Invention Grant
- Patent Title: Flexible mandrel for highly contoured composite stringer
- Patent Title (中): 用于高度轮廓的复合纵梁的柔性心轴
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Application No.: US11964133Application Date: 2007-12-26
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Publication No.: US07901531B2Publication Date: 2011-03-08
- Inventor: Doan D. Pham , Mark Tollan
- Applicant: Doan D. Pham , Mark Tollan
- Applicant Address: US IL Chicago
- Assignee: The Boeing Company
- Current Assignee: The Boeing Company
- Current Assignee Address: US IL Chicago
- Agency: Ostrager Chong Flaherty & Broitman P.C.
- Main IPC: B32B37/10
- IPC: B32B37/10 ; B29C65/70 ; B29C70/54 ; B29C33/76

Abstract:
An aircraft stringer lay-up assembly is provided comprising a contoured curing block and a first mandrel element positioned thereon. The first mandrel assembly includes a first bar assembly having a plurality of rigidity reducing first slots formed along a first mandrel length. The plurality of rigidity reducing first slots protruding partially through a first mandrel depth of the first mandrel element to allow the first bar assembly to conform to the contoured curing block. A composite ply assembly is laid up onto the first mandrel element and cured while conformed to said contoured curing block such that a contoured composite stringer element is generated.
Public/Granted literature
- US20080099597A1 FLEXIBLE MANDREL FOR HIGHLY CONTOURED COMPOSITE STRINGER Public/Granted day:2008-05-01
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