FIELD: aeronautical engineering; surface and water transport. SUBSTANCE: turbojet engine includes case 1 made in form of semi-closed spindle-shaped chamber, axial shaft 2 mounted inside case in supports 3, compressor with blades mounted at inlet hole, combustion chamber 5, turbine with blades having inner side 7 and outer side 8 formed by spirals shaped grooves 9 in tail section of case; depth of these grooves increases smoothly in direction of outlet nozzle. Case is mounted for axial rotation in bearings 10. Engine is also provided with injectors 11, jet nozzle 12 and cooling blades 13. EFFECT: enhanced reliability. 3 cl, 6 dwg
Title | Year | Author | Number |
---|---|---|---|
TURBOJET ENGINE | 1995 |
|
RU2096642C1 |
COMBUSTION CHAMBER FOR TURBOJET THREE-CIRCUIT ENGINE WITH TWO HIGH PRESSURE TURBINES | 2018 |
|
RU2699161C1 |
TURBOJET ENGINE | 0 |
|
SU1813909A1 |
HYBRID JET ENGINE | 2005 |
|
RU2272926C1 |
GAS-TURBINE TURBOFAN ENGINE | 2003 |
|
RU2271460C2 |
METHOD OF CREATING A TRAIL AND POWER INSTALLATION FOR ITS IMPLEMENTATION | 2017 |
|
RU2680214C1 |
HYPERSONIC AIRCRAFT WITH COMPOUND PROPULSION SYSTEM AND COOLING SYSTEM OF SUCH AIRCRAFT TURBOJET HIGH-PRESSURE TURBINE | 2015 |
|
RU2615842C2 |
CREATION OF PROPULSIVE FORCE FOR AIRCRAFT DISPLACEMENT AND TURBOJET TO THIS END | 2012 |
|
RU2557830C2 |
METHOD FOR CREATING DRIVING FORCE FOR MOVEMENT OF TRANSPORT VEHICLE AND JET ENGINE FOR ITS IMPLEMENTATION | 2010 |
|
RU2436987C1 |
TURBOJET ENGINE | 2019 |
|
RU2727532C1 |
Authors
Dates
1997-11-20—Published
1995-02-28—Filed