Invention Grant
- Patent Title: Method for constructing a rotor blade intended for a rotorcraft, blade and rotorcraft
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Application No.: US17328896Application Date: 2021-05-24
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Publication No.: US11691719B2Publication Date: 2023-07-04
- Inventor: Alexandre Madeira , Francois Malburet , Lionel Roucoules
- Applicant: AIRBUS HELICOPTERS
- Applicant Address: FR Marignane
- Assignee: AIRBUS HELICOPTERS
- Current Assignee: AIRBUS HELICOPTERS
- Current Assignee Address: FR Marignane
- Agency: Brooks Kushman P.C.
- Priority: FR 05703 2020.05.29
- Main IPC: B64C27/467
- IPC: B64C27/467 ; B64C27/473

Abstract:
A blade in which the aerodynamic profiles of a blade root, a blade neck and a central part of a profiled zone of the blade respectively comprise a leading edge section and a trailing edge section that are symmetrical to each other relative to an axis of symmetry. The present disclosure also concerns a method for constructing such a blade. The axis of symmetry is perpendicular to a segment connecting the leading edge to the trailing edge of each profile and is positioned in the middle of the segment. An intermediate upper surface section and an intermediate lower surface section connect the leading edge section and the trailing edge section in order to respectively form a lower surface of the aerodynamic profile.
Public/Granted literature
- US20210371095A1 METHOD FOR CONSTRUCTING A ROTOR BLADE INTENDED FOR A ROTORCRAFT, BLADE AND ROTORCRAFT Public/Granted day:2021-12-02
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