- Patent Title: Method and apparatus to improve lift to drag ratio of a rotor blade
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Application No.: US15843039Application Date: 2017-12-15
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Publication No.: US10604234B2Publication Date: 2020-03-31
- Inventor: Christopher E. Foskey , Brendan P. Lanigan
- 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
- Agency: Timmer Law Group, PLLC
- Main IPC: B64C11/18
- IPC: B64C11/18 ; B64C11/24 ; B64C27/473 ; F03D1/06 ; B64C29/00

Abstract:
In a first aspect, there is a method for improving a lift to drag ratio of a rotor blade, including providing a blade member having a leading edge and a trailing edge; providing a leading edge extension member; and coupling the leading edge extension member to a portion of the leading edge of the blade member to form the rotor blade. In a second aspect, there is a rotor blade including a blade member having a leading edge, and a trailing edge; and a leading edge extension member disposed on the leading edge of the blade member, wherein the leading edge extension member is configured to extend the chord length of at least a portion of the rotor blade. In a third aspect, there is a leading edge extension member for a rotor blade including a convex exterior surface configured to extend at least a portion of the chord length of the rotor blade.
Public/Granted literature
- US20180362145A1 METHOD AND APPARATUS TO IMPROVE LIFT TO DRAG RATIO OF A ROTOR BLADE Public/Granted day:2018-12-20
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