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JOINT CONSTRUCTION AND METHOD OF FABRICATION
   
Document Number
US Patent 3725981
Issued Date
April 10, 1973
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Abstract
A structural joint construction for connecting a first member of composite material to a second member which may be of composite material or of some other material. The construction enables tensile, compressive, torsional, and bending loads to be transmitted from the first member to the second member with a high degree of efficiency. One end of the first member is in abutting relationship with a free end of the second member such that a plurality of ends of first filament material integral with the core extends beyond its end and overlies the outer surface of the second member. The outer surface of the second member is contoured to include a central portion of minimal cross-sectional area bounded by opposing portions of greater cross-sectional areas. Other filament material is wrapped around the first filament material in a direction transverse to the axes of the first and second members such that the ends of the first filament material conform to the contour of the outer surface of the second member and are held fast to the second member.
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JOINT CONSTRUCTION AND METHOD OF FABRICATION - US Patent 3725981 Drawing
Drawing from US Patent 3725981
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Number of Claims:
11
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Owner
The Boeing Company (Seattle, WA)
Published
April 10, 1973
Application Number
05/078,727
Filed
October 7, 1970
US Classification
24/122.3   24/115A 403/341
Int'l Classification
F16D   3/50   (20060101)   F16C   3/02   (20060101)   F16C   7/00   (20060101)   F16D   3/72   (20060101)  
USPTO Field of Search
287/82   287/124   24/122.3   24/122.6   24/123W   24/115A  
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