CH219738A - Multi-stage axial compressor. - Google Patents

Multi-stage axial compressor.

Info

Publication number
CH219738A
CH219738A CH219738DA CH219738A CH 219738 A CH219738 A CH 219738A CH 219738D A CH219738D A CH 219738DA CH 219738 A CH219738 A CH 219738A
Authority
CH
Switzerland
Prior art keywords
axial compressor
stage axial
stage
compressor
axial
Prior art date
Application number
Other languages
German (de)
Inventor
Aktiengesellschaft Gebr Sulzer
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
Publication of CH219738A publication Critical patent/CH219738A/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
    • F04D19/00—Axial-flow pumps
    • F04D19/02—Multi-stage pumps
    • F04D19/028—Layout of fluid flow through the stages

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
CH219738D 1940-11-19 1940-11-19 Multi-stage axial compressor. CH219738A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH219738T 1940-11-19

Publications (1)

Publication Number Publication Date
CH219738A true CH219738A (en) 1942-02-28

Family

ID=4451324

Family Applications (1)

Application Number Title Priority Date Filing Date
CH219738D CH219738A (en) 1940-11-19 1940-11-19 Multi-stage axial compressor.

Country Status (1)

Country Link
CH (1) CH219738A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102015223210B3 (en) * 2015-11-24 2017-04-27 MTU Aero Engines AG Compressor, process and turbomachinery

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102015223210B3 (en) * 2015-11-24 2017-04-27 MTU Aero Engines AG Compressor, process and turbomachinery
US10641288B2 (en) 2015-11-24 2020-05-05 MTU Aero Engines AG Method for operating a compressor of a turbomachine comprising providing a plurality of stages in a front compressor area, a rear compressor area, and allowing a swirl in the rear compressor area

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