Invention Grant
- Patent Title: Composite spars
- Patent Title (中): 复合翼梁
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Application No.: US12632893Application Date: 2009-12-08
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Publication No.: US08061253B2Publication Date: 2011-11-22
- Inventor: Tim Wybrow
- Applicant: Tim Wybrow
- Applicant Address: GB
- Assignee: GE Aviation Systems Limited
- Current Assignee: GE Aviation Systems Limited
- Current Assignee Address: GB
- Agency: Global Patent Operation
- Agent Jonathan E. Thomas
- Priority: GB0900115.7 20090107
- Main IPC: D04C1/06
- IPC: D04C1/06

Abstract:
According to one aspect, the present invention relates to a method of manufacturing at least one non-uniform thickness composite spar component. The method comprises braiding a plurality of fibers over a non-cylindrical mandrel to form a variable thickness shaped fiber preform, flattening the shaped fiber preform and cutting the flattened shaped fiber preform to obtain the at least one non-uniform thickness composite spar component. Spars made according to various embodiments of the present invention are faster and less expensive to manufacture than conventional composite spar components.
Public/Granted literature
- US20100170990A1 COMPOSITE SPARS Public/Granted day:2010-07-08
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