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Recent German Patents

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 October 1940

Abstract

Claim The trailing edge of the main wing is composed of a flap 4 movable around an axis 3. A lever 5 is rigidly connected with the flap. A crosshead engaged in a slotted guide member 7. If this is moved in the direction of the arrow P from the cockpit, the position of the crosshead running in an inclined groove or a slot is altered. The result of this is that the lever 5 rotates around 3 and thus displaces the flap 4.

Citation

(1940), "Recent German Patents", Aircraft Engineering and Aerospace Technology, Vol. 12 No. 10, pp. 319-319. https://doi.org/10.1108/eb030707

Publisher

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MCB UP Ltd

Copyright © 1940, MCB UP Limited