BR112015027221A2 - câmara de admissão de ar e sistema de motor de turbina a gás - Google Patents

câmara de admissão de ar e sistema de motor de turbina a gás

Info

Publication number
BR112015027221A2
BR112015027221A2 BR112015027221A BR112015027221A BR112015027221A2 BR 112015027221 A2 BR112015027221 A2 BR 112015027221A2 BR 112015027221 A BR112015027221 A BR 112015027221A BR 112015027221 A BR112015027221 A BR 112015027221A BR 112015027221 A2 BR112015027221 A2 BR 112015027221A2
Authority
BR
Brazil
Prior art keywords
turbine engine
gas turbine
intake chamber
air intake
engine system
Prior art date
Application number
BR112015027221A
Other languages
English (en)
Other versions
BR112015027221B1 (pt
BR112015027221B8 (pt
Inventor
Pecchioli Mario
Morriello Pierenzo
Merlo Roberto
Original Assignee
Nuovo Pignone Srl
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 Nuovo Pignone Srl filed Critical Nuovo Pignone Srl
Publication of BR112015027221A2 publication Critical patent/BR112015027221A2/pt
Publication of BR112015027221B1 publication Critical patent/BR112015027221B1/pt
Publication of BR112015027221B8 publication Critical patent/BR112015027221B8/pt

Links

Classifications

    • 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
    • F02C7/00Features, 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
    • F02C7/04Air intakes for gas-turbine plants or jet-propulsion plants
    • 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
    • F01D25/28Supporting or mounting arrangements, e.g. for turbine casing
    • F01D25/285Temporary support structures, e.g. for testing, assembling, installing, repairing; Assembly methods using such structures
    • 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
    • F02C3/04Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • 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
    • F02C5/00Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
    • 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
    • F05D2220/00Application
    • F05D2220/30Application in turbines
    • F05D2220/32Application in turbines in gas turbines
    • 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
    • F05D2230/00Manufacture
    • F05D2230/70Disassembly methods
    • 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
    • F05D2230/00Manufacture
    • F05D2230/72Maintenance
    • 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
    • F05D2300/00Materials; Properties thereof
    • F05D2300/40Organic materials
    • F05D2300/43Synthetic polymers, e.g. plastics; Rubber
    • 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
    • F05D2300/00Materials; Properties thereof
    • F05D2300/60Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/603Composites; e.g. fibre-reinforced

Abstract

resumo “câmara de admissão de ar e sistema de motor de turbina a gás” é descrita uma câmara de admissão de ar para um motor de turbina a gás. a câmara de admissão de ar (3) compreende a corpo oco (17) que tem uma abertura de admissão de ar (19) e uma abertura de saída de ar (21) disposta e configurada para conexão com o motor de turbina a gás (6). a câmara de admissão de ar (3) compreende pelo menos uma porção removível (23l, 23r), que é removível a partir do corpo oco (17) quando a câmara de admissão de ar (3) é conectada a um motor de turbina a gás (6). a câmara de admissão de ar é, pelo menos parcialmente, produzida a partir de plástico reforçado com fibra.
BR112015027221A 2013-05-03 2014-04-30 Câmara de admissão de ar e sistema de motor de turbina a gás BR112015027221B8 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
ITFI2013A000100 2013-05-03
IT000100A ITFI20130100A1 (it) 2013-05-03 2013-05-03 "composite material inlet plenum and gas turbine engine system comprising said plenum"
PCT/EP2014/058916 WO2014177658A1 (en) 2013-05-03 2014-04-30 Composite material inlet plenum and gas turbine engine system comprising said plenum

Publications (3)

Publication Number Publication Date
BR112015027221A2 true BR112015027221A2 (pt) 2017-07-25
BR112015027221B1 BR112015027221B1 (pt) 2022-02-08
BR112015027221B8 BR112015027221B8 (pt) 2022-10-18

Family

ID=48793383

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112015027221A BR112015027221B8 (pt) 2013-05-03 2014-04-30 Câmara de admissão de ar e sistema de motor de turbina a gás

Country Status (11)

