PL3542033T3 - Dysza wlotowa o niskim współczynniku tarcia do turboekspandera - Google Patents

Dysza wlotowa o niskim współczynniku tarcia do turboekspandera

Info

Publication number
PL3542033T3
PL3542033T3 PL16922031.6T PL16922031T PL3542033T3 PL 3542033 T3 PL3542033 T3 PL 3542033T3 PL 16922031 T PL16922031 T PL 16922031T PL 3542033 T3 PL3542033 T3 PL 3542033T3
Authority
PL
Poland
Prior art keywords
turboexpander
low
inlet nozzle
friction
friction inlet
Prior art date
Application number
PL16922031.6T
Other languages
English (en)
Inventor
Jingfeng Liu
Original Assignee
L'Air Liquide, Société Anonyme pour l'Etude et l'Exploitation des Procédés Georges Claude
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 L'Air Liquide, Société Anonyme pour l'Etude et l'Exploitation des Procédés Georges Claude filed Critical L'Air Liquide, Société Anonyme pour l'Etude et l'Exploitation des Procédés Georges Claude
Publication of PL3542033T3 publication Critical patent/PL3542033T3/pl

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
    • F01D17/00Regulating or controlling by varying flow
    • F01D17/10Final actuators
    • F01D17/12Final actuators arranged in stator parts
    • F01D17/14Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/16Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • F01D17/165Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes for radial flow, i.e. the vanes turning around axes which are essentially parallel to the rotor centre line
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B37/00Engines characterised by provision of pumps driven at least for part of the time by exhaust
    • F02B37/12Control of the pumps
    • F02B37/24Control of the pumps by using pumps or turbines with adjustable guide vanes
    • 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
    • F05D2220/40Application in turbochargers
    • 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
    • F05D2220/60Application making use of surplus or waste energy
    • 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
    • F05D2240/00Components
    • F05D2240/90Mounting on supporting structures or systems
    • 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
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Control Of Turbines (AREA)
  • Vaporization, Distillation, Condensation, Sublimation, And Cold Traps (AREA)
PL16922031.6T 2016-11-18 2016-11-18 Dysza wlotowa o niskim współczynniku tarcia do turboekspandera PL3542033T3 (pl)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/CN2016/106323 WO2018090307A1 (en) 2016-11-18 2016-11-18 A low friction inlet nozzle for a turbo expander

Publications (1)

Publication Number Publication Date
PL3542033T3 true PL3542033T3 (pl) 2024-02-05

Family

ID=62145036

Family Applications (1)

Application Number Title Priority Date Filing Date
PL16922031.6T PL3542033T3 (pl) 2016-11-18 2016-11-18 Dysza wlotowa o niskim współczynniku tarcia do turboekspandera

Country Status (11)

Country Link
US (1) US11143053B2 (pl)
EP (1) EP3542033B1 (pl)
JP (1) JP6868689B2 (pl)
KR (1) KR102256400B1 (pl)
CN (1) CN109983204B (pl)
CA (1) CA3043949C (pl)
ES (1) ES2959754T3 (pl)
FI (1) FI3542033T3 (pl)
PL (1) PL3542033T3 (pl)
PT (1) PT3542033T (pl)
WO (1) WO2018090307A1 (pl)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3929407A1 (de) * 2020-06-23 2021-12-29 ABB Schweiz AG Modularer düsenring für eine turbinenstufe einer strömungsmaschine
CN116220913B (zh) * 2023-05-08 2023-08-18 中国航发四川燃气涡轮研究院 一种低损失的发动机预旋供气系统

