GB2030653B - Gas turbine engine combustion gas temperature variation - Google Patents

Gas turbine engine combustion gas temperature variation

Info

Publication number
GB2030653B
GB2030653B GB7925598A GB7925598A GB2030653B GB 2030653 B GB2030653 B GB 2030653B GB 7925598 A GB7925598 A GB 7925598A GB 7925598 A GB7925598 A GB 7925598A GB 2030653 B GB2030653 B GB 2030653B
Authority
GB
United Kingdom
Prior art keywords
turbine engine
temperature variation
engine combustion
gas turbine
combustion gas
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
GB7925598A
Other languages
English (en)
Other versions
GB2030653A (en
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of GB2030653A publication Critical patent/GB2030653A/en
Application granted granted Critical
Publication of GB2030653B publication Critical patent/GB2030653B/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • F23R3/06—Arrangement of apertures along the flame tube
    • 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
    • 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)
  • Turbine Rotor Nozzle Sealing (AREA)
GB7925598A 1978-10-02 1979-07-23 Gas turbine engine combustion gas temperature variation Expired GB2030653B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US94791978A 1978-10-02 1978-10-02

Publications (2)

Publication Number Publication Date
GB2030653A GB2030653A (en) 1980-04-10
GB2030653B true GB2030653B (en) 1983-05-05

Family

ID=25486990

Family Applications (1)

Application Number Title Priority Date Filing Date
GB7925598A Expired GB2030653B (en) 1978-10-02 1979-07-23 Gas turbine engine combustion gas temperature variation

Country Status (6)

Country Link
JP (1) JPS5560625A (ja)
CA (1) CA1148755A (ja)
DE (1) DE2939563A1 (ja)
FR (1) FR2438166B1 (ja)
GB (1) GB2030653B (ja)
IT (1) IT1165348B (ja)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2727193B1 (fr) * 1994-11-23 1996-12-20 Snecma Chambre de combustion a deux tetes fonctionnant du ralenti au plein gaz
US7234304B2 (en) 2002-10-23 2007-06-26 Pratt & Whitney Canada Corp Aerodynamic trip to improve acoustic transmission loss and reduce noise level for gas turbine engine
FR2948987B1 (fr) * 2009-08-04 2011-12-09 Snecma Chambre de combustion de turbomachine comportant des orifices d'entree d'air ameliores
WO2020250389A1 (ja) * 2019-06-13 2020-12-17 株式会社アシックス 靴

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3126705A (en) * 1956-03-26 1964-03-31 Combustion system
NL108658C (ja) * 1958-07-31
DE1199541B (de) * 1961-12-04 1965-08-26 Jan Jerie Dr Ing Sammler von Treibgasen fuer das Leitrad von Gasturbinen
US3608310A (en) * 1966-06-27 1971-09-28 Gen Motors Corp Turbine stator-combustor structure

Also Published As

Publication number Publication date
GB2030653A (en) 1980-04-10
IT1165348B (it) 1987-04-22
DE2939563A1 (de) 1980-04-17
JPS6236142B2 (ja) 1987-08-05
JPS5560625A (en) 1980-05-07
FR2438166B1 (fr) 1986-07-11
FR2438166A1 (fr) 1980-04-30
CA1148755A (en) 1983-06-28
IT7926087A0 (it) 1979-09-28

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee