FIELD: mechanical engineering; turbines.
SUBSTANCE: proposed internal combustion turbine contains centrifugal air compressor, annular combustion chamber and reaction turbine with nozzles. Centrifugal air compressor and reaction turbine are connected into monoblock rotating on one shaft owing to reactive force of gases ejected from nozzles and transmitting rotation to driven sets through drive gear.
EFFECT: increased efficiency and power of internal combustion turbine, reduced harmful exhaust.
2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| ROTARY GAS TURBINE ENGINE | 2016 |
|
RU2623592C1 |
| ROTARY BIROTATE GAS TURBINE ENGINE | 2019 |
|
RU2702317C1 |
| REACTIVE STEAM-GAS POWER STATION | 2004 |
|
RU2249706C1 |
| STEAM-TURBINE ENGINE | 1994 |
|
RU2086790C1 |
| ROTARY ENGINE | 0 |
|
SU1809858A3 |
| AIRCRAFT ENGINE | 1991 |
|
RU2013630C1 |
| DESIGN OF A CROSS-FLOW DIGITALLY CONTROLLED GAS TURBINE ENGINE | 2022 |
|
RU2784789C1 |
| LOW-FLYING MULTIFUNCTIONAL DEVICE AND JET TURBINE ENGINE WITH TWO FLOW CHANNELS | 2013 |
|
RU2586996C2 |
| INTERNAL COMBUSTION ENGINE | 2012 |
|
RU2597351C2 |
| METHOD OF CREATING A TRAIL AND POWER INSTALLATION FOR ITS IMPLEMENTATION | 2017 |
|
RU2680214C1 |
