CH258672A - Gasturbinentriebwerk. - Google Patents

Gasturbinentriebwerk.

Info

Publication number
CH258672A
CH258672A CH258672DA CH258672A CH 258672 A CH258672 A CH 258672A CH 258672D A CH258672D A CH 258672DA CH 258672 A CH258672 A CH 258672A
Authority
CH
Switzerland
Prior art keywords
gas turbine
turbine engine
engine
gas
turbine
Prior art date
Application number
Other languages
English (en)
Inventor
Power Jets Research De Limited
Original Assignee
Power Jets Res & Dev 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 GB4968/44A external-priority patent/GB594285A/en
Application filed by Power Jets Res & Dev Ltd filed Critical Power Jets Res & Dev Ltd
Publication of CH258672A publication Critical patent/CH258672A/de

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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/44—Combustion chambers comprising a single tubular flame tube within a tubular casing
    • 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
    • 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
    • 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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/46—Combustion chambers comprising an annular arrangement of several essentially tubular flame tubes within a common annular casing or within individual casings
    • 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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/46—Combustion chambers comprising an annular arrangement of several essentially tubular flame tubes within a common annular casing or within individual casings
    • F23R3/48—Flame tube interconnectors, e.g. cross-over tubes
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
CH258672D 1944-03-16 1945-11-30 Gasturbinentriebwerk. CH258672A (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB4968/44A GB594285A (en) 1944-03-16 Improvements relating to combustion apparatus

Publications (1)

Publication Number Publication Date
CH258672A true CH258672A (de) 1948-12-15

Family

ID=9787280

Family Applications (1)

Application Number Title Priority Date Filing Date
CH258672D CH258672A (de) 1944-03-16 1945-11-30 Gasturbinentriebwerk.

Country Status (4)

Country Link
US (1) US2475911A (de)
BE (1) BE461591A (de)
CH (1) CH258672A (de)
FR (1) FR918088A (de)

Families Citing this family (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2581999A (en) * 1946-02-01 1952-01-08 Gen Electric Hemispherical combustion chamber end dome having cooling air deflecting means
FR962862A (de) * 1946-10-26 1950-06-22
US2603064A (en) * 1946-12-12 1952-07-15 Chrysler Corp Combustion chamber with multiple conical sections providing multiple air paths for gas turbines
US2541171A (en) * 1947-01-25 1951-02-13 Kellogg M W Co Air inlet structure for combustion chambers
US2620625A (en) * 1947-05-16 1952-12-09 Edward A Phaneuf Jet engine having an air compressor driven solely by a fuel gas turbine
GB684670A (en) * 1947-10-21 1952-12-24 Power Jets Res & Dev Ltd Improvements in or relating to combustion apparatus
NL72524C (de) * 1947-11-03
US2659201A (en) * 1947-11-26 1953-11-17 Phillips Petroleum Co Gas turbine combustion chamber with provision for turbulent mixing of air and fuel
US2552492A (en) * 1948-06-07 1951-05-08 Power Jets Res & Dev Ltd Air ducting arrangement for combustion chambers
US2553091A (en) * 1948-09-11 1951-05-15 Harold R Horning Heater
US2627720A (en) * 1948-10-08 1953-02-10 Packard Motor Car Co Circumferentially arranged combustion chamber with arcuate walls defining an air flow path between chambers
US2646664A (en) * 1949-02-24 1953-07-28 A V Roe Canada Ltd Annular fuel vaporizer for gas turbine engines
US2628474A (en) * 1949-05-13 1953-02-17 Floyd T Hague Annular combustion liner having conical reentrant walls with fuel reversing elements
US2696076A (en) * 1949-11-28 1954-12-07 Ivan F Weeks Turbulence and combustion-promoting device for ram jet motors
US2718757A (en) * 1951-01-17 1955-09-27 Lummus Co Aircraft gas turbine and jet
US2729938A (en) * 1951-01-26 1956-01-10 Gen Motors Corp Combustion chamber crossover tube
US2692478A (en) * 1951-02-24 1954-10-26 Boeing Co Turbine burner incorporating removable burner liner
US2984979A (en) * 1951-03-27 1961-05-23 Eldon R Babcock Vortex pilot flame source for ramjet engines
US2765620A (en) * 1951-06-23 1956-10-09 Gen Motors Corp Flow deflector for combustion chamber apparatus
US2780916A (en) * 1952-08-22 1957-02-12 Continental Aviat & Engineerin Pilot burner for jet engines
US2823628A (en) * 1953-01-21 1958-02-18 Babcock & Wilcox Co Multi-fuel burner
US2979899A (en) * 1953-06-27 1961-04-18 Snecma Flame spreading device for combustion equipments
US6231334B1 (en) * 1998-11-24 2001-05-15 John Zink Company Biogas flaring unit
FR2808500B1 (fr) * 2000-05-04 2002-08-16 Philippe Michel Autorespirateur subaquatique a rechargement manuel integre
US6840048B2 (en) * 2002-09-26 2005-01-11 General Electric Company Dynamically uncoupled can combustor
GB2461542B (en) * 2008-07-03 2010-10-13 Rolls Royce Plc Combustion Arrangement with Dilution and Trim Ports
US20110271654A1 (en) * 2010-05-05 2011-11-10 General Electric Company Diffuser for gas turbine system
US9476355B2 (en) * 2012-02-29 2016-10-25 Siemens Energy, Inc. Mid-section of a can-annular gas turbine engine with a radial air flow discharged from the compressor section
US9546601B2 (en) * 2012-11-20 2017-01-17 General Electric Company Clocked combustor can array
US11940151B2 (en) * 2022-01-12 2024-03-26 General Electric Company Combustor with baffle

