FR959791A - - Google Patents

Info

Publication number
FR959791A
FR959791A FR959791DA FR959791A FR 959791 A FR959791 A FR 959791A FR 959791D A FR959791D A FR 959791DA FR 959791 A FR959791 A FR 959791A
Authority
FR
France
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
Other languages
French (fr)
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.)
Publication date
Priority claimed from US793375A external-priority patent/US2667033A/en
Application granted granted Critical
Publication of FR959791A publication Critical patent/FR959791A/fr
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04Air inlet arrangements
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/16Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • F23R3/18Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
    • F23R3/20Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants incorporating fuel injection means
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient 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)
  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
FR959791D 1947-01-09 Expired FR959791A (no)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
GB271829X 1947-01-09
US793375A US2667033A (en) 1947-01-09 1947-12-23 Combustion apparatus for operation in fast-moving air streams
US357999A US2826039A (en) 1947-01-09 1953-05-28 Gas inlet structure for combustion chambers

Publications (1)

Publication Number Publication Date
FR959791A true FR959791A (no) 1950-04-05

Family

ID=32329572

Family Applications (1)

Application Number Title Priority Date Filing Date
FR959791D Expired FR959791A (no) 1947-01-09

Country Status (6)

Country Link
US (1) US2826039A (no)
BE (1) BE479471A (no)
CH (1) CH271829A (no)
FR (1) FR959791A (no)
GB (1) GB620343A (no)
NL (3) NL207253A (no)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1123868B (de) * 1958-08-26 1962-02-15 Schweizerische Lokomotiv Brennkammer, insbesondere fuer Gasturbinen
GB970189A (en) * 1963-01-31 1964-09-16 Rolls Royce Combustion equipment for a gas turbine engine
US4590769A (en) * 1981-01-12 1986-05-27 United Technologies Corporation High-performance burner construction
WO1989012788A1 (en) * 1988-06-22 1989-12-28 The Secretary Of State For Defence In Her Britanni Gas turbine engine combustors
US5372008A (en) * 1992-11-10 1994-12-13 Solar Turbines Incorporated Lean premix combustor system
US5321947A (en) * 1992-11-10 1994-06-21 Solar Turbines Incorporated Lean premix combustion system having reduced combustion pressure oscillation
TWI567343B (zh) * 2015-01-16 2017-01-21 國家中山科學研究院 助燃器
US20160223196A1 (en) * 2015-02-02 2016-08-04 The Government Of The United States Of America, As Represented By The Secretary Of The Navy Crude Oil Spray Combustor
CN106287814B (zh) * 2016-09-29 2019-04-19 南京航空航天大学 一种轴向进气的地面燃气轮机单管燃烧室

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB578764A (en) * 1942-09-08 1946-07-11 Rover Co Ltd Improvements relating to combustion chambers for internal combustion turbines
US2546432A (en) * 1944-03-20 1951-03-27 Power Jets Res & Dev Ltd Apparatus for deflecting a fuel jet towards a region of turbulence in a propulsive gaseous stream
BE489359A (no) * 1944-10-05
US2610467A (en) * 1946-04-03 1952-09-16 Westinghouse Electric Corp Combustion chamber having telescoping walls and corrugated spacers
US2448561A (en) * 1946-05-01 1948-09-07 Westinghouse Electric Corp Gas turbine apparatus
US2531810A (en) * 1946-06-05 1950-11-28 Kellogg M W Co Air inlet arrangement for combustion chamber flame tubes
US2541171A (en) * 1947-01-25 1951-02-13 Kellogg M W Co Air inlet structure for combustion chambers
BE482256A (no) * 1947-05-23

Also Published As

Publication number Publication date
BE479471A (no)
US2826039A (en) 1958-03-11
NL90479C (no)
GB620343A (en) 1949-03-23
NL207253A (no)
NL82911C (no)
CH271829A (de) 1950-11-15

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