CN105874171B - 飞机涡轮螺旋桨或涡轮风扇的涡轮发动机压缩机 - Google Patents

飞机涡轮螺旋桨或涡轮风扇的涡轮发动机压缩机 Download PDF

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Publication number
CN105874171B
CN105874171B CN201480069646.3A CN201480069646A CN105874171B CN 105874171 B CN105874171 B CN 105874171B CN 201480069646 A CN201480069646 A CN 201480069646A CN 105874171 B CN105874171 B CN 105874171B
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CN
China
Prior art keywords
control ring
compressor
hole
turbine engine
pin
Prior art date
Legal status (The legal status 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 status listed.)
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Application number
CN201480069646.3A
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English (en)
Chinese (zh)
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CN105874171A (zh
Inventor
皮埃尔-阿兰·弗朗西斯·克劳德·赛布热切特
塞巴斯蒂安·科考恩
阿诺德·朗格卢瓦
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
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Publication date
Application filed by SNECMA SAS filed Critical SNECMA SAS
Publication of CN105874171A publication Critical patent/CN105874171A/zh
Application granted granted Critical
Publication of CN105874171B publication Critical patent/CN105874171B/zh
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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
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/12—Final actuators arranged in stator parts
    • F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • 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
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/12—Final actuators arranged in stator parts
    • F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • F01D17/162—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes for axial flow, i.e. the vanes turning around axes which are essentially perpendicular to the rotor centre line
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/40—Casings; Connections of working fluid
    • F04D29/52—Casings; Connections of working fluid for axial pumps
    • F04D29/54—Fluid-guiding means, e.g. diffusers
    • F04D29/56—Fluid-guiding means, e.g. diffusers adjustable
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/40—Casings; Connections of working fluid
    • F04D29/52—Casings; Connections of working fluid for axial pumps
    • F04D29/54—Fluid-guiding means, e.g. diffusers
    • F04D29/56—Fluid-guiding means, e.g. diffusers adjustable
    • F04D29/563—Fluid-guiding means, e.g. diffusers adjustable specially adapted for elastic fluid pumps
    • 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
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/12—Final actuators arranged in stator parts
    • F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • F01D17/167—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes of vanes moving in translation
    • 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
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • F05D2220/321—Application in turbines in gas turbines for a special turbine stage
    • F05D2220/3216—Application in turbines in gas turbines for a special turbine stage for a special compressor stage
    • 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
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • F05D2220/323—Application in turbines in gas turbines for aircraft propulsion, e.g. jet engines
    • 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
    • F05D2240/00—Components
    • F05D2240/10—Stators
    • F05D2240/12—Fluid guiding means, e.g. vanes
    • 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
    • F05D2270/00—Control
    • F05D2270/50—Control logic embodiments
    • F05D2270/58—Control logic embodiments by mechanical means, e.g. levers, gears or cams

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
CN201480069646.3A 2013-12-19 2014-12-04 飞机涡轮螺旋桨或涡轮风扇的涡轮发动机压缩机 Active CN105874171B (zh)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1362972 2013-12-19
FR1362972A FR3015594B1 (fr) 2013-12-19 2013-12-19 Compresseur de turbomachine, en particulier de turbopropulseur ou de turboreacteur d'avion
PCT/FR2014/053163 WO2015092197A1 (fr) 2013-12-19 2014-12-04 Compresseur de turbomachine, en particulier de turbopropulseur ou de turboréacteur d'avion

Publications (2)

Publication Number Publication Date
CN105874171A CN105874171A (zh) 2016-08-17
CN105874171B true CN105874171B (zh) 2018-06-12

Family

ID=50137899

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201480069646.3A Active CN105874171B (zh) 2013-12-19 2014-12-04 飞机涡轮螺旋桨或涡轮风扇的涡轮发动机压缩机

Country Status (9)

