MX2007015633A - Control del turboalimentador basado en modelos. - Google Patents

Control del turboalimentador basado en modelos.

Info

Publication number
MX2007015633A
MX2007015633A MX2007015633A MX2007015633A MX2007015633A MX 2007015633 A MX2007015633 A MX 2007015633A MX 2007015633 A MX2007015633 A MX 2007015633A MX 2007015633 A MX2007015633 A MX 2007015633A MX 2007015633 A MX2007015633 A MX 2007015633A
Authority
MX
Mexico
Prior art keywords
stage
compressor stage
pressure compressor
pressure
pressure turbine
Prior art date
Application number
MX2007015633A
Other languages
English (en)
Inventor
William De Ojeda
Original Assignee
Int Engine Intellectual Prop
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 Int Engine Intellectual Prop filed Critical Int Engine Intellectual Prop
Publication of MX2007015633A publication Critical patent/MX2007015633A/es

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B37/00Engines characterised by provision of pumps driven at least for part of the time by exhaust
    • F02B37/12Control of the pumps
    • F02B37/24Control of the pumps by using pumps or turbines with adjustable guide vanes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B37/00Engines characterised by provision of pumps driven at least for part of the time by exhaust
    • F02B37/013Engines characterised by provision of pumps driven at least for part of the time by exhaust with exhaust-driven pumps arranged in series
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B37/00Engines characterised by provision of pumps driven at least for part of the time by exhaust
    • F02B37/004Engines characterised by provision of pumps driven at least for part of the time by exhaust with exhaust drives arranged in series
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B37/00Engines characterised by provision of pumps driven at least for part of the time by exhaust
    • F02B37/12Control of the pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B37/00Engines characterised by provision of pumps driven at least for part of the time by exhaust
    • F02B37/12Control of the pumps
    • F02B37/16Control of the pumps by bypassing charging air
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B37/00Engines characterised by provision of pumps driven at least for part of the time by exhaust
    • F02B37/12Control of the pumps
    • F02B37/18Control of the pumps by bypassing exhaust from the inlet to the outlet of turbine or to the atmosphere
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B39/00Component parts, details, or accessories relating to, driven charging or scavenging pumps, not provided for in groups F02B33/00 - F02B37/00
    • F02B39/16Other safety measures for, or other control of, pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D23/00Controlling engines characterised by their being supercharged
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D41/00Electrical control of supply of combustible mixture or its constituents
    • F02D41/0002Controlling intake air
    • F02D41/0007Controlling intake air for control of turbo-charged or super-charged engines
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

Landscapes

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

Abstract

Cuando una fase del compresor de alta presión opera en una zona de operación eficiente en un rendimiento del compresor a un lado de una línea de rendimiento óptimo se separa de, pero es generalmente paralela a un línea límite de estrangulación, el turboalimentador se controla por el control de ciclo de cierre de los álabes de la fase de turbina de alta presión mientras un conducto de derivación alrededor de la fase de turbina de alta presión se mantiene cerrado. Cuando la fase del compresor de alta presión opera en una zona entre la línea de rendimiento óptimo y la línea límite de estrangulación, los álabes de la fase de turbina de alta presión se abren cada vez más cuando la operación de la fase del compresor de alta presión se aproxima cada vez más a la línea límite de estrangulación. Cuando los álabes se han abierto a un grado máximo y la fase del compresor de alta presión se ha vuelto incapaz de proporcionar suficiente presión de sobrealimentación, el conducto de derivación de turbina de alta presión se abre para iniciar la ruta de flujo de escape a una turbina de baja presión que opera una fase del compresor de baja presión, por lo que se evita la estrangulación del flujo de aire de carga por la fase del compresor de alta presión.
MX2007015633A 2006-12-20 2007-12-10 Control del turboalimentador basado en modelos. MX2007015633A (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US11/613,789 US20080148727A1 (en) 2006-12-20 2006-12-20 Model-based turbocharger control

Publications (1)

Publication Number Publication Date
MX2007015633A true MX2007015633A (es) 2009-02-12

Family

ID=39166802

Family Applications (1)

Application Number Title Priority Date Filing Date
MX2007015633A MX2007015633A (es) 2006-12-20 2007-12-10 Control del turboalimentador basado en modelos.

