GB699166A - Improvements in or relating to gas turbine plants - Google Patents

Improvements in or relating to gas turbine plants

Info

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
Application number
GB3057/52A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rheinmetall Air Defence AG
Maschinenfabrik Oerlikon AG
Original Assignee
Werkzeugmaschinenfabrik Oerlikon Buhrle AG
Maschinenfabrik Oerlikon AG
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Werkzeugmaschinenfabrik Oerlikon Buhrle AG, Maschinenfabrik Oerlikon AG filed Critical Werkzeugmaschinenfabrik Oerlikon Buhrle AG
Publication of GB699166A publication Critical patent/GB699166A/en
Expired legal-status Critical Current

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
    • 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.
GB3057/52A 1951-03-21 1952-02-05 Improvements in or relating to gas turbine plants Expired GB699166A (en)

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

Cited By (2)

* Cited by examiner, † Cited by third party
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
CH288843A (en) 1953-02-15
NL80279C (en)

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