Invention Application
- Patent Title: Brazed structural assembly and associated system and method for manufacture
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Application No.: US11059287Application Date: 2005-02-16
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Publication No.: US20060180705A1Publication Date: 2006-08-17
- Inventor: David Nansen , Marc Matsen , Terry Smith , William Herb , Ronald Brown , Lee Firth
- Applicant: David Nansen , Marc Matsen , Terry Smith , William Herb , Ronald Brown , Lee Firth
- Assignee: The Boeing Company
- Current Assignee: The Boeing Company
- Main IPC: B64C1/00
- IPC: B64C1/00

Abstract:
A structural assembly and an associated system and method for manufacture are provided. The structural assembly includes an elongate member and a first connector member that is connected to an end of the elongate member by a braze joint. A second connector member can be connected to an end of the elongate member opposite the first connector by another braze joint. The elongate member is formed of a metal matrix composite material that includes a plurality of fibers of a reinforcement material disposed in a metal matrix. Each connector member is formed of a material that is dissimilar to the material of the elongate member. The braze joints can be formed by selectively heating the braze material, e.g., with an inductive coil that extends circumferentially around only a portion of the structural assembly.
Public/Granted literature
- US07621437B2 Brazed structural assembly and associated system and method for manufacture Public/Granted day:2009-11-24
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