FIELD: power industry.
SUBSTANCE: invention relates to power industry. An overhaul method of aircraft jet turbine engines, at which rotationally renewable stock of reworked parts - modules, assemblies, assembly units which remained after replacement from the previous early repaired engines is created and used for replacement on the next engine being repaired. During tests, a retractable interceptor is used, which excludes intermediate stops and starts of the thoroughly repaired engine. Besides, a jet turbine engine repaired according to the method, as well as an overhaul method of a batch is presented.
EFFECT: invention allows reducing labour costs, power consumption and duration of an overhaul, improving operating characteristics, as well as reliable determination of gas-dynamic stability of engine operation without any transition of the engine to surging.
21 cl, 3 dwg
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JET TURBINE ENGINE OVERHAUL METHOD (VERSIONS) AND JET TURBINE ENGINE REPAIRED ACCORDING TO THIS METHOD (VERSIONS), OVERHAUL OF BATCH, RESUPPLIED GROUP OF JET TURBINE ENGINES AND JET TURBINE ENGINE REPAIRED BY THIS METHOD | 2013 |
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OPERATING METHOD OF GAS-TURBINE ENGINE AND GAS-TURBINE ENGINE OPERATED BY MEANS OF THIS METHOD | 2013 |
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TURBOJET, METHOD OF TURBOJET TESTING (VERSIONS) AND METHOD OF TURBOJET PRODUCTION, METHOD OF TURBOJET INDUSTRIAL PRODUCTION, METHOD OF TURBOJET OVERHAUL, AND METHOD OF TURBOJET OPERATION | 2012 |
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TURBOJET OVERHAUL (VERSIONS) AND TURBOJET THUS REPAIRED (VERSIONS), OVERHAUL OF LOT TURBOJET FILLED-UP GROUP AND TURBOJET THUS REPAIRED | 2013 |
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JET TURBINE ENGINE | 2013 |
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JET TURBINE ENGINE | 2013 |
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Authors
Dates
2015-07-10—Published
2013-11-08—Filed