GB967091A - Improvements in or relating to three-stage radial-flow compressors - Google Patents

Improvements in or relating to three-stage radial-flow compressors

Info

Publication number
GB967091A
GB967091A GB9546/62A GB954662A GB967091A GB 967091 A GB967091 A GB 967091A GB 9546/62 A GB9546/62 A GB 9546/62A GB 954662 A GB954662 A GB 954662A GB 967091 A GB967091 A GB 967091A
Authority
GB
United Kingdom
Prior art keywords
compressor
driven
stage
wheel
gear
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
GB9546/62A
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.)
Borsig GmbH
Original Assignee
Borsig GmbH
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 Borsig GmbH filed Critical Borsig GmbH
Publication of GB967091A publication Critical patent/GB967091A/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
    • F04D25/00Pumping installations or systems
    • F04D25/16Combinations of two or more pumps ; Producing two or more separate gas flows
    • F04D25/163Combinations of two or more pumps ; Producing two or more separate gas flows driven by a common gearing arrangement

Landscapes

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

Abstract

967,091. Centrifugal compressors. BORSIG A.G. March 13, 1962 [April 14, 1961], No. 9546/62. Heading F1C. In a three-stage radial-flow compressor for gas or air provided with double intermediate cooling and a gearing arrangement having a large central gear-wheel adapted to co-operate with three pinion shafts distributed over the periphery thereof, each of the stages has associated therewith an individual pinion shaft having a compressor rotor mounted overhung on an extension of the shaft and driven at a most favourable speed of the stage concerned, and the compressor housings for the three rotors are cast or flanged on the gearing housing. Three stages 17, 18, 19, Fig. 1, of a compressor are respectively driven at their most favourable speed through pinions 2, 3, 4, of suitable diameters, meshing with a large central gearwheel 1 driven by an electric motor 5 through an intermediate shaft 6 and two couplings 7, 8. The pinions 2, 3, 4 are preferably arranged around the gear-wheel 1 as shown in Fig. 2 with the intermediate pinion 3 above or below the gear-wheel 1. Further, the stages 17, 18, 19 are preferably arranged as shown, but they may be arranged all on one side of the gear-wheel 1 or, any stage may be placed opposite the two others. Interstage coolers 14 and 16 are provided. In an alternative embodiment (not shown), the compressor stages may instead be driven by a steam turbine which may be cast or flanged to the gearing housing and is connected either directly, or through an intermediate shaft and two couplings; to one of the pinion shafts. The pinion shaft chosen is the one associated with the compressor stage whose speed corresponds best with that of the turbine, thereby avoiding the use of additional transmission gearing. It is stated to be known to have a four-stage compressor in which a large central gear-wheel driven by an electric motor drives four pinions each of a size adapted to the rotor of its respective stage. Each rotor disc is driven by a pinion shaft constructed as a torsion rod and is supported at its other side by a pin fixed on or integral with the compressor housing and extending into a central blind bore in the rotor disc. Specification 714,765 is referred to.
GB9546/62A 1961-04-14 1962-03-13 Improvements in or relating to three-stage radial-flow compressors Expired GB967091A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DEB0062136 1961-04-14

Publications (1)

Publication Number Publication Date
GB967091A true GB967091A (en) 1964-08-19

Family

ID=6973462

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9546/62A Expired GB967091A (en) 1961-04-14 1962-03-13 Improvements in or relating to three-stage radial-flow compressors

Country Status (3)

Country Link
BE (1) BE615360A (en)
GB (1) GB967091A (en)
NL (1) NL276194A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1691081A2 (en) 2005-01-19 2006-08-16 Man Turbo Ag Multistage turbocompressor
EP2740941A1 (en) 2011-08-05 2014-06-11 Mitsubishi Heavy Industries Compressor Corporation Centrifugal compressor
WO2014180688A1 (en) 2013-05-08 2014-11-13 Voith Patent Gmbh Transmission and compressor system for a transmission
EP2902737A2 (en) 2014-01-24 2015-08-05 Air Products And Chemicals, Inc. Systems and methods for compressing air
GB2536774A (en) * 2015-02-06 2016-09-28 Man Diesel & Turbo Se Geared turbomachine
EP2711503A3 (en) * 2012-09-19 2017-08-23 MAN Diesel & Turbo SE Geared turbomachine
EP3617519A1 (en) * 2018-08-27 2020-03-04 Siemens Aktiengesellschaft Radially compressor rotor, radial compressor, gear-driven compressor

