘要 |
<p>A tiltrotor aircraft (11) has a multi-mode tiltrotor nacelle control system with integrated envelope protection (13). The tiltrotor aircraft (11) has a fuselage (15), a tail section (17), a left wing member (21a), a right wing member (21b), a right engine nacelle (23b), a left engine nacelle (23a), a left proprotor (25a), and a right proprotor (25b). Activation of the nacelle control system causes preselected rotational movement of the tiltrotor assembly.</p> |
申请公布号 |
EP1282555(B1) |
申请公布日期 |
2010.08.18 |
申请号 |
EP20010935546 |
申请日期 |
2001.05.16 |
申请人 |
BELL HELICOPTER TEXTRON INC. |
发明人 |
KING, DAVID, W.;SHULTZ, PETER, M. |
分类号 |
B64C29/00;B64C13/04;B64C13/50;B64C27/56;B64D31/02 |
主分类号 |
B64C29/00 |
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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