DE1953671C3 - Vorrichtung zum Vorverdampfen von flüssigem Brennstoff in einer Brennkammer - Google Patents

Vorrichtung zum Vorverdampfen von flüssigem Brennstoff in einer Brennkammer

Info

Publication number
DE1953671C3
DE1953671C3 DE1953671A DE1953671A DE1953671C3 DE 1953671 C3 DE1953671 C3 DE 1953671C3 DE 1953671 A DE1953671 A DE 1953671A DE 1953671 A DE1953671 A DE 1953671A DE 1953671 C3 DE1953671 C3 DE 1953671C3
Authority
DE
Germany
Prior art keywords
combustion chamber
pipe
arms
liquid fuel
inner channel
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
DE1953671A
Other languages
German (de)
English (en)
Other versions
DE1953671A1 (de
DE1953671B2 (de
Inventor
Jacques Emile Jules Dammarie- Les-Lys Caruel
Armand Jean-Baptiste Itteville Lacroix
Herve Alain Issy- Les-Moulineaux Quillevere
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
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
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 Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Publication of DE1953671A1 publication Critical patent/DE1953671A1/de
Publication of DE1953671B2 publication Critical patent/DE1953671B2/de
Application granted granted Critical
Publication of DE1953671C3 publication Critical patent/DE1953671C3/de
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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Spray-Type Burners (AREA)
  • Production Of Liquid Hydrocarbon Mixture For Refining Petroleum (AREA)
DE1953671A 1968-11-04 1969-10-24 Vorrichtung zum Vorverdampfen von flüssigem Brennstoff in einer Brennkammer Expired DE1953671C3 (de)

Applications Claiming Priority (1)

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

Publications (3)

Publication Number Publication Date
DE1953671A1 DE1953671A1 (de) 1970-05-06
DE1953671B2 DE1953671B2 (de) 1979-03-01
DE1953671C3 true DE1953671C3 (de) 1979-10-18

Family

ID=8656455

Family Applications (1)

Application Number Title Priority Date Filing Date
DE1953671A Expired DE1953671C3 (de) 1968-11-04 1969-10-24 Vorrichtung zum Vorverdampfen von flüssigem Brennstoff in einer Brennkammer

Country Status (4)

Country Link
US (1) US3626444A (US20080094685A1-20080424-C00004.png)
DE (1) DE1953671C3 (US20080094685A1-20080424-C00004.png)
FR (1) FR1590542A (US20080094685A1-20080424-C00004.png)
GB (1) GB1280715A (US20080094685A1-20080424-C00004.png)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2131790B1 (US20080094685A1-20080424-C00004.png) * 1971-02-19 1974-09-27 Snecma
GB1392739A (en) * 1971-07-16 1975-04-30 Snecma Devices for pre-vaporising liquid fuel
FR2189630B1 (US20080094685A1-20080424-C00004.png) * 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 (de) * 1978-04-13 1983-11-03 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Ringbrennkammer mit Brennstoff-Vorverdampfung für Gasturbinentriebwerke
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
US5613357A (en) * 1993-07-07 1997-03-25 Mowill; R. Jan Star-shaped single stage low emission combustor system
US5377483A (en) * 1993-07-07 1995-01-03 Mowill; R. Jan Process for single stage premixed constant fuel/air ratio combustion
US6220034B1 (en) 1993-07-07 2001-04-24 R. Jan Mowill Convectively cooled, single stage, fully premixed controllable fuel/air combustor
US5638674A (en) * 1993-07-07 1997-06-17 Mowill; R. Jan Convectively cooled, single stage, fully premixed controllable fuel/air combustor with tangential admission
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
FR2730555B1 (fr) * 1995-02-15 1997-03-14 Snecma Ensemble d'injection de carburant pour chambre de combustion de turbines a gaz
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 (fr) * 2017-05-02 2020-03-06 Safran Helicopter Engines Canne de prevaporisation pour une turbomachine
FR3101696B1 (fr) * 2019-10-08 2021-10-29 Safran Helicopter Engines Canne de prevaporisation pour une chambre de combustion de turbomachine

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

Also Published As

Publication number Publication date
US3626444A (en) 1971-12-07
GB1280715A (en) 1972-07-05
DE1953671A1 (de) 1970-05-06
FR1590542A (US20080094685A1-20080424-C00004.png) 1970-04-13
DE1953671B2 (de) 1979-03-01

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Legal Events

Date Code Title Description
C3 Grant after two publication steps (3rd publication)
8339 Ceased/non-payment of the annual fee