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP6395683B2 (en) * 2015-09-02 2018-09-26 株式会社神戸製鋼所 Compressor

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1691081A3 (en) * 2005-01-19 2008-05-14 Man Turbo Ag Multistage turbocompressor
US7559200B2 (en) 2005-01-19 2009-07-14 Man Turbo Ag Multistage turbocompressor
CN100516543C (en) * 2005-01-19 2009-07-22 慕阿恩动力涡轮股份公司 Multistage turbocompressor
EP1691081A2 (en) 2005-01-19 2006-08-16 Man Turbo Ag Multistage turbocompressor
US9714658B2 (en) 2011-08-05 2017-07-25 Mitsubishi Heavy Industries Compressor Corporation Centrifugal compressor
EP2740941A1 (en) 2011-08-05 2014-06-11 Mitsubishi Heavy Industries Compressor Corporation Centrifugal compressor
EP2711503A3 (en) * 2012-09-19 2017-08-23 MAN Diesel & Turbo SE Geared turbomachine
WO2014180688A1 (en) 2013-05-08 2014-11-13 Voith Patent Gmbh Transmission and compressor system for a transmission
US10100837B2 (en) 2013-05-08 2018-10-16 Voith Patent Gmbh Transmission and geared compressor system
EP2902737A2 (en) 2014-01-24 2015-08-05 Air Products And Chemicals, Inc. Systems and methods for compressing air
GB2536774A (en) * 2015-02-06 2016-09-28 Man Diesel & Turbo Se Geared turbomachine
EP3617519A1 (en) * 2018-08-27 2020-03-04 Siemens Aktiengesellschaft Radially compressor rotor, radial compressor, gear-driven compressor
WO2020043379A1 (en) * 2018-08-27 2020-03-05 Siemens Aktiengesellschaft Radial compressor rotor, radial compressor, geared compressor

Also Published As

Publication number Publication date
NL276194A (en) 1964-10-12
BE615360A (en) 1962-07-16

Similar Documents

Publication Publication Date Title
US2454738A (en) Internal-combustion turbine power plant
GB967091A (en) Improvements in or relating to three-stage radial-flow compressors
GB1294324A (en) Engine installations
GB757577A (en) Axial flow turbines and compressors
GB1229007A (en)
US2073191A (en) Combustion turbine
GB992651A (en) Improvements in centrifugal compressors
GB202295A (en) Improvements in multi-stage centrifugal compressors
GB1278570A (en) Ducted fan gas turbine engines
GB579780A (en) Improvements in or relating to compressors, pumps and the like
GB787739A (en) Combustion turbine power units
US2661594A (en) Coaxial combustion products generator, turbine, and compressors
GB579820A (en) Improvements in or relating to power-gas-generators for internal-combustion power units
GB628697A (en) Improvements in and relating to a gas turbine plant
GB614160A (en) Improvements relating to combustion turbine power plant
US3091382A (en) Gas turbine engines
GB1048966A (en) Improvements in or relating to compressors
GB583469A (en) Improvements in turbo compressors
GB676589A (en) Rotor composed of rotary elements axially connected together, for multi-stage axial-flow turbines and compressors
GB1007131A (en) Improvements in and relating to rotary piston compressors combined with drive transmissions therefor
GB720201A (en) Gas-turbine actuated propelling unit for motor vehicles
GB1000134A (en) Improvements in multi-stage compressors with intercooling
GB592615A (en) Improvements in or relating to internal combustion turbine power plants
GB797311A (en) Improvements in rotary compressor systems
US2253970A (en) Turbine driven gear arrangement and the like