GB699166A - Improvements in or relating to gas turbine plants - Google Patents
Improvements in or relating to gas turbine plantsInfo
- Publication number
- GB699166A GB699166A GB3057/52A GB305752A GB699166A GB 699166 A GB699166 A GB 699166A GB 3057/52 A GB3057/52 A GB 3057/52A GB 305752 A GB305752 A GB 305752A GB 699166 A GB699166 A GB 699166A
- Authority
- GB
- United Kingdom
- Prior art keywords
- combustion chamber
- combustion
- turbine
- fuel
- gaseous fuel
- 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
- 238000002485 combustion reaction Methods 0.000 abstract 8
- 239000000446 fuel Substances 0.000 abstract 4
- 239000002737 fuel gas Substances 0.000 abstract 2
- 239000000567 combustion gas Substances 0.000 abstract 1
- 239000007789 gas Substances 0.000 abstract 1
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
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/08—Heating air supply before combustion, e.g. by exhaust gases
-
- 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
-
- 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
- F02C3/36—Open cycles
-
- 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
- F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
- F02C6/18—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use using the waste heat of gas-turbine plants outside the plants themselves, e.g. gas-turbine power heat plants
-
- 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
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/12—Cooling of plants
- F02C7/16—Cooling of plants characterised by cooling medium
- F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
Abstract
699,166. Generating combustion products under pressure. MASCHINENFABRIK OERLIKON. Feb. 5, 1952 [March 21, 1951], No. 3057/52. Class 51(i) [Also in Group XXVI] In a combustion chamber of a gas turbine plant using gaseous fuel only a part of the fuel is burnt with combustion air introduced from outside, the remainder of the gaseous fuel is separately introduced into the combustion chamber so as to reduce the temperature of the combustion gases and walls of the combustion chamber. In the arrangement shown, the fuel gas is compressed in a compressor 5 and preheated in a recuperator 2 before passing to a combustion chamber 3 feeding a turbine 4 which exhausts through the recuperator 2. Only a part of the fuel gas is burnt in the combustion chamber 3 with air supplied by the compressor 1, the remainder is passed through a line 6 to mix with the combustion products before they enter the turbine. The exhaust of the turbine 4 may be used as a gaseous fuel for other purposes.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CH699166X | 1951-03-21 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB699166A true GB699166A (en) | 1953-10-28 |
Family
ID=4529881
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB3057/52A Expired GB699166A (en) | 1951-03-21 | 1952-02-05 | Improvements in or relating to gas turbine plants |
Country Status (4)
| Country | Link |
|---|---|
| CH (1) | CH288843A (en) |
| FR (1) | FR1051609A (en) |
| GB (1) | GB699166A (en) |
| NL (1) | NL80279C (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3798898A (en) * | 1970-10-22 | 1974-03-26 | J Delahaye | Gas turbine prime mover |
| 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 |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE956552C (en) * | 1954-01-14 | 1957-01-17 | Eschweiler Bergwerksverein | Process for the combined operation of thermal degassing devices with open gas turbine systems |
| DE1240338B (en) * | 1961-07-12 | 1967-05-11 | Ladislav Michalicka | Gas turbine plant with a pressure combustion chamber for solid fuel |
| DE1173291B (en) * | 1961-07-17 | 1964-07-02 | Ingersoll Rand Co | Dust separator for a gas turbine |
| DE102011109948A1 (en) * | 2011-08-10 | 2013-02-14 | h s beratung GmbH & Co. KG | gas turbine |
| DE102011088872A1 (en) * | 2011-12-16 | 2013-06-20 | Siemens Aktiengesellschaft | Gas turbine used in gas and steam power plant, has compressor connected with heat exchanger that is coupled with combustion chamber or expander in order to supply heated air to combustion chamber or expander |
-
0
- NL NL80279D patent/NL80279C/xx active
-
1951
- 1951-03-21 CH CH288843D patent/CH288843A/en unknown
-
1952
- 1952-02-05 GB GB3057/52A patent/GB699166A/en not_active Expired
- 1952-02-11 FR FR1051609D patent/FR1051609A/en not_active Expired
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3798898A (en) * | 1970-10-22 | 1974-03-26 | J Delahaye | Gas turbine prime mover |
| 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 |
Also Published As
| Publication number | Publication date |
|---|---|
| FR1051609A (en) | 1954-01-18 |
| NL80279C (en) | |
| CH288843A (en) | 1953-02-15 |
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