Invention Grant
- Patent Title: Stringer stiffened composite panels having improved pull-off strength
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Application No.: US15913488Application Date: 2018-03-06
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Publication No.: US10689085B2Publication Date: 2020-06-23
- Inventor: Forouzan Behzadpour , 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: Hanley, Flight & Zimmerman, LLC
- Main IPC: B64C1/06
- IPC: B64C1/06 ; B64C3/18 ; B64C3/26 ; B64C1/12 ; B64F5/10 ; B64C1/00

Abstract:
Stringer stiffened composite panels having improved pull-off strength are disclosed. An example stringer includes a first surface, a second surface, an edge, and a chamfer. The second surface is located opposite the first surface and is to be coupled to a composite structure of an aircraft. The edge extends from the second surface toward the first surface. The chamfer extends from the first surface to the edge at an angle between twelve and eighteen degrees relative to the first surface.
Public/Granted literature
- US20190047676A1 STRINGER STIFFENED COMPOSITE PANELS HAVING IMPROVED PULL-OFF STRENGTH Public/Granted day:2019-02-14
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