Joint assemblies

Details Joint assemblies Joint assemblies

1997-04-24

1999-08-31

Jordan, Charles T.

Aeronautics and astronautics

Aircraft structure

Details

244123, 244132, 403335, B64C 106, B64C 112, F16B 300

Patent

active

059442867

ABSTRACT:
A joint assembly and an aircraft wing assembly containing such a joint assembly are provided. Each joint assembly for connecting together a first member (1) and a second member (4) comprises a second channel member (5) affixed to the first member (1) having a first channel member (12) with sidewalls (15, 16) engageable with first and second elements (8, 9) of the second channel member. The second member (4) has a flange which engages a flat surface (14) of a base portion (13) thereof. The various elements are held together by bolts (19, 20, 23) and tolerance adjustment in both horizontal and vertical directions is provided by mutual sliding of the surfaces prior to drilling apertures for the bolts.

REFERENCES:
patent: 1967901 (1934-07-01), Ragsdale
patent: 2367750 (1945-01-01), Berkow et al.
patent: 2382358 (1945-08-01), Watter
patent: 2392788 (1946-01-01), Watter
patent: 2661083 (1953-12-01), Henderson
patent: 3004645 (1961-10-01), Moul, Jr.
patent: 3219158 (1965-11-01), Carter et al.
patent: 3920206 (1975-11-01), Bigham et al.
patent: 4390153 (1983-06-01), Wuermseer
patent: 5484221 (1996-01-01), DeCoux

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