Invention Grant
- Patent Title: Tail rotor configurations for rotorcraft yaw control systems
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Application No.: US17108592Application Date: 2020-12-01
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Publication No.: US11772785B2Publication Date: 2023-10-03
- Inventor: Marc Ouellet , Guillaume Biron , Alexis Dugré , Thuvaragan Senthilnathan
- Applicant: Textron Innovations Inc.
- Applicant Address: US RI Providence
- Assignee: Textron Innovations Inc.
- Current Assignee: Textron Innovations Inc.
- Current Assignee Address: US RI Providence
- Agency: Lawrence Youst PLLC
- Main IPC: B64C27/82
- IPC: B64C27/82 ; B64C27/00
Abstract:
A yaw control system coupled to a tailboom of a helicopter includes tail rotors. The tail rotors include a clockwise tail rotor and a counterclockwise tail rotor. The clockwise tail rotor is configured to rotate in a first rotational direction. The counterclockwise tail rotor is configured to rotate in a second rotational direction, the second rotational direction opposite of the first rotational direction.
Public/Granted literature
- US20220169375A1 Tail Rotor Configurations for Rotorcraft Yaw Control Systems Public/Granted day:2022-06-02
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