Invention Grant
- Patent Title: High modulus hybrid material rotor blade spar
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Application No.: US14915162Application Date: 2014-08-07
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Publication No.: US10648340B2Publication Date: 2020-05-12
- Inventor: David A. Darrow, Jr.
- 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: Cantor Colburn LLP
- International Application: PCT/US2014/050090 WO 20140807
- International Announcement: WO2015/069344 WO 20150514
- Main IPC: F01D5/14
- IPC: F01D5/14 ; B29D99/00 ; B29C70/20 ; B29C70/30 ; B29K105/10 ; B29K307/04 ; B29L31/08 ; B29K63/00 ; B29K105/00

Abstract:
A composite spar having an upper and lower wall region connected by leading and trailing edge regions is provided including a plurality of first laminates and a plurality of second laminates. The plurality of first laminates includes one or more intermediate modulus graphite plies having an intermediate modulus. The plurality of first laminates is arranged in one or more intermediate modulus layers to form at least a portion of the upper wall region, lower wall region, leading edge region and trailing edge region. The plurality of second laminates includes one or more high modulus graphite plies having a high modulus. The plurality of second laminates is arranged in one or more high modulus layers. The high modulus layers are generally interposed between intermediate modulus layers.
Public/Granted literature
- US20160208616A1 HIGH MODULUS HYBRID MATERIAL ROTOR BLADE SPAR Public/Granted day:2016-07-21
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