GB305214A - Improvements in or relating to means for controlling the running of centrifugal machines - Google Patents

Improvements in or relating to means for controlling the running of centrifugal machines

Info

Publication number
GB305214A
GB305214A GB3019/29A GB301929A GB305214A GB 305214 A GB305214 A GB 305214A GB 3019/29 A GB3019/29 A GB 3019/29A GB 301929 A GB301929 A GB 301929A GB 305214 A GB305214 A GB 305214A
Authority
GB
United Kingdom
Prior art keywords
diffuser
ring
vanes
rings
moved
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
GB3019/29A
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.)
Rateau SA
Original Assignee
Rateau 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 Rateau SA filed Critical Rateau SA
Publication of GB305214A publication Critical patent/GB305214A/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
    • F04D29/00Details, component parts, or accessories
    • F04D29/40Casings; Connections of working fluid
    • F04D29/42Casings; Connections of working fluid for radial or helico-centrifugal pumps
    • F04D29/44Fluid-guiding means, e.g. diffusers
    • F04D29/46Fluid-guiding means, e.g. diffusers adjustable
    • F04D29/462Fluid-guiding means, e.g. diffusers adjustable especially adapted for elastic fluid pumps
    • F04D29/464Fluid-guiding means, e.g. diffusers adjustable especially adapted for elastic fluid pumps adjusting flow cross-section, otherwise than by using adjustable stator blades
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/40Casings; Connections of working fluid
    • F04D29/42Casings; Connections of working fluid for radial or helico-centrifugal pumps
    • F04D29/44Fluid-guiding means, e.g. diffusers
    • F04D29/46Fluid-guiding means, e.g. diffusers adjustable
    • F04D29/462Fluid-guiding means, e.g. diffusers adjustable especially adapted for elastic fluid pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00Geometry
    • F05D2250/50Inlet or outlet
    • F05D2250/52Outlet

Landscapes

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

Abstract

305,214. Soc. Rateau. Feb. 2, 1928, [Convention date]. Void [Published. under Sect. 91 of the Acts]. Regulating or controlling; casings.-A centrifugal fan or pump is controlled by the introduction of a ring member into the diffuser, the member being displaced in a direction parallel to the axis. In the form shown in Fig. 1, the rotor a delivers fluid to the volute b through the diffuser c. A vane ring d can be inserted into, or withdrawn from the diffuser according to the conditions of pressure and output required. Pipes h, f connected to the volute and rotor chamber respectively, may be connected by a cock i to a tube g. With the tubes h, g in connection, as shown, the vane ring d is moved to position in the diffuser, whilst when the tubes f, g are in connection the ring d is moved out of the diffuser which is then vaneless. The ring may be mounted on helicoidal slides to promote even movement. Two vaned rings may be employed, a ring being mounted on each side of the machine, the vanes of the rings being adapted for different running conditions. In a modification, two combined rings d<1>, d<2>, Fig. 5, with vanes of different pitch, can be brought into position in the diffuser by means of a number of screws j. In another modification the ring d, Fig. 6, is left in the diffuser and the delivery is modified by moving the cheek k by means of the screw j to vary the effective width of the vanes. In another modification the vane block d, Fig. 7, can be retracted from the diffuser, and the cheek k can be moved to vary the distance between the diffuser walls. The arrangement may be applied to multi-stage machines.
GB3019/29A 1928-02-02 1929-01-29 Improvements in or relating to means for controlling the running of centrifugal machines Expired GB305214A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
BE305214X 1928-02-02

Publications (1)

Publication Number Publication Date
GB305214A true GB305214A (en) 1929-10-31

Family

ID=3867467

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3019/29A Expired GB305214A (en) 1928-02-02 1929-01-29 Improvements in or relating to means for controlling the running of centrifugal machines

Country Status (1)

Country Link
GB (1) GB305214A (en)

