FR919127A - Perfectionnements apportés aux appareils à combustion - Google Patents

Perfectionnements apportés aux appareils à combustion

Info

Publication number
FR919127A
FR919127A FR919127DA FR919127A FR 919127 A FR919127 A FR 919127A FR 919127D A FR919127D A FR 919127DA FR 919127 A FR919127 A FR 919127A
Authority
FR
France
Prior art keywords
combustion appliances
appliances
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
Other languages
English (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.)
Power Jets Research and Development Ltd
Original Assignee
Power Jets Research and Development 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
Priority claimed from GB4967/44A external-priority patent/GB595831A/en
Application filed by Power Jets Research and Development Ltd filed Critical Power Jets Research and Development Ltd
Application granted granted Critical
Publication of FR919127A publication Critical patent/FR919127A/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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • F23R3/10—Air inlet arrangements for primary air
    • F23R3/12—Air inlet arrangements for primary air inducing a vortex
    • F23R3/14—Air inlet arrangements for primary air inducing a vortex by using swirl vanes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
    • F02K3/105—Heating the by-pass flow
    • F02K3/11—Heating the by-pass flow by means of burners or combustion chambers
    • 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
    • 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
    • F23R3/045—Air inlet arrangements using pipes
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
FR919127D 1944-03-16 1945-12-18 Perfectionnements apportés aux appareils à combustion Expired FR919127A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB4967/44A GB595831A (en) 1944-03-16 Improvements relating to combustion apparatus

Publications (1)

Publication Number Publication Date
FR919127A true FR919127A (fr) 1947-02-27

Family

ID=9787260

Family Applications (1)

Application Number Title Priority Date Filing Date
FR919127D Expired FR919127A (fr) 1944-03-16 1945-12-18 Perfectionnements apportés aux appareils à combustion

Country Status (5)

Country Link
US (1) US2637974A (fr)
BE (1) BE462134A (fr)
CH (1) CH260402A (fr)
FR (1) FR919127A (fr)
NL (1) NL78931C (fr)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2635420A (en) * 1947-05-14 1953-04-21 Shell Dev Jet propulsion engine with auxiliary pulse jet engine
US2673445A (en) * 1949-06-21 1954-03-30 Bruno W Bruckmann Turbojet and rocket motor combination with hot gas ignition system for nonself-reaction rocket fuels
DE914570C (de) * 1952-04-20 1954-07-05 E H Dr Phil H C Ernst Heinkel Mehrkreis-Strahltriebwerk
DE945967C (de) * 1951-06-20 1956-07-19 Snecma Zweikreis-Turbinenstrahltriebwerk
DE955558C (de) * 1952-04-20 1957-01-03 Max Adolf Mueller Dipl Ing Strahltriebwerk
DE1095050B (de) * 1957-02-05 1960-12-15 Joseph Szydlowski Brennkammer, auch Nachbrennkammer fuer Strahltriebwerke, z.B. Turbo-Strahltriebwerke

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2782597A (en) * 1952-03-15 1957-02-26 Gen Electric Combustion chamber having improved air inlet means
US2930192A (en) * 1953-12-07 1960-03-29 Gen Electric Reverse vortex combustion chamber
US3099134A (en) * 1959-12-24 1963-07-30 Havilland Engine Co Ltd Combustion chambers
US3338051A (en) * 1965-05-28 1967-08-29 United Aircraft Corp High velocity ram induction burner
US5636510A (en) * 1994-05-25 1997-06-10 Westinghouse Electric Corporation Gas turbine topping combustor
US6442930B1 (en) * 2000-03-31 2002-09-03 General Electric Company Combined cycle pulse detonation turbine engine
FR2930291B1 (fr) * 2008-04-21 2010-06-04 Mbda France Moteur a detonations pulsees.

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2405723A (en) * 1946-08-13 Propulsion apparatus
US2432359A (en) * 1947-12-09 Internal-combustion turbine power
US2445114A (en) * 1948-07-13 Arrangement of jet propulsion
USRE23149E (en) * 1949-09-20 Combustion burner
US938182A (en) * 1908-08-11 1909-10-26 Fred T Todd Gas-burner.
US2000733A (en) * 1933-04-13 1935-05-07 Edgar T Avery Burner installation for domestic boilers
US2222031A (en) * 1939-06-01 1940-11-19 Malleable Iron Fittings Co Oil burner
BE460697A (fr) * 1939-12-09
US2404334A (en) * 1939-12-09 1946-07-16 Power Jets Res & Dev Ltd Aircraft propulsion system and power unit
US2398654A (en) * 1940-01-24 1946-04-16 Anglo Saxon Petroleum Co Combustion burner
US2405919A (en) * 1940-03-02 1946-08-13 Power Jets Res & Dev Ltd Fluid flow energy transformer
US2402377A (en) * 1943-02-09 1946-06-18 Westinghouse Electric Corp Turbine apparatus
US2595999A (en) * 1943-11-23 1952-05-06 Westinghouse Electric Corp Power plant combustion apparatus having apertured combustion chamber walls

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2635420A (en) * 1947-05-14 1953-04-21 Shell Dev Jet propulsion engine with auxiliary pulse jet engine
US2673445A (en) * 1949-06-21 1954-03-30 Bruno W Bruckmann Turbojet and rocket motor combination with hot gas ignition system for nonself-reaction rocket fuels
DE945967C (de) * 1951-06-20 1956-07-19 Snecma Zweikreis-Turbinenstrahltriebwerk
DE914570C (de) * 1952-04-20 1954-07-05 E H Dr Phil H C Ernst Heinkel Mehrkreis-Strahltriebwerk
DE955558C (de) * 1952-04-20 1957-01-03 Max Adolf Mueller Dipl Ing Strahltriebwerk
DE1095050B (de) * 1957-02-05 1960-12-15 Joseph Szydlowski Brennkammer, auch Nachbrennkammer fuer Strahltriebwerke, z.B. Turbo-Strahltriebwerke

Also Published As

Publication number Publication date
CH260402A (de) 1949-03-15
NL78931C (fr)
BE462134A (fr)
US2637974A (en) 1953-05-12

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