ELEVON CONTROL MECHANISM Russian patent published in 2014 - IPC F42B15/00 

Abstract RU 2518486 C2

FIELD: weapons and ammunition.

SUBSTANCE: elevon control mechanism consists of a rotation shaft placed on the housing of the rocket, a lever rigidly fixed to the shaft, and installed servo unit in the rocket housing, which rod is pivotally connected to the lever. One end of the shaft enters to the opening of a spherical bearing with the ability of axial displacement. The spherical bearing is mounted in the sleeve having the ability to rotate in the rocket housing. At the other end of the shaft the charger is pivotally mounted, which is pivotally connected to the leash fixedly secured to the elevon of the foldable wing. The axis of the pivotal connection of the leash and the charger is aligned with the axis of rotation of the wing, on the leash a tooth is formed, on the charger the groove is formed, in which the tooth of the leash is placed.

EFFECT: improved operation of elevon.

4 dwg

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RU 2 518 486 C2

Authors

Shestakov Sergej Aleksandrovich

Zemskov Vjacheslav Aleksandrovich

Dates

2014-06-10Published

2012-08-31Filed