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An external integrated displacement sensor installation mechanism adapted to electromechanical actuators

A technology of displacement sensor and electromechanical actuator, applied in the field of aerospace servo system, can solve the problems of high cost, difficult processing, and complicated zero adjustment.

Active Publication Date: 2020-10-23
BEIJING RES INST OF PRECISE MECHATRONICS CONTROLS +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] The technical problem to be solved in the present invention is: to overcome the deficiencies of the prior art, such as high structural complexity, high processing difficulty, complicated zero adjustment, and high cost, and propose an external integrated displacement sensor installation mechanism suitable for electromechanical actuators

Method used

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  • An external integrated displacement sensor installation mechanism adapted to electromechanical actuators
  • An external integrated displacement sensor installation mechanism adapted to electromechanical actuators

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Embodiment Construction

[0030] An external integrated displacement sensor installation mechanism adapted to electromechanical actuators of the present invention will be described in detail below in conjunction with the accompanying drawings and embodiments.

[0031] Such as figure 1 , figure 2 As shown, an external integrated displacement sensor installation mechanism adapted to electromechanical actuators of the present invention includes a deep groove ball bearing 1, a first guide column 2, a resistance assembly 3, a brush assembly 4, and a second guide column 5. Sliding block 6, piston rod 7, sealing ring 8 and wear reducing ring 9.

[0032] The number of deep groove ball bearings 1 is 2, the material of the inner and outer rings and rolling elements of the bearing is 9Cr18, and the material of the cage is molded polyimide;

[0033] The brush assembly 4 is installed on the sliding block 6; the resistance assembly 3 is installed on the housing of the sensor, and the brush wire of the brush assem...

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Abstract

The invention belongs to the technical field of aerospace servo systems, and particularly relates to an external integrated displacement sensor mounting mechanism adapting to an electromechanical actuator. The mechanism comprises a deep groove ball bearing, a first guide column, a resistor assembly, an electric brush assembly, a second guide column, a sliding block, a piston rod, a sealing ring and an anti-attrition ring, the deep groove ball bearing and the guide column are installed, and the electric brush assembly is installed between a displacement sensor sheet and the sliding block; brushwires of the electric brush assembly are in contact with the resistor assembly; a sliding block is installed in the displacement sensor and fixedly connected with the extending part of the guide column through a sealing ring, and the displacement sensor is integrally installed on a shell of the electromechanical actuator and can independently conduct adjustment and other operations. The mechanismcan be applied to various electromechanical actuators, the structural reliability and stability of the product are improved, and the cost is reduced while the environmental adaptability of the product is improved; and meanwhile, the mechanism can be popularized and applied to an electromechanical actuator with the mechanism, and the machining difficulty caused by the fact that a split type platedisplacement sensor needs to be installed on an actuator shell is reduced.

Description

technical field [0001] The invention belongs to the technical field of aerospace servo systems, and in particular relates to an external integrated displacement sensor installation mechanism adapted to electromechanical actuators. Background technique [0002] At present, the electromechanical servo actuator scheme is widely used in the series of aerospace vehicles; in recent years, with the continuous improvement of the reliability of electronic products, the application in aerospace electromechanical servo systems has become more and more extensive, and a large number of servo systems have adopted Electromechanical servo actuator solutions. [0003] This type of electromechanical servo actuator is mainly composed of lug assembly, permanent magnet synchronous servo motor (including resolver), flat key, ball screw actuator, displacement sensor, bolt head assembly, etc. The electromechanical actuator mainly sends position control instructions to the servo motor according to ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): H02K11/21H02K7/06
Inventor 成兆义侯鹏飞李俊岩陈安平邓涛刘亚冬魏凯
Owner BEIJING RES INST OF PRECISE MECHATRONICS CONTROLS
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