MX2012008746A - Dispositivo para ajustar alabes guia variables. - Google Patents

Dispositivo para ajustar alabes guia variables.

Info

Publication number
MX2012008746A
MX2012008746A MX2012008746A MX2012008746A MX2012008746A MX 2012008746 A MX2012008746 A MX 2012008746A MX 2012008746 A MX2012008746 A MX 2012008746A MX 2012008746 A MX2012008746 A MX 2012008746A MX 2012008746 A MX2012008746 A MX 2012008746A
Authority
MX
Mexico
Prior art keywords
joint
bracket
guide vanes
axial
variable guide
Prior art date
Application number
MX2012008746A
Other languages
English (en)
Inventor
Colm Keegan
Michael Tibenham
Original Assignee
Siemens Ag
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 Siemens Ag filed Critical Siemens Ag
Publication of MX2012008746A publication Critical patent/MX2012008746A/es

Links

Classifications

    • 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
    • F01D17/162—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
    • 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
    • F05D2260/70—Adjusting of angle of incidence or attack of rotating blades
    • F05D2260/79—Bearing, support or actuation arrangements therefor

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Control Of Turbines (AREA)

Abstract

De acuerdo con la invención, un dispositivo (3) para ajustar álabes guía variables (10, 11) de una máquina de flujo axial que comprende al menos una varilla de control (50) para ajustar una posición angular de las álabes guía variables (10, 11) y un eje giratorio (61) al cual está giratoriamente conectada al menos una varilla de control (50); además, se proporcionan una primera ménsula (70) y una segunda ménsula (72), cada una con un primer extremo (73, 74) que se puede conectar a una camisa (2) de la máquina de flujo axial; se incluyen una primera junta (80) y una segunda junta (81), la primera junta (80) fija a un segundo extremo (75) de la primera ménsula (70) y proporcionando posicionamiento ajustable de un primer extremo (62) del eje (61) y la segunda junta (81) fija a un segundo extremo (76) de la segunda ménsula (72) y proporcionando posicionamiento ajustable de un segundo extremo (63) del eje (61); la primera junta (80) y la segunda junta (81) están espacialmente colocadas entre sí únicamente a través de una primera conexión fija entre el primer extremo (73) de la primera ménsula (70) a la camisa (2) de la máquina de flujo axial y a través de una segunda conexión fija entre el primer extremo (74) de la segunda ménsula (72) a la camisa (2) de la máquina de flujo axial; la primera junta (80) y la segunda junta (81) es una combinación de una junta de rótula y una junta con pasador deslizante.
MX2012008746A 2010-01-28 2010-11-17 Dispositivo para ajustar alabes guia variables. MX2012008746A (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
EP10000879A EP2354560A1 (en) 2010-01-28 2010-01-28 Device for adjusting variable guide vanes
PCT/EP2010/067656 WO2011091881A1 (en) 2010-01-28 2010-11-17 Device for adjusting variable guide vanes

Publications (1)

Publication Number Publication Date
MX2012008746A true MX2012008746A (es) 2012-08-31

Family

ID=42260355

Family Applications (1)

Application Number Title Priority Date Filing Date
MX2012008746A MX2012008746A (es) 2010-01-28 2010-11-17 Dispositivo para ajustar alabes guia variables.

Country Status (8)

Country Link
US (1) US9188138B2 (es)
EP (2) EP2354560A1 (es)
CN (1) CN102713309B (es)
AU (1) AU2010344031A1 (es)
BR (1) BR112012018875A2 (es)
MX (1) MX2012008746A (es)
RU (1) RU2559107C2 (es)
WO (1) WO2011091881A1 (es)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102012007129A1 (de) * 2012-04-10 2013-10-10 Rolls-Royce Deutschland Ltd & Co Kg Leitschaufelverstellvorrichtung einer Gasturbine
WO2014189574A2 (en) * 2013-03-13 2014-11-27 United Technologies Corporation Variable vane control system
FR3014152B1 (fr) * 2013-11-29 2015-12-25 Snecma Dispositif de guidage d'aubes de redresseur a angle de calage variable de turbomachine et procede d'assemblage d'un tel dispositif
KR101850237B1 (ko) * 2014-07-10 2018-04-18 미츠비시 히타치 파워 시스템즈 가부시키가이샤 가변 정익 장치의 메인터넌스 방법 및 가변 정익 장치
WO2016070329A1 (en) * 2014-11-04 2016-05-12 Siemens Aktiengesellschaft Method for determining angular positions of multiple compressor guide vanes
DE102015004648A1 (de) * 2015-04-15 2016-10-20 Man Diesel & Turbo Se Leitschaufelverstellvorrichtung und Strömungsmaschine
FR3036093B1 (fr) * 2015-05-12 2017-06-02 Snecma Dispositif a bras de levier pour la commande de l'orientation des pales de soufflante d'une turbomachine a soufflante non carenee
US20170108032A1 (en) * 2015-10-16 2017-04-20 General Electric Company Stepped shaft assembly
DE102016225482A1 (de) * 2016-12-19 2018-06-21 Rolls-Royce Deutschland Ltd & Co Kg Verstelleinrichtung für die Verstellung mehrerer Leitschaufeln eines Triebwerks
CN110131194B (zh) * 2018-02-09 2020-09-25 中国航发商用航空发动机有限责任公司 自适应的装配式多级可调叶片操纵机构

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3487992A (en) 1967-11-01 1970-01-06 Gen Electric Stator adjusting mechanism for axial flow compressors
RU2098670C1 (ru) 1995-06-26 1997-12-10 Акционерное общество "Авиадвигатель" Устройство для регулирования положения поворотных направляющих лопаток компрессора или турбины газотурбинного двигателя
US5560208A (en) * 1995-07-28 1996-10-01 Halimi; Edward M. Motor-assisted variable geometry turbocharging system
CN1100200C (zh) * 1999-07-06 2003-01-29 孙敏超 一种车用内燃机用的涡轮增压器
US6551057B1 (en) * 1999-11-22 2003-04-22 General Electric Company Damped torque shaft assembly
US8435000B2 (en) * 2008-03-07 2013-05-07 Rolls-Royce Corporation Variable vane actuation system
GB0811286D0 (en) * 2008-06-20 2008-07-30 Rolls Royce Plc Multi-rotational crankshaft

Also Published As

Publication number Publication date
US9188138B2 (en) 2015-11-17
RU2012136627A (ru) 2014-03-10
EP2499380B1 (en) 2014-12-31
WO2011091881A1 (en) 2011-08-04
CN102713309B (zh) 2015-02-25
BR112012018875A2 (pt) 2016-04-12
US20130058763A1 (en) 2013-03-07
EP2499380A1 (en) 2012-09-19
AU2010344031A1 (en) 2012-07-19
CN102713309A (zh) 2012-10-03
EP2354560A1 (en) 2011-08-10
RU2559107C2 (ru) 2015-08-10

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