RU2014100841A - HYDROGEN GAS TURBINE ENGINE - Google Patents
HYDROGEN GAS TURBINE ENGINE Download PDFInfo
- Publication number
- RU2014100841A RU2014100841A RU2014100841/06A RU2014100841A RU2014100841A RU 2014100841 A RU2014100841 A RU 2014100841A RU 2014100841/06 A RU2014100841/06 A RU 2014100841/06A RU 2014100841 A RU2014100841 A RU 2014100841A RU 2014100841 A RU2014100841 A RU 2014100841A
- Authority
- RU
- Russia
- Prior art keywords
- compressor
- gas turbine
- heat exchanger
- hydrogen
- turbine engine
- Prior art date
Links
Landscapes
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
1. Водородный газотурбинный двигатель, содержащий воздухозаборник, корпус, компрессор с ротором компрессора, камеру сгорания, установленную за компрессором и соединенную с ним воздушным трактом, газовую турбину, вал, соединяющий компрессор и газовую турбину, и реактивное сопло, отличающийся тем, что за компрессором выполнен воздушный тракт, в котором установлен теплообменник, внутри воздушного тракта коаксиально валу установлена водородная турбина, которая имеет входной и выходной коллекторы, входной коллектор соединен с выходом их теплообменника, а выходной - с камерой сгорания, при этом водородная турбина и второй компрессор соединены вторым валом установленным коаксиально первому, отличающийся тем, что теплообменник установлен на входе в воздушный тракт.2. Водородный газотурбинный двигатель по п. 1, отличающийся тем, что реактивное сопло выполнено сверхзвуковым.1. A hydrogen gas turbine engine containing an air intake, a housing, a compressor with a compressor rotor, a combustion chamber installed behind the compressor and connected to it by an air path, a gas turbine, a shaft connecting the compressor and the gas turbine, and a jet nozzle, characterized in that behind the compressor an air path is made in which a heat exchanger is installed, a hydrogen turbine is installed inside the air path coaxially to the shaft, which has an input and output collectors, the input collector is connected to the outlet of their heat a heat exchanger, and the output one with a combustion chamber, while the hydrogen turbine and the second compressor are connected by a second shaft mounted coaxially to the first, characterized in that the heat exchanger is installed at the entrance to the air duct. 2. A hydrogen gas turbine engine according to claim 1, characterized in that the jet nozzle is made supersonic.
Claims (2)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2014100841/06A RU2014100841A (en) | 2014-01-10 | 2014-01-10 | HYDROGEN GAS TURBINE ENGINE |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2014100841/06A RU2014100841A (en) | 2014-01-10 | 2014-01-10 | HYDROGEN GAS TURBINE ENGINE |
Publications (1)
Publication Number | Publication Date |
---|---|
RU2014100841A true RU2014100841A (en) | 2015-08-10 |
Family
ID=53795611
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU2014100841/06A RU2014100841A (en) | 2014-01-10 | 2014-01-10 | HYDROGEN GAS TURBINE ENGINE |
Country Status (1)
Country | Link |
---|---|
RU (1) | RU2014100841A (en) |
-
2014
- 2014-01-10 RU RU2014100841/06A patent/RU2014100841A/en unknown
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP2784267A3 (en) | A gas turbine engine cooling arrangement | |
WO2014158244A3 (en) | Intercooled gas turbine with closed combined power cycle | |
RU2008100463A (en) | TURBO-FAN ENGINE | |
RU2015106468A (en) | GAS-TURBINE ENGINE WITH A SHORTED MIDDLE PART | |
RU2014100841A (en) | HYDROGEN GAS TURBINE ENGINE | |
RU2013152094A (en) | GAS TURBINE ENGINE | |
RU2011114620A (en) | GAS-TURBINE INSTALLATION FOR PROCESSING OF ASSOCIATED OIL GAS IN ELECTRICITY | |
RU2013138163A (en) | DEVICE AND METHOD FOR ECONOMIC PRODUCTION OF ELECTRIC POWER AND HEAT | |
RU2014101280A (en) | TWO-COMPONENT AIR-REACTIVE ENGINE | |
RU2017141680A (en) | VENTILATING POWER INSTALLATION | |
RU2014105197A (en) | CHARGING SYSTEM FOR INLET TRAIN OF THE INTERNAL COMBUSTION ENGINE USING THE ENERGY OF EXHAUST GASES | |
RU2011106274A (en) | TURBO COMPRESSOR WIND GENERATOR | |
RU2015155124A (en) | GAS-TURBINE ENGINE WITH EXTERNAL HEAT EXCHANGER | |
ES2571627A1 (en) | Composite motor (Machine-translation by Google Translate, not legally binding) | |
RU2013159095A (en) | GAS-TURBINE ENGINE DISCONTINUOUS SYSTEM | |
RU2014109324A (en) | METHOD FOR IMPROVING ECONOMICITY OF GAS-TURBINE ENGINE AND GAS-TURBINE ENGINE | |
RU2014101065A (en) | TWO-FUEL AIR-REACTIVE ENGINE | |
RU2012116486A (en) | INTERNAL COMBUSTION ENGINE | |
RU2007147567A (en) | FAN AIRCRAFT ENGINE | |
RU2013154731A (en) | GAS TURBINE ELECTRIC GENERATOR | |
RU2017121550A (en) | Turbofan engine | |
RU2015157286A (en) | HELICOPTER GAS-TURBINE POWER PLANT | |
RU2010115169A (en) | TURBOROTOR AIR-REACTIVE ENGINE AND THE SYSTEM OF ITS INTERNAL AIR COOLING | |
RU2013119016A (en) | ENERGY INSTALLATION | |
RU2010117441A (en) | METHOD FOR INCREASING EFFICIENCY OF GAS-TURBINE INSTALLATIONS |