GB717553A - Multi-stage axial flow compressor - Google Patents

Multi-stage axial flow compressor

Info

Publication number
GB717553A
GB717553A GB18389/52A GB1838952A GB717553A GB 717553 A GB717553 A GB 717553A GB 18389/52 A GB18389/52 A GB 18389/52A GB 1838952 A GB1838952 A GB 1838952A GB 717553 A GB717553 A GB 717553A
Authority
GB
United Kingdom
Prior art keywords
compressor
stage axial
axial flow
flow compressor
blades
Prior art date
Legal status (The legal status 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 status listed.)
Expired
Application number
GB18389/52A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
BBC Brown Boveri AG Germany
BBC Brown Boveri France SA
Original Assignee
Brown Boveri und Cie AG Germany
BBC Brown Boveri France SA
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 Brown Boveri und Cie AG Germany, BBC Brown Boveri France SA filed Critical Brown Boveri und Cie AG Germany
Publication of GB717553A publication Critical patent/GB717553A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D19/00Axial-flow pumps
    • F04D19/02Multi-stage pumps
    • F04D19/028Layout 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

717,553. Axial-flow compressors. AKT.-GES., BROWN, BOVERI & CIE. July 21, 1952 [July 19, 1951], No. 18389/52. Class 110(1) In a multi-stage axial-flow compressor, one or more rows of moving blades, at least one of which is situated at the discharge end of the compressor, act as turbine blades at a pressure which either remains constant or increases, for the purpose of recuperating the velocity energy of the working, medium. In the compressor shown, rotor blades h, i and l, m act as turbine blades.
GB18389/52A 1951-07-19 1952-07-21 Multi-stage axial flow compressor Expired GB717553A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH717553X 1951-07-19

Publications (1)

Publication Number Publication Date
GB717553A true GB717553A (en) 1954-10-27

Family

ID=4531253

Family Applications (1)

Application Number Title Priority Date Filing Date
GB18389/52A Expired GB717553A (en) 1951-07-19 1952-07-21 Multi-stage axial flow compressor

Country Status (1)

Country Link
GB (1) GB717553A (en)

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