FIELD: aircraft manufacture. SUBSTANCE: power plant for flying vehicle includes working medium source installed in fuselage which is provided with gas-turbine engine and is connected with turbodriven screw propellers through system of gas lines. Working medium source is provided with turbo-compressor unit whose turbine is mounted in series with turbine of gas-turbine engine and recuperative heat exchanger for preheating the working medium; one chamber of heat exchanger is connected with outlet of compressor of turbo-compressor unit and other chamber is connected with outlet of turbine of turbo-compressor unit. EFFECT: enhanced reliability. 4 cl, 3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIRCRAFT GAS TURBINE ENGINE AND METHOD OF ITS SPEEDUP | 2014 |
|
RU2562822C2 |
| TURBOHEATING REFRIGERATING UNIT WITH ELECTRIC DRIVE | 1994 |
|
RU2096698C1 |
| TURBINE DRIVE | 1992 |
|
RU2049246C1 |
| METHOD OF PREPARING LOWER OLEFINS, REACTOR FOR PYROLYSIS OF HYDROCARBONS, AND APPARATUS FOR HARDENING PYROLYSIS GASES | 1998 |
|
RU2124039C1 |
| GAS-TURBINE EXPANSION MACHINE OPERATION PROCESS | 1994 |
|
RU2096640C1 |
| METHOD OF BUILDING UP HIGH PRESSURE OF AIR OF GAS IN COMPRESSOR PLANT | 1999 |
|
RU2140569C1 |
| METHOD AND DESIGN OF TURBINE MACHINE POWER COMBINING | 2011 |
|
RU2610872C2 |
| GAS PUMPING UNIT | 2017 |
|
RU2685802C1 |
| MICROTURBINE | 2007 |
|
RU2334113C1 |
| METHOD OF AND DEVICE FOR RECONSTRUCTION OF COMPRESSOR STATION | 2000 |
|
RU2170369C1 |
