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FR1135631A - Combustion chamber for jet engine, gas turbine or other engine - Google Patents

Combustion chamber for jet engine, gas turbine or other engine

Info

Publication number
FR1135631A
FR1135631A FR1135631DA FR1135631A FR 1135631 A FR1135631 A FR 1135631A FR 1135631D A FR1135631D A FR 1135631DA FR 1135631 A FR1135631 A FR 1135631A
Authority
FR
France
Prior art keywords
engine
combustion chamber
gas turbine
jet
jet engine
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 FR1135631A publication Critical patent/FR1135631A/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
    • 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)
  • Pre-Mixing And Non-Premixing Gas Burner (AREA)
FR1135631D 1953-02-24 1955-11-17 Combustion chamber for jet engine, gas turbine or other engine Expired FR1135631A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB511953A GB741488A (en) 1953-02-24 1953-02-24 Combustion chambers for jet-propulsion engines, gas turbines and other prime movers

Publications (1)

Publication Number Publication Date
FR1135631A true FR1135631A (en) 1957-05-02

Family

ID=9790071

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1135631D Expired FR1135631A (en) 1953-02-24 1955-11-17 Combustion chamber for jet engine, gas turbine or other engine

Country Status (2)

Country Link
FR (1) FR1135631A (en)
GB (1) GB741488A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1245644B (en) * 1963-06-20 1967-07-27 Rolls Royce Combustion chamber for gas turbine engines

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2996884A (en) * 1959-03-11 1961-08-22 Rolls Royce Combustion chamber
NL268838A (en) * 1960-09-13
DE1626040B1 (en) * 1968-03-02 1971-06-24 Lucas Industries Ltd Annular combustion chamber for gas turbine engines
US4527386A (en) * 1983-02-28 1985-07-09 United Technologies Corporation Diffuser for gas turbine engine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1245644B (en) * 1963-06-20 1967-07-27 Rolls Royce Combustion chamber for gas turbine engines

Also Published As

Publication number Publication date
GB741488A (en) 1955-12-07

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