Country Link
US (1) US20160076447A1 (pt)
EP (1) EP2992186B1 (pt)
JP (1) JP6484221B2 (pt)
KR (1) KR102204720B1 (pt)
CN (1) CN105339602B (pt)
AU (1) AU2014261404B2 (pt)
BR (1) BR112015027221B8 (pt)
CA (1) CA2910055C (pt)
IT (1) ITFI20130100A1 (pt)
RU (1) RU2673029C2 (pt)
WO (1) WO2014177658A1 (pt)

Families Citing this family (31)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3052743B1 (fr) * 2016-06-20 2018-07-06 Airbus Operations Ensemble pour aeronef comprenant des moteurs a propulsion par ingestion de la couche limite
WO2018208513A1 (en) * 2017-05-11 2018-11-15 Dresser-Rand As Gas turbine inlet interface assembly
US11111029B2 (en) * 2017-07-28 2021-09-07 The Boeing Company System and method for operating a boundary layer ingestion fan
US10906657B2 (en) * 2018-06-19 2021-02-02 Raytheon Technologies Corporation Aircraft system with distributed propulsion
US10759545B2 (en) 2018-06-19 2020-09-01 Raytheon Technologies Corporation Hybrid electric aircraft system with distributed propulsion
US11002189B2 (en) 2019-09-13 2021-05-11 Bj Energy Solutions, Llc Mobile gas turbine inlet air conditioning system and associated methods
US10815764B1 (en) 2019-09-13 2020-10-27 Bj Energy Solutions, Llc Methods and systems for operating a fleet of pumps
CA3092865C (en) 2019-09-13 2023-07-04 Bj Energy Solutions, Llc Power sources and transmission networks for auxiliary equipment onboard hydraulic fracturing units and associated methods
CA3092829C (en) 2019-09-13 2023-08-15 Bj Energy Solutions, Llc Methods and systems for supplying fuel to gas turbine engines
US11015594B2 (en) 2019-09-13 2021-05-25 Bj Energy Solutions, Llc Systems and method for use of single mass flywheel alongside torsional vibration damper assembly for single acting reciprocating pump
US10895202B1 (en) 2019-09-13 2021-01-19 Bj Energy Solutions, Llc Direct drive unit removal system and associated methods
CA3197583A1 (en) 2019-09-13 2021-03-13 Bj Energy Solutions, Llc Fuel, communications, and power connection systems and related methods
US11708829B2 (en) 2020-05-12 2023-07-25 Bj Energy Solutions, Llc Cover for fluid systems and related methods
US10968837B1 (en) 2020-05-14 2021-04-06 Bj Energy Solutions, Llc Systems and methods utilizing turbine compressor discharge for hydrostatic manifold purge
US11428165B2 (en) 2020-05-15 2022-08-30 Bj Energy Solutions, Llc Onboard heater of auxiliary systems using exhaust gases and associated methods
US11208880B2 (en) 2020-05-28 2021-12-28 Bj Energy Solutions, Llc Bi-fuel reciprocating engine to power direct drive turbine fracturing pumps onboard auxiliary systems and related methods
US11109508B1 (en) 2020-06-05 2021-08-31 Bj Energy Solutions, Llc Enclosure assembly for enhanced cooling of direct drive unit and related methods
US11208953B1 (en) 2020-06-05 2021-12-28 Bj Energy Solutions, Llc Systems and methods to enhance intake air flow to a gas turbine engine of a hydraulic fracturing unit
US10954770B1 (en) 2020-06-09 2021-03-23 Bj Energy Solutions, Llc Systems and methods for exchanging fracturing components of a hydraulic fracturing unit
US11066915B1 (en) 2020-06-09 2021-07-20 Bj Energy Solutions, Llc Methods for detection and mitigation of well screen out
US11933153B2 (en) 2020-06-22 2024-03-19 Bj Energy Solutions, Llc Systems and methods to operate hydraulic fracturing units using automatic flow rate and/or pressure control
US11028677B1 (en) 2020-06-22 2021-06-08 Bj Energy Solutions, Llc Stage profiles for operations of hydraulic systems and associated methods
US11939853B2 (en) 2020-06-22 2024-03-26 Bj Energy Solutions, Llc Systems and methods providing a configurable staged rate increase function to operate hydraulic fracturing units
US11125066B1 (en) 2020-06-22 2021-09-21 Bj Energy Solutions, Llc Systems and methods to operate a dual-shaft gas turbine engine for hydraulic fracturing
US11466680B2 (en) 2020-06-23 2022-10-11 Bj Energy Solutions, Llc Systems and methods of utilization of a hydraulic fracturing unit profile to operate hydraulic fracturing units
US11473413B2 (en) 2020-06-23 2022-10-18 Bj Energy Solutions, Llc Systems and methods to autonomously operate hydraulic fracturing units
US11149533B1 (en) 2020-06-24 2021-10-19 Bj Energy Solutions, Llc Systems to monitor, detect, and/or intervene relative to cavitation and pulsation events during a hydraulic fracturing operation
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
US11193360B1 (en) 2020-07-17 2021-12-07 Bj Energy Solutions, Llc Methods, systems, and devices to enhance fracturing fluid delivery to subsurface formations during high-pressure fracturing operations
CN216406972U (zh) * 2021-04-25 2022-04-29 烟台杰瑞石油装备技术有限公司 涡轮压裂设备
US11639654B2 (en) 2021-05-24 2023-05-02 Bj Energy Solutions, Llc Hydraulic fracturing pumps to enhance flow of fracturing fluid into wellheads and related methods

