EP1433958A3 - Upstream stator for turbomachine - Google Patents

Upstream stator for turbomachine Download PDF

Info

Publication number
EP1433958A3
EP1433958A3 EP03016559A EP03016559A EP1433958A3 EP 1433958 A3 EP1433958 A3 EP 1433958A3 EP 03016559 A EP03016559 A EP 03016559A EP 03016559 A EP03016559 A EP 03016559A EP 1433958 A3 EP1433958 A3 EP 1433958A3
Authority
EP
European Patent Office
Prior art keywords
turbomachine
guide vanes
inlet guide
upstream stator
vorleitstator
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.)
Withdrawn
Application number
EP03016559A
Other languages
German (de)
French (fr)
Other versions
EP1433958A2 (en
Inventor
Michael Bauerle
Gunter Winkler
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.)
Robert Bosch GmbH
Original Assignee
Robert Bosch 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 Robert Bosch GmbH filed Critical Robert Bosch GmbH
Publication of EP1433958A2 publication Critical patent/EP1433958A2/en
Publication of EP1433958A3 publication Critical patent/EP1433958A3/en
Withdrawn legal-status Critical Current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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D27/00Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
    • F04D27/02Surge control
    • F04D27/0246Surge control by varying geometry within the pumps, e.g. by adjusting vanes
    • 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
    • F04D29/4206Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps
    • F04D29/4213Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps suction ports
    • 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
    • F05D2250/51Inlet

Landscapes

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

Abstract

Die Erfindung betrifft einen Vorleitstator (10) für Strömungsmaschinen, insbesondere für Turboverdichter (12), mit mehreren im Anströmbereich eines Verdichterrads (14) angeordneten Eintrittsleitschaufeln (16), deren drallerzeugender Schaufelwinkel in Abhängigkeit eines Fluidvolumenstroms durch die Strömungsmaschine bzw. durch den Turboverdichter (10) verstellbar ist.The invention relates to a Vorleitstator (10) for Turbomachines, in particular for turbocompressors (12), with several in the inflow region of a compressor wheel (14) arranged inlet guide vanes (16) whose swirl-producing blade angle in Dependence of a fluid volume flow through the Turbomachine or through the turbo compressor (10) is adjustable.

Es ist vorgesehen, dass die Eintrittsleitschaufeln (16) sich bei verändernden Strömungsverhältnissen verformen.

Figure 00000001
It is envisaged that the inlet guide vanes (16) deform with changing flow conditions.
Figure 00000001

EP03016559A 2002-12-23 2003-07-24 Upstream stator for turbomachine Withdrawn EP1433958A3 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE10261789 2002-12-23
DE10261789A DE10261789A1 (en) 2002-12-23 2002-12-23 Vorleitstator for flow machines

Publications (2)

Publication Number Publication Date
EP1433958A2 EP1433958A2 (en) 2004-06-30
EP1433958A3 true EP1433958A3 (en) 2005-01-12

Family

ID=32404395

Family Applications (1)

Application Number Title Priority Date Filing Date
EP03016559A Withdrawn EP1433958A3 (en) 2002-12-23 2003-07-24 Upstream stator for turbomachine

Country Status (2)

Country Link
EP (1) EP1433958A3 (en)
DE (1) DE10261789A1 (en)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
DE102005017975A1 (en) * 2005-04-19 2006-11-02 Audi Ag Radial compressor arrangement for supercharger, has spiral guide vanes formed within housing to guide fluid medium flow with minimal effect on its high flow rates or high volume throughputs
EP1719887A1 (en) * 2005-05-04 2006-11-08 ABB Turbo Systems AG Charging control of a combustion engine
DE102005045194B4 (en) * 2005-09-21 2016-06-09 Fev Gmbh Guide for a turbo compressor of an internal combustion engine
DE102006058071A1 (en) 2006-05-19 2007-11-29 Mahle International Gmbh Fresh gas system
DE102008046220A1 (en) 2008-09-08 2010-03-11 Bosch Mahle Turbo Systems Gmbh & Co. Kg Swirl producing device for use in exhaust gas turbocharger in internal-combustion engine of motor vehicle, has guide vane movably arranged with respect to vane length that extends in radial and/or transverse directions in flow channel
DE102008052256A1 (en) 2008-10-18 2010-04-22 Volkswagen Ag Exhaust-gas turbocharger for internal combustion engine, particularly motor vehicle, has turbine and compressor, where switchable device is provided in intake port, which covers predetermined surface of intake air flow cross-section
DE102009014279A1 (en) 2009-03-20 2010-09-23 Bosch Mahle Turbo Systems Gmbh & Co. Kg Spin generator for spin impinged inflow of compressor impeller of loading device, particularly exhaust gas turbocharger for internal combustion engine, has multiple guide blades arranged in flow channel in periphery direction
FR2950105B1 (en) * 2009-09-14 2013-07-05 Coutier Moulage Gen Ind TOURBILLONARY SYSTEM FOR AIR CONDUIT
US8651800B2 (en) * 2010-06-04 2014-02-18 Gm Global Technology Operations Llp Induction system with air flow rotation and noise absorber for turbocharger applications
DE102013007333A1 (en) * 2013-04-27 2014-10-30 Volkswagen Ag Compressor of a charging device of an internal combustion engine and method for operating a compressor of a charging device of an internal combustion engine
CN217107202U (en) 2020-09-23 2022-08-02 博格华纳公司 Compressor assembly and turbocharger for vehicle

