| 摘要 |
A gas-turbine unit is comprises a turbine, a combustion chamber and a compressor to suction chamber of which injector is connected with supplementary source of compressed air to start the work of the unit, shutoff bodies, pipeline for air takeoff. The working nozzle of the injector is connected to the pipeline from the source of compressed air with its shutoff body and the pipeline for air takeoff by stages of the compressor, with its shutoff body, and the outlet of the injector is connected to the suction mains before the inlet of the compressor.
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