Integrated lightweight electro-hydraulic servo system
A hydraulic servo system and lightweight technology, applied in servo motors, fluid pressure actuators, mechanical equipment, etc., can solve problems such as difficult to meet, achieve effective absorption and ensure safety
Active Publication Date: 2013-07-03
中国航天科技集团公司第一研究院第十八研究所
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Problems solved by technology
At present, existing electro-hydraulic servo system is difficult to meet above-mentioned comprehensive index requirement
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[0015] Each servo system includes: one electro-hydraulic energy source, two servo actuators and one servo controller. Electricity
[0017] Each servo actuator includes: a servo valve 14, a differential pressure sensor 10 and a dual displacement sensor 15.
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Abstract
The invention provides an integrated lightweight electro-hydraulic servo system, which belongs to the technical field of electro-hydraulic servo systems. It has the characteristics of simple structure, small size, light weight, long working time, high reliability, excellent and stable performance, and easy use and maintenance. It can make the missile fly accurately and stably according to the predetermined track. Hydraulic servo system, including: one electrohydraulic energy source, two servo actuators and one servo controller, one electric servo energy source provides hydraulic energy for two servo actuators, each servo controller is responsible for each servo system Control and measurement of two servo actuators and one electro-hydraulic energy source. It is used to realize thrust vector control and aerodynamic control when the missile flies in the atmosphere for a long time.
Description
Integrated lightweight electro-hydraulic servo system technical field The present invention belongs to electrohydraulic servo system technical field, specifically a kind of machine-electricity-hydraulic-pneumatic integration Lightweight electro-hydraulic servo system. Background technique In order to meet the requirements of military warfare in the new era, the full-range atmospheric flight and the full-range mobile campaign tactical guide developed bomb, the only actuator of its guidance and attitude control system is the servo system. According to the task requirements of the model, it is required that the servo system must meet It meets the comprehensive index requirements of "large load moment, high output speed, long working time, compact structure and installation, and harsh working environment". Therefore, there is a need for a compact structure, small size, light weight, long working hours, high reliability, excellent and stable performance and easy to use E...
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IPC IPC(8): F15B9/09F15B1/02
Inventor 沈波曹泽生景光辉何俊赵守军颜峰金阳王毅王宇浩王伟
Owner 中国航天科技集团公司第一研究院第十八研究所
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