Invention Grant
- Patent Title: Ply stackings for solid laminate stiffened panel
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Application No.: US16551165Application Date: 2019-08-26
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Publication No.: US11318705B2Publication Date: 2022-05-03
- Inventor: Jiangtian Cheng
- Applicant: The Boeing Company
- Applicant Address: US IL Chicago
- Assignee: The Boeing Company
- Current Assignee: The Boeing Company
- Current Assignee Address: US IL Chicago
- Agency: MH2 Technology Law Group LLP
- Main IPC: B32B5/12
- IPC: B32B5/12 ; B32B5/26 ; B64C1/00

Abstract:
A composite panel includes a plurality of segments, wherein each segment includes a plurality of reinforcement plies such as carbon fiber plies. Collimated fiber bands (e.g., carbon fibers) within each reinforcement ply are oriented in a single direction, which can be, for example, 0°, 45°, 90°, and −45°. Each segment can include a stack of reinforcement plies, wherein the collimated fiber bands of each reinforcement ply are oriented in one of these directions. The orientations of the collimated fiber bands that form the reinforcement plies in a stack determine a stiffness of the stack and the segment that includes the stack. The stiffness of each segment is controlled to reduce a stiffness mismatch between adjacent segments that form the composite panel, thereby reducing separation of the segments during use.
Public/Granted literature
- US20210060894A1 PLY STACKINGS FOR SOLID LAMINATE STIFFENED PANEL Public/Granted day:2021-03-04
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