FR1381149A - Liquid fuel combustion apparatus for jet propulsion engine, gas turbine or other prime mover - Google Patents

Liquid fuel combustion apparatus for jet propulsion engine, gas turbine or other prime mover

Info

Publication number
FR1381149A
FR1381149A FR962434A FR962434A FR1381149A FR 1381149 A FR1381149 A FR 1381149A FR 962434 A FR962434 A FR 962434A FR 962434 A FR962434 A FR 962434A FR 1381149 A FR1381149 A FR 1381149A
Authority
FR
France
Prior art keywords
gas turbine
liquid fuel
prime mover
combustion apparatus
fuel 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
FR962434A
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
Priority to FR962434A priority Critical patent/FR1381149A/en
Priority claimed from US346278A external-priority patent/US3232054A/en
Application granted granted Critical
Publication of FR1381149A publication Critical patent/FR1381149A/en
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
    • F23R3/10Air inlet arrangements for primary air

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR962434A 1964-02-03 1964-02-03 Liquid fuel combustion apparatus for jet propulsion engine, gas turbine or other prime mover Expired FR1381149A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR962434A FR1381149A (en) 1964-02-03 1964-02-03 Liquid fuel combustion apparatus for jet propulsion engine, gas turbine or other prime mover

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR962434A FR1381149A (en) 1964-02-03 1964-02-03 Liquid fuel combustion apparatus for jet propulsion engine, gas turbine or other prime mover
US346278A US3232054A (en) 1964-02-20 1964-02-20 Liquid fuel combustion apparatus, for jet-propulsion engines, gas turbines, or other prime movers

Publications (1)

Publication Number Publication Date
FR1381149A true FR1381149A (en) 1964-12-04

Family

ID=26205688

Family Applications (1)

Application Number Title Priority Date Filing Date
FR962434A Expired FR1381149A (en) 1964-02-03 1964-02-03 Liquid fuel combustion apparatus for jet propulsion engine, gas turbine or other prime mover

Country Status (1)

Country Link
FR (1) FR1381149A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4373327A (en) * 1979-07-04 1983-02-15 Rolls-Royce Limited Gas turbine engine combustion chambers

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4373327A (en) * 1979-07-04 1983-02-15 Rolls-Royce Limited Gas turbine engine combustion chambers

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