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RU2004123585A - Усовершенствованное устройство регулирования выпрямителей компрессора турбореактивного двигателя - Google Patents

Усовершенствованное устройство регулирования выпрямителей компрессора турбореактивного двигателя Download PDF

Info

Publication number
RU2004123585A
RU2004123585A RU2004123585/06A RU2004123585A RU2004123585A RU 2004123585 A RU2004123585 A RU 2004123585A RU 2004123585/06 A RU2004123585/06 A RU 2004123585/06A RU 2004123585 A RU2004123585 A RU 2004123585A RU 2004123585 A RU2004123585 A RU 2004123585A
Authority
RU
Russia
Prior art keywords
section
optical signals
lighting
coding element
light
Prior art date
Application number
RU2004123585/06A
Other languages
English (en)
Russian (ru)
Inventor
Жерар ЖОЛИБУА (FR)
Жерар ЖОЛИБУА
Даниель Жорж ПЛОНА (FR)
Даниель Жорж ПЛОНА
Original Assignee
Снекма Мотер (Fr)
Снекма Мотер
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 Снекма Мотер (Fr), Снекма Мотер filed Critical Снекма Мотер (Fr)
Publication of RU2004123585A publication Critical patent/RU2004123585A/ru

Links

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
    • 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
    • F04D29/563—Fluid-guiding means, e.g. diffusers adjustable specially adapted for elastic fluid pumps

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Optical Transform (AREA)
  • Length Measuring Devices By Optical Means (AREA)
  • Arrangements For Transmission Of Measured Signals (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
RU2004123585/06A 2003-07-31 2004-07-30 Усовершенствованное устройство регулирования выпрямителей компрессора турбореактивного двигателя RU2004123585A (ru)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0309453 2003-07-31
FR0309453A FR2858371B1 (fr) 2003-07-31 2003-07-31 Dispositif perfectionne de calage de redresseurs d'un compresseur de turboreacteur

Publications (1)

Publication Number Publication Date
RU2004123585A true RU2004123585A (ru) 2006-01-27

Family

ID=33523038

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2004123585/06A RU2004123585A (ru) 2003-07-31 2004-07-30 Усовершенствованное устройство регулирования выпрямителей компрессора турбореактивного двигателя

Country Status (6)

Country Link
US (1) US20050079046A1 (fr)
EP (1) EP1503041A1 (fr)
JP (1) JP2005054794A (fr)
CA (1) CA2475423A1 (fr)
FR (1) FR2858371B1 (fr)
RU (1) RU2004123585A (fr)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1867877A1 (fr) * 2006-06-16 2007-12-19 Ansaldo Energia S.P.A. Compresseur d'une turbine à gaz
US7527471B2 (en) * 2006-07-31 2009-05-05 General Electric Company Stator vane and gas turbine engine assembly including same
ATE440263T1 (de) * 2006-08-28 2009-09-15 Siemens Ag Vorrichtung zur bestimmung der winkellage einer drehbaren verdichterleitschaufel
EP2336498A1 (fr) * 2009-12-15 2011-06-22 Siemens Aktiengesellschaft Dispositif destiné à la détermination de la position angulaire d'une aube directrice de compresseur pivotante
US8528207B2 (en) * 2010-08-19 2013-09-10 Rolls-Royce Corporation Variable vane calibration method
JP6332740B2 (ja) 2014-03-13 2018-05-30 三菱日立パワーシステムズ株式会社 角度計測方法、測定治具

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH330258A (de) * 1955-04-30 1958-05-31 Sulzer Ag Verdichter
US5137353A (en) * 1991-10-10 1992-08-11 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Angular displacement measuring device
GB2346414B (en) * 1999-02-04 2002-06-05 Alstom Gas Turbines Ltd Gas turbine engine with variable guide vane indicator

Also Published As

Publication number Publication date
CA2475423A1 (fr) 2005-01-31
FR2858371A1 (fr) 2005-02-04
JP2005054794A (ja) 2005-03-03
US20050079046A1 (en) 2005-04-14
EP1503041A1 (fr) 2005-02-02
FR2858371B1 (fr) 2005-09-30

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Legal Events

Date Code Title Description
FA92 Acknowledgement of application withdrawn (lack of supplementary materials submitted)

Effective date: 20060814