Invention Application
- Patent Title: BRAIDED REINFORCEMENT FOR AIRCRAFT FUSELAGE FRAMES AND METHOD OF PRODUCING THE SAME
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Application No.: PCT/US2008/051690Application Date: 2008-01-22
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Publication No.: WO2008091883A3Publication Date: 2008-07-31
- Inventor: HEAD, Andrew, Atkins , GOETZ, Brad , PETER, John , STENARD, Steven, Charles , STORY, Thomas, C.
- Applicant: A & P TECHNOLOGY, INC. , HEAD, Andrew, Atkins , GOETZ, Brad , PETER, John , STENARD, Steven, Charles , STORY, Thomas, C.
- Applicant Address: 4595 East Tech Drive Cincinnati, OH 45245-1055 US
- Assignee: A & P TECHNOLOGY, INC.,HEAD, Andrew, Atkins,GOETZ, Brad,PETER, John,STENARD, Steven, Charles,STORY, Thomas, C.
- Current Assignee: A & P TECHNOLOGY, INC.,HEAD, Andrew, Atkins,GOETZ, Brad,PETER, John,STENARD, Steven, Charles,STORY, Thomas, C.
- Current Assignee Address: 4595 East Tech Drive Cincinnati, OH 45245-1055 US
- Agency: LEASON, David et al.
- Priority: US60/886,010 20070122
- Main IPC: D04C3/42
- IPC: D04C3/42
Abstract:
A machine and method for applying braid by means of a braiding machine to a mandrel, where the mandrel has a shape that approximates a wheel but has an irregularly varying radius of curvature. The machine includes drive/positioning wheel assemblies that are used to continuously reposition a cross-section of the mandrel relative to the braiding machine such that a center point of cross-section of the mandrel is maintained to be coaxial with a braiding point of the braiding machine as the mandrel (18) is rotationally advanced by the drive/positioning wheel assemblies. Repositioning of the drive/positioning wheel assemblies is controlled by a computer numerical control (CNC) controller, based on information describing one or more radiuses of curvature for sections of the mandrel and a current position of the mandrel relative to the drive/positioning wheel assemblies.
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