RU2012137128A

RU2012137128A - ELEVON CONTROL MECHANISM

Info

Publication number: RU2012137128A
Application number: RU2012137128/11A
Authority: RU
Inventors: Сергей Александрович Шестаков; Вячеслав Александрович Земсков
Priority date: 2012-08-31
Filing date: 2012-08-31
Publication date: 2014-03-10
Also published as: RU2518486C2

Abstract

Механизм управления элевоном, состоящий из размещенного на корпусе ракеты вала вращения, соединенного с элевоном, шарнирно установленным на задней кромке крыла, рычага, закрепленного на валу, и рулевой машинки установленной в корпусе ракеты, шток которой шарнирно соединен с рычагом, отличающийся тем, что вал, расположенный в корпусе ракеты, жестко соединен с рычагом, шарнирно соединенного со штоком рулевой машинки закрепленной в корпусе ракеты, при этом один конец вала с возможностью осевого перемещения входит в отверстие сферической опоры, установленной во втулке, размещенной в корпусе ракеты, а на другом конце вала шарнирно закреплена обойма, шарнирно соединенная с поводком, жестко закрепленным на элевоне складываемого крыла, при этом ось шарнирного соединения поводка и обоймы совмещена с осью вращения крыла, на поводке выполнен зуб, на обойме выполнен паз, в котором размещен зуб поводка.Elevon control mechanism, consisting of a rotation shaft located on the rocket body connected to the elevon pivotally mounted on the trailing edge of the wing, a lever mounted on the shaft, and a steering gear mounted in the rocket body, the rod of which is pivotally connected to the lever, characterized in that the shaft located in the rocket housing is rigidly connected to a lever pivotally connected to the rod of the steering gear mounted in the rocket housing, while one end of the shaft with the possibility of axial movement enters the hole of a spherical ry mounted in the sleeve, placed in the rocket body, and on the other end of the shaft pivotally mounted clip, pivotally connected to a leash, rigidly mounted on the elevon of the folding wing, while the axis of the hinged connection of the leash and the cage is aligned with the axis of rotation of the wing, the tooth is made on the leash , a groove is made on the clip in which the tooth of the leash is placed.

Claims

Elevon control mechanism, consisting of a rotation shaft located on the rocket body connected to the elevon pivotally mounted on the trailing edge of the wing, a lever mounted on the shaft, and a steering gear mounted in the rocket body, the rod of which is pivotally connected to the lever, characterized in that the shaft located in the rocket housing is rigidly connected to a lever pivotally connected to the rod of the steering gear mounted in the rocket housing, while one end of the shaft with the possibility of axial movement enters the hole of a spherical ry mounted in the sleeve, placed in the rocket body, and on the other end of the shaft pivotally mounted clip, pivotally connected to a leash, rigidly mounted on the elevon of the folding wing, while the axis of the hinged connection of the leash and the cage is aligned with the axis of rotation of the wing, the tooth is made on the leash , a groove is made on the clip in which the tooth of the leash is placed.