| 摘要 |
measurement technology, test and diagnostics of condition of aviation equipment. SUBSTANCE: gear testing parameters of airborne complex of aircraft has buncher of parameters Ux to which input tested parameters of airborne complex come in process of ground tests, switch of parameters U§, multipurpose meter ( null detector ), registering unit connected in series and former of allowances and reference voltages. Gear is supplemented with additional buncher of parameters U§´, to which input tested parameters of airborne complex registered in flight come and switch of parameters U§´. This approach to design of gear makes it feasible to expand functional capabilities of equipment of aviation diagnostics by way of timely comparison of results of test of parameters of airborne complex during ground tests with parameters recorded in flight. EFFECT: expanded capabilities of gear. 1 dwg
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