FR918158A - Perfectionnements apportés aux turbines à gaz - Google Patents

Perfectionnements apportés aux turbines à gaz

Info

Publication number
FR918158A
FR918158A FR918158DA FR918158A FR 918158 A FR918158 A FR 918158A FR 918158D A FR918158D A FR 918158DA FR 918158 A FR918158 A FR 918158A
Authority
FR
France
Prior art keywords
gas turbines
turbines
gas
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
Application filed by Power Jets Research and Development Ltd filed Critical Power Jets Research and Development Ltd
Application granted granted Critical
Publication of FR918158A publication Critical patent/FR918158A/fr
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/30Exhaust heads, chambers, or the like
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/04Mounting 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)
  • Control Of Turbines (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR918158D 1942-02-02 1945-11-30 Perfectionnements apportés aux turbines à gaz Expired FR918158A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB257833X 1942-02-02

Publications (1)

Publication Number Publication Date
FR918158A true FR918158A (fr) 1947-01-31

Family

ID=10233221

Family Applications (1)

Application Number Title Priority Date Filing Date
FR918158D Expired FR918158A (fr) 1942-02-02 1945-11-30 Perfectionnements apportés aux turbines à gaz

Country Status (6)

Country Link
US (1) US2516819A (fr)
BE (1) BE462020A (fr)
CH (1) CH257833A (fr)
FR (1) FR918158A (fr)
GB (1) GB582978A (fr)
NL (1) NL62040C (fr)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2828603A (en) * 1948-04-09 1958-04-01 Westinghouse Electric Corp Afterburner for turbo jet engines and the like
US2714287A (en) * 1950-01-03 1955-08-02 Westinghouse Electric Corp Flameholder device for turbojet afterburner
GB685939A (en) * 1950-05-17 1953-01-14 Rolls Royce Improvements in or relating to gas-turbine engine structures
US2813396A (en) * 1952-02-20 1957-11-19 Solar Aircraft Co Tail cone and resilient mounting therefor
GB761444A (en) * 1953-06-26 1956-11-14 Glover Webb Liversidge Ltd Improvements in or relating to tipping vehicles
US2938336A (en) * 1956-12-06 1960-05-31 United Aircraft Corp Gas flow straightening vanes
US2919888A (en) * 1957-04-17 1960-01-05 United Aircraft Corp Turbine bearing support
US3024969A (en) * 1957-12-26 1962-03-13 Gen Electric Compressor rear frame
CA623385A (en) * 1959-03-13 1961-07-04 R. Reese Homer Elastic fluid branch conduit structure
US3778185A (en) * 1972-08-28 1973-12-11 United Aircraft Corp Composite strut joint construction
FR2534222A1 (fr) * 1982-10-06 1984-04-13 Aerospatiale Agencement de rotor de queue a poussee accrue pour aeronef a voilure tournante et dispositif pour accroitre la poussee d'un tel agencement
US4989406A (en) * 1988-12-29 1991-02-05 General Electric Company Turbine engine assembly with aft mounted outlet guide vanes
DE4329623A1 (de) * 1993-09-02 1995-03-09 Abb Management Ag Abgasdiffusor
DE19729433C1 (de) * 1997-07-09 1998-08-13 Siemens Ag Stützvorrichtung für einen temperaturbeaufschlagten Kanal
US6584766B1 (en) * 2000-03-24 2003-07-01 General Electric Co. Methods and apparatus for minimizing thermal stresses in a centerbody
US6807803B2 (en) * 2002-12-06 2004-10-26 General Electric Company Gas turbine exhaust diffuser
FR2988434B1 (fr) * 2012-03-20 2016-02-05 Aircelle Sa Cone d'ejection des gaz pour turboreacteurs d'aeronefs
EP2971613B1 (fr) * 2013-03-13 2020-10-07 United Technologies Corporation Support de cône d'entrée
EP2971614B1 (fr) * 2013-03-14 2020-10-14 Rolls-Royce Corporation Amortisseur subsonique
US9644497B2 (en) * 2013-11-22 2017-05-09 Siemens Energy, Inc. Industrial gas turbine exhaust system with splined profile tail cone
DE102017130563A1 (de) * 2017-12-19 2019-06-19 Rolls-Royce Deutschland Ltd & Co Kg Schubdüse für ein Turbofan-Triebwerk eines Überschallflugzeugs

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE319776C (de) * 1920-04-03 Hannoversche Waggonfabrik Akt Bekleidung fuer zwei oder mehr Flugzeugverspannungsorgane
FR15364E (fr) * 1911-07-03 1912-06-25 Societe R Bourbeau Et H Devaux Aéroplane à coque directrice
US1065118A (en) * 1912-05-23 1913-06-17 Albert B Doering Flame and spark arrester.
GB126707A (en) * 1917-02-21 1919-05-22 William John Dickinson An Improvement in the Means for Utilising the Kinitic Energy of Air Currents.
US2207522A (en) * 1938-03-24 1940-07-09 Bell Telephone Labor Inc Concentric conductor transmission line
US2393808A (en) * 1943-12-29 1946-01-29 Westinghouse Electric Corp Blower apparatus

Also Published As

Publication number Publication date
US2516819A (en) 1950-07-25
GB582978A (en) 1946-12-04
NL62040C (fr)
BE462020A (fr)
CH257833A (de) 1948-10-31

Similar Documents

Publication Publication Date Title
FR944726A (fr) Perfectionnements aux turbines à gaz
FR944314A (fr) Perfectionnements aux turbines à gaz ou aux propulseurs à gaz à réaction
FR918158A (fr) Perfectionnements apportés aux turbines à gaz
FR895652A (fr) Installation de turbines à gaz
FR981975A (fr) Perfectionnement aux turbines à gaz
FR897716A (fr) Turbine à gaz refroidie
FR879755A (fr) Rotor de turbine à gaz
FR897710A (fr) Rotor refroidi de turbine à gaz
FR885677A (fr) Briquet à gaz
FR907145A (fr) Turbine à gaz
FR975597A (fr) Perfectionnements aux brûleurs à gaz
FR887975A (fr) Turbine à gaz
FR52343E (fr) Turbine à gaz
FR976989A (fr) Perfectionnements aux pompes à gaz
FR950005A (fr) Turbine à gaz
FR943198A (fr) Perfectionnements aux turbo-moteurs à gaz à régénération
FR885311A (fr) Perfectionnements aux moteurs thermiques à turbine à gaz
FR938717A (fr) Perfectionnements aux turbines à gaz
FR55571E (fr) Perfectionnements aux installations comportant des turbinet à gaz
FR977144A (fr) Perfectionnements aux installations comportant des turbines à gaz
FR931583A (fr) Perfectionnement apporté aux turbines à vapeur ou à gaz
FR943188A (fr) Perfectionnements aux turbines
FR891410A (fr) Installation de turbine à gaz
FR896738A (fr) Brûleur à gaz
FR887847A (fr) Perfectionnements aux mélangeurs de gaz