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随着舵机技术的不断发展,功能单一的气源已不能满足舵机模拟试验要求。为了满足舵机试验要求,北京领邦仪器研发了新型导弹飞行滞止压力模拟系统,对舵机飞行的压力环境进行模拟,为用户提供了舵机设计的试验与验证平台。经少量修改后,本系统还可适用于各种气动部件的压力环境模拟及测试,如舵机、气动阀门等。
With the continuous development of steering gear technology, the single function gas source can not meet the requirement of steering gear simulation test. In order to meet the servo test requirements, Beijing Ling State Instrument has developed a new missile flight hold-off pressure simulation system to simulate the pressure environment of the steering gear flight, providing the user with a test and verification platform for the steering gear design. After a small amount of modification, the system can also be applied to a variety of pneumatic components of the pressure environment simulation and testing, such as steering gear, pneumatic valves.