CN106687665B - 驱动用于调整叶片定向的构件的机构 - Google Patents

驱动用于调整叶片定向的构件的机构 Download PDF

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Publication number
CN106687665B
CN106687665B CN201580047858.6A CN201580047858A CN106687665B CN 106687665 B CN106687665 B CN 106687665B CN 201580047858 A CN201580047858 A CN 201580047858A CN 106687665 B CN106687665 B CN 106687665B
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CN
China
Prior art keywords
gear
adjustment member
turbine
stage
drive mechanism
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.)
Active
Application number
CN201580047858.6A
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English (en)
Chinese (zh)
Other versions
CN106687665A (zh
Inventor
皮埃尔-艾伦·弗朗西斯·克劳德·西布雷希特
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
Safran Aircraft Engines SAS
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 Safran Aircraft Engines SAS filed Critical Safran Aircraft Engines SAS
Publication of CN106687665A publication Critical patent/CN106687665A/zh
Application granted granted Critical
Publication of CN106687665B publication Critical patent/CN106687665B/zh
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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
    • F01D17/162Final 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/40Casings; Connections of working fluid
    • F04D29/52Casings; Connections of working fluid for axial pumps
    • F04D29/54Fluid-guiding means, e.g. diffusers
    • F04D29/56Fluid-guiding means, e.g. diffusers adjustable
    • F04D29/563Fluid-guiding means, e.g. diffusers adjustable specially adapted for elastic fluid pumps
    • 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
    • F05D2220/323Application in turbines in gas turbines for aircraft propulsion, e.g. jet engines
    • 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
    • F05D2260/00Function
    • F05D2260/40Transmission of power
    • F05D2260/403Transmission of power through the shape of the drive components
    • F05D2260/4031Transmission of power through the shape of the drive components as in toothed gearing
    • 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
    • F05D2260/00Function
    • F05D2260/50Kinematic linkage, i.e. transmission of position
    • F05D2260/53Kinematic linkage, i.e. transmission of position using gears

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Transmission Devices (AREA)
  • Gear Transmission (AREA)
  • Supercharger (AREA)
CN201580047858.6A 2014-09-05 2015-09-03 驱动用于调整叶片定向的构件的机构 Active CN106687665B (zh)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1458344A FR3025577B1 (fr) 2014-09-05 2014-09-05 Mecanisme d'entrainement d'organes de reglage de l'orientation des pales
FR1458344 2014-09-05
PCT/FR2015/052325 WO2016034816A1 (fr) 2014-09-05 2015-09-03 Mécanisme d'entraînement d'organes de réglage de l'orientation des pales

Publications (2)

Publication Number Publication Date
CN106687665A CN106687665A (zh) 2017-05-17
CN106687665B true CN106687665B (zh) 2019-06-14

Family

ID=51932450

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201580047858.6A Active CN106687665B (zh) 2014-09-05 2015-09-03 驱动用于调整叶片定向的构件的机构

Country Status (9)

Country Link
US (1) US10502088B2 (enExample)
EP (1) EP3189216B1 (enExample)
JP (1) JP6621807B2 (enExample)
CN (1) CN106687665B (enExample)
BR (1) BR112017003746B1 (enExample)
CA (1) CA2959879C (enExample)
FR (1) FR3025577B1 (enExample)
RU (1) RU2705529C2 (enExample)
WO (1) WO2016034816A1 (enExample)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR102058810B1 (ko) * 2016-08-10 2019-12-23 미츠비시 히타치 파워 시스템즈 가부시키가이샤 베어링 장치 및 회전 기계
FR3057327B1 (fr) 2016-10-07 2018-12-07 Safran Aircraft Engines Mecanisme d'entrainement d'organes de reglage de l'orientation des pales
AU2020376271B9 (en) * 2019-10-31 2023-11-09 Daikin Industries, Ltd. Inlet guide vane actuator assembly

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB706139A (en) * 1950-10-07 1954-03-24 Hellmut Weinrich Improvements in continuous, automatically regulating gears
US20070020090A1 (en) * 2005-07-20 2007-01-25 United Technologies Corporation Rack and pinion variable vane synchronizing mechanism for inner diameter vane shroud
CN1944961A (zh) * 2006-10-13 2007-04-11 成都发动机(集团)有限公司 精确调节顶压和紧急全关静叶的调节机构
CN202250255U (zh) * 2011-08-04 2012-05-30 中国南方航空工业(集团)有限公司 涡轮机导向叶片调节器
EP2626521A1 (en) * 2012-02-13 2013-08-14 Rolls-Royce plc A unison ring gear assembly for a gas turbine

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5174716A (en) * 1990-07-23 1992-12-29 General Electric Company Pitch change mechanism
US5498135A (en) * 1995-01-17 1996-03-12 Newport News Shipbuilding And Dry Dock Company Actuator for a variable pitch propeller
US6039534A (en) * 1998-09-21 2000-03-21 Northern Research And Engineering Corp Inlet guide vane assembly
FR2856424B1 (fr) 2003-06-20 2005-09-23 Snecma Moteurs Dispositif de calage variable de deux etages d'aubes fixes sur un turboreacteur
FR2885969B1 (fr) * 2005-05-17 2007-08-10 Snecma Moteurs Sa Systeme de commande d'etages d'aubes de stator a angle de calage variable de turbomachine
US7413401B2 (en) * 2006-01-17 2008-08-19 General Electric Company Methods and apparatus for controlling variable stator vanes
US8240983B2 (en) * 2007-10-22 2012-08-14 United Technologies Corp. Gas turbine engine systems involving gear-driven variable vanes
FR3030649B1 (fr) * 2014-12-18 2017-01-27 Snecma Mecanisme d'entrainement d'organes de reglage de l'orientation des pales

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB706139A (en) * 1950-10-07 1954-03-24 Hellmut Weinrich Improvements in continuous, automatically regulating gears
US20070020090A1 (en) * 2005-07-20 2007-01-25 United Technologies Corporation Rack and pinion variable vane synchronizing mechanism for inner diameter vane shroud
CN1944961A (zh) * 2006-10-13 2007-04-11 成都发动机(集团)有限公司 精确调节顶压和紧急全关静叶的调节机构
CN202250255U (zh) * 2011-08-04 2012-05-30 中国南方航空工业(集团)有限公司 涡轮机导向叶片调节器
EP2626521A1 (en) * 2012-02-13 2013-08-14 Rolls-Royce plc A unison ring gear assembly for a gas turbine

Also Published As

Publication number Publication date
CA2959879A1 (fr) 2016-03-10
BR112017003746A2 (pt) 2017-12-05
RU2017111042A (ru) 2018-10-05
FR3025577B1 (fr) 2016-12-23
EP3189216B1 (fr) 2025-04-30
JP6621807B2 (ja) 2019-12-18
FR3025577A1 (fr) 2016-03-11
RU2017111042A3 (enExample) 2019-03-14
CN106687665A (zh) 2017-05-17
BR112017003746B1 (pt) 2022-10-18
WO2016034816A1 (fr) 2016-03-10
US20170260870A1 (en) 2017-09-14
US10502088B2 (en) 2019-12-10
RU2705529C2 (ru) 2019-11-07
CA2959879C (fr) 2022-09-20
JP2017527736A (ja) 2017-09-21
EP3189216A1 (fr) 2017-07-12

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