MISSILE FOLDING WING Russian patent published in 2006 - IPC F42B10/14 

Abstract RU 2288434 C1

FIELD: armament.

SUBSTANCE: the missile folding wing has a blade, whose root jointly with the inserts hinge-joined to it is located in a recess of the base rigidly fastened on the missile body, deployment device in the form of a plate spring interacting with the inserts and located in the base of the fixing device, which is made in the form of spring-loaded single-arm levers hinge-installed in the recesses of the base through slots on both sides of the recess. The hinge pins with the lever springs installed on them are fastened in the upper section of the slots. The lever ends opposite the hinge can be engageable with the shoulders made in the inserts.

EFFECT: enhanced reliability of the folding wing.

2 dwg

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RU 2 288 434 C1

Authors

Kuznetsov Vladimir Markovich

Kapustin Anatolij Sergeevich

Kolonitskij Evgenij Konstantinovich

Dates

2006-11-27Published

2005-04-13Filed