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German Patent Abstracts

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 January 1954



Translated Abstracts of a Selection from the New Post‐war Series of Patents Granted in the German Federal Republic. The invention consists in the provision of the detonator fuse inside the fuselage connected with the explosive cap. The edge of the section of the fuselage (1) is stiffened by a rib (2) to which the strengthening frame (3) for the hood (4) is secured by rivets. Between the strengthening frame (3) and the fastening edge (5) for the hood (4) there is provided a closed detonator fuse (6) which is in connexion with an explosive cap (7) secured to the frame (2). The fuse (6) runs round the hood body (4) on the strengthening frame (3) in the fastening edge (5) above the securing rivets (4) for the hood (4). The explosive cap (7) is protected towards the inside of the fuselage (1) by a protecting wall (8) of armour plating. To the protecting wall (8) there is secured a housing (9) covered by a lid (10) which serves for the reception of the draw ring (11) for firing the explosive cap (7).


(1954), "German Patent Abstracts", Aircraft Engineering and Aerospace Technology, Vol. 26 No. 1, pp. 32-32.




Copyright © 1954, MCB UP Limited

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