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Improvements in or relating to Fin Assemblies for Missiles, and Missiles Provided With Improved Fin Assemblies.
Improvements in or relating to Fin Assemblies for Missiles, and Missiles Provided With Improved Fin Assemblies.
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机译：导弹鳍组件和具有改进鳍组件的导弹的改进或与之相关的改进。
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1,155,314. Missile fins. DYNAMIT NOBEL A.G. 3 Aug., 1966 [3 Aug., 1965], No. 34875/66. Heading F3A. Missile 1 for firing from a tube 13 is provided with a fin divided into " mirror " symmetrical fin-halves which are each subdivided into parts 3 and 4 hinged together at 6 and 7 and to the casing of the missile, whereby, on launching the missile, a spring 8 brings the fin-halves together from the collapsed position shown into an erect position (Fig. 1, not shown) where they may be fastened together by a pin 11 and corresponding socket 12. A centrally, partly tapered stop 2 may be provided together with stops (not shown) on each of the hinges. Overhanging portions (14, Figs. 3 and 4, not shown) on the leading edge of one inner part 3 and the leading edge of the outer part of the other fin-half overlap the adjacent inner and outer parts of the erected fin to give a streamlined edge.
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机译：1,155,314。导弹鳍。 DYNAMIT NOBEL A.G.，1966年8月3日[1965年8月3日]，第34875/66号。标题F3A。用于从管子13发射的导弹1设有翼片，该翼片被分成“镜”形对称的半片，每个半片被细分为分别在6和7处铰接在一起的部分3和4以及导弹的外壳，从而在发射时导弹上，弹簧8将半翅片从所示的折叠位置放到直立位置（图1，未显示），在这里可以通过销钉11和相应的插座12将其固定在一起。中央的部分锥形挡块2可以在每个铰链上与挡块（未示出）一起提供。一个内部部分3的前缘和另一半个翅片的外部的前缘上的伸出部分（图3和4中的14）未重叠，因此竖立的翅片的相邻的内部和外部重叠。流线型的边缘。
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