FIELD: gas turbine engine engineering. SUBSTANCE: gas turbine engine has combustion chamber interposed between the centrifugal compressor and centripetal turbine and secured to the common rotor and combustion chamber mounted on the same rotor and tangentially inclined oppositely to the direction of the rotation of the rotor and radially inclined to the axis of the rotor. EFFECT: enhanced efficiency. 7 cl, 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| HEAT ENGINE | 1996 |
|
RU2099560C1 |
| METHOD FOR CREATING DRIVING FORCE FOR MOVEMENT OF TRANSPORT VEHICLE AND JET ENGINE FOR ITS IMPLEMENTATION | 2010 |
|
RU2436987C1 |
| CREATION OF PROPULSIVE FORCE FOR AIRCRAFT DISPLACEMENT AND TURBOJET TO THIS END | 2012 |
|
RU2557830C2 |
| METHOD AND DEVICE TO MOVE IN GASEOUS OR FLUID MEDIUM | 2008 |
|
RU2380281C1 |
| METHOD AND DEVICE TO MOVE IN GASES OR FLUIDS | 2009 |
|
RU2412082C1 |
| METHOD OF SEPARATION OF MULTI-COMPONENT MIXTURE AND DEVICE FOR REALIZATION OF THIS METHOD | 2002 |
|
RU2206388C1 |
| METHOD OF MULTICOMPONENT MIX SEPARATION AND DEVICE TO THIS END | 2014 |
|
RU2567612C1 |
| METHOD AND DEVICE TO MOVE IN GASES OR FLUIDS | 2010 |
|
RU2453474C1 |
| MINIATURE GAS TURBINE ENGINE | 2007 |
|
RU2354836C1 |
| METHOD OF PRODUCING DESALINATED WATER AND APPARATUS THEREFOR | 2014 |
|
RU2567615C1 |
