CH327080A - Dispositif propulseur à turbine à gaz - Google Patents

Dispositif propulseur à turbine à gaz

Info

Publication number
CH327080A
CH327080A CH327080DA CH327080A CH 327080 A CH327080 A CH 327080A CH 327080D A CH327080D A CH 327080DA CH 327080 A CH327080 A CH 327080A
Authority
CH
Switzerland
Prior art keywords
gas turbine
propellant device
turbine propellant
gas
turbine
Prior art date
Application number
Other languages
English (en)
Inventor
Thompson Purvis Joseph
Original Assignee
Canadian Patents Dev
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 Canadian Patents Dev filed Critical Canadian Patents Dev
Publication of CH327080A publication Critical patent/CH327080A/fr

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/78—Other construction of jet pipes
    • F02K1/82—Jet pipe walls, e.g. liners
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/30—Exhaust heads, chambers, or the like
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/04—Mounting of an exhaust cone in the jet pipe

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
CH327080D 1951-09-27 1954-05-26 Dispositif propulseur à turbine à gaz CH327080A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US248535A US2710523A (en) 1951-09-27 1951-09-27 Gas turbine tail cone

Publications (1)

Publication Number Publication Date
CH327080A true CH327080A (fr) 1958-01-15

Family

ID=22939560

Family Applications (1)

Application Number Title Priority Date Filing Date
CH327080D CH327080A (fr) 1951-09-27 1954-05-26 Dispositif propulseur à turbine à gaz

Country Status (3)

Country Link
US (1) US2710523A (fr)
CH (1) CH327080A (fr)
GB (1) GB712080A (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0073689A1 (fr) * 1981-08-31 1983-03-09 Elliott Turbomachinery Company, Inc. Méthode et dispositif pour contrôler les dilatations thermiques

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2917276A (en) * 1955-02-28 1959-12-15 Orenda Engines Ltd Segmented stator ring assembly
US3058205A (en) * 1955-02-28 1962-10-16 Lodge & Shipley Co Lightweight plurality of generally conical, hollow, metallic objects
US2851214A (en) * 1955-10-12 1958-09-09 Stork Koninklijke Maschf Axial flow fans or axial flow pumps
DE1008533B (de) * 1955-12-21 1957-05-16 Daimler Benz Ag Diffusoranordnung an Turbinen
US3021669A (en) * 1957-03-04 1962-02-20 Ralph A Nye Sectional formed combustion power chamber for varying driving impulses for jet motors
US3321179A (en) * 1965-09-13 1967-05-23 Caterpillar Tractor Co Gas turbine engines
US3797236A (en) * 1971-06-11 1974-03-19 Rolls Royce Annular combustion chamber with ceramic annular ring
CH643050A5 (de) * 1979-10-01 1984-05-15 Proizv Ob Nevsky Z Im V I Gasturbinentriebwerk mit ringbrennkammer.
US4369016A (en) * 1979-12-21 1983-01-18 United Technologies Corporation Turbine intermediate case
US4348957A (en) * 1980-07-28 1982-09-14 The United States Of America As Represented By The Secretary Of The Army Boattail emergence by ejecting nozzle exit cone
DE3407945A1 (de) * 1984-03-03 1985-09-05 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Verfahren und mittel zur vermeidung der entstehung von titanfeuer
DE3407946A1 (de) * 1984-03-03 1985-09-05 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Einrichtung zur verhinderung der ausbreitung von titanfeuer bei turbomaschinen, insbesondere gasturbinen- bzw. gasturbinenstrahltriebwerken
US6062814A (en) * 1995-10-31 2000-05-16 Siemens Aktiengesellschaft Transition element between components of a flue-gas duct of a gas turbine
US5605438A (en) * 1995-12-29 1997-02-25 General Electric Co. Casing distortion control for rotating machinery
US5669812A (en) * 1996-02-21 1997-09-23 Braden Manufacturing Exhaust gas diffuser interface
US6896483B2 (en) * 2001-07-02 2005-05-24 Allison Advanced Development Company Blade track assembly
US8875520B2 (en) * 2008-12-31 2014-11-04 Rolls-Royce North American Technologies, Inc. Gas turbine engine device
US20110088379A1 (en) * 2009-10-15 2011-04-21 General Electric Company Exhaust gas diffuser
CN103147805B (zh) * 2013-03-01 2014-11-26 哈尔滨汽轮机厂有限责任公司 一种轴向排汽汽轮机组的排汽缸
US9644497B2 (en) * 2013-11-22 2017-05-09 Siemens Energy, Inc. Industrial gas turbine exhaust system with splined profile tail cone
US9695713B2 (en) * 2014-09-15 2017-07-04 Siemens Energy, Inc. Damping design to reduce vibratory response in the turbine exhaust manifold centerbody
US10337353B2 (en) * 2014-12-31 2019-07-02 General Electric Company Casing ring assembly with flowpath conduction cut
RU2724378C2 (ru) * 2015-04-24 2020-06-23 Нуово Пиньоне Текнолоджи Срл Газотурбинный двигатель, содержащий кожух с охлаждающими ребрами
US12071858B2 (en) * 2021-10-13 2024-08-27 General Electric Company Fire retardant engine casing apparatus
CN114151227B (zh) * 2021-10-20 2023-05-05 中国航发四川燃气涡轮研究院 一种用于二元矢量喷管的隔热屏结构

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2442019A (en) * 1943-06-11 1948-05-25 Allis Chalmers Mfg Co Turbine construction
US2427244A (en) * 1944-03-07 1947-09-09 Gen Electric Gas turbine
GB584820A (en) * 1944-12-22 1947-01-23 Lucas Ltd Joseph Improvements relating to internal combustion prime movers
BE463344A (fr) * 1945-01-23
US2620157A (en) * 1947-05-06 1952-12-02 Rolls Royce Gas-turbine engine
FR965713A (fr) * 1947-05-07 1950-09-20
US2625793A (en) * 1949-05-19 1953-01-20 Westinghouse Electric Corp Gas turbine apparatus with air-cooling means

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0073689A1 (fr) * 1981-08-31 1983-03-09 Elliott Turbomachinery Company, Inc. Méthode et dispositif pour contrôler les dilatations thermiques

Also Published As

Publication number Publication date
GB712080A (en) 1954-07-14
US2710523A (en) 1955-06-14

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