Device to support rudders and trailing edge flaps of aircraft an

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

Patent

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16164, 244215, 244 87, 114165, B64C 902, B64C 350

Patent

active

042302951

ABSTRACT:
A supporting device is disclosed for an arrangement of articulated elements such as a fin-rudder arrangement, wing-trailing edge flap arrangement, and the like, for aircraft or watercraft. The disclosure more particularly relates to the cover for the gap existing between the two articulated elements. There is disclosed an arrangement of levers and bearing points which allow the cover to maintain a constant length and approximately constant curvature over its length as the two elements move relatively to each other. The arrangement of the disclosure eliminates corners and folds in the elastic cover without also requiring parts protruding beyond the elastic cover and without requiring high forces to deflect the cover.

REFERENCES:
patent: 2086085 (1937-07-01), Lachmann et al.
patent: 2158676 (1939-05-01), Engelhardt
patent: 2563453 (1951-08-01), Briend
patent: 2589026 (1952-03-01), Phillips
patent: 2608364 (1952-08-01), Gordon et al.
patent: 2721353 (1955-10-01), Mackintosh
patent: 4012013 (1977-03-01), Ball et al.
patent: 4131253 (1978-12-01), Zapel

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