Family Cites Families (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3393917A (en) * 1965-10-23 1968-07-23 Menasco Mfg Company Fluid seal
US3751907A (en) * 1971-12-08 1973-08-14 Caterpillar Tractor Co Inertial air cleaner for gas turbine
US3945760A (en) * 1974-10-29 1976-03-23 Westinghouse Electric Corporation Outer cylinder for a low pressure turbine apparatus
IT1150185B (it) * 1982-02-05 1986-12-10 Nuovo Pignone Spa Carro ponte perfezionato per cabinati di turbine a gas di potenza
JPH01171858A (ja) * 1987-12-25 1989-07-06 Nikkiso Co Ltd 繊維強化樹脂積層体
JPH0552235U (ja) * 1991-12-24 1993-07-13 石川島播磨重工業株式会社 ガスタービン発電装置の吸気室
WO1997030276A1 (en) * 1996-02-13 1997-08-21 Kvaerner Energy A.S Turbine pack and method for adapting a turbine pack
JPH11159056A (ja) * 1997-11-26 1999-06-15 Toray Ind Inc ハウジング用パネル、ハウスおよびそれらの製造方法
JP4667810B2 (ja) * 2004-09-27 2011-04-13 日本無機株式会社 ガスタービン吸気用フィルタユニット
US7338703B2 (en) * 2004-11-24 2008-03-04 Touchstone Research Laboratory, Ltd. Metallic-polymeric composite materials
JP2007001226A (ja) * 2005-06-27 2007-01-11 Toray Ind Inc 金属シートと繊維強化プラスチックの複合部材の成形方法、及び該成形に使用する金属シートと繊維強化プラスチック基材の複合基材
JP4736795B2 (ja) * 2005-12-26 2011-07-27 トヨタ自動車株式会社 繊維強化プラスチック構造体
DE102006017377A1 (de) * 2006-04-11 2007-11-08 Rolls-Royce Deutschland Ltd & Co Kg Klappendichtung für eine Strömungsmaschine
US8672606B2 (en) * 2006-06-30 2014-03-18 Solar Turbines Inc. Gas turbine engine and system for servicing a gas turbine engine
FR2906568B1 (fr) * 2006-10-02 2012-01-06 Aircelle Sa Structure d'entree d'air deposable pour nacelle de turboreacteur.
FR2913053B1 (fr) * 2007-02-23 2009-05-22 Snecma Sa Procede de fabrication d'un carter de turbine a gaz en materiau composite et carter ainsi obtenu
GB0722319D0 (en) * 2007-11-14 2007-12-27 Rolls Royce Plc Component monitoring arrangement
US8105012B2 (en) * 2008-03-12 2012-01-31 Opra Technologies B.V. Adjustable compressor bleed system and method
EP2116728A1 (en) * 2008-05-07 2009-11-11 Siemens Aktiengesellschaft Fluid intake assembly
US8152461B2 (en) * 2008-11-19 2012-04-10 Mra Systems, Inc. Integrated inlet design
FR2941673B1 (fr) * 2009-02-04 2011-01-14 Aircelle Sa Ensemble de suspension pour turboreacteur d'aeronef
US8839625B2 (en) * 2010-06-08 2014-09-23 Hamilton Sunstrand Corporation Gas turbine engine diffuser having air flow channels with varying widths
US8444083B2 (en) * 2011-06-30 2013-05-21 Hamilton Sundstrand Corporation Auxiliary power unit inlet
US8894361B2 (en) * 2011-08-30 2014-11-25 Siemens Energy, Inc. Gas turbine compressor inlet with reduced flow distortion
RU119460U1 (ru) * 2011-12-29 2012-08-20 Открытое акционерное общество "Протон-Пермские моторы" (ОАО "Протон-ПМ") Стенд для испытаний газотурбинных установок газоперекачивающих агрегатов магистральных газопроводов