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US910665A (en) * 1908-05-16 1909-01-26 August W H Griepe Gas turbine-engine.
US990222A (en) * 1910-09-12 1911-04-25 Julius Brown Explosive gas-turbine engine.
US2164954A (en) * 1936-10-06 1939-07-04 Thomas J Stephens Combustion and gas mixing assembly for gas circulating systems
CH206286A (de) * 1937-11-18 1939-07-31 Messerschmitt Boelkow Blohm Brennkammer für Gasströmungsmaschinen, wie z. B. Gasturbinen, insbesondere zur Verwendung bei Luftfahrzeugen.
US2353929A (en) * 1940-01-29 1944-07-18 Allis Chalmers Mfg Co Combustion turbine

Also Published As

Publication number Publication date
US2475911A (en) 1949-07-12
FR918088A (fr) 1947-01-29
BE461591A (de)

Similar Documents

Publication Publication Date Title
CH258672A (de) Gasturbinentriebwerk.
CH265627A (de) Gasturbine.
CH265007A (de) Verbrennungseinrichtung für Gasturbinenanlagen.
CH271480A (de) Gasturbinen-Kraftanlage.
CH263473A (de) Luftfahrzeug-Verbrennungsturbinenkraftanlage.
CH257833A (de) Gasturbine.
CH262382A (de) Verbrennungsturbinenanlage.
CH264090A (de) Verbrennungsturbinen-Kraftanlage.
CH241750A (de) Brennraum für Gasturbinenanlage.
CH250477A (de) Verbrennungsturbinenaggregat.
CH253794A (de) Verbrennungskammer.
CH257003A (de) Verbrennungsturbinenanlage.
CH259565A (de) Verbrennungskammer für Verbrennungsturbinen.
CH270343A (de) Gasturbinentriebwerk.
DK67991C (da) Forbrændingsmotor.
ES174696A1 (es) Una instalación de turbina de gas regenerativa.
CH264091A (de) Verbrennungseinrichtung an Gasturbinen-Kraftanlagen.
FR917953A (fr) Moteur-turbine à explosion continue
CH239033A (de) Gasdrucklader.
FR994130A (fr) Turbine à combustion
CH239721A (de) Gaserzeugungsanlage.
CH241266A (de) Turbokompressorgruppe.
CH228273A (de) Turbomaschine.
FI22779A (fi) Kaasuturpini
CH264419A (de) Gasturbinenanlage.