Country Status (8)

Country Link
US (1) US20080148727A1 (es)
EP (1) EP1936147A3 (es)
JP (1) JP2008157236A (es)
KR (1) KR20080058235A (es)
CN (1) CN101205829A (es)
BR (1) BRPI0704864A (es)
CA (1) CA2611215A1 (es)
MX (1) MX2007015633A (es)

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US7735320B2 (en) * 2006-08-29 2010-06-15 Gm Global Technology Operations, Inc. Dual stage turbocharger control system
US20080078176A1 (en) * 2006-10-02 2008-04-03 International Engine Intellectual Property Company Strategy for control of recirculated exhaust gas to null turbocharger boost error
IN2009KN02408A (es) * 2006-12-21 2015-08-07 Borgwarner Inc
US8205606B2 (en) * 2008-07-03 2012-06-26 International Engine Intellectual Property Company, Llc Model for inferring temperature of exhaust gas at an exhaust manifold using temperature measured at entrance of a diesel oxidation catalyst
FR2936278A1 (fr) * 2008-09-19 2010-03-26 Peugeot Citroen Automobiles Sa Procede de commande d'une vanne dans un bipasse d'un turbocompresseur, support d'enregistrement et unite de commande pour ce procede et vehicule equipe de cette unite
JP5045848B2 (ja) * 2009-04-24 2012-10-10 トヨタ自動車株式会社 内燃機関の過給機システム
US8096123B2 (en) * 2009-05-29 2012-01-17 GM Global Technology Operations LLC System and method for mode transition for a two-stage series sequential turbocharger
US8038067B2 (en) * 2009-06-19 2011-10-18 Target Brands, Inc. Transaction card with oscillating member
US8276378B2 (en) * 2009-07-22 2012-10-02 GM Global Technology Operations LLC System and method for controlling a two-stage series sequential turbocharger using bypass valve leakage control
JP4962659B2 (ja) * 2009-10-26 2012-06-27 トヨタ自動車株式会社 過給機付き内燃機関の制御装置
US8468821B2 (en) * 2009-11-19 2013-06-25 GM Global Technology Operations LLC Dual-loop control systems and methods for a sequential turbocharger
US20110120123A1 (en) * 2009-11-23 2011-05-26 International Engine Intellectual Property Company , Llc Low pressure turbine waste gate for diesel engine having two stage turbocharger
US8635856B2 (en) * 2010-02-12 2014-01-28 International Engine Intellectual Property Company, Llc System for disabling diesel particulate filter regeneration during electric operation
JP5874161B2 (ja) * 2010-10-28 2016-03-02 いすゞ自動車株式会社 ターボ過給システム
CN103184927B (zh) * 2011-12-31 2016-10-05 中国第一汽车股份有限公司 基于模型的发动机涡轮增压控制方法
US9587590B2 (en) 2012-01-17 2017-03-07 International Engine Intellectual Property Company, Llc. Coordinating variable valve actuation and turbocharger operation in an internal combustion engine
CN103225553B (zh) 2012-01-31 2018-04-17 万国引擎知识产权有限责任公司 涡轮增压器控制
GB2501922B (en) * 2012-05-10 2018-04-18 Gm Global Tech Operations Llc Method of controlling a two-stage turbocharger of an internal combustion engine
US9574489B2 (en) * 2012-06-07 2017-02-21 Boise State University Multi-stage turbo with continuous feedback control
US9188058B2 (en) * 2012-10-17 2015-11-17 Ford Global Technologies, Llc Method for controlling a turbocharger arrangement with an electric actuator and spring
FR3002001A3 (fr) * 2013-02-13 2014-08-15 Renault Sa Gestion du fonctionnement d'une suralimentation etagee en fonction du debit d'air frais
US10018157B2 (en) * 2013-03-14 2018-07-10 Ford Global Technologies, Llc Methods and systems for boost control
DE102013