IT949676B - IMPROVEMENT IN GAS TURBINES - Google Patents

IMPROVEMENT IN GAS TURBINES

Info

Publication number
IT949676B
IT949676B IT47877/72A IT4787772A IT949676B IT 949676 B IT949676 B IT 949676B IT 47877/72 A IT47877/72 A IT 47877/72A IT 4787772 A IT4787772 A IT 4787772A IT 949676 B IT949676 B IT 949676B
Authority
IT
Italy
Prior art keywords
improvement
gas turbines
turbines
gas
Prior art date
Application number
IT47877/72A
Other languages
Italian (it)
Original Assignee
Secr Defence Brit
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 Secr Defence Brit filed Critical Secr Defence Brit
Application granted granted Critical
Publication of IT949676B publication Critical patent/IT949676B/en

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
    • F23R3/08—Arrangement of apertures along the flame tube between annular flame tube sections, e.g. flame tubes with telescopic sections
    • 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)
IT47877/72A 1971-01-25 1972-01-22 IMPROVEMENT IN GAS TURBINES IT949676B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB305371 1971-01-25

Publications (1)

Publication Number Publication Date
IT949676B true IT949676B (en) 1973-06-11

Family

ID=9751092

Family Applications (1)

Application Number Title Priority Date Filing Date
IT47877/72A IT949676B (en) 1971-01-25 1972-01-22 IMPROVEMENT IN GAS TURBINES

Country Status (4)

Country Link
US (1) US3737152A (en)
FR (1) FR2123386B1 (en)
GB (1) GB1320482A (en)
IT (1) IT949676B (en)

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1429677A (en) * 1973-03-20 1976-03-24 Rolls Royce Gas turbine engine combustion equipment
FR2406075A1 (en) * 1977-10-11 1979-05-11 Snecma COMBUSTION APPARATUS AND ITS EMBODIMENT PROCESS
US4233123A (en) * 1978-12-18 1980-11-11 General Motors Corporation Method for making an air cooled combustor
FR2450349A1 (en) * 1979-03-01 1980-09-26 Snecma IMPROVEMENT IN COOLING OF COMBUSTION CHAMBER WALLS BY AIR FILM
GB2044912B (en) * 1979-03-22 1983-02-23 Rolls Royce Gas turbine combustion chamber
US4232527A (en) * 1979-04-13 1980-11-11 General Motors Corporation Combustor liner joints
US4242871A (en) * 1979-09-18 1981-01-06 United Technologies Corporation Louver burner liner
US4923371A (en) * 1988-04-01 1990-05-08 General Electric Company Wall having cooling passage
GB2221979B (en) * 1988-08-17 1992-03-25 Rolls Royce Plc A combustion chamber for a gas turbine engine
WO1995025932A1 (en) * 1989-08-31 1995-09-28 Alliedsignal Inc. Turbine combustor cooling system
US5329773A (en) * 1989-08-31 1994-07-19 Alliedsignal Inc. Turbine combustor cooling system
US5181379A (en) * 1990-11-15 1993-01-26 General Electric Company Gas turbine engine multi-hole film cooled combustor liner and method of manufacture
US5307637A (en) * 1992-07-09 1994-05-03 General Electric Company Angled multi-hole film cooled single wall combustor dome plate
US5261223A (en) * 1992-10-07 1993-11-16 General Electric Company Multi-hole film cooled combustor liner with rectangular film restarting holes
US6021570A (en) * 1997-11-20 2000-02-08 Caterpillar Inc. Annular one piece combustor liner
FR2914986B1 (en) * 2007-04-12 2015-04-10 Saint Gobain Isover INTERNAL COMBUSTION BURNER
US9494081B2 (en) 2013-05-09 2016-11-15 Siemens Aktiengesellschaft Turbine engine shutdown temperature control system with an elongated ejector
US11867402B2 (en) * 2021-03-19 2024-01-09 Rtx Corporation CMC stepped combustor liner
CN117091159A (en) 2022-05-13 2023-11-21 通用电气公司 Combustor liner
CN117091157A (en) 2022-05-13 2023-11-21 通用电气公司 Plate hanger structure for durable combustor liner
CN117091158A (en) 2022-05-13 2023-11-21 通用电气公司 Combustor chamber mesh structure
CN117091162A (en) 2022-05-13 2023-11-21 通用电气公司 Burner with dilution hole structure
CN117091161A (en) 2022-05-13 2023-11-21 通用电气公司 Combustor liner hollow plate design and construction

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL69245C (en) * 1946-01-09
US3623711A (en) * 1970-07-13 1971-11-30 Avco Corp Combustor liner cooling arrangement

Also Published As

Publication number Publication date
GB1320482A (en) 1973-06-13
FR2123386A1 (en) 1972-09-08
US3737152A (en) 1973-06-05
DE2202356B2 (en) 1976-02-19
DE2202356A1 (en) 1972-08-10
FR2123386B1 (en) 1976-07-23

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