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BR112015015516A2 - conjunto de mecanismo motor de turbina - Google Patents

conjunto de mecanismo motor de turbina

Info

Publication number
BR112015015516A2
BR112015015516A2 BR112015015516A BR112015015516A BR112015015516A2 BR 112015015516 A2 BR112015015516 A2 BR 112015015516A2 BR 112015015516 A BR112015015516 A BR 112015015516A BR 112015015516 A BR112015015516 A BR 112015015516A BR 112015015516 A2 BR112015015516 A2 BR 112015015516A2
Authority
BR
Brazil
Prior art keywords
passages
turbine engine
turbine
section
heat exchanger
Prior art date
Application number
BR112015015516A
Other languages
English (en)
Inventor
Delgado Adon
Dale Mathias Christopher
Ann Oakes Deborah
Jay Esptein Michael
Kupiszewski Thomas
James Buchholz Todd
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 BR112015015516A2 publication Critical patent/BR112015015516A2/pt

Links

Classifications

    • 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
    • F02C3/20—Gas-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
    • F02C3/22—Gas-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 the fuel or oxidant being gaseous at standard temperature and pressure
    • 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
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/12—Cooling of plants
    • F02C7/16—Cooling of plants characterised by cooling medium
    • 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
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/22—Fuel supply systems
    • F02C7/224—Heating fuel before feeding to the burner
    • 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
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/213—Heat transfer, e.g. cooling by the provision of a heat exchanger within the cooling circuit
    • 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
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/232—Heat transfer, e.g. cooling characterized by the cooling medium
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient 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)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)

Abstract

resumo “conjunto de mecanismo motor de turbina” trata-se de conjuntos de mecanismo motor de turbina que incluem um conjunto de mecanismo motor de turbina que tem um núcleo de turbina que compreende uma seção de compressor, uma seção de combustão, uma seção de turbina e uma seção de bocal, que são axialmente alinhadas, em que a seção de combustão compreende um estojo, em geral, anular que tem paredes interna e externa, um trocador de calor que compreende múltiplas passagens em proximidade a pelo menos uma das paredes interna e externa, com as passagens dispostas em torno de pelo menos uma porção do estojo e em comunicação fluida entre si de modo que o fluido possa fluir através das passagens e um sistema de combustível criogênico que tem um tanque de combustível criogênico com uma linha de suprimento acoplada a uma das passagens, em que o combustível criogênico pode ser suprido a partir do tanque de combustível criogênico, através da linha de suprimento, às passagens do trocador de calor, em que o combustível nas passagens pode ser aquecido pela seção de combustão. o trocador de calor pode ser um vaporizador único ou de múltiplos estágios.
BR112015015516A 2012-12-28 2013-11-26 conjunto de mecanismo motor de turbina BR112015015516A2 (pt)

Applications Claiming Priority (7)

Application Number Priority Date Filing Date Title
US201261746673P 2012-12-28 2012-12-28
US201261746855P 2012-12-28 2012-12-28
US201261746882P 2012-12-28 2012-12-28
US201261746847P 2012-12-28 2012-12-28
US201261746915P 2012-12-28 2012-12-28
US201261746872P 2012-12-28 2012-12-28
PCT/US2013/071775 WO2014105327A1 (en) 2012-12-28 2013-11-26 Turbine engine assembly comprising a cryogenic fuel system

Publications (1)

Publication Number Publication Date
BR112015015516A2 true BR112015015516A2 (pt) 2017-07-11

Family

ID=49766170

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112015015516A BR112015015516A2 (pt) 2012-12-28 2013-11-26 conjunto de mecanismo motor de turbina

Country Status (7)

Country Link
US (1) US20150337730A1 (pt)
EP (1) EP2938851A1 (pt)
JP (1) JP2016504523A (pt)
CN (1) CN105026726A (pt)
BR (1) BR112015015516A2 (pt)
CA (1) CA2896463A1 (pt)
WO (1) WO2014105327A1 (pt)

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US11220895B1 (en) 2020-06-24 2022-01-11 Bj Energy Solutions, Llc Automated diagnostics of electronic instrumentation in a system for fracturing a well and associated methods
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Also Published As

Publication number Publication date
CA2896463A1 (en) 2014-07-03
WO2014105327A1 (en) 2014-07-03
JP2016504523A (ja) 2016-02-12
CN105026726A (zh) 2015-11-04
US20150337730A1 (en) 2015-11-26
EP2938851A1 (en) 2015-11-04

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Legal Events

Date Code Title Description
B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]

Free format text: REFERENTE A 5A ANUIDADE.

B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]

Free format text: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2494 DE 23-10-2018 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDO O ARQUIVAMENTO DO PEDIDO DE PATENTE, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.