DE1118535B - Flammrohr fuer Gasturbinen-Brennkammern - Google Patents

Flammrohr fuer Gasturbinen-Brennkammern

Info

Publication number
DE1118535B
DE1118535B DEU6592A DEU0006592A DE1118535B DE 1118535 B DE1118535 B DE 1118535B DE U6592 A DEU6592 A DE U6592A DE U0006592 A DEU0006592 A DE U0006592A DE 1118535 B DE1118535 B DE 1118535B
Authority
DE
Germany
Prior art keywords
flame tube
air
jacket
tube according
gas turbine
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.)
Pending
Application number
DEU6592A
Other languages
German (de)
English (en)
Inventor
George Reeder Benson
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.)
Raytheon Technologies Corp
Original Assignee
United Aircraft Corp
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 United Aircraft Corp filed Critical United Aircraft Corp
Publication of DE1118535B publication Critical patent/DE1118535B/de
Pending 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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/34—Feeding into different combustion zones
    • 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
    • F23R3/10—Air inlet arrangements for primary air
    • F23R3/12—Air inlet arrangements for primary air inducing a vortex
    • F23R3/14—Air inlet arrangements for primary air inducing a vortex by using swirl vanes
    • 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)
  • Pre-Mixing And Non-Premixing Gas Burner (AREA)
  • Spray-Type Burners (AREA)
DEU6592A 1959-03-31 1959-10-19 Flammrohr fuer Gasturbinen-Brennkammern Pending DE1118535B (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US803175A US2951339A (en) 1959-03-31 1959-03-31 Combustion chamber swirler

Publications (1)

Publication Number Publication Date
DE1118535B true DE1118535B (de) 1961-11-30

Family

ID=25185787

Family Applications (1)

Application Number Title Priority Date Filing Date
DEU6592A Pending DE1118535B (de) 1959-03-31 1959-10-19 Flammrohr fuer Gasturbinen-Brennkammern

Country Status (4)

Country Link
US (1) US2951339A (fr)
DE (1) DE1118535B (fr)
FR (1) FR1238089A (fr)
GB (1) GB887829A (fr)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3099134A (en) * 1959-12-24 1963-07-30 Havilland Engine Co Ltd Combustion chambers
DE2538134C2 (de) * 1974-08-27 1984-11-08 Mitsubishi Jukogyo K.K., Tokio/Tokyo Ölbrenner
US4173118A (en) * 1974-08-27 1979-11-06 Mitsubishi Jukogyo Kabushiki Kaisha Fuel combustion apparatus employing staged combustion
US3991562A (en) * 1975-07-21 1976-11-16 United Technologies Corporation Combustion chamber assembly having removable center liner
US5197278A (en) * 1990-12-17 1993-03-30 General Electric Company Double dome combustor and method of operation
US5253478A (en) * 1991-12-30 1993-10-19 General Electric Company Flame holding diverging centerbody cup construction for a dry low NOx combustor
US6430919B1 (en) * 2000-03-02 2002-08-13 Direct Propulsion Devices, Inc. Shaped charged engine
US7574865B2 (en) * 2004-11-18 2009-08-18 Siemens Energy, Inc. Combustor flow sleeve with optimized cooling and airflow distribution

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB670092A (en) * 1949-01-03 1952-04-16 Rolls Royce Improvements relating to combustion equipment for gas-turbine engines
US2676460A (en) * 1950-03-23 1954-04-27 United Aircraft Corp Burner construction of the can-an-nular type having means for distributing airflow to each can

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2175866A (en) * 1934-04-16 1939-10-10 Philip S Arnold Fuel burner
GB800512A (en) * 1955-01-03 1958-08-27 Lucas Industries Ltd Liquid fuel combustion chambers
US2813397A (en) * 1957-01-02 1957-11-19 United Aircraft Corp Thermal expansion means for combustion chambers

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB670092A (en) * 1949-01-03 1952-04-16 Rolls Royce Improvements relating to combustion equipment for gas-turbine engines
US2676460A (en) * 1950-03-23 1954-04-27 United Aircraft Corp Burner construction of the can-an-nular type having means for distributing airflow to each can

Also Published As

Publication number Publication date
GB887829A (en) 1962-01-24
FR1238089A (fr) 1960-08-05
US2951339A (en) 1960-09-06

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