FR1095756A - Engine combustion chamber - Google Patents

Engine combustion chamber

Info

Publication number
FR1095756A
FR1095756A FR1095756DA FR1095756A FR 1095756 A FR1095756 A FR 1095756A FR 1095756D A FR1095756D A FR 1095756DA FR 1095756 A FR1095756 A FR 1095756A
Authority
FR
France
Prior art keywords
combustion chamber
engine combustion
engine
chamber
combustion
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
Other languages
French (fr)
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.)
ZF International UK Ltd
Original Assignee
Lucas Industries Ltd
Joseph Lucas Industries Ltd
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 Lucas Industries Ltd, Joseph Lucas Industries Ltd filed Critical Lucas Industries Ltd
Application granted granted Critical
Publication of FR1095756A publication Critical patent/FR1095756A/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
    • F23R3/10—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
    • 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
    • F23R3/045—Air inlet arrangements using pipes

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Gas Burners (AREA)
  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
  • Nozzles For Spraying Of Liquid Fuel (AREA)
FR1095756D 1953-01-19 1954-03-16 Engine combustion chamber Expired FR1095756A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1463/53A GB736823A (en) 1953-01-19 1953-01-19 Engine combustion chambers

Publications (1)

Publication Number Publication Date
FR1095756A true FR1095756A (en) 1955-06-06

Family

ID=9722419

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1095756D Expired FR1095756A (en) 1953-01-19 1954-03-16 Engine combustion chamber

Country Status (4)

Country Link
US (1) US2807139A (en)
DE (1) DE961672C (en)
FR (1) FR1095756A (en)
GB (1) GB736823A (en)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB980363A (en) * 1961-12-04 1965-01-13 Jan Jerie Improvements in or relating to gas turbines
US4301657A (en) * 1978-05-04 1981-11-24 Caterpillar Tractor Co. Gas turbine combustion chamber
DE4242650A1 (en) * 1992-12-17 1994-06-23 Asea Brown Boveri Gas turbine combustion chamber
GB9407029D0 (en) * 1994-04-08 1994-06-08 Rolls Royce Plc Gas turbine engine combustion apparatus
FR2748088B1 (en) * 1996-04-24 1998-05-29 Snecma OPTIMIZATION OF THE MIXTURE OF BURNED GASES IN AN ANNULAR COMBUSTION CHAMBER
US20090090110A1 (en) * 2007-10-04 2009-04-09 Honeywell International, Inc. Faceted dome assemblies for gas turbine engine combustors
US8141365B2 (en) * 2009-02-27 2012-03-27 Honeywell International Inc. Plunged hole arrangement for annular rich-quench-lean gas turbine combustors
US8171740B2 (en) * 2009-02-27 2012-05-08 Honeywell International Inc. Annular rich-quench-lean gas turbine combustors with plunged holes
GB2589885A (en) * 2019-12-11 2021-06-16 Rolls Royce Plc Combustor

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB583211A (en) * 1940-01-24 1946-12-12 Anglo Saxon Petroleum Co Improved process and apparatus for the continuous generation of gases by reaction between air and liquid or pulverulent combustible material
GB578764A (en) * 1942-09-08 1946-07-11 Rover Co Ltd Improvements relating to combustion chambers for internal combustion turbines
GB595831A (en) * 1944-03-16 1947-12-18 Power Jets Ltd Improvements relating to combustion apparatus
NL67339C (en) * 1944-11-28
US2517015A (en) * 1945-05-16 1950-08-01 Bendix Aviat Corp Combustion chamber with shielded fuel nozzle
US2531810A (en) * 1946-06-05 1950-11-28 Kellogg M W Co Air inlet arrangement for combustion chamber flame tubes
US2488911A (en) * 1946-11-09 1949-11-22 Surface Combustion Corp Combustion apparatus for use with turbines
US2541171A (en) * 1947-01-25 1951-02-13 Kellogg M W Co Air inlet structure for combustion chambers
NL74196C (en) * 1947-08-11
US2607193A (en) * 1947-10-25 1952-08-19 Curtiss Wright Corp Annular combustion chamber with multiple notched fuel nozzles
US2671314A (en) * 1950-01-26 1954-03-09 Socony Vacuum Oil Co Inc Gas turbine and method of operation therefor
FR1025198A (en) * 1950-09-27 1953-04-13 Continuous combustion chamber and explosive waves
GB715909A (en) * 1952-02-01 1954-09-22 Rolls Royce Improvements in or relating to combustion equipment of gas-turbine engines
FR1052475A (en) * 1952-03-15 1954-01-25 Snecma Combustion chambers particularly suitable for gas turbines

Also Published As

Publication number Publication date
US2807139A (en) 1957-09-24
DE961672C (en) 1957-04-11
GB736823A (en) 1955-09-14

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