BR0010110A - Sistema turbocompressor de geometria variável para utilização em um motor de combustão interna, e, processo para controlar um sistema de turbocompressão de geometria variável - Google Patents

Sistema turbocompressor de geometria variável para utilização em um motor de combustão interna, e, processo para controlar um sistema de turbocompressão de geometria variável

Info

Publication number
BR0010110A
BR0010110A BR0010110-9A BR0010110A BR0010110A BR 0010110 A BR0010110 A BR 0010110A BR 0010110 A BR0010110 A BR 0010110A BR 0010110 A BR0010110 A BR 0010110A
Authority
BR
Brazil
Prior art keywords
variable geometry
turbocharger system
geometry turbocharger
combustion engine
internal combustion
Prior art date
Application number
BR0010110-9A
Other languages
English (en)
Inventor
Craig R Markyvech
Joseph A Williamson
Kyle G Wick
Paul L Powell Iii
Original Assignee
Detroit Diesel 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 Detroit Diesel Corp filed Critical Detroit Diesel Corp
Publication of BR0010110A publication Critical patent/BR0010110A/pt

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02D—CONTROLLING COMBUSTION ENGINES
    • F02D41/00—Electrical control of supply of combustible mixture or its constituents
    • F02D41/0002—Controlling intake air
    • F02D41/0007—Controlling intake air for control of turbo-charged or super-charged engines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02D—CONTROLLING COMBUSTION ENGINES
    • F02D23/00—Controlling engines characterised by their being supercharged
    • 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
    • F02B37/24—Control of the pumps by using pumps or turbines with adjustable guide vanes
    • 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)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)

Abstract

"SISTEMA TURBOCOMPRESSOR DE GEOMETRIA VARIàVEL PARA UTILIZAçâO EM UM MOTOR DE COMBUSTãO INTERNA, E, PROCESSO PARA CONTROLAR UM SISTEMA DE TURBOCOMPRESSãO DE GEOMETRIA VARIáVEL". Um sistema de turbocompressão de geometria variável 70, para utilização em um motor de combustão interna, utiliza um conjunto de bobina fónica 110. O conjunto de bobina fónica 110 inclui um campo 116 e uma armadura 140. O conjunto de bobina fónica 110 pode é atuado para mover a armadura 140 em relação ao campo 116 e é conectado ao turbocompressor 112 de modo que aquele movimento da armadura 140 em relação ao campo 116 muda a geometria do turbocompressor 112. Um transdutor resistivo linear 152 é fornecido para realimentação da posição da armadura.
BR0010110-9A 1999-04-28 2000-03-27 Sistema turbocompressor de geometria variável para utilização em um motor de combustão interna, e, processo para controlar um sistema de turbocompressão de geometria variável BR0010110A (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/301,189 US6134889A (en) 1999-04-28 1999-04-28 Variable geometry turbocharging system and method
PCT/US2000/008066 WO2000065216A1 (en) 1999-04-28 2000-03-27 Variable geometry turbocharging system and method

Publications (1)

Publication Number Publication Date
BR0010110A true BR0010110A (pt) 2002-02-19

Family

ID=23162331

Family Applications (1)

Application Number Title Priority Date Filing Date
BR0010110-9A BR0010110A (pt) 1999-04-28 2000-03-27 Sistema turbocompressor de geometria variável para utilização em um motor de combustão interna, e, processo para controlar um sistema de turbocompressão de geometria variável

Country Status (9)

Country Link
US (1) US6134889A (pt)
EP (1) EP1180209A4 (pt)
JP (1) JP2002543325A (pt)
KR (1) KR20020005018A (pt)
AU (1) AU767987B2 (pt)
BR (1) BR0010110A (pt)
CA (1) CA2367768A1 (pt)
MX (1) MXPA01010334A (pt)
WO (1) WO2000065216A1 (pt)

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Also Published As

Publication number Publication date
US6134889A (en) 2000-10-24
WO2000065216A1 (en) 2000-11-02
AU767987B2 (en) 2003-11-27
JP2002543325A (ja) 2002-12-17
CA2367768A1 (en) 2000-11-02
MXPA01010334A (es) 2002-03-27
EP1180209A1 (en) 2002-02-20
KR20020005018A (ko) 2002-01-16
AU4033300A (en) 2000-11-10
EP1180209A4 (en) 2009-05-06

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Legal Events

Date Code Title Description
FA10 Dismissal: dismissal - article 33 of industrial property law
B11Y Definitive dismissal - extension of time limit for request of examination expired [chapter 11.1.1 patent gazette]