BE462020A - - Google Patents

Info

Publication number
BE462020A
BE462020A BE462020DA BE462020A BE 462020 A BE462020 A BE 462020A BE 462020D A BE462020D A BE 462020DA BE 462020 A BE462020 A BE 462020A
Authority
BE
Belgium
Application number
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.)
Publication of BE462020A publication Critical patent/BE462020A/xx

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)
BE462020D 1942-02-02 BE462020A (ko)

Applications Claiming Priority (1)

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

Publications (1)

Publication Number Publication Date
BE462020A true BE462020A (ko)

Family

ID=10233221

Family Applications (1)

Application Number Title Priority Date Filing Date
BE462020D BE462020A (ko) 1942-02-02

Country Status (6)

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

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 (en) * 2013-03-13 2020-10-07 United Technologies Corporation Nosecone support
WO2014158283A1 (en) * 2013-03-14 2014-10-02 Bronwyn Power A subsonic shock strut
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
FR918158A (fr) 1947-01-31
CH257833A (de) 1948-10-31
NL62040C (ko)
GB582978A (en) 1946-12-04

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