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公开(公告)号:US11427314B2
公开(公告)日:2022-08-30
申请号:US15980452
申请日:2018-05-15
Applicant: Bell Textron Inc.
Inventor: Kynn Jerald Schulte , Troy Cyril Schank
Abstract: In one embodiment, a local control system for a rotor assembly of an apparatus includes a first actuator disposed in the rotor assembly and configured to control motion of a first controllable element in the rotor assembly. The rotor assembly is mounted to the apparatus and is rotated responsive to torque and rotational energy provided thereto. The local control system also includes a first sensor disposed in the rotor assembly and configured to provide position feedback in relation to the first controllable element. The local control system also includes a first local control computer disposed in the rotor assembly and communicably coupled to a first central control computer disposed in the apparatus external to the rotor assembly, where the first local control computer is configured to transmit a control signal to the first actuator and receive a feedback signal from the first sensor.
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公开(公告)号:US20230192276A1
公开(公告)日:2023-06-22
申请号:US17555024
申请日:2021-12-17
Applicant: Bell Textron Inc.
Inventor: Kyle Thomas Cravener , Patrick Smith , Troy Cyril Schank , Brady Garrett Atkins , Kynn Jerald Schulte
CPC classification number: B64C27/008 , B64C27/35 , G01D5/145
Abstract: A rotor-hub flap-measurement system includes a rotor hub operable to flap relative to a main-rotor axis, a flap-linkage arm, a first end of the flap-linkage arm rotatably coupled to the rotor hub, the flap-linkage arm responsive to flapping of the rotor hub, and a magneto-resistive sensor system rotatably coupled to a second end of the flap-linkage arm and responsive to movement of the flap-linkage arm.
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公开(公告)号:US12145721B2
公开(公告)日:2024-11-19
申请号:US17555024
申请日:2021-12-17
Applicant: Bell Textron Inc.
Inventor: Kyle Thomas Cravener , Patrick Smith , Troy Cyril Schank , Brady Garrett Atkins , Kynn Jerald Schulte
Abstract: A rotor-hub flap-measurement system includes a rotor hub operable to flap relative to a main-rotor axis, a flap-linkage arm, a first end of the flap-linkage arm rotatably coupled to the rotor hub, the flap-linkage arm responsive to flapping of the rotor hub, and a magneto-resistive sensor system rotatably coupled to a second end of the flap-linkage arm and responsive to movement of the flap-linkage arm.
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公开(公告)号:US11971277B2
公开(公告)日:2024-04-30
申请号:US17555104
申请日:2021-12-17
Applicant: Bell Textron Inc.
Inventor: Kyle Thomas Cravener , Patrick Smith , Troy Cyril Schank , Brady Garrett Atkins , Kynn Jerald Schulte
Abstract: A rotor-hub-flap anisotropic-sensor system includes a rotor hub, a plurality of anisotropic-sensor arrangements interoperably coupled to the rotor hub and operable to measure flapping of the rotor hub, a plurality of rotor blades connected to the rotor hub, and at least one flight control computer interoperably coupled to the plurality of anisotropic-sensor arrangements.
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公开(公告)号:US20230194312A1
公开(公告)日:2023-06-22
申请号:US17555104
申请日:2021-12-17
Applicant: Bell Textron Inc.
Inventor: Kyle Thomas Cravener , Patrick Smith , Troy Cyril Schank , Brady Garrett Atkins , Kynn Jerald Schulte
IPC: G01D5/16
Abstract: A rotor-hub-flap anisotropic-sensor system includes a rotor hub, a plurality of anisotropic-sensor arrangements interoperably coupled to the rotor hub and operable to measure flapping of the rotor hub, a plurality of rotor blades connected to the rotor hub, and at least one flight control computer interoperably coupled to the plurality of anisotropic-sensor arrangements.
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