Method and system for fastening aircraft assemblies

Aeronautics and astronautics – Aircraft structure – Details

Patent

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Details

244123, 244132, B64C 100, B64C 106

Patent

active

059246502

ABSTRACT:
A system for fastening aircraft assemblies is disclosed. The system comprises a first wing clip (10) having an anchor plate (12) with at least one ear (20) for affixing to a first assembly (16); a second wing clip (11) having an anchor plate (14) and at least one ear (20) for affixing to a second assembly (18); and a fastener (44) for joining the first wing clip (10) to the second wing clip (11).

REFERENCES:
patent: 1835338 (1931-12-01), Rossman
patent: 1835339 (1931-12-01), Rossman
patent: 2565065 (1951-08-01), Chakeres
patent: 2881994 (1959-04-01), Michael
patent: 3613150 (1971-10-01), Osborn
patent: 3920206 (1975-11-01), Bigham et al.
patent: 4160609 (1979-07-01), Jackson et al.
patent: 4388030 (1983-06-01), Skaale
patent: 4610562 (1986-09-01), Dunn

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