发明名称 |
Vibration isolation engine mount system and method for ducted fans |
摘要 |
A vibration isolation engine mount system and method for ducted fan aircraft, such as ducted fan vertical takeoff and landing (VTOL) aircraft, includes an engine for driving the ducted fan. The system includes an engine support structure for supporting the engine within the ducted fan. A rotor of the ducted fan is coupled to an engine shaft of the engine via a rotor hub. The system includes a plurality of vibration isolators configured to mount the engine to the engine support structure. Each of the plurality of vibration isolators is substantially concentrically oriented along a surface of a sphere. A center of the sphere is located at a center of the rotor hub.
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申请公布号 |
US2006248873(A1) |
申请公布日期 |
2006.11.09 |
申请号 |
US20050228336 |
申请日期 |
2005.09.19 |
申请人 |
PARKS ROBERT;LEDE JEAN-CHARLES |
发明人 |
PARKS ROBERT;LEDE JEAN-CHARLES |
分类号 |
F02K99/00 |
主分类号 |
F02K99/00 |
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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