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3723021A (en) * 1971-01-28 1973-03-27 Caterpillar Tractor Co Flexible airfoil for compressor
DE3817839A1 (en) * 1988-05-26 1989-12-07 Audi Ag Device for imparting a swirl effect to the inflow regions of fluid flow machines
DE19955510C1 (en) * 1999-11-18 2000-09-21 Daimler Chrysler Ag Exhaust gas turbo charger has a radial compressor with air guide paddles which swing on a radial axis against a torsion spring to reduce the twist in the air flow on an increased mass flow

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3723021A (en) * 1971-01-28 1973-03-27 Caterpillar Tractor Co Flexible airfoil for compressor
DE3817839A1 (en) * 1988-05-26 1989-12-07 Audi Ag Device for imparting a swirl effect to the inflow regions of fluid flow machines
DE19955510C1 (en) * 1999-11-18 2000-09-21 Daimler Chrysler Ag Exhaust gas turbo charger has a radial compressor with air guide paddles which swing on a radial axis against a torsion spring to reduce the twist in the air flow on an increased mass flow

Also Published As

Publication number Publication date
DE10261789A1 (en) 2004-07-08
EP1433958A2 (en) 2004-06-30

Similar Documents

Publication Publication Date Title
DE10250302B4 (en) Swirl generating device for a compressor
EP1433958A3 (en) Upstream stator for turbomachine
EP1362984A3 (en) Gas turbine engine
EP1726814A3 (en) Jet engine
JP5451247B2 (en) Turbocharger connection for reverse rotation of passive pre-turn
US8550775B2 (en) Compressor
EP2518272A3 (en) High area ratio turbine vane
EP1270873A3 (en) Gas turbine blade
EP1643134A3 (en) Cooling fan
EP1688603A3 (en) Gas turbine engine assembly
EP2685065A3 (en) A gas turbine engine
JP5351941B2 (en) Centrifugal compressor, its impeller, its operating method, and impeller design method
EP1112928A3 (en) Airfoil with performance enhancing trailing edge
WO2007051444A3 (en) Multistage compressor for a gas turbine, comprising discharge ports and injection ports to stabilize the compressor flow
EP1621733A3 (en) Flow device for a gas turbine
EP1253295A3 (en) Axial-flow turbine having a stepped portion in a flow passage
EP1990544A3 (en) Multistage centrifugal compressor
EP1632648A3 (en) Gas turbine flow path
EP1707744A3 (en) Stator vane with inner and outer shroud
EP1522679A3 (en) Guide vanes for turbine
EP1722080A3 (en) Internal combustion engine and method of operation thereof
EP1936203A3 (en) Vacuum pump with ventilator
EP1591624A1 (en) Compressor blade and compressor.
KR102346583B1 (en) Discharge region of a turbocharger turbine
ATE512296T1 (en) EXHAUST TURBOCHARGER FOR AN INTERNAL COMBUSTION ENGINE

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

AK Designated contracting states

Kind code of ref document: A2

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LI LU MC NL PT RO SE SI SK TR

AX Request for extension of the european patent

Extension state: AL LT LV MK

PUAL Search report despatched

Free format text: ORIGINAL CODE: 0009013

AK Designated contracting states

Kind code of ref document: A3

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LI LU MC NL PT RO SE SI SK TR

AX Request for extension of the european patent

Extension state: AL LT LV MK

17P Request for examination filed

Effective date: 20050712

AKX Designation fees paid

Designated state(s): DE ES FR GB

17Q First examination report despatched

Effective date: 20071227

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN

18D Application deemed to be withdrawn

Effective date: 20160202