ES435685A1 - Pre-whirl turbo charger apparatus - Google Patents

Pre-whirl turbo charger apparatus

Info

Publication number
ES435685A1
ES435685A1 ES435685A ES435685A ES435685A1 ES 435685 A1 ES435685 A1 ES 435685A1 ES 435685 A ES435685 A ES 435685A ES 435685 A ES435685 A ES 435685A ES 435685 A1 ES435685 A1 ES 435685A1
Authority
ES
Spain
Prior art keywords
compressor
whirl
velocity
turbo charger
air entering
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
ES435685A
Other languages
Spanish (es)
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.)
Wallace Murray Corp
Original Assignee
Wallace Murray Corp
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 Wallace Murray Corp filed Critical Wallace Murray Corp
Publication of ES435685A1 publication Critical patent/ES435685A1/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B37/00—Engines characterised by provision of pumps driven at least for part of the time by exhaust
    • F02B37/12—Control of the pumps
    • F02B37/22—Control of the pumps by varying cross-section of exhaust passages or air passages, e.g. by throttling turbine inlets or outlets or by varying effective number of guide conduits
    • F02B37/225—Control of the pumps by varying cross-section of exhaust passages or air passages, e.g. by throttling turbine inlets or outlets or by varying effective number of guide conduits air passages
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/40—Casings; Connections of working fluid
    • F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
    • F04D29/4206—Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps
    • F04D29/4213—Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps suction ports
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/40—Casings; Connections of working fluid
    • F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
    • F04D29/44—Fluid-guiding means, e.g. diffusers
    • F04D29/46—Fluid-guiding means, e.g. diffusers adjustable
    • F04D29/462—Fluid-guiding means, e.g. diffusers adjustable especially adapted for elastic fluid pumps
    • F04D29/464—Fluid-guiding means, e.g. diffusers adjustable especially adapted for elastic fluid pumps adjusting flow cross-section, otherwise than by using adjustable stator blades
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/50—Inlet or outlet
    • F05D2250/51—Inlet
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/14—Preswirling
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/10—Internal combustion engine [ICE] based vehicles
    • Y02T10/12—Improving ICE efficiencies

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Supercharger (AREA)
  • Control Of Positive-Displacement Air Blowers (AREA)

Abstract

A prewhirl construction for the compressor of a turbocharger. The periphery of the compressor input opening is provided with a plurality of slanted spin vanes which impart a tangential velocity to air entering the compressor. The air is thus provided with a velocity component similar to the compressor's impeller velocity. The input duct to the compressor carries a butterfly valve whose setting controls the amount of air entering through the peripheral spin vanes. The operating surge line is moved so as to increase the flow range of the compressor.
ES435685A 1974-03-18 1975-03-17 Pre-whirl turbo charger apparatus Expired ES435685A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US452369A US3922108A (en) 1974-03-18 1974-03-18 Pre-whirl turbo charger apparatus

Publications (1)

Publication Number Publication Date
ES435685A1 true ES435685A1 (en) 1977-01-16

Family

ID=23796198

Family Applications (1)

Application Number Title Priority Date Filing Date
ES435685A Expired ES435685A1 (en) 1974-03-18 1975-03-17 Pre-whirl turbo charger apparatus

Country Status (10)

Country Link
US (1) US3922108A (en)
JP (1) JPS5812479B2 (en)
BR (1) BR7500109D0 (en)
CA (1) CA1025829A (en)
DE (1) DE2500496A1 (en)
ES (1) ES435685A1 (en)
FR (1) FR2264995A1 (en)
GB (1) GB1480871A (en)
IT (1) IT1033365B (en)
SE (1) SE7500233L (en)