Also Published As

Publication number Publication date
KR102204720B1 (ko) 2021-01-20
AU2014261404A1 (en) 2015-11-12
CN105339602B (zh) 2017-09-08
WO2014177658A1 (en) 2014-11-06
ITFI20130100A1 (it) 2014-11-04
EP2992186A1 (en) 2016-03-09
EP2992186B1 (en) 2020-09-09
US20160076447A1 (en) 2016-03-17
RU2015145321A (ru) 2017-06-08
RU2673029C2 (ru) 2018-11-21
BR112015027221B1 (pt) 2022-02-08
CA2910055A1 (en) 2014-11-06
KR20160003834A (ko) 2016-01-11
BR112015027221B8 (pt) 2022-10-18
CN105339602A (zh) 2016-02-17
CA2910055C (en) 2021-11-16
AU2014261404B2 (en) 2017-09-14
JP2016516945A (ja) 2016-06-09
JP6484221B2 (ja) 2019-03-13

Similar Documents

Publication Publication Date Title
BR112015027221A2 (pt) câmara de admissão de ar e sistema de motor de turbina a gás
BR112015017847A2 (pt) montagem de ventilador
BRPI0907478A2 (pt) flap de admissão de mecanismo propulsor para aplicação à caixa de uma entrada de ar de um mecanismo propulsor de aeronave bem como mecanismo propulsor com flap de admissão de mecanismo propulsor e sistema de aeronave
WO2012027210A3 (en) Ventilation system for engine and aftertreatment compartments and components
BR112012008685A2 (pt) conjunto de um motor com turbina a gás e de uma nacela
WO2013171452A3 (en) A fan
BR112012011700A2 (pt) sistema de tratamento/aditivo de gás de escapamento e misturador para uso nele
FR2970465B1 (fr) Nacelle pour un turboreacteur d'aeronef double flux.
BR112014000942A2 (pt) ventilador
WO2013171450A3 (en) A fan
BR112017011595A2 (pt) bomba de vácuo acionada pneumaticamente para prover vácuo, sistema de ar para um motor turbo-alimentado e sistema de ar para um motor normalmente aspirado
GB201208619D0 (en) A fan
WO2012121800A3 (en) Gaseous fuel-powered engine system having turbo-compounding
BR112014013017A2 (pt) filtro de ar
BR112014017524A2 (pt) ventilador tipo ejetor com precipitador eletrostático
BR112014000931A2 (pt) ventilador
BR112013033566A2 (pt) método e dispositivo para reduzir o fluxo de massa de ar em um motor de turbina a gás de eixo único
BR112015018986A2 (pt) sistema de geração de energia e método de operação de um sistema de geração de energia
BR112012022051A2 (pt) tanque de água auxiliar para um sistema de resfriamento de motor e sistema de resfriamento de motor
BR112015020829A2 (pt) sistemas de escape de difusor radial para uso com um motor de turbina a gás
ATE445771T1 (de) Triebwerk für ein flugzeug
BRPI0922445A2 (pt) exaustor de sucção
ES2394332B1 (es) Caja de ventilacion
GB201113034D0 (en) An conditioning system exhaust silencer for an aircraft
EP2559858A3 (en) Compressors with integrated secondary air flow systems

Legal Events

Date Code Title Description
B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B06U Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette]
B350 Update of information on the portal [chapter 15.35 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]

Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 30/04/2014, OBSERVADAS AS CONDICOES LEGAIS.

B25A Requested transfer of rights approved

Owner name: NUOVO PIGNONE TECNOLOGIE S.R.L. (IT)