Cited By (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2519151A (en) * 1944-08-16 1950-08-15 Machf Gebr Stork & Co N V Centrifugal fan or centrifugal pump for two directions of rotation
US2739782A (en) * 1952-10-07 1956-03-27 Fairchild Engine & Airplane Variable area turbine nozzle
DE1011671B (en) * 1953-04-24 1957-07-04 Power Jets Res & Dev Ltd Radial turbo machine with adjustable nozzle
US2803396A (en) * 1954-09-29 1957-08-20 Gen Electric Compressor
US2814431A (en) * 1954-09-29 1957-11-26 Gen Electric Compressor
DE1034192B (en) * 1953-10-22 1958-07-17 Sncf Device for regulating turbomachinery with a substantially radial flow by means of an axially movable wall of the flow paths
US2976013A (en) * 1955-08-17 1961-03-21 Fairchild Engine & Airplane Turbine construction
US3032259A (en) * 1957-12-23 1962-05-01 Sulzer Ag Turbocompressor having a radial diffuser
US3236500A (en) * 1961-12-09 1966-02-22 Geratebau Eberspacher Ohg Turbine
US3426964A (en) * 1966-10-11 1969-02-11 Dresser Ind Compressor apparatus
US3489391A (en) * 1967-02-02 1970-01-13 Dominion Eng Works Ltd Hydraulic ring gate force balancing
US3695367A (en) * 1970-06-08 1972-10-03 North American Rockwell Hydraulic power tool
US3749513A (en) * 1970-09-22 1973-07-31 Eaton Corp Fluid turbomotor
US4219305A (en) * 1978-12-26 1980-08-26 Carrier Corporation Diffuser control
US4257733A (en) * 1978-12-26 1981-03-24 Carrier Corporation Diffuser control
EP0099847A1 (en) * 1982-06-28 1984-02-01 Carrier Corporation Diffuser throttle ring control
US4499732A (en) * 1981-11-14 1985-02-19 Holset Engineering Company Limited Turbocharger having a variable inlet area turbine
EP0134748A2 (en) * 1983-09-12 1985-03-20 Carrier Corporation Variable width diffuser
EP0148101A1 (en) * 1983-12-19 1985-07-10 Carrier Corporation Method and apparatus for the control of a centrifugal compressor
US4802817A (en) * 1987-12-23 1989-02-07 Sundstrand Corporation Centrifugal pump with self-regulating impeller discharge shutter
GB2234295A (en) * 1989-07-21 1991-01-30 Rolls Royce Plc Gas turbine engine compressor assembly
EP1260676A1 (en) * 2001-05-25 2002-11-27 Iveco Motorenforschung AG Device for controlling a variable inlet nozzle of a turbine
US6726447B2 (en) 2001-05-25 2004-04-27 Iveco Motorenforschung Ag Variable geometry turbine
WO2011141425A1 (en) * 2010-05-12 2011-11-17 Siemens Aktiengesellschaft Adjustable radial compressor diffuser
US20150240655A1 (en) * 2014-02-25 2015-08-27 Fluid Equipment Development Company, Llc Method and system for varying the width of a turbine nozzle
JP2017508100A (en) * 2014-03-12 2017-03-23 グリー エレクトリック アプライアンスィズ,インコーポレーテッド オブ ジュハイ Centrifugal compressor and centrifuge unit provided with the same
US10527059B2 (en) 2013-10-21 2020-01-07 Williams International Co., L.L.C. Turbomachine diffuser

