MX2007013349A - Montaje de motor de turboventilador y metodo para ensamblar el mismo. - Google Patents

Montaje de motor de turboventilador y metodo para ensamblar el mismo.

Info

Publication number
MX2007013349A
MX2007013349A MX2007013349A MX2007013349A MX2007013349A MX 2007013349 A MX2007013349 A MX 2007013349A MX 2007013349 A MX2007013349 A MX 2007013349A MX 2007013349 A MX2007013349 A MX 2007013349A MX 2007013349 A MX2007013349 A MX 2007013349A
Authority
MX
Mexico
Prior art keywords
pressure turbine
turbofan engine
engine assembly
counter
assembly
Prior art date
Application number
MX2007013349A
Other languages
English (en)
Inventor
Robert Joseph Orlando
Thomas Ory Moniz
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of MX2007013349A publication Critical patent/MX2007013349A/es

Links

Classifications

    • 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
    • F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
    • F01D1/24—Non-positive-displacement machines or engines, e.g. steam turbines characterised by counter-rotating rotors subjected to same working fluid stream without intermediate stator blades or the like
    • 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
    • F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
    • F01D1/24—Non-positive-displacement machines or engines, e.g. steam turbines characterised by counter-rotating rotors subjected to same working fluid stream without intermediate stator blades or the like
    • F01D1/26—Non-positive-displacement machines or engines, e.g. steam turbines characterised by counter-rotating rotors subjected to same working fluid stream without intermediate stator blades or the like traversed by the working-fluid substantially axially
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/06—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages
    • F02C3/067—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages having counter-rotating rotors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants 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
    • F02K3/04—Plants 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
    • F02K3/072—Plants 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 with counter-rotating, e.g. fan rotors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/40—Transmission of power
    • F05D2260/403—Transmission of power through the shape of the drive components
    • F05D2260/4031—Transmission of power through the shape of the drive components as in toothed gearing
    • F05D2260/40311—Transmission of power through the shape of the drive components as in toothed gearing of the epicyclical, planetary or differential type

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Retarders (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

Se proporciona un montaje (20) de motor de turbina. Un montaje (20) de motor de turbina incluye un motor (12) de turbina de núcleo de gas que incluye un compresor (18) de alta presión, un combustor (20) y una turbina (22) de alta presión. El montaje (20) de motor de turbina también incluye un compresor (30) de arranque acoplado corriente arriba desde el motor de turbina de núcleo de gas. El montaje (20) de motor de turbina también incluye una turbia (32) de presión intermedia acoplado con el compresor de arranque, la turbina de presión intermedia está dispuesta corriente abajo desde el motor de turbina de núcleo de gas. Un montaje (20) de motor de turbina también incluye un montaje (16) de ventilador contra-giratorio dispuesto corriente arriba desde el compresor de arranque, el montaje de ventilador contra-giratorio incluye un primer montaje (50) de ventilador configurado para girar en una primera dirección y un segundo montaje (52) de ventilador configurado para girar en una segunda dirección, opuesta. El montaje (20) de motor de turbina también incluye una turbina (14) de baja presión dispuesto corriente abajo desde la turbina de presión intermedia, la turbina de baja presión se configura para accionar el montaje de ventilador contra-giratorio.
MX2007013349A 2006-10-31 2007-10-25 Montaje de motor de turboventilador y metodo para ensamblar el mismo. MX2007013349A (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US11/555,045 US7921634B2 (en) 2006-10-31 2006-10-31 Turbofan engine assembly and method of assembling same

Publications (1)

Publication Number Publication Date
MX2007013349A true MX2007013349A (es) 2009-02-19

Family

ID=39154387

Family Applications (1)

Application Number Title Priority Date Filing Date
MX2007013349A MX2007013349A (es) 2006-10-31 2007-10-25 Montaje de motor de turboventilador y metodo para ensamblar el mismo.

Country Status (5)

Country Link
US (1) US7921634B2 (es)
EP (1) EP1921253B1 (es)
JP (1) JP5662629B2 (es)
CA (1) CA2607042A1 (es)
MX (1) MX2007013349A (es)

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Also Published As

Publication number Publication date
EP1921253A3 (en) 2014-01-22
CA2607042A1 (en) 2008-04-30
EP1921253B1 (en) 2015-02-25
JP2008115858A (ja) 2008-05-22
US7921634B2 (en) 2011-04-12
EP1921253A2 (en) 2008-05-14
JP5662629B2 (ja) 2015-02-04
US20080098717A1 (en) 2008-05-01

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