FIELD: aircraft engine engineering. SUBSTANCE: plant has internal combustion engine whose inlet is connected with the outlet of a heat exchanger. The working space of the internal combustion engine is in communication with the inlet and outlet of passages of semi-closed cooling system through valves. A system for gas dynamic control of the combustion chamber has jet nozzles with ejectors, receiver, and gas distributor whose inlet is connected to the outlet of the internal combustion engine. EFFECT: enhanced efficiency. 3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| POWER PLANT | 1989 |
|
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| POWER UNIT | 1988 |
|
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| GAS TRANSFER UNIT | 2020 |
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| I.C. ENGINE WARMING-UP AND STARTING SYSTEM | 0 |
|
SU937754A1 |
| COMPRESSED AIR OR GAS COOLING METHOD AND COMPRESSOR PLANT FOR IMPLEMENTING THIS METHOD | 1999 |
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| TURBO JET ENGINE (TJE) AFTERBURNER SYSTEM OPERATION METHOD AND THE AFTERBURNER SYSTEM OPERATING BY THIS METHOD, AFTERBURNER PUMP OPERATION METHOD AND THE AFTERBURNER PUMP OPERATING BY THIS METHOD, TJE OPERATION METHOD AND THE TJE OPERATING BY THIS METHOD | 2017 |
|
RU2656525C1 |
| GAS PUMPING UNIT | 2021 |
|
RU2773994C1 |
