BE525244A - - Google Patents

Info

Publication number
BE525244A
BE525244A BE525244DA BE525244A BE 525244 A BE525244 A BE 525244A BE 525244D A BE525244D A BE 525244DA BE 525244 A BE525244 A BE 525244A
Authority
BE
Belgium
Prior art keywords
cooling fluid
turbine
established
stream
installation
Prior art date
Application number
Other languages
English (en)
French (fr)
Publication of BE525244A publication Critical patent/BE525244A/fr

Links

Classifications

    • 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
    • F02K1/06Varying effective area of jet pipe or nozzle
    • F02K1/08Varying effective area of jet pipe or nozzle by axially moving or transversely deforming an internal member, e.g. the exhaust cone
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/20Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
    • F02C3/30Adding water, steam or other fluids for influencing combustion, e.g. to obtain cleaner exhaust gases
    • F02C3/305Increasing the power, speed, torque or efficiency of a gas turbine or the thrust of a turbojet engine by injecting or adding water, steam or other fluids
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K3/00Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/20Heat transfer, e.g. cooling
    • F05D2260/212Heat transfer, e.g. cooling by water injection
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
BE525244D BE525244A (it)

Publications (1)

Publication Number Publication Date
BE525244A true BE525244A (it)

Family

ID=159598

Family Applications (1)

Application Number Title Priority Date Filing Date
BE525244D BE525244A (it)

Country Status (1)

Country Link
BE (1) BE525244A (it)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2669680A1 (fr) * 1986-06-21 1992-05-29 British Aerospace Prefectionnements apportes a des moteurs a turbine a gaz ou les concernants.
WO1997043530A1 (en) * 1996-05-14 1997-11-20 The Dow Chemical Company Process and apparatus for achieving power augmentation in gas turbines via wet compression
EP1344928A2 (en) 2002-03-12 2003-09-17 ROLLS-ROYCE plc Variable area nozzle
WO2007093760A1 (en) * 2006-02-18 2007-08-23 Rolls-Royce Plc A gas turbine engine
EP3263849A1 (fr) * 2016-06-28 2018-01-03 Safran Aero Boosters SA Aéronef comprenant un système de propulsion

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2669680A1 (fr) * 1986-06-21 1992-05-29 British Aerospace Prefectionnements apportes a des moteurs a turbine a gaz ou les concernants.
WO1997043530A1 (en) * 1996-05-14 1997-11-20 The Dow Chemical Company Process and apparatus for achieving power augmentation in gas turbines via wet compression
EP1108870A3 (en) * 1996-05-14 2003-12-17 The Dow Chemical Company Process and apparatus for achieving power augmentation in gas turbines via wet compression
EP1344928A2 (en) 2002-03-12 2003-09-17 ROLLS-ROYCE plc Variable area nozzle
EP1344928A3 (en) * 2002-03-12 2005-03-23 ROLLS-ROYCE plc Variable area nozzle
WO2007093760A1 (en) * 2006-02-18 2007-08-23 Rolls-Royce Plc A gas turbine engine
US8453458B2 (en) 2006-02-18 2013-06-04 Rolls-Royce Plc Gas turbine engine variable exhaust nozzle
EP3263849A1 (fr) * 2016-06-28 2018-01-03 Safran Aero Boosters SA Aéronef comprenant un système de propulsion
BE1024315B1 (fr) * 2016-06-28 2018-01-30 Safran Aero Boosters Sa Système de propulsion pour aéronef

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