CH485124A - Multi-stage axial compressor - Google Patents

Multi-stage axial compressor

Info

Publication number
CH485124A
CH485124A CH56868A CH56868A CH485124A CH 485124 A CH485124 A CH 485124A CH 56868 A CH56868 A CH 56868A CH 56868 A CH56868 A CH 56868A CH 485124 A CH485124 A CH 485124A
Authority
CH
Switzerland
Prior art keywords
axial compressor
stage axial
stage
compressor
axial
Prior art date
Application number
CH56868A
Other languages
German (de)
Inventor
Rene Dipl Ing Strub
Original Assignee
Sulzer 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 Sulzer Ag filed Critical Sulzer Ag
Priority to CH56868A priority Critical patent/CH485124A/en
Priority to NL6801665A priority patent/NL6801665A/xx
Priority to US740271A priority patent/US3508839A/en
Priority to FR1590020D priority patent/FR1590020A/fr
Publication of CH485124A publication Critical patent/CH485124A/en

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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
CH56868A 1968-01-15 1968-01-15 Multi-stage axial compressor CH485124A (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
CH56868A CH485124A (en) 1968-01-15 1968-01-15 Multi-stage axial compressor
NL6801665A NL6801665A (en) 1968-01-15 1968-02-06
US740271A US3508839A (en) 1968-01-15 1968-06-26 Plural-stage axial compressor
FR1590020D FR1590020A (en) 1968-01-15 1968-10-25

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH56868A CH485124A (en) 1968-01-15 1968-01-15 Multi-stage axial compressor

Publications (1)

Publication Number Publication Date
CH485124A true CH485124A (en) 1970-01-31

Family

ID=4190011

Family Applications (1)

Application Number Title Priority Date Filing Date
CH56868A CH485124A (en) 1968-01-15 1968-01-15 Multi-stage axial compressor

Country Status (4)

Country Link
US (1) US3508839A (en)
CH (1) CH485124A (en)
FR (1) FR1590020A (en)
NL (1) NL6801665A (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6039534A (en) * 1998-09-21 2000-03-21 Northern Research And Engineering Corp Inlet guide vane assembly
EP1803903A1 (en) * 2006-01-02 2007-07-04 Siemens Aktiengesellschaft Actuator for the rotation of adjustable blades of a turbine
US20100172743A1 (en) 2009-01-06 2010-07-08 General Electric Company Variable position guide vane actuation system and method
US8297918B2 (en) * 2009-01-06 2012-10-30 General Electric Company Variable position guide vane actuation system and method
TWI614410B (en) 2013-12-17 2018-02-11 財團法人工業技術研究院 Inlet guide vane (i. g. v) assembly
CN104895839A (en) * 2015-04-22 2015-09-09 南京航空航天大学 Axial-flow compressor stator blade system with adjustable first and second half of segments and working method thereof

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2778564A (en) * 1953-12-01 1957-01-22 Havilland Engine Co Ltd Stator blade ring assemblies for axial flow compressors and the like
FR1238098A (en) * 1958-10-30 1960-08-05 Licentia Gmbh Axial turbo-machine, preferably axial compressor, comprising at least two crowns of adjustable blades, in particular guide blades
DE1428106B2 (en) * 1963-03-02 1971-12-16 Gutehoffnung shutte Sterkrade AG, 4200 Oberhausen ADJUSTMENT DEVICE FOR JOINT ADJUSTMENT OF THE GUIDE BLADES OF THE AXIAL STAGES OF A MULTISTAGE CENTRIFUGAL COMPRESSOR
CH415933A (en) * 1964-06-23 1966-06-30 Bbc Brown Boveri & Cie Method for preventing corrosion damage to the adjustment mechanisms of guide vanes in turbo machines and turbo machines for carrying out the method

Also Published As

Publication number Publication date
NL6801665A (en) 1969-07-17
US3508839A (en) 1970-04-28
FR1590020A (en) 1970-04-06

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Legal Events

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