Country Link
US (1) US10590794B2 (enExample)
EP (1) EP3084141B1 (enExample)
JP (1) JP6419831B2 (enExample)
CN (1) CN105874171B (enExample)
BR (1) BR112016013833B1 (enExample)
CA (1) CA2932998C (enExample)
FR (1) FR3015594B1 (enExample)
RU (1) RU2670473C1 (enExample)
WO (1) WO2015092197A1 (enExample)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9835037B2 (en) * 2015-06-22 2017-12-05 General Electric Company Ducted thrust producing system with asynchronous fan blade pitching
FR3041714B1 (fr) 2015-09-30 2020-02-14 Safran Aircraft Engines Compresseur de turbomachine, en particulier de turbopropulseur ou de turboreacteur d'avion
GB201717091D0 (en) * 2017-10-18 2017-11-29 Rolls Royce Plc A variable vane actuation arrangement
FR3100272B1 (fr) * 2019-08-27 2025-04-25 Safran Aircraft Engines Guignol pour un dispositif de calage variable d’une turbomachine
CN112360816A (zh) * 2020-12-08 2021-02-12 成都成发科能动力工程有限公司 一种轴流压缩机承缸和应用其的轴流压缩机
US12510004B2 (en) * 2024-06-14 2025-12-30 General Electric Company Outward facing load reacting bodies for use with unison rings

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1592922A (enExample) * 1968-11-21 1970-05-19
US4737071A (en) * 1985-04-22 1988-04-12 Williams International Corporation Variable geometry centrifugal compressor diffuser
CN1811136A (zh) * 2004-12-16 2006-08-02 斯奈克玛公司 由电动机装置移动的旋转致动环致动的定子叶片级
CN101892874A (zh) * 2009-01-06 2010-11-24 通用电气公司 可变位置导向叶片致动系统和方法

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3066488A (en) * 1959-11-04 1962-12-04 Bendix Corp Power output control for a gas turbine engine
US3314595A (en) * 1965-06-09 1967-04-18 Gen Electric Adjustment mechanism for axial flow compressors
US3861822A (en) * 1974-02-27 1975-01-21 Gen Electric Duct with vanes having selectively variable pitch
US5993152A (en) * 1997-10-14 1999-11-30 General Electric Company Nonlinear vane actuation
GB2402180B (en) * 2003-05-30 2006-09-20 Rolls Royce Plc Variable stator vane actuating levers
FR2857404B1 (fr) * 2003-07-10 2007-03-09 Snecma Moteurs Dispositif de guidage en rotation d'aubes a calage variable dans une turbomachine
FR2882570B1 (fr) * 2005-02-25 2007-04-13 Snecma Moteurs Sa Dipositif de commande d'aubes a calage variable dans une turbomachine
FR2890136B1 (fr) * 2005-08-30 2007-11-09 Snecma Bielle a longueur evolutive en fonctionnement
US7413401B2 (en) * 2006-01-17 2008-08-19 General Electric Company Methods and apparatus for controlling variable stator vanes
US20110176913A1 (en) * 2010-01-19 2011-07-21 Stephen Paul Wassynger Non-linear asymmetric variable guide vane schedule

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1592922A (enExample) * 1968-11-21 1970-05-19
US4737071A (en) * 1985-04-22 1988-04-12 Williams International Corporation Variable geometry centrifugal compressor diffuser
CN1811136A (zh) * 2004-12-16 2006-08-02 斯奈克玛公司 由电动机装置移动的旋转致动环致动的定子叶片级
CN101892874A (zh) * 2009-01-06 2010-11-24 通用电气公司 可变位置导向叶片致动系统和方法

Also Published As

Publication number Publication date
EP3084141B1 (fr) 2018-02-07
CA2932998C (fr) 2022-04-19
WO2015092197A1 (fr) 2015-06-25
FR3015594B1 (fr) 2018-04-06
BR112016013833B1 (pt) 2022-02-08
US10590794B2 (en) 2020-03-17
BR112016013833A2 (enExample) 2017-08-08
JP6419831B2 (ja) 2018-11-07
RU2016123656A (ru) 2018-01-24
RU2670473C1 (ru) 2018-10-23
CN105874171A (zh) 2016-08-17
US20160348530A1 (en) 2016-12-01
FR3015594A1 (fr) 2015-06-26
EP3084141A1 (fr) 2016-10-26
CA2932998A1 (fr) 2015-06-25
JP2017501334A (ja) 2017-01-12

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