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公开(公告)号：US20210107625A1
公开(公告)日：2021-04-15
申请号：US17069816
申请日：2020-10-13
Applicant: Bell Textron Inc.
Inventor： Luke Dafydd Gillett , James Rigsby , Jeffrey Kirkman , Craig Lovell , Andrew Carter , Aaron Alexander Acee
Abstract: A rotorcraft has a horizontal stabilizer movable about an axis of rotation and a horizontal stabilizer control system configured to control the horizontal stabilizer to at least one of move the rotorcraft into a minimum drag position, maintain the aircraft in a minimum drag position, efficiently achieve a maneuver, enter efficient autorotation, and maintain efficient autorotation.
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公开(公告)号：USD894814S1
公开(公告)日：2020-09-01
申请号：US29707473
申请日：2019-09-27
Applicant: Bell Textron Inc.
Designer： James Everett Kooiman , Michael Edwin Rinehart , Lynn Francis Eschete , Jason Paul Winter , Derek Ray Eddins , Steven Allen Robedeau, Jr. , Clegg Benjamin Brian Smith , Mark Loring Isaac , Andrew Thomas Carter , Aaron Alexander Acee , Glenn Alan Shimek , Jared Mark Paulson , Andrew Paul Haldeman , Brent Chadwick Ross , Steven Ray Ivans
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公开(公告)号：US20210394894A1
公开(公告)日：2021-12-23
申请号：US16905558
申请日：2020-06-18
Applicant: Bell Textron Inc.
Inventor： Albert G. Brand , Michael S. Seifert , Andrew Thomas Carter , Aaron Alexander Acee
Abstract: One embodiment includes a rotary aircraft, including: a main drive rotor; an aircraft body mechanically coupled to the main drive rotor; and first and second flight assist wings passively rotatably coupled to the aircraft body.
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公开(公告)号：US11414184B2
公开(公告)日：2022-08-16
申请号：US16354591
申请日：2019-03-15
Applicant: Bell Textron Inc.
Inventor： Aaron Alexander Acee , Andrew Paul Haldeman , Eric Albert Sinusas , Yann Lavallee , Albert G. Brand
Abstract: An exemplary electric distributed propulsion system includes two or more rotors that are individually controlled by the rotational speed of associated motors, an input control connected to the associated motors to provide rotational speed control to the two or more rotors to produce a desired net thrust, and a logic connected to the input control and the associated motors, the logic for controlling speed and direction of the two or more rotors to achieve the desired net thrust and to avoid a motor speed condition.
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公开(公告)号：US20210122460A1
公开(公告)日：2021-04-29
申请号：US16666347
申请日：2019-10-28
Applicant: Bell Textron Inc.
Inventor： Aaron Alexander Acee
Abstract: A rotorcraft having pusher propeller generated power during autorotations. The rotorcraft has an engine powered mode and an autorotation mode. The rotorcraft includes an engine and a drivetrain configured to receive torque and rotational energy from the engine in the engine powered mode. A main rotor system is coupled to the drivetrain and is rotatable to generate lift and forward thrust for the rotorcraft in the engine powered mode. A pusher propeller is coupled to the drivetrain and is rotatable to generate forward thrust for the rotorcraft in the engine powered mode. In the autorotation mode, the pusher propeller is aerodynamically driven responsive to airflow therethrough and the drivetrain is configured to receive torque and rotational energy from the pusher propeller, thereby providing power to the main rotor system.
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Patent Agency Ranking
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公开(公告)号：US12202594B2
公开(公告)日：2025-01-21
申请号：US17165068
申请日：2021-02-02
Applicant: Bell Textron Inc.
Inventor： Eric Albert Sinusas , Edward Lambert , Yann Lavallee , Aaron Alexander Acee , Albert G. Brand
Abstract: An aircraft having an electric motor coupled to a rotor and an instrument electronically connected to the electric motor and configured to communicate a time available value before a motor condition reaches a motor condition limit.
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公开(公告)号：US11814162B2
公开(公告)日：2023-11-14
申请号：US16905558
申请日：2020-06-18
Applicant: Bell Textron Inc.
Inventor： Albert G. Brand , Michael S. Seifert , Andrew Thomas Carter , Aaron Alexander Acee
Abstract: One embodiment includes a rotary aircraft, including: a main drive rotor; an aircraft body mechanically coupled to the main drive rotor; and first and second flight assist wings passively rotatably coupled to the aircraft body.
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公开(公告)号：US11685515B2
公开(公告)日：2023-06-27
申请号：US17069816
申请日：2020-10-13
Applicant: Bell Textron Inc.
Inventor： Luke Dafydd Gillett , James Rigsby , Jeffrey Kirkman , Craig Lovell , Andrew Carter , Aaron Alexander Acee
CPC classification number: B64C13/16 , B64C5/02 , B64C5/16 , B64C27/06 , B64C2027/8281
Abstract: A rotorcraft has a horizontal stabilizer movable about an axis of rotation and a horizontal stabilizer control system configured to control the horizontal stabilizer to at least one of move the rotorcraft into a minimum drag position, maintain the aircraft in a minimum drag position, efficiently achieve a maneuver, enter efficient autorotation, and maintain efficient autorotation.
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公开(公告)号：US20220126991A1
公开(公告)日：2022-04-28
申请号：US17082601
申请日：2020-10-28
Applicant: Bell Textron Inc.
Inventor： Aaron Alexander Acee , Andrew Paul Haldeman , Paul Wayne Woolbright , Timothy McClellan Mosig
Abstract: A rotor system includes a drive hub, a set of rotor blades extending radially from the drive hub, and a set of tension-torsion straps connecting the rotor blades to the drive hub. The drive hub has a rotor mast opening extending along a mast axis. The rotor system is configured to rotate about the mast axis. The drive hub further has a set of mounting slots for mounting the tension-torsion straps. The mounting slots are arranged along a circle around the drive hub, each mounting slot extending through the drive hub along a respective mounting axis. The mounting axis of each of the mounting slots is biased relative to the mast axis. The tension-torsion straps are mounted to the drive hub at their corresponding mounting slots.
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