Invention Grant
- Patent Title: Blade fold system using flap hinge
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Application No.: US15336195Application Date: 2016-10-27
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Publication No.: US10933992B2Publication Date: 2021-03-02
- Inventor: Bryan Kenneth Baskin , Frank P. D'Anna , Mark R. Alber
- Applicant: Sikorsky Aircraft Corporation
- Applicant Address: US CT Stratford
- Assignee: Sikorsky Aircraft Corporation
- Current Assignee: Sikorsky Aircraft Corporation
- Current Assignee Address: US CT Stratford
- Agency: Foley & Lardner LLP
- Main IPC: B64C29/02
- IPC: B64C29/02 ; B64C11/28 ; B64C27/50

Abstract:
A rotor system of a tail-sitter aerial vehicle configured to rotate about an axis of rotation is provided including a rotor hub which rotates about the axis of rotation and at least one rotor blade operably coupled to the rotor hub. The at least one rotor blade is configured to rotate about a folding axis between an extended position where the at least one rotor blade is substantially within a plane perpendicular to the axis of rotation and a stowed position where the rotor blade is arranged out of the plane of at an angle less than ninety degrees to the axis of rotation.
Public/Granted literature
- US20170297678A1 BLADE FOLD SYSTEM USING FLAP HINGE Public/Granted day:2017-10-19
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