FR2189630B1 - - Google Patents

Info

Publication number
FR2189630B1
FR2189630B1 FR7222811A FR7222811A FR2189630B1 FR 2189630 B1 FR2189630 B1 FR 2189630B1 FR 7222811 A FR7222811 A FR 7222811A FR 7222811 A FR7222811 A FR 7222811A FR 2189630 B1 FR2189630 B1 FR 2189630B1
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
FR7222811A
Other languages
French (fr)
Other versions
FR2189630A1 (en
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.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
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 SNECMA SAS filed Critical SNECMA SAS
Priority to FR7222811A priority Critical patent/FR2189630B1/fr
Priority to GB2830873A priority patent/GB1427540A/en
Priority to DE2331723A priority patent/DE2331723A1/en
Priority to US372514A priority patent/US3869865A/en
Publication of FR2189630A1 publication Critical patent/FR2189630A1/fr
Application granted granted Critical
Publication of FR2189630B1 publication Critical patent/FR2189630B1/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
FR7222811A 1972-06-23 1972-06-23 Expired FR2189630B1 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR7222811A FR2189630B1 (en) 1972-06-23 1972-06-23
GB2830873A GB1427540A (en) 1972-06-23 1973-06-14 Devices for prevapourising liquid fuel
DE2331723A DE2331723A1 (en) 1972-06-23 1973-06-22 DEVICE FOR PRE-EVAPORATION OF LIQUID FUEL
US372514A US3869865A (en) 1972-06-23 1973-06-22 Devices for prevaporising liquid fuel

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7222811A FR2189630B1 (en) 1972-06-23 1972-06-23

Publications (2)

Publication Number Publication Date
FR2189630A1 FR2189630A1 (en) 1974-01-25
FR2189630B1 true FR2189630B1 (en) 1980-03-14

Family

ID=9100723

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7222811A Expired FR2189630B1 (en) 1972-06-23 1972-06-23

Country Status (4)

Country Link
US (1) US3869865A (en)
DE (1) DE2331723A1 (en)
FR (1) FR2189630B1 (en)
GB (1) GB1427540A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6220034B1 (en) 1993-07-07 2001-04-24 R. Jan Mowill Convectively cooled, single stage, fully premixed controllable fuel/air combustor

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RO66212A2 (en) * 1975-03-19 1978-04-15 Inst Pentru Creatie Stintific COMBUSTION PROCESS AND BURNERS FOR LIQUID FUEL
DE2524319C2 (en) * 1975-06-02 1984-03-08 Société Nationale d'Etude et de Construction de Moteurs d'Aviation, 75015 Paris Combustion chamber with a stepped flame tube
US4070826A (en) * 1975-12-24 1978-01-31 General Electric Company Low pressure fuel injection system
US4735044A (en) * 1980-11-25 1988-04-05 General Electric Company Dual fuel path stem for a gas turbine engine
US4838029A (en) * 1986-09-10 1989-06-13 The United States Of America As Represented By The Secretary Of The Air Force Externally vaporizing system for turbine combustor
GB2215029B (en) * 1988-02-06 1991-10-09 Rolls Royce Plc Gas turbine engine fuel burner
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
US5613357A (en) * 1993-07-07 1997-03-25 Mowill; R. Jan Star-shaped single stage low emission combustor system
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
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
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
CN105716120B (en) * 2016-02-22 2018-02-16 中国科学院工程热物理研究所 A kind of fuel oil cooled evaporates tubular construction
FR3101696B1 (en) * 2019-10-08 2021-10-29 Safran Helicopter Engines PREVAPORIZATION ROD FOR A TURBOMACHINE COMBUSTION CHAMBER

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1995934A (en) * 1933-09-18 1935-03-26 Trust Company Gas burner
US2780061A (en) * 1953-05-08 1957-02-05 Lucas Industries Ltd Liquid fuel burner for a combustion chamber provided with a surrounding air jacket
US2926495A (en) * 1955-12-29 1960-03-01 Gen Electric Fuel injection nozzle
FR1525092A (en) * 1967-01-23 1968-05-17 Snecma Hot gas flow and cold air flow turbo-reactor
FR1590542A (en) * 1968-11-04 1970-04-13

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6220034B1 (en) 1993-07-07 2001-04-24 R. Jan Mowill Convectively cooled, single stage, fully premixed controllable fuel/air combustor

Also Published As

Publication number Publication date
FR2189630A1 (en) 1974-01-25
DE2331723A1 (en) 1974-01-10
US3869865A (en) 1975-03-11
GB1427540A (en) 1976-03-10

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Legal Events

Date Code Title Description
ST Notification of lapse