RU2014120089A - GAS-TURBINE INSTALLATION WITH MIXING WORKERS - Google Patents
GAS-TURBINE INSTALLATION WITH MIXING WORKERS Download PDFInfo
- Publication number
- RU2014120089A RU2014120089A RU2014120089/06A RU2014120089A RU2014120089A RU 2014120089 A RU2014120089 A RU 2014120089A RU 2014120089/06 A RU2014120089/06 A RU 2014120089/06A RU 2014120089 A RU2014120089 A RU 2014120089A RU 2014120089 A RU2014120089 A RU 2014120089A
- Authority
- RU
- Russia
- Prior art keywords
- turbine installation
- gas
- workers
- mixing
- nozzles
- Prior art date
Links
- 238000009434 installation Methods 0.000 title claims abstract 3
- 238000002485 combustion reaction Methods 0.000 claims abstract 4
- 239000012530 fluid Substances 0.000 claims abstract 2
- 239000000446 fuel Substances 0.000 claims abstract 2
- 239000002440 industrial waste Substances 0.000 claims abstract 2
- 239000007788 liquid Substances 0.000 claims abstract 2
- 239000000203 mixture Substances 0.000 claims abstract 2
Landscapes
- Nozzles (AREA)
- Nozzles For Spraying Of Liquid Fuel (AREA)
Abstract
Газотурбинная установка со смешением рабочих тел, включающая компрессор, турбину, расположенную между ними камеру сгорания, форсунки, одни из которых для впрыскивания топлива расположены в камере сгорания, отличающаяся тем, что другие форсунки для впрыскивания жидких горючих отходов промышленных производств расположены на входе в компрессор.A gas turbine installation with a mixture of working fluids, including a compressor, a turbine, a combustion chamber located between them, nozzles, some of which are located in the combustion chamber for injecting fuel, characterized in that the other nozzles for injecting liquid combustible industrial waste are located at the compressor inlet.
Claims (1)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2014120089/06A RU2014120089A (en) | 2014-05-19 | 2014-05-19 | GAS-TURBINE INSTALLATION WITH MIXING WORKERS |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2014120089/06A RU2014120089A (en) | 2014-05-19 | 2014-05-19 | GAS-TURBINE INSTALLATION WITH MIXING WORKERS |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| RU2014120089A true RU2014120089A (en) | 2015-11-27 |
Family
ID=54753321
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2014120089/06A RU2014120089A (en) | 2014-05-19 | 2014-05-19 | GAS-TURBINE INSTALLATION WITH MIXING WORKERS |
Country Status (1)
| Country | Link |
|---|---|
| RU (1) | RU2014120089A (en) |
-
2014
- 2014-05-19 RU RU2014120089/06A patent/RU2014120089A/en not_active Application Discontinuation
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| IN2015DN03238A (en) | ||
| EP2902708A4 (en) | COMBUSTION CHAMBER FOR GAS FUEL TURBINE | |
| EP3480523A4 (en) | GAS TURBINE COMBUSTION CHAMBER | |
| EA201300308A1 (en) | INSTALLATION FOR BURNING FUEL WITH HIGH TEMPERATURE AND HIGH PRESSURE | |
| CL2018003189A1 (en) | Biorenewable kerosene, fuel for aviation turbines, fuel mixture for aviation turbines, and manufacturing method. | |
| CN106461221A8 (en) | The burner of the axially biased burning with classification | |
| GB201516977D0 (en) | A Fuel Injector For A Gas Turbine Engine Combustion Chamber | |
| GB2569449B (en) | A gas turbine engine combustion chamber arrangement | |
| GB201115043D0 (en) | Steam injected gas turbine engine | |
| WO2015163962A3 (en) | Gas turbine engine accessory architecture | |
| GB2540315A (en) | Liquid and gaseous multi-fuel compression ignition engines | |
| GB2516584A (en) | Gas fuel turbine engine for reduced oscillations | |
| MX378011B (en) | BURNER. | |
| MX381907B (en) | CENTRIFUGAL FAN SYSTEM WITH INTERNAL GAS MIXTURE AND GAS PHASE CHEMICAL REACTOR THAT INCORPORATES THE SAME. | |
| GB2545873A (en) | Flame arresters | |
| CL2014003058A1 (en) | Mixing injector for a gas torch comprises an injector body, a central passage, a second part of the central passage that includes an injector hole, a third part of the central passage comprising a mixing chamber and a gas inlet port; blowtorch; method to mix gases. | |
| MX2018007821A (en) | Staged steam injection system. | |
| EP3535529A4 (en) | PREMIX FUEL NOZZLE FOR GAS TURBINE AND COMBUSTION CHAMBER | |
| MX2017001095A (en) | CASCADE IMPACTOR. | |
| MX2016014772A (en) | PIROTECNIA CONTAINING OLEORRESIN. | |
| RU2014120089A (en) | GAS-TURBINE INSTALLATION WITH MIXING WORKERS | |
| FR3033030B1 (en) | AIR-FUEL MIX INJECTION SYSTEM IN AN AIRCRAFT TURBOMACHINE COMBUSTION CHAMBER, COMPRISING A PERFORATED AIR INJECTION HOLES VENTURI | |
| GB2562394A8 (en) | Gas turbine engine | |
| RU2013101380A (en) | METHOD FOR ORGANIZING THE WORK OF A GAS-TURBINE INSTALLATION | |
| FI20145215L (en) | Piston engine and method of operating a piston engine |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| FA92 | Acknowledgement of application withdrawn (lack of supplementary materials submitted) |
Effective date: 20160202 |