Hinge line skin system for an aircraft

Details Hinge line skin system for an aircraft Hinge line skin system for an aircraft

1997-05-08

1999-08-24

Jordan, Charles T.

Aeronautics and astronautics

Aircraft structure

Details

244123, 244133, 244213, 244219, B64C 106, B64C 358

Patent

active

059414804

ABSTRACT:
A hinge line system (52) for an aircraft has a structural block (22) attached to a first edge of a hinge line. The structural block (22) has a flange (28) attached to a first end of an elastic sheet (32). A second structural block (24) is attached to a second edge of the hinge line. The second structural block (24) has a second flange (30) attached to a second end of the elastic sheet (32).

REFERENCES:
patent: 1460053 (1923-06-01), Cleghorn
patent: 1590783 (1926-06-01), Tesse
patent: 2368702 (1945-02-01), Bourne
patent: 4429844 (1984-02-01), Brown et al.
patent: 4761324 (1988-08-01), Rautenberg et al.
patent: 5222699 (1993-06-01), Albach et al.
patent: 5385774 (1995-01-01), Cramer et al.
patent: 5794893 (1998-08-01), Diller et al.

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