GB629832A - Improvements in or relating to gas turbine power plants - Google Patents

Improvements in or relating to gas turbine power plants

Info

Publication number
GB629832A
GB629832A GB29252/47A GB2925247A GB629832A GB 629832 A GB629832 A GB 629832A GB 29252/47 A GB29252/47 A GB 29252/47A GB 2925247 A GB2925247 A GB 2925247A GB 629832 A GB629832 A GB 629832A
Authority
GB
United Kingdom
Prior art keywords
gas turbine
relating
nov
power plants
turbine power
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
GB29252/47A
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.)
Ljungstroms Angturbin AB
Original Assignee
Ljungstroms Angturbin AB
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 Ljungstroms Angturbin AB filed Critical Ljungstroms Angturbin AB
Publication of GB629832A publication Critical patent/GB629832A/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
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/02—Plural gas-turbine plants having a common power output
    • 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
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/055—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor being of the positive-displacement type
    • 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
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)

Abstract

629,832. Heating gases. AKTIEBOLAGET LJUNGSTROMS ANGTURBIN. Nov. 3, 1947, No. 29252. Convention date, Nov. 2, 1946. [Class 64(iii)] [Also in Group XXVI] Compressed air for the combustion chambers of a gas turbine plant is heated by the turbine exhaust gases in a heat exchanger, Fig. 6, comprising inlet headers 108a, 110a and exit headers 112a, 114a connected by banks of U-shaped tubes 142 of flattened cross-section with internal and external fins. The exhaust gases flow from the outer space 90 to the inner space 102 and then axially to the discharge.
GB29252/47A 1946-11-02 1947-11-03 Improvements in or relating to gas turbine power plants Expired GB629832A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE629832X 1946-11-02

Publications (1)

Publication Number Publication Date
GB629832A true GB629832A (en) 1949-09-29

Family

ID=20313490

Family Applications (1)

Application Number Title Priority Date Filing Date
GB29252/47A Expired GB629832A (en) 1946-11-02 1947-11-03 Improvements in or relating to gas turbine power plants

Country Status (1)

Country Link
GB (1) GB629832A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2962487A1 (en) * 2010-07-06 2012-01-13 Turbomeca HEAT EXCHANGE ARCHITECTURE INTEGRATED WITH THE EXHAUST OF A TURBOMACHINE

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2962487A1 (en) * 2010-07-06 2012-01-13 Turbomeca HEAT EXCHANGE ARCHITECTURE INTEGRATED WITH THE EXHAUST OF A TURBOMACHINE
WO2012004515A3 (en) * 2010-07-06 2012-03-22 Turbomeca Heat-exchange architecture built into the exhaust of a turbine engine
US9500128B2 (en) 2010-07-06 2016-11-22 Turbomeca Heat-exchange architecture built into the exhaust of a turbine engine
RU2609039C2 (en) * 2010-07-06 2017-01-30 Турбомека Design of heat exchanger integrated into turbine machine outlet

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