CH419426A - Multi-stage centrifugal compressor with axial and radial stages - Google Patents

Multi-stage centrifugal compressor with axial and radial stages

Info

Publication number
CH419426A
CH419426A CH258164A CH258164A CH419426A CH 419426 A CH419426 A CH 419426A CH 258164 A CH258164 A CH 258164A CH 258164 A CH258164 A CH 258164A CH 419426 A CH419426 A CH 419426A
Authority
CH
Switzerland
Prior art keywords
axial
centrifugal compressor
stage centrifugal
radial stages
stages
Prior art date
Application number
CH258164A
Other languages
German (de)
Inventor
Rurik Josef
Weinrich Hellmut
Original Assignee
Gutehoffnungshuette Sterkrade
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 Gutehoffnungshuette Sterkrade filed Critical Gutehoffnungshuette Sterkrade
Publication of CH419426A publication Critical patent/CH419426A/en

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
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D17/00—Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
    • F04D17/02—Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps having non-centrifugal stages, e.g. centripetal
    • F04D17/025—Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps having non-centrifugal stages, e.g. centripetal comprising axial flow and radial flow stages

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
CH258164A 1963-03-02 1964-03-02 Multi-stage centrifugal compressor with axial and radial stages CH419426A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DEG0037187 1963-03-02

Publications (1)

Publication Number Publication Date
CH419426A true CH419426A (en) 1966-08-31

Family

ID=7125578

Family Applications (1)

Application Number Title Priority Date Filing Date
CH258164A CH419426A (en) 1963-03-02 1964-03-02 Multi-stage centrifugal compressor with axial and radial stages

Country Status (3)

Country Link
US (1) US3303989A (en)
CH (1) CH419426A (en)
DE (1) DE1428106B2 (en)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH485124A (en) * 1968-01-15 1970-01-31 Sulzer Ag Multi-stage axial compressor
CH533768A (en) * 1971-01-20 1973-02-15 Bbc Sulzer Turbomaschinen Multi-stage compressor
JPS597708A (en) * 1982-07-07 1984-01-14 Hitachi Ltd Mounting angle variable device of stationary blade in axial flow machine
FR2748533B1 (en) * 1996-05-07 1999-07-23 Inst Francais Du Petrole POLYPHASIC AND CENTRIFUGAL PUMPING SYSTEM
US6547514B2 (en) 2001-06-08 2003-04-15 Schlumberger Technology Corporation Technique for producing a high gas-to-liquid ratio fluid
EP2639429A1 (en) * 2012-03-16 2013-09-18 MTU Aero Engines GmbH Aircraft engine
US10428823B2 (en) 2014-11-06 2019-10-01 General Electric Company Centrifugal compressor apparatus
GB2551551B (en) * 2016-06-22 2018-09-05 Rolls Royce Plc Gas Turbine Engine
CN109707671A (en) * 2019-02-02 2019-05-03 沈阳透平机械股份有限公司 A kind of built-in Silence Process mechanism of Axial Flow Compressor

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1093374A (en) * 1911-12-15 1914-04-14 Ingersoll Rand Co Pressure-equalizer for rotary blowers.
CH70671A (en) * 1915-06-24 1915-10-16 Oerlikon Maschf Two-stage fan
CH71107A (en) * 1915-07-05 1915-12-01 Oerlikon Maschf Multi-stage turbo fan
CH71244A (en) * 1915-07-12 1915-12-16 Oerlikon Maschf Multi-stage turbo fan
CH102821A (en) * 1922-08-12 1924-01-02 Bbc Brown Boveri & Cie Multi-stage centrifugal compressor.
NL43877C (en) * 1936-10-26 1938-07-16
US2371706A (en) * 1941-02-10 1945-03-20 Eugene Andre Paul Axial flow compressor
US2500070A (en) * 1945-06-15 1950-03-07 Westinghouse Electric Corp Multistage, axial flow, gas compressor
US3060680A (en) * 1957-12-30 1962-10-30 Rolls Royce By-pass gas-turbine engine and control therefor
CH374143A (en) * 1960-01-25 1963-12-31 Bbc Brown Boveri & Cie Adjustment device for rows of guide vanes in flow machines

Also Published As

Publication number Publication date
US3303989A (en) 1967-02-14
DE1428106B2 (en) 1971-12-16
DE1428106A1 (en) 1969-02-06

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