Enhancement and extension of structural integrity of...

Details Enhancement and extension of structural integrity of... Enhancement and extension of structural integrity of...

2006-05-22

2010-02-09

Swiatek, Rob (Department: 3643)

Aeronautics and astronautics

Aircraft structure

Fuselage and body construction

C244S131000

Reexamination Certificate

active

07658348

ABSTRACT:
A method and apparatus for modifying aircraft having a fuselage and center fuselage carry through structure that support wing structures, comprising placing a load transferring member to extend through the center fuselage carry through structure, and transferring the tension loads from the wing structures to the center fuselage carry through structure so as to provide a redundant load path that is resistant to the hazards of single point failures modes.

REFERENCES:
patent: 1749951 (1930-03-01), Lake
patent: 3018985 (1962-01-01), Voigt
patent: 4535958 (1985-08-01), Hutchison
patent: 6843450 (2005-01-01), Bath et al.

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