Families Citing this family (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL8105790A (en) * 1981-12-22 1983-07-18 Thomassen Holland Bv METHOD FOR IMPROVING THE PARTIAL LOAD BEHAVIOR OF A FLOWING MACHINE, COMPRESSOR OR PUMP ORIENTED FOR APPLYING THIS METHOD
JPS58169118U (en) * 1982-05-08 1983-11-11 株式会社クボタ supercharger
SE451873B (en) * 1982-07-29 1987-11-02 Do G Pk I Experiment AXIALFLEKT
JPS6078484U (en) * 1983-10-31 1985-05-31 白井　修 Removable binding device
SE445061B (en) * 1984-10-10 1986-05-26 Do Politekh Inst FLEET WITH DEVICE FOR ROTATING THE AIR FLOW INCOMING
DE3502648A1 (en) * 1985-01-26 1986-07-31 Carl Prof. Dr.-Ing. 5100 Aachen Kramer DEVICE FOR MIXING A MAIN GAS FLOW WITH AT LEAST ONE SUB GAS FLOW
DE3529281C1 (en) * 1985-08-16 1986-09-11 Daimler-Benz Ag, 7000 Stuttgart Device for changing the direction of an air flow entering through the inlet of a compressor of an exhaust gas turbocharger of an internal combustion engine
US4832642A (en) * 1985-10-08 1989-05-23 Thompson Marine Propulsion Systems, Inc. Outboard boat propulsion installation
GB2224076A (en) * 1988-08-03 1990-04-25 Atomic Energy Authority Uk Controlling pumps
US5266003A (en) * 1992-05-20 1993-11-30 Praxair Technology, Inc. Compressor collector with nonuniform cross section
DE19514707A1 (en) * 1995-04-21 1996-10-24 Johannes Werner Flow guide unit for radial compressor
BE1012901A3 (en) * 1999-09-15 2001-05-08 Atlas Copco Airpower Nv METHOD FOR CONTROLLING THE FLOW IN A PIPE FOR GAS-FLUID AND PIPE PROVIDED WITH A FLOW CONTROL.
GB2391265A (en) * 2002-07-13 2004-02-04 Imra Europ S A Uk Res Ct Compressor inlet with swirl vanes, inner sleeve and shut-off valve
DE102004039299A1 (en) * 2004-08-13 2006-02-23 Fev Motorentechnik Gmbh Turbo compressor for internal combustion engine, has adjustable inlet turning device provided in area of compressor inlet, where inlet turning device has load-controlled device for tangential supply of intake air to compressor wheel
FR2878914B1 (en) * 2004-12-03 2010-09-03 Inst Francais Du Petrole AIR COMPRESSOR, ESPECIALLY FOR AN INTERNAL COMBUSTION ENGINE, INCLUDING AN ADJUSTED AIR ROTATION CHAMBER
DE102005023647B4 (en) * 2005-05-21 2014-09-04 Daimler Ag Exhaust gas turbocharger with a compressor
DE102007047506A1 (en) * 2007-10-04 2008-10-23 Voith Patent Gmbh Method for creating swirl-affected flow of medium entails first partial flow being created with first swirl, second partial flow being created, and two partial flows being brought together and fed to turbomachine
DE102007058615A1 (en) * 2007-12-04 2009-06-10 Daimler Ag Exhaust gas turbocharger for an internal combustion engine and device for switching an air guide device of an exhaust gas turbocharger
JP5451247B2 (en) 2008-09-10 2014-03-26 ボーグワーナー インコーポレーテッド Turbocharger connection for reverse rotation of passive pre-turn
JP2010168916A (en) * 2009-01-20 2010-08-05 Otics Corp Compressor for supercharger
US8950183B2 (en) * 2012-09-10 2015-02-10 Caterpillar Inc. Engine system having intake conduit with surge inhibitor and method
JP6109291B2 (en) * 2013-02-22 2017-04-05 三菱重工業株式会社 Centrifugal compressor
WO2016181427A1 (en) * 2015-05-14 2016-11-17 日産ライトトラック株式会社 Compressed air production device, and turbocharger and internal combustion engine equipped with same
US20170284407A1 (en) * 2016-03-29 2017-10-05 Michael Xuwang Cao Automatic Inlet Swirl Device for Turbomachinery
US9932991B2 (en) 2016-04-04 2018-04-03 Ford Global Technologies, Llc Active swirl device for turbocharger compressor
US11207628B2 (en) 2018-09-27 2021-12-28 Noram Engineering And Constructors Ltd. Processes and devices for separating entrainment from sulphuric acid plant process gas
US11208971B2 (en) * 2019-01-16 2021-12-28 Ford Global Technologies, Llc Methods and systems for mitigating condensate formation
CN114026336B (en) * 2019-07-23 2024-11-12 E·C·门德勒 Hybrid Electric Turbocharger
CN111503059B (en) * 2020-04-10 2022-01-25 上海交通大学 Inlet airflow pulsation adjusting device of centrifugal compressor
CN113217464B (en) * 2021-03-31 2022-08-19 江苏科技大学 Combined type compressor casing structure

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1517329A (en) * 1921-08-29 1924-12-02 Weiss Leo Centrifugal fan or blower
US2140148A (en) * 1935-10-30 1938-12-13 Davidson & Co Ltd Control of centrifugal fans, pumps, and the like
US2405282A (en) * 1938-02-02 1946-08-06 Fed Reserve Bank Variable ratio compressor
US2336010A (en) * 1942-09-17 1943-12-07 Fairchild Engine & Airplane Supercharger
US2690293A (en) * 1951-01-20 1954-09-28 Westinghouse Electric Corp Fan
US2798658A (en) * 1955-03-01 1957-07-09 Westinghouse Electric Corp Volume controls for centrifugal fans
US3672786A (en) * 1970-11-02 1972-06-27 Carrier Corp Capacity control mechanism for centrifugal gas compressors

Also Published As

Publication number Publication date
JPS50125116A (en) 1975-10-01
CA1025829A (en) 1978-02-07
JPS5812479B2 (en) 1983-03-08
US3922108A (en) 1975-11-25
SE7500233L (en) 1975-09-19
BR7500109D0 (en) 1975-12-16
DE2500496A1 (en) 1975-09-25
GB1480871A (en) 1977-07-27
FR2264995A1 (en) 1975-10-17
IT1033365B (en) 1979-07-10

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