FIELD: power engineering. SUBSTANCE: plant has compressor, combustion chamber with fuel and hot-water or steam injectors and with air inlet ports, housing, multistage jet apparatus, tubular tower covered with external heat-insulating layer and used to mount power unit in the form of windmill-and-gas-turbine engine provided with contraction for air flow admission. Power unit has multistage turbine with nozzle assemblies and ejector. The latter is, essentially, annular nozzle arranged coaxially to housing. Housing has diffuser and front contraction assembly provided with pipe hinged to tubular tower pile. EFFECT: improved efficiency of power plant. 5 cl, 7 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD OF AND DEVICE FOR INCREASING TEMPERATURE DIFFERENCE IN HEAT ENGINE | 1998 |
|
RU2151310C1 |
| WIND-DRIVEN THERMAL POWER PLANT | 2010 |
|
RU2446310C1 |
| WINDMILL ELECTRIC GENERATING PLANT | 1996 |
|
RU2132966C1 |
| WINDMILL ELECTRIC GENERATING PLANT | 1998 |
|
RU2147693C1 |
| FISH RAISING COMPLEX | 2005 |
|
RU2297137C2 |
| METHOD OF DRIVING AIR-CUSHION VEHICLE AND AIRCUSHION VEHICLE TO THIS END | 2009 |
|
RU2411138C1 |
| METHOD TO OPERATE MULTI-FUEL THERMAL ENGINE AND COMPRESSOR AND DEVICE TO THIS EFFECT (VERSIONS) | 2008 |
|
RU2386825C2 |
| ENERGY CONVERSION PROCESS AND DEVICE (DESIGN VERSIONS) | 1997 |
|
RU2154738C2 |
| VTOL AIRCRAFT | 2012 |
|
RU2490173C1 |
| COMPLEX FOR REACTIVE FLIGHT | 2008 |
|
RU2387582C2 |
