GB1084108A - - Google Patents
Info
- Publication number
- GB1084108A GB1084108A GB1084108DA GB1084108A GB 1084108 A GB1084108 A GB 1084108A GB 1084108D A GB1084108D A GB 1084108DA GB 1084108 A GB1084108 A GB 1084108A
- Authority
- GB
- United Kingdom
- Prior art keywords
- combustion chamber
- air
- auxiliary combustion
- methane
- compressor
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/20—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
- F02C3/22—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products the fuel or oxidant being gaseous at standard temperature and pressure
Abstract
1,084,108. Gas turbine plant. PRVNI BRNENSKA STROJIRNA ZAVODY KLEMENTA GOTTWALDA NARODNI PODNIK. March 25, 1965, No.12662/65. Headings F1G and F1L. In a gas turbine installation suitable for burning small amounts of combustible gases in air, e. g. methane and air such as mine air, the air-methane mixture is supplied to a catalytic combustion chamber 5 filter 1 a compressor 2 and either an exhaust gas heated heater 4 or a parallel connected auxiliary combustion chamber 3 having its own fuel supply. The auxiliary combustion chamber pre-heats the mixture during starting. The products from the combustion chamber 5 drive a turbine 6 the shaft of which is common to the compressor 2, an electric generator 7, an exciter 8 and a starting motor 9. Clean air may be injected at the compressor inlet to alter the concentration of methane in the mixture and limit the temperature before the turbine. The clean air injection and the fuel supply to the auxiliary combustion chamber may be controlled automatically. The heater 4 may be omitted, in which case the auxiliary combustion chamber is operated continuously.
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB1084108A true GB1084108A (en) | 1900-01-01 |
Family
ID=1758776
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1084108D Expired GB1084108A (en) |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB1084108A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0271360A2 (en) * | 1986-12-12 | 1988-06-15 | AlliedSignal Inc. | Power generating device and method |
| CN102562304A (en) * | 2012-02-09 | 2012-07-11 | 中煤科工集团重庆研究院 | Power generator of catalytic combustion gas turbine |
| CN103277193A (en) * | 2013-06-20 | 2013-09-04 | 中煤科工集团重庆研究院 | Combustion gas turbine power generation method adopting low calorific value gas to perform catalytic combustion |
-
0
- GB GB1084108D patent/GB1084108A/en not_active Expired
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0271360A2 (en) * | 1986-12-12 | 1988-06-15 | AlliedSignal Inc. | Power generating device and method |
| EP0271360A3 (en) * | 1986-12-12 | 1990-02-28 | AlliedSignal Inc. | Power generating device and method |
| CN102562304A (en) * | 2012-02-09 | 2012-07-11 | 中煤科工集团重庆研究院 | Power generator of catalytic combustion gas turbine |
| CN103277193A (en) * | 2013-06-20 | 2013-09-04 | 中煤科工集团重庆研究院 | Combustion gas turbine power generation method adopting low calorific value gas to perform catalytic combustion |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| SU712040A3 (en) | Method of internal combustion engine fuel supply | |
| GB1084108A (en) | ||
| GB1138165A (en) | Improvements in or relating to a gas turbine plant | |
| US3462948A (en) | Continuous flow combustion engine | |
| US8936005B2 (en) | Method for operating a stationary power generating plant | |
| CA1116415A (en) | Process and apparatus for operating a gas turbine on vaporized fuel oil | |
| GB191506353A (en) | Improvements in and relating to Hot Air and the like Motive Power Plant. | |
| GB166517A (en) | Improvements in gas operated air heating installations | |
| GB191129097A (en) | Improvements in and relating to Gas Turbine and like Plants. | |
| GB407151A (en) | Improvements in and relating to steam generating plants | |
| RU2711260C1 (en) | Steam-gas plant | |
| SU259830A1 (en) | METHOD OF HEATING TECHNOLOGICAL INSTALLATIONS | |
| GB680717A (en) | Improvements relating to rocket motors | |
| US833137A (en) | Apparatus for manufacturing and mixing gases. | |
| GB190930598A (en) | Improvements in Gas Turbine Plant. | |
| US835531A (en) | Process and apparatus for generating steam, &c. | |
| SU260320A1 (en) | METHOD OF USING MINE METHANE AS A FUEL FOR GAS TURBINE INSTALLATION | |
| GB189817898A (en) | Improved Method and Apparatus for Preparing and Applying as Motive Fluid a Mixture of Air and Steam. | |
| GB1471494A (en) | Arrangement for starting an aircraft-engine and for driving aircraft auxiliary equipment | |
| GB186083A (en) | Improved method of and apparatus for the economic transformation of the energy of steam by turbines | |
| GB163997A (en) | Improvements in apparatus and plant for the production of motive power | |
| GB189806394A (en) | Generators of Mixed Gas and Steam and Utilization of such Mixture in Motor Engines. | |
| GB191300711A (en) | Improved Method or Process for Treating Combustible Oils, Tar, and Pitch. | |
| GB190309868A (en) | New or Improved Vapour Driven Turbine or Rotary Heat Engine. | |
| GB151986A (en) | Improvements in or relating to a process for working multistage combustion turbines |