Family Cites Families (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6075601U (ja) * 1983-10-31 1985-05-27 株式会社日立製作所 可変ノズルを備えた膨張タービン
JPH0610403B2 (ja) * 1984-02-22 1994-02-09 日産自動車株式会社 ラジアルタ−ビンの可変ノズル
JPS6314843U (pl) * 1986-07-14 1988-01-30
JPH09268902A (ja) * 1996-04-01 1997-10-14 Mitsubishi Heavy Ind Ltd ラジアルタービンノズル
US5851104A (en) * 1997-12-15 1998-12-22 Atlas Copco Rotoflow, Inc. Nozzle adjusting mechanism
DE19961613A1 (de) 1999-12-21 2001-07-19 Daimler Chrysler Ag Abgasturbine eines Abgasturboladers für eine Brennkraftmaschine
US7794200B2 (en) * 2003-05-08 2010-09-14 Honeywell International, Inc. Turbocharger with a variable nozzle device
DE10329281A1 (de) * 2003-06-30 2005-01-20 Daimlerchrysler Ag Verdichter im Ansaugtrakt einer Brennkraftmaschine
DE102004030798B4 (de) * 2004-06-25 2014-12-24 Volkswagen Ag Abgasturbolader für eine Brennkraftmaschine mit variabler Turbinengeometrie
CN101663466A (zh) * 2007-06-26 2010-03-03 博格华纳公司 可变几何形状的涡轮增压器
DE102008005405B4 (de) * 2008-01-21 2021-03-04 BMTS Technology GmbH & Co. KG Turbine, insbesondere für einen Abgasturbolader, sowie Abgasturbolader
DE102008005658A1 (de) * 2008-01-23 2009-07-30 Bosch Mahle Turbo Systems Gmbh & Co. Kg Ladeeinrichtung
DE102008060251B4 (de) * 2008-12-03 2021-08-12 BMTS Technology GmbH & Co. KG Abgasturbolader mit variabler Turbinengeometrie
DE102009005938A1 (de) 2009-01-23 2010-07-29 Bosch Mahle Turbo Systems Gmbh & Co. Kg Ladeeinrichtung
KR20120105055A (ko) 2010-02-25 2012-09-24 가부시키가이샤 아이에이치아이 가변 용량형 터보 차저
IT1400053B1 (it) * 2010-05-24 2013-05-17 Nuovo Pignone Spa Metodi e sistemi per ugelli di ingresso a geometria variabile per uso in turboespansori.
DE102012103412A1 (de) * 2012-04-19 2013-10-24 Ihi Charging Systems International Gmbh Turbine für einen Abgasturbolader
DE102012211417A1 (de) 2012-07-02 2014-01-02 Bosch Mahle Turbo Systems Gmbh & Co. Kg Leitschaufel-Anordnung für einen Abgasturbolader
EP2818642A1 (de) * 2013-06-28 2014-12-31 Siemens Aktiengesellschaft Dichtringsegment für einen Stator einer Turbine
CN203756318U (zh) * 2013-12-24 2014-08-06 张运波 一种涡轮增压器稳压阀及发动机涡轮增压器
JP6349745B2 (ja) 2014-01-29 2018-07-04 株式会社Ihi 可変ノズルユニット及び可変容量型過給機
US9611749B2 (en) * 2014-03-26 2017-04-04 General Electric Company Face seal with locally compliant hydrodynamic pads
CN203835466U (zh) * 2014-04-04 2014-09-17 苏州制氧机有限责任公司 一种透平膨胀机喷嘴结构
US9353645B1 (en) 2015-02-16 2016-05-31 Borgwarner Inc. Vane ring thermal strain relief cuts

Also Published As

Publication number Publication date
CA3043949A1 (en) 2018-05-24
CA3043949C (en) 2021-03-23
US11143053B2 (en) 2021-10-12
KR102256400B1 (ko) 2021-05-26
US20190345840A1 (en) 2019-11-14
FI3542033T3 (fi) 2023-10-12
CN109983204A (zh) 2019-07-05
PT3542033T (pt) 2023-10-17
KR20190069569A (ko) 2019-06-19
EP3542033A1 (en) 2019-09-25
EP3542033B1 (en) 2023-07-26
JP6868689B2 (ja) 2021-05-12
CN109983204B (zh) 2021-11-23
EP3542033A4 (en) 2020-05-27
ES2959754T3 (es) 2024-02-28
WO2018090307A1 (en) 2018-05-24
JP2019533117A (ja) 2019-11-14

Similar Documents

Publication Publication Date Title
GB201412189D0 (en) A nozzle arrangement for a gas turbine engine
GB201513236D0 (en) A nozzle guide vane passage
GB201611674D0 (en) A turbine arrangement
GB201621331D0 (en) A Nozzle
GB201513232D0 (en) A nozzle guide vane passage
GB2558072B (en) Turbine for a turbine engine
GB201709183D0 (en) A wingsail
GB2554764B (en) A capo
PL3542033T3 (pl) Dysza wlotowa o niskim współczynniku tarcia do turboekspandera
PL3439789T3 (pl) Wysokociśnieniowa dysza wirnikowa
PL3280879T3 (pl) Układ do turbiny
GB201813223D0 (en) A atroller
GB2525305B (en) A turbine
GB201419449D0 (en) A gas fed atomiser
GB201612570D0 (en) A turbine
GB2552770B (en) A compressor
GB201711717D0 (en) A turbine
GB201513234D0 (en) A nozzle guide vane passage
AU201711825S (en) a dress
AU201711821S (en) a dress
AU201711820S (en) a dress
GB201618172D0 (en) Assembly for a game
AU201617324S (en) A dress
AU201613522S (en) A Dress
AU201617330S (en) A dress