Missile wing structure

The utility model relates to a missile wing structure which comprises a missile wing body, the top of the missile wing body is provided with a missile wing guide plate, the missile wing guide plate is connected with the missile wing body through a quick connecting mechanism, the quick connecting mec...

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Bibliographische Detailangaben
1. Verfasser: XU JIANMENG
Format: Patent
Sprache:chi ; eng
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Beschreibung
Zusammenfassung:The utility model relates to a missile wing structure which comprises a missile wing body, the top of the missile wing body is provided with a missile wing guide plate, the missile wing guide plate is connected with the missile wing body through a quick connecting mechanism, the quick connecting mechanism comprises a clamping groove formed in the top of the missile wing body and a plurality of fastening bolts arranged on the two sides of the clamping groove, and the ends of the fastening bolts extend into the clamping groove. One side of the missile wing guide plate extends into the clamping groove and is fixedly locked through a fastening bolt; according to the actual requirements of a missile body, the missile wing guide plate can be disassembled and assembled at any time, so that the specification and size of the missile wing are conveniently changed, and operation is flexible. 本实用新型涉及一种弹翼结构,包括弹翼本体,弹翼本体的顶部设有弹翼导向板,弹翼导向板通过快接机构连接弹翼本体,快接机构包括设置在弹翼本体顶部的卡槽,设置在卡槽两侧的多个紧固螺栓,紧固螺栓的端部伸入到卡槽内,所述弹翼导向板的一侧伸入到卡槽内并通过紧固螺栓固定锁紧;