GB709147A - Method of operating gas-turbine plants - Google Patents
Method of operating gas-turbine plantsInfo
- Publication number
- GB709147A GB709147A GB2325/52A GB232552A GB709147A GB 709147 A GB709147 A GB 709147A GB 2325/52 A GB2325/52 A GB 2325/52A GB 232552 A GB232552 A GB 232552A GB 709147 A GB709147 A GB 709147A
- Authority
- GB
- United Kingdom
- Prior art keywords
- gas
- turbine
- combustion chamber
- combustion
- supplied
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
Abstract
709,147. Gas turbine plant. LICENCIA TALALMANYOKAT ERTEKESITO VALLALAT. Jan. 28, 1952 [Jan. 29, 1951], No. 2325/52. Class 110(3) A gas turbine plant adapted to utilize a natural source of gas which may be incombustible gas or a mixture of incombustible gas with a combustible gas comprises a compressor which supplies only sufficient air for complete combustion of the fuel to a combustion chamber feeding the turbine, a supply duct which supplies natural gas to the combustion chamber to cool the combustion gases and control means responsive to the temperature at the outlet of the combustion chamber to control the supply of natural gas. Air from the compressor 12 is heated by the exhaust gases from the turbine 10 in a heat exchanger 21 before passing to a combustion chamber 11. Only sufficient air for the combustion of the fuel supplied through the conduit 22 is supplied by the compressor 12. The temperature of the gases supplied to the turbine 10 is reduced by mixing natural incombustible gas from a source 25 with the gases. The amount of gas supplied is controlled by a valve 34 operated by a temperature sensitive element 33 to maintain the inlet temperature to the turbine constant If the pressure at the source 25 is considerably higher than that in the combustion chamber 11. the natural gas may be throttled or expanded in a turbine or other prime mover 27 before being supplied to the combustion chamber. If a turbine or other prime mover is used the natural gas may be preheated before use in the turbine 27 in an exhaust gas heat exchanger 32. A modification in which the natural gas is mixed with the combustion gases in a chamber integral with but separate from the combustion chamber is described. The natural gas may be a mixture of CH 4 and CO 2 in the ratio of 35-65 per cent by volume.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| HU709147X | 1951-01-29 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB709147A true GB709147A (en) | 1954-05-19 |
Family
ID=10980067
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB2325/52A Expired GB709147A (en) | 1951-01-29 | 1952-01-28 | Method of operating gas-turbine plants |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB709147A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2504593A1 (en) * | 1981-04-27 | 1982-10-29 | Exxon Production Research Co | METHOD FOR USING THE COMBUSTION STAGE OF A GAS TURBINE ENGINE AND ENGINE FOR HEATING A RESIDUAL GAS, AND ENGINE AND GAS TURBINE SYSTEM USED THEREFOR |
| GB2263314A (en) * | 1992-01-14 | 1993-07-21 | Hendrick Walterus Klavers | Power generation process. |
| CN109882292A (en) * | 2019-03-27 | 2019-06-14 | 赫普科技发展（北京）有限公司 | A kind of LNG gas turbine coupling cold energy generation system and electricity-generating method |
| CN113309612A (en) * | 2021-06-15 | 2021-08-27 | 东北大学 | Combined cooling, heating and power system for coupling pressure energy, compressed air energy storage and solar energy |
| CN113567143A (en) * | 2021-08-27 | 2021-10-29 | 华能国际电力股份有限公司 | Visual gas turbine combustion chamber experimental system |
-
1952
- 1952-01-28 GB GB2325/52A patent/GB709147A/en not_active Expired
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2504593A1 (en) * | 1981-04-27 | 1982-10-29 | Exxon Production Research Co | METHOD FOR USING THE COMBUSTION STAGE OF A GAS TURBINE ENGINE AND ENGINE FOR HEATING A RESIDUAL GAS, AND ENGINE AND GAS TURBINE SYSTEM USED THEREFOR |
| GB2263314A (en) * | 1992-01-14 | 1993-07-21 | Hendrick Walterus Klavers | Power generation process. |
| CN109882292A (en) * | 2019-03-27 | 2019-06-14 | 赫普科技发展（北京）有限公司 | A kind of LNG gas turbine coupling cold energy generation system and electricity-generating method |
| CN113309612A (en) * | 2021-06-15 | 2021-08-27 | 东北大学 | Combined cooling, heating and power system for coupling pressure energy, compressed air energy storage and solar energy |
| CN113567143A (en) * | 2021-08-27 | 2021-10-29 | 华能国际电力股份有限公司 | Visual gas turbine combustion chamber experimental system |
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