GB620073A - Improvements in or relating to combustion systems for gas turbines with heat exchangers - Google Patents

Improvements in or relating to combustion systems for gas turbines with heat exchangers

Info

Publication number
GB620073A
GB620073A GB172/47A GB17247A GB620073A GB 620073 A GB620073 A GB 620073A GB 172/47 A GB172/47 A GB 172/47A GB 17247 A GB17247 A GB 17247A GB 620073 A GB620073 A GB 620073A
Authority
GB
United Kingdom
Prior art keywords
tube
heat
burner
exchanger
primary air
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
GB172/47A
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.)
CA Parsons and Co Ltd
Original Assignee
CA Parsons and Co Ltd
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 CA Parsons and Co Ltd filed Critical CA Parsons and Co Ltd
Priority to GB172/47A priority Critical patent/GB620073A/en
Publication of GB620073A publication Critical patent/GB620073A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23L—SUPPLYING AIR OR NON-COMBUSTIBLE LIQUIDS OR GASES TO COMBUSTION APPARATUS IN GENERAL ; VALVES OR DAMPERS SPECIALLY ADAPTED FOR CONTROLLING AIR SUPPLY OR DRAUGHT IN COMBUSTION APPARATUS; INDUCING DRAUGHT IN COMBUSTION APPARATUS; TOPS FOR CHIMNEYS OR VENTILATING SHAFTS; TERMINALS FOR FLUES
    • F23L15/00—Heating of air supplied for combustion
    • 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
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E20/00—Combustion technologies with mitigation potential
    • Y02E20/34—Indirect CO2mitigation, i.e. by acting on non CO2directly related matters of the process, e.g. pre-heating or heat recovery

Abstract

620,073. Burners. PARSONS & CO., Ltd., C. A., and BOWDEN, A. T. Jan. 2, 1947, No. 172. [Class 75(i)] [Also in Groups XII and XXVI] In a gas turbine plant, using an exhaust gas heat-exchanger, the primary air for the burner in a combustion chamber is taken from the air-compressor delivery in front of the heat-exchanger. The primary air may be passed through a heat-exchanger which, during normal running, is used to cool it and which, for starting may be used to heat it. The combustion chamber comprises a tube E, Fig. 2, within a conduit O. The primary air is led to a burner tube R, Fig. 3, through ports T. The main stream of air enters the conduit O at A and is divided by the nozzle B, part passing outside the tube E and part entering the tube. Of the latter, some enters a sleeve S, Fig. 3, surrounding the burner tube R, through ports P and passes to swirl blades C. The fuel oil supplied to the burner is governed by the amount released to the return line.
GB172/47A 1947-01-02 1947-01-02 Improvements in or relating to combustion systems for gas turbines with heat exchangers Expired GB620073A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB172/47A GB620073A (en) 1947-01-02 1947-01-02 Improvements in or relating to combustion systems for gas turbines with heat exchangers

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB172/47A GB620073A (en) 1947-01-02 1947-01-02 Improvements in or relating to combustion systems for gas turbines with heat exchangers

Publications (1)

Publication Number Publication Date
GB620073A true GB620073A (en) 1949-03-18

Family

ID=9699675

Family Applications (1)

Application Number Title Priority Date Filing Date
GB172/47A Expired GB620073A (en) 1947-01-02 1947-01-02 Improvements in or relating to combustion systems for gas turbines with heat exchangers

Country Status (1)

Country Link
GB (1) GB620073A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4505665A (en) * 1980-02-19 1985-03-19 Southern California Edison Method and burner tip for suspressing emissions of nitrogen oxides
US4618323A (en) * 1980-02-19 1986-10-21 Southers California Edison Method and burner tip for suppressing emissions of nitrogen oxides
GB2326197A (en) * 1997-06-11 1998-12-16 Solar Turbines Inc Gas turbine engine with recuperator

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4505665A (en) * 1980-02-19 1985-03-19 Southern California Edison Method and burner tip for suspressing emissions of nitrogen oxides
US4618323A (en) * 1980-02-19 1986-10-21 Southers California Edison Method and burner tip for suppressing emissions of nitrogen oxides
GB2326197A (en) * 1997-06-11 1998-12-16 Solar Turbines Inc Gas turbine engine with recuperator

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