Invention Grant
- Patent Title: Blade with reduced torsional rigidity, and rotor equipped with such a blade
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Application No.: US14315088Application Date: 2014-06-25
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Publication No.: US10661890B2Publication Date: 2020-05-26
- Inventor: Damien Reveillon , Laurent Bianchi
- 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: com.zzzhc.datahub.patent.etl.us.BibliographicData$PriorityClaim@44539014
- Main IPC: B64C27/473
- IPC: B64C27/473 ; F01D5/14 ; B64C27/72 ; B64C11/20

Abstract:
A blade of a rotor for a rotary-wing aircraft is equipped with an outer covering extending along the span of the blade. This outer covering is provided with an extrados skin and with an intrados skin defining a cavity. The blade also includes a structure that extends into the cavity and connects the blade to a hub of the rotor. The cavity is filled with a filling material that includes at least one partition parallel to a chord of the blade and at least two independent blocks of filling material filling the cavity, thereby allowing the reduction of the torsional rigidity along the span of the blade.
Public/Granted literature
- US20150298802A1 BLADE WITH REDUCED TORSIONAL RIGIDITY, AND ROTOR EQUIPPED WITH SUCH A BLADE Public/Granted day:2015-10-22
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