- 专利标题: Tiltrotor with Inboard Engines
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申请号: US14960486申请日: 2015-12-07
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公开(公告)号: US20170158323A1公开(公告)日: 2017-06-08
- 发明人: Brent C. Ross , Steven R. Ivans
- 申请人: Bell Helicopter Textron Inc.
- 申请人地址: US TX Fort Worth
- 专利权人: Bell Helicopter Textron Inc.
- 当前专利权人: Bell Helicopter Textron Inc.
- 当前专利权人地址: US TX Fort Worth
- 主分类号: B64C29/00
- IPC分类号: B64C29/00 ; B64C27/26 ; B64C3/18 ; B64D35/08
摘要:
According to one embodiment, an aircraft features a fuselage, a wing coupled to the fuselage, and a first rotor system. The first rotor system includes a first proprotor system and a first engine. The first proprotor system is coupled proximate to a first wing tip of the wing and is tiltable between a helicopter mode position and an airplane mode position. The first engine is in mechanical communication with the first proprotor system and coupled above the wing, outboard of the fuselage and inboard of the first pylon.
公开/授权文献
- US10183745B2 Tiltrotor with inboard engines 公开/授权日:2019-01-22
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