GB854127A - Improvements in or relating to radial-flow compressors and turbines - Google Patents

Improvements in or relating to radial-flow compressors and turbines

Info

Publication number
GB854127A
GB854127A GB2056257A GB2056257A GB854127A GB 854127 A GB854127 A GB 854127A GB 2056257 A GB2056257 A GB 2056257A GB 2056257 A GB2056257 A GB 2056257A GB 854127 A GB854127 A GB 854127A
Authority
GB
United Kingdom
Prior art keywords
radial
stage
turbines
flow compressors
volute
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
GB2056257A
Inventor
James Brown
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.)
Power Jets Research and Development Ltd
Original Assignee
Power Jets Research and Development Ltd
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 Power Jets Research and Development Ltd filed Critical Power Jets Research and Development Ltd
Priority to GB2056257A priority Critical patent/GB854127A/en
Publication of GB854127A publication Critical patent/GB854127A/en
Expired legal-status Critical Current

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
    • F04D17/00—Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
    • F04D17/08—Centrifugal pumps
    • F04D17/10—Centrifugal pumps for compressing or evacuating
    • F04D17/12—Multi-stage pumps
    • F04D17/122—Multi-stage pumps the individual rotor discs being, one for each stage, on a common shaft and axially spaced, e.g. conventional centrifugal multi- stage compressors

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

854,127. Radial-flow compressors and turbines. POWER JETS (RESEARCH & DEVELOPMENT) Ltd. June 30, 1958 [June 28, 1957], No. 20562/57. Classes 110 (1) and 110(3). An arrangement of two radial-flow compressors or turbines comprises a volute for each compressor or turbine, and a partition forming a common wall for both volutes, the partition being disposed obliquely with respect to the. common axis of the rotors. In the two-stage centrifugal compressor shown, the air enters the first stage by way of a guide wall 11 and guideblades 3 and is discharged by way of diffusers 5 and a volute 9 to a transfer duct 18 and thence to the second stage, which is similar to the first stage. The outlet duct 19 is substantially diametrically opposite the transfer duct 18.
GB2056257A 1957-06-28 1957-06-28 Improvements in or relating to radial-flow compressors and turbines Expired GB854127A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2056257A GB854127A (en) 1957-06-28 1957-06-28 Improvements in or relating to radial-flow compressors and turbines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2056257A GB854127A (en) 1957-06-28 1957-06-28 Improvements in or relating to radial-flow compressors and turbines

Publications (1)

Publication Number Publication Date
GB854127A true GB854127A (en) 1960-11-16

Family

ID=10147962

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2056257A Expired GB854127A (en) 1957-06-28 1957-06-28 Improvements in or relating to radial-flow compressors and turbines

Country Status (1)

Country Link
GB (1) GB854127A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0187645A2 (en) * 1985-01-08 1986-07-16 Alexander Greenspan Centrifugal, inline, opposed balance gas blower
EP0757179A1 (en) * 1995-07-31 1997-02-05 Sulzer Turbo AG Compression device
US11519424B2 (en) * 2017-06-27 2022-12-06 Ebm-Papst Mulfingen Gmbh & Co. Kg Return channels for a multi-stage turbocompressor

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0187645A2 (en) * 1985-01-08 1986-07-16 Alexander Greenspan Centrifugal, inline, opposed balance gas blower
EP0187645A3 (en) * 1985-01-08 1988-06-15 Alexander Greenspan Centrifugal, inline, opposed balance gas blower
EP0757179A1 (en) * 1995-07-31 1997-02-05 Sulzer Turbo AG Compression device
US5791159A (en) * 1995-07-31 1998-08-11 Sulzer Turbo Ag Compression apparatus
US11519424B2 (en) * 2017-06-27 2022-12-06 Ebm-Papst Mulfingen Gmbh & Co. Kg Return channels for a multi-stage turbocompressor

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