ATA18462000A - EXHAUST TURBOCHARGER FOR AN INTERNAL COMBUSTION ENGINE - Google Patents

EXHAUST TURBOCHARGER FOR AN INTERNAL COMBUSTION ENGINE

Info

Publication number
ATA18462000A
ATA18462000A AT18462000A AT18462000A ATA18462000A AT A18462000 A ATA18462000 A AT A18462000A AT 18462000 A AT18462000 A AT 18462000A AT 18462000 A AT18462000 A AT 18462000A AT A18462000 A ATA18462000 A AT A18462000A
Authority
AT
Austria
Prior art keywords
combustion engine
internal combustion
exhaust turbocharger
turbocharger
exhaust
Prior art date
Application number
AT18462000A
Other languages
German (de)
Other versions
AT410697B (en
Inventor
Otto Ing Blank
Original Assignee
Otto Ing Blank
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 Otto Ing Blank filed Critical Otto Ing Blank
Priority to AT18462000A priority Critical patent/AT410697B/en
Priority to AT01890300T priority patent/ATE312274T1/en
Priority to EP20010890300 priority patent/EP1201881B1/en
Priority to DE50108296T priority patent/DE50108296D1/en
Publication of ATA18462000A publication Critical patent/ATA18462000A/en
Application granted granted Critical
Publication of AT410697B publication Critical patent/AT410697B/en

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/12—Final actuators arranged in stator parts
    • F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • F01D17/165—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes for radial flow, i.e. the vanes turning around axes which are essentially parallel to the rotor centre line
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/12—Final actuators arranged in stator parts
    • F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/12—Final actuators arranged in stator parts
    • F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/146—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by throttling the volute inlet of radial machines or engines
    • 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
    • F05D2220/00—Application
    • F05D2220/40—Application in turbochargers

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
AT18462000A 2000-10-31 2000-10-31 Exhaust gas turbo charger, for an IC motor, has structured flow paths in the spiral housing with groups of jets aligned at the turbine wheel for a high power at slow running speeds and a rapid response AT410697B (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
AT18462000A AT410697B (en) 2000-10-31 2000-10-31 Exhaust gas turbo charger, for an IC motor, has structured flow paths in the spiral housing with groups of jets aligned at the turbine wheel for a high power at slow running speeds and a rapid response
AT01890300T ATE312274T1 (en) 2000-10-31 2001-10-25 EXHAUST TURBOCHARGER
EP20010890300 EP1201881B1 (en) 2000-10-31 2001-10-25 Turbocharger
DE50108296T DE50108296D1 (en) 2000-10-31 2001-10-25 turbocharger

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
AT18462000A AT410697B (en) 2000-10-31 2000-10-31 Exhaust gas turbo charger, for an IC motor, has structured flow paths in the spiral housing with groups of jets aligned at the turbine wheel for a high power at slow running speeds and a rapid response

Publications (2)

Publication Number Publication Date
ATA18462000A true ATA18462000A (en) 2002-11-15
AT410697B AT410697B (en) 2003-06-25

Family

ID=3689112

Family Applications (1)

Application Number Title Priority Date Filing Date
AT18462000A AT410697B (en) 2000-10-31 2000-10-31 Exhaust gas turbo charger, for an IC motor, has structured flow paths in the spiral housing with groups of jets aligned at the turbine wheel for a high power at slow running speeds and a rapid response

Country Status (1)

Country Link
AT (1) AT410697B (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7644585B2 (en) * 2004-08-31 2010-01-12 The United States Of America As Represented By The Administrator Of The U.S. Environmental Protection Agency Multi-stage turbocharging system with efficient bypass
US20090000296A1 (en) * 2007-06-29 2009-01-01 David Andrew Pierpont Turbocharger having divided housing with integral valve

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4512714A (en) * 1982-02-16 1985-04-23 Deere & Company Variable flow turbine
JPS61215424A (en) * 1985-03-19 1986-09-25 Mazda Motor Corp Exhaust turbosupercharger
JPH01227803A (en) * 1988-03-08 1989-09-12 Honda Motor Co Ltd Variable capacity turbine
DE4242494C1 (en) * 1992-12-16 1993-09-09 Mercedes-Benz Aktiengesellschaft, 70327 Stuttgart, De Adjustable flow-guide for engine exhaust turbocharger - has axially-adjustable annular insert in sectors forming different kinds of guide grilles supplied simultaneously by spiral passages
JP3725287B2 (en) * 1996-04-25 2005-12-07 アイシン精機株式会社 Variable capacity turbocharger

Also Published As

Publication number Publication date
AT410697B (en) 2003-06-25

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Legal Events

Date Code Title Description
ELJ Ceased due to non-payment of the annual fee