TY  - JOUR
AB  - Translated Abstracts of a Selection from the New Post‐war Scries of Patents Granted in the German Federal Republic. In the drawings, the control surface I, constructed as a landing flap, is open at one side. The framework 2 consists of a nose part 3 and of a finger‐like part 4 running from the nose part towards the rear edge of the surface. The frame 2 is covered on one side with a skin 5 and connected thereto by welding or the like at 6, 7. A cross‐beam 8 serves for stiffening the nose part 3 (FIG. 1). The control surface may be operable in both directions, the frame consisting of two parts 9, 10, of opposite hands. They are connected together by welding at points 11, 12. The frame 1 is covered on both sides with a skin 5 (FIG. 2).
VL  - 25
IS  - 12
SN  - 0002-2667
DO  - 10.1108/eb032374
UR  - https://doi.org/10.1108/eb032374
PY  - 1953
Y1  - 1953/01/01
TI  - German Patent Abstracts
T2  - Aircraft Engineering and Aerospace Technology
PB  - MCB UP Ltd
SP  - 390
EP  - 390
Y2  - 2024/04/24
ER  -