FR74688E - 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
FR74688E
FR74688E FR782401A FR782401A FR74688E FR 74688 E FR74688 E FR 74688E FR 782401 A FR782401 A FR 782401A FR 782401 A FR782401 A FR 782401A FR 74688 E FR74688 E FR 74688E
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
FR782401A
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 FR782401A priority Critical patent/FR74688E/en
Application granted granted Critical
Publication of FR74688E publication Critical patent/FR74688E/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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR782401A 1958-12-22 1958-12-22 Combustion chamber for jet engine, gas turbine or other engine Expired FR74688E (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR782401A FR74688E (en) 1958-12-22 1958-12-22 Combustion chamber for jet engine, gas turbine or other engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR782401A FR74688E (en) 1958-12-22 1958-12-22 Combustion chamber for jet engine, gas turbine or other engine

Publications (1)

Publication Number Publication Date
FR74688E true FR74688E (en) 1960-12-26

Family

ID=8709535

Family Applications (1)

Application Number Title Priority Date Filing Date
FR782401A Expired FR74688E (en) 1958-12-22 1958-12-22 Combustion chamber for jet engine, gas turbine or other engine

Country Status (1)

Country Link
FR (1) FR74688E (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0651207A1 (en) * 1993-10-27 1995-05-03 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Diffuser with a varying circumferential supply

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0651207A1 (en) * 1993-10-27 1995-05-03 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Diffuser with a varying circumferential supply
FR2711771A1 (en) * 1993-10-27 1995-05-05 Snecma Variable circumferential feed chamber diffuser.
US5592820A (en) * 1993-10-27 1997-01-14 Societe National D'etdue Et De Construction De Moteurs D'aviation S.N.E.C.M.A Gas turbine diffuser

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