FR1590542A - - Google Patents

Info

Publication number
FR1590542A
FR1590542A FR172477A FR1590542DA FR1590542A FR 1590542 A FR1590542 A FR 1590542A FR 172477 A FR172477 A FR 172477A FR 1590542D A FR1590542D A FR 1590542DA FR 1590542 A FR1590542 A FR 1590542A
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
FR172477A
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.)
Filing date
Publication date
Application filed filed Critical
Application granted granted Critical
Publication of FR1590542A publication Critical patent/FR1590542A/fr
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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/30—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising devices
    • F23R3/32—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising devices being tubular
FR172477A 1968-11-04 1968-11-04 Expired FR1590542A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR172477 1968-11-04

Publications (1)

Publication Number Publication Date
FR1590542A true FR1590542A (en) 1970-04-13

Family

ID=8656455

Family Applications (1)

Application Number Title Priority Date Filing Date
FR172477A Expired FR1590542A (en) 1968-11-04 1968-11-04

Country Status (4)

Country Link
US (1) US3626444A (en)
DE (1) DE1953671C3 (en)
FR (1) FR1590542A (en)
GB (1) GB1280715A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2730555A1 (en) * 1995-02-15 1996-08-14 Snecma FUEL INJECTION KIT FOR GAS TURBINE COMBUSTION CHAMBER

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2131790B1 (en) * 1971-02-19 1974-09-27 Snecma
GB1392739A (en) * 1971-07-16 1975-04-30 Snecma Devices for pre-vaporising liquid fuel
FR2189630B1 (en) * 1972-06-23 1980-03-14 Snecma
GB1435083A (en) * 1972-08-10 1976-05-12 Rolls Royce Gas turbine engine combustion equipment
US4005572A (en) * 1975-04-18 1977-02-01 Giffhorn William A Gas turbine engine control system
DE2815916C2 (en) * 1978-04-13 1983-11-03 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Annular combustion chamber with fuel pre-evaporation for gas turbine engines
GB2112125B (en) * 1981-12-24 1985-06-26 Rolls Royce Fuel vapouriser for a gas turbine engine combustion chamber
GB2236588B (en) * 1989-08-31 1993-08-18 Rolls Royce Plc Improved fuel vapouriser
US5156002A (en) * 1990-03-05 1992-10-20 Rolf J. Mowill Low emissions gas turbine combustor
US5628182A (en) * 1993-07-07 1997-05-13 Mowill; R. Jan Star combustor with dilution ports in can portions
US5638674A (en) * 1993-07-07 1997-06-17 Mowill; R. Jan Convectively cooled, single stage, fully premixed controllable fuel/air combustor with tangential admission
US5377483A (en) * 1993-07-07 1995-01-03 Mowill; R. Jan Process for single stage premixed constant fuel/air ratio combustion
US5613357A (en) * 1993-07-07 1997-03-25 Mowill; R. Jan Star-shaped single stage low emission combustor system
US6220034B1 (en) 1993-07-07 2001-04-24 R. Jan Mowill Convectively cooled, single stage, fully premixed controllable fuel/air combustor
US5572862A (en) * 1993-07-07 1996-11-12 Mowill Rolf Jan Convectively cooled, single stage, fully premixed fuel/air combustor for gas turbine engine modules
US5924276A (en) * 1996-07-17 1999-07-20 Mowill; R. Jan Premixer with dilution air bypass valve assembly
US6155819A (en) * 1998-06-12 2000-12-05 Precision Combustion, Inc. Dry, low NOx catalytic pilot
US6925809B2 (en) 1999-02-26 2005-08-09 R. Jan Mowill Gas turbine engine fuel/air premixers with variable geometry exit and method for controlling exit velocities
FR3066009B1 (en) * 2017-05-02 2020-03-06 Safran Helicopter Engines PREVAPORIZATION ROD FOR A TURBOMACHINE
FR3101696B1 (en) * 2019-10-08 2021-10-29 Safran Helicopter Engines PREVAPORIZATION ROD FOR A TURBOMACHINE COMBUSTION CHAMBER

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2982098A (en) * 1953-04-22 1961-05-02 Power Jets Res & Dev Ltd Liquid fuel vaporizing combustion systems
US2956404A (en) * 1956-10-02 1960-10-18 Avco Mfg Corp Fuel vaporizer

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2730555A1 (en) * 1995-02-15 1996-08-14 Snecma FUEL INJECTION KIT FOR GAS TURBINE COMBUSTION CHAMBER
EP0727615A1 (en) * 1995-02-15 1996-08-21 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Fuel injector for gas turbine combustion chamber
US5651252A (en) * 1995-02-15 1997-07-29 Societe Nationale D'etude Et De Construction De Moteurs D'aviation S.N.E.C.M.A. Fuel injection assembly for a gas turbine engine

Also Published As

Publication number Publication date
GB1280715A (en) 1972-07-05
US3626444A (en) 1971-12-07
DE1953671B2 (en) 1979-03-01
DE1953671A1 (en) 1970-05-06
DE1953671C3 (en) 1979-10-18

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Legal Events

Date Code Title Description
ST Notification of lapse