Cited By (35)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2519151A (en) * 1944-08-16 1950-08-15 Machf Gebr Stork & Co N V Centrifugal fan or centrifugal pump for two directions of rotation
US2739782A (en) * 1952-10-07 1956-03-27 Fairchild Engine & Airplane Variable area turbine nozzle
DE1011671B (en) * 1953-04-24 1957-07-04 Power Jets Res & Dev Ltd Radial turbo machine with adjustable nozzle
DE1034192B (en) * 1953-10-22 1958-07-17 Sncf Device for regulating turbomachinery with a substantially radial flow by means of an axially movable wall of the flow paths
US2803396A (en) * 1954-09-29 1957-08-20 Gen Electric Compressor
US2814431A (en) * 1954-09-29 1957-11-26 Gen Electric Compressor
US2976013A (en) * 1955-08-17 1961-03-21 Fairchild Engine & Airplane Turbine construction
US3032259A (en) * 1957-12-23 1962-05-01 Sulzer Ag Turbocompressor having a radial diffuser
US3236500A (en) * 1961-12-09 1966-02-22 Geratebau Eberspacher Ohg Turbine
US3426964A (en) * 1966-10-11 1969-02-11 Dresser Ind Compressor apparatus
US3489391A (en) * 1967-02-02 1970-01-13 Dominion Eng Works Ltd Hydraulic ring gate force balancing
US3695367A (en) * 1970-06-08 1972-10-03 North American Rockwell Hydraulic power tool
US3749513A (en) * 1970-09-22 1973-07-31 Eaton Corp Fluid turbomotor
US4219305A (en) * 1978-12-26 1980-08-26 Carrier Corporation Diffuser control
US4257733A (en) * 1978-12-26 1981-03-24 Carrier Corporation Diffuser control
US4499732A (en) * 1981-11-14 1985-02-19 Holset Engineering Company Limited Turbocharger having a variable inlet area turbine
US4460310A (en) * 1982-06-28 1984-07-17 Carrier Corporation Diffuser throttle ring control
EP0099847A1 (en) * 1982-06-28 1984-02-01 Carrier Corporation Diffuser throttle ring control
EP0134748A2 (en) * 1983-09-12 1985-03-20 Carrier Corporation Variable width diffuser
EP0134748A3 (en) * 1983-09-12 1985-07-03 Carrier Corporation Variable width diffuser
EP0148101A1 (en) * 1983-12-19 1985-07-10 Carrier Corporation Method and apparatus for the control of a centrifugal compressor
US4802817A (en) * 1987-12-23 1989-02-07 Sundstrand Corporation Centrifugal pump with self-regulating impeller discharge shutter
GB2234295A (en) * 1989-07-21 1991-01-30 Rolls Royce Plc Gas turbine engine compressor assembly
US5059091A (en) * 1989-07-21 1991-10-22 Rolls-Royce Plc Gas turbine engine compressor assembly
GB2234295B (en) * 1989-07-21 1993-07-21 Rolls Royce Plc Gas turbine engine compressor assembly
EP1260676A1 (en) * 2001-05-25 2002-11-27 Iveco Motorenforschung AG Device for controlling a variable inlet nozzle of a turbine
US6726447B2 (en) 2001-05-25 2004-04-27 Iveco Motorenforschung Ag Variable geometry turbine
US6810666B2 (en) 2001-05-25 2004-11-02 Iveco Motorenforschung Ag Variable geometry turbine
WO2011141425A1 (en) * 2010-05-12 2011-11-17 Siemens Aktiengesellschaft Adjustable radial compressor diffuser
US10527059B2 (en) 2013-10-21 2020-01-07 Williams International Co., L.L.C. Turbomachine diffuser
US20150240655A1 (en) * 2014-02-25 2015-08-27 Fluid Equipment Development Company, Llc Method and system for varying the width of a turbine nozzle
US9845701B2 (en) * 2014-02-25 2017-12-19 Fluid Equipment Development Company, Llc Method and system for varying the width of a turbine nozzle
JP2017508100A (en) * 2014-03-12 2017-03-23 グリー エレクトリック アプライアンスィズ,インコーポレーテッド オブ ジュハイ Centrifugal compressor and centrifuge unit provided with the same
EP3118462A4 (en) * 2014-03-12 2017-11-08 Gree Electric Appliances, Inc. of Zhuhai Centrifugal compressor and centrifugal facility having same
US10323653B2 (en) 2014-03-12 2019-06-18 Gree Electric Appliances, Inc. Of Zhuhai Centrifugal compressor and centrifugal unit having the same

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