FIELD: internal combustion engines.
SUBSTANCE: invention relates to internal combustion engines, in particular to gas turbine engines. The effect is achieved due to the fact that the internal combustion engine containing a working turbine, a blowing turbine, a combustion chamber, a spark plug, is characterized in that the blowing turbine and the working turbine are mounted along the edges of a cylindrical combustion chamber, while the blowing turbine is made in the form of a hollow sleeve with blades closed at the ends with flat disks and a flange, on the outside in the cavity of which a gas reducer is mounted, made with the possibility of supplying gaseous fuel, and a nozzle is mounted in the hollow sleeve on the side of the combustion chamber; the working turbine is made in the form of a drum with arc-shaped plates radially mounted along its outer edge, closed at the ends by disk-shaped walls, while blind drilling is made in the center of the drum, radial nozzles are made from the inner surface of which towards the outer side of the drum, the ends of which are located between the plates.
EFFECT: engine torque increased.
1 cl, 6 dwg
Title | Year | Author | Number |
---|---|---|---|
MULTI-CHAMBER GAS-AIR PULSE-DETONATION TURBINE ENGINE | 2019 |
|
RU2750082C2 |
METHOD OF CREATING A TRAIL AND POWER INSTALLATION FOR ITS IMPLEMENTATION | 2017 |
|
RU2680214C1 |
INTERNAL COMBUSTION ENGINE | 1992 |
|
RU2048651C1 |
YUGI TURBO-ROTARY ENGINE | 2008 |
|
RU2372503C1 |
ROTARY PISTON JET INTERNAL COMBUSTION ENGINE | 1993 |
|
RU2082892C1 |
INTERNAL COMBUSTION TURBINE ENGINE | 2004 |
|
RU2291305C2 |
LOW-FLYING MULTIFUNCTIONAL DEVICE AND JET TURBINE ENGINE WITH TWO FLOW CHANNELS | 2013 |
|
RU2586996C2 |
REACTIVE STEAM-GAS POWER STATION | 2004 |
|
RU2249706C1 |
GAS-TURBINE ENGINE | 0 |
|
SU1787200A3 |
METHOD OF AND DEVICE FOR CONVERTING ENERGY FORMED AT COMBUSTION OF ORGANIC FUEL INTO ROTARY MOTION | 2003 |
|
RU2258828C2 |
Authors
Dates
2022-05-24—Published
2021-10-01—Filed