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公开(公告)号:US10011349B2
公开(公告)日:2018-07-03
申请号:US15252545
申请日:2016-08-31
Applicant: Bell Helicopter Textron Inc.
Inventor: Steven Ray Ivans , Nathan Gabriel Wu
CPC classification number: B64C29/0033 , B64C3/38 , B64C5/08 , B64C7/02 , B64C11/00 , B64C27/28 , B64C29/02 , Y02T50/14
Abstract: A pylon assembly for a tiltrotor aircraft includes a fixed pylon having an outboard end. A rotor assembly is rotatably coupled to the fixed pylon and is operable to rotate between a generally vertical orientation in a vertical takeoff and landing mode and a generally horizontal orientation in a forward flight mode. The rotor assembly includes a proprotor operable to produce a generally vertical slipstream in the vertical takeoff and landing mode and a generally horizontal slipstream in the forward flight mode. A wing extension is rotatably coupled to the outboard end of the fixed pylon. The wing extension is operable to rotate generally with the rotor assembly such that a minimal dimension of the wing extension remains in the slipstream of the proprotor.
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公开(公告)号:US20180057159A1
公开(公告)日:2018-03-01
申请号:US15252545
申请日:2016-08-31
Applicant: Bell Helicopter Textron Inc.
Inventor: Steven Ray Ivans , Nathan Gabriel Wu
CPC classification number: B64C29/0033 , B64C3/38 , B64C5/08 , B64C7/02 , B64C11/00 , B64C27/28 , B64C29/02
Abstract: A pylon assembly for a tiltrotor aircraft includes a fixed pylon having an outboard end. A rotor assembly is rotatably coupled to the fixed pylon and is operable to rotate between a generally vertical orientation in a vertical takeoff and landing mode and a generally horizontal orientation in a forward flight mode. The rotor assembly includes a proprotor operable to produce a generally vertical slipstream in the vertical takeoff and landing mode and a generally horizontal slipstream in the forward flight mode. A wing extension is rotatably coupled to the outboard end of the fixed pylon. The wing extension is operable to rotate generally with the rotor assembly such that a minimal dimension of the wing extension remains in the slipstream of the proprotor.
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公开(公告)号:US10173771B2
公开(公告)日:2019-01-08
申请号:US15990610
申请日:2018-05-26
Applicant: Bell Helicopter Textron Inc.
Inventor: Steven Ray Ivans , Nathan Gabriel Wu
Abstract: A pylon assembly for a tiltrotor aircraft includes a fixed pylon having an outboard end. A rotor assembly is rotatably coupled to the fixed pylon and is operable to rotate between a a vertical takeoff and landing orientation and a forward flight orientation. The rotor assembly includes a proprotor operable to produce a slipstream. A wing extension is rotatably coupled to the outboard end of the fixed pylon. The wing extension is operable to rotate generally with the rotor assembly such that a minimal dimension of the wing extension remains in the slipstream of the proprotor.
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公开(公告)号:US20180273169A1
公开(公告)日:2018-09-27
申请号:US15990610
申请日:2018-05-26
Applicant: Bell Helicopter Textron Inc.
Inventor: Steven Ray Ivans , Nathan Gabriel Wu
CPC classification number: B64C29/0033 , B64C3/38 , B64C5/08 , B64C7/02 , B64C27/28 , B64C29/02 , Y02T50/14
Abstract: A pylon assembly for a tiltrotor aircraft includes a fixed pylon having an outboard end. A rotor assembly is rotatably coupled to the fixed pylon and is operable to rotate between a a vertical takeoff and landing orientation and a forward flight orientation. The rotor assembly includes a proprotor operable to produce a slipstream. A wing extension is rotatably coupled to the outboard end of the fixed pylon. The wing extension is operable to rotate generally with the rotor assembly such that a minimal dimension of the wing extension remains in the slipstream of the proprotor.
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