发明名称 |
Tilt Rotor Aircraft with Fixed Engine Arrangement |
摘要 |
The system of the present application includes an engine and pylon arrangement for a tilt rotor aircraft in which the engine is fixed in relation to a wing portion of the aircraft, while the pylon is rotatable. The pylon supports a rotor hub having a plurality of rotor blades. Rotation of the pylon allows the aircraft to selectively fly in a helicopter mode and an airplane mode, as well as any combination thereof. |
申请公布号 |
US2012199699(A1) |
申请公布日期 |
2012.08.09 |
申请号 |
US201213357981 |
申请日期 |
2012.01.25 |
申请人 |
ISAAC MARK L.;ELLIOTT DAVID A.;ROSS BRENT C.;BELL HELICOPTER TEXTRON INC. |
发明人 |
ISAAC MARK L.;ELLIOTT DAVID A.;ROSS BRENT C. |
分类号 |
B64C27/26;B64D35/00 |
主分类号 |
B64C27/26 |
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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