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A Pointing Mechanism of Orthogonal Double Joint Type Electric Thruster

A technology of electric thruster and pointing mechanism, which is applied in the directions of propulsion system devices of space navigation vehicles, etc., can solve the problems of heavy weight and large volume.

Active Publication Date: 2022-04-12
沈阳中科新宇空间智能装备有限公司 +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] In view of the above problems, the object of the present invention is to provide an orthogonal double-joint electric thruster pointing mechanism to overcome the problems of large volume and heavy weight in the existing electric propulsion pointing mechanism

Method used

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  • A Pointing Mechanism of Orthogonal Double Joint Type Electric Thruster
  • A Pointing Mechanism of Orthogonal Double Joint Type Electric Thruster
  • A Pointing Mechanism of Orthogonal Double Joint Type Electric Thruster

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Embodiment Construction

[0030] In order to make the object, technical solution and advantages of the present invention clearer, the present invention will be described in detail below in conjunction with the accompanying drawings and specific embodiments.

[0031] like Figure 1-3 As shown, the present invention provides an orthogonal double-joint type electric thruster pointing mechanism, including a rotary actuator I1, a universal joint ring 2, an electric thruster 3, an upper rotating frame 4, a lower fixing frame 7 and a rotary actuator Ⅱ9, wherein the universal joint ring 2 is installed on the lower fixed frame 7 so that the Y axis is rotatable, the rotary actuator Ⅱ9 is arranged on the lower fixed frame 7, and the output end of the rotary actuator Ⅱ9 is connected with the universal joint ring 2, and the rotation is executed Device II9 is ​​used to drive the universal joint ring 2 to rotate around the Y axis; the upper rotating frame 4 is connected to the universal joint ring 2 so as to rotate a...

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Abstract

The invention relates to a mechanism for adjusting thrust direction of an electric thruster in a spacecraft, in particular to an orthogonal double-joint electric thruster pointing mechanism. The mechanism includes a rotary actuator Ⅰ, a universal joint ring, an electric thruster, an upper rotating frame, a lower fixed frame and a rotary actuator Ⅱ, wherein the universal joint ring is installed on the lower fixed frame so that the Y axis rotates, and the rotary actuator Ⅱ Set on the lower fixed frame, and the output end of the rotary actuator II is connected with the universal joint ring, and the rotary actuator II is used to drive the universal joint ring to rotate around the Y axis; the upper rotary frame rotates around the X axis and connects with the universal joint The rotary actuator I is set on the upper rotary frame, and the output end of the rotary actuator I is connected with the universal joint ring, and the rotary actuator I is used to drive the upper rotary frame to rotate around the X axis; the electric thruster is set on the upper on the swivel stand. The present invention achieves the purpose of adjusting the rotation of the upper bracket by using a universal joint ring, and can realize the orientation of the upper rotating frame of the mechanism in any direction within the travel range.

Description

technical field [0001] The invention relates to a mechanism for adjusting thrust direction of an electric thruster in a spacecraft, in particular to an orthogonal double-joint type electric thruster pointing mechanism. Background technique [0002] At present, both at home and abroad, whether it is maintaining the position of the spacecraft in orbit or changing the orbit of the spacecraft, the thrust of the propeller is required. Compared with chemical propulsion, electric propulsion has the advantages of high specific impulse, small disturbance, and small mass. Therefore, at this stage, it is a good method to use electric propulsion technology to control the operation of satellites in orbit. How to effectively and accurately control the direction of the propulsion force is an important issue to be studied, which requires an electric propulsion pointing mechanism to control the direction of the propulsion force. Most of the electric thrusters used today are large in size an...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64G1/40
CPCB64G1/40
Inventor 张赵威张茶花潘友胜张伟于涛
Owner 沈阳中科新宇空间智能装备有限公司
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