Aerodynamic body with internal actuating drives

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

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244215, 244213, B64C 344

Patent

active

060708344

ABSTRACT:
A segment 1 of an aerodynamic body has as the internal actuating drive an actuator 7, which acts on an upper profile shell 2 with one working piston 9 and on a lower profile shell with a working piston 8 acting in the opposite direction to generate oppositely directed arches of the segment 1. The profile shells 2 and 3 are mounted displaceably in relation to one another in dovetail guides 4 and 5.

REFERENCES:
patent: 1344244 (1920-06-01), Patterson
patent: 1856578 (1932-05-01), Miguel et al.
patent: 2650047 (1953-08-01), Carhart et al.
patent: 3179357 (1965-04-01), Lyon
patent: 4247066 (1981-01-01), Frost et al.
patent: 4349169 (1982-09-01), McAnally
patent: 4671471 (1987-06-01), Patmont
patent: 5538202 (1996-07-01), Thornburg
patent: 5839698 (1998-11-01), Moppert
Navy Technical Catalog No. 0164, Navy Technical Disclosure Bulletin vol. 10, No. 4, Jun., 1985, pp. 101-106.

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