| 摘要 |
FIELD: engines and pumps.SUBSTANCE: invention relates to aircraft engine building, namely to aircraft gas-turbine engines. A batch production method of a gas-turbine engine involves manufacture of parts and completing of assembly units, components and assemblies of modules and systems of the engine. Modules are assembled in the amount of at least eight - from a low-pressure compressor to an all-mode adjustable jet nozzle. After assembly is completed, engine tests are performed as per a multi-cycle programme. When performing the test steps, alteration of the modes, which exceed as to duration the programmed flight time, is performed. Typical flight cycles are shaped, on the basis of which there determined as per the programme is damageability of the most loaded parts. The required number of loading cycles during the test is determined based on the above. Full scope of tests is formed, including a quick change of cycles in the complete register from quick selection of maximum or full forced power mode till complete stop of the engine, and then, representative cycle of continuous operation with multiple alteration of modes in the whole working spectrum with various span of range of the mode change, which exceeds the flight time at least by 5 times. Quick selection of maximum or forced power mode in some part of the test cycle is performed at the rate of acceleration and discharge.EFFECT: improvement of reliability of test results at a batch production stage and enlargement of representativeness of evaluation of service life and reliability of operation of a gas-turbine engine in a wide range of regional and seasonal conditions of further flight operation of engines.13 cl, 2 dwg |
