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公开(公告)号:US11091258B2
公开(公告)日:2021-08-17
申请号:US16442288
申请日:2019-06-14
Applicant: Bell Textron Inc.
Inventor: Kirk L. Groninga , Daniel B. Robertson
Abstract: An exemplary tiltrotor aircraft having a vertical takeoff and landing (VTOL) flight mode and a forward flight mode includes tiltable rotors located at forward boom ends, tiltable ducted fans located at wings aft of the forward boom ends, and aft rotors located on aft boom portions.
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公开(公告)号:US11613375B2
公开(公告)日:2023-03-28
申请号:US16414402
申请日:2019-05-16
Applicant: Bell Textron Inc.
Inventor: Kirk L. Groninga , Daniel B. Robertson
Abstract: An exemplary dual motor input includes a common shaft for coupling to a member to be rotationally driven, a first motor rotationally coupled to a first drive shaft, the first drive shaft coupled to the common shaft, and a second motor rotationally coupled to a second drive shaft, the second drive shaft coupled to the common shaft.
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公开(公告)号:US11873085B2
公开(公告)日:2024-01-16
申请号:US17366834
申请日:2021-07-02
Applicant: Bell Textron Inc.
Inventor: Kirk L. Groninga , Daniel B. Robertson
CPC classification number: B64C29/0033 , B64C29/0025 , B64C39/04 , B64D2027/026
Abstract: An exemplary tiltrotor aircraft having a vertical takeoff and landing (VTOL) flight mode and a forward flight mode includes tiltable rotors located at forward boom ends, tiltable ducted fans located at wings aft of the forward boom ends, and aft rotors located on aft boom portions.
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公开(公告)号:US11117655B2
公开(公告)日:2021-09-14
申请号:US16436406
申请日:2019-06-10
Applicant: Bell Textron Inc.
Inventor: Kirk L. Groninga , Daniel B. Robertson
Abstract: An exemplary tail rotor includes a first blade assembly configured to rotate in a first direction about an axis of rotation and a second blade assembly configured to rotate in a second direction about the axis of rotation.
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公开(公告)号:US12246827B1
公开(公告)日:2025-03-11
申请号:US18530482
申请日:2023-12-06
Applicant: Bell Textron Inc.
Inventor: Kirk L. Groninga , Daniel B. Robertson
Abstract: An exemplary tiltrotor aircraft having a vertical takeoff and landing (VTOL) flight mode and a forward flight mode includes tiltable rotors located at forward boom ends, tiltable ducted fans located at wings aft of the forward boom ends, and aft rotors located on aft boom portions.
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公开(公告)号:US11097838B2
公开(公告)日:2021-08-24
申请号:US16442180
申请日:2019-06-14
Applicant: Bell Textron Inc.
Inventor: Kirk L. Groninga , Daniel B. Robertson , Matthew E. Louis
Abstract: An exemplary ducted fan with an optimized stator includes a duct surrounding a rotor hub from which blades radially extend and the stator having a stator span extending horizontally across an inside diameter of the duct, the stator having a stator chord extending from a leading edge to a trailing edge, wherein a length of the stator chord varies across the stator span.
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