- Patent Title: Composite yoke fitting for bearing attachment to rotorcraft blade
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Application No.: US14669977Application Date: 2015-03-26
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Publication No.: US10654567B2Publication Date: 2020-05-19
- Inventor: Andrew Haldeman , Frank Bradley Stamps , Drew Sutton
- Applicant: Bell Helicopter Textron Inc.
- Applicant Address: US TX Fort Worth
- Assignee: BELL HELICOPTER TEXTRON INC.
- Current Assignee: BELL HELICOPTER TEXTRON INC.
- Current Assignee Address: US TX Fort Worth
- Main IPC: B64C27/46
- IPC: B64C27/46 ; B64C27/48 ; B64C27/473

Abstract:
A rotor blade assembly includes a rotor blade comprising an inboard end and an outboard end. A composite yoke fitting made from a composite material is attached to the rotor blade. The composite yoke fitting includes an outboard portion inserted into the inboard end of the rotor blade, an inboard portion, and a flexure region about which the rotor blade is configured to flex. The inboard portion and the flexure region are outside the rotor blade.
Public/Granted literature
- US20160280367A1 COMPOSITE YOKE FITTING FOR BEARING ATTACHMENT TO ROTORCRAFT BLADE Public/Granted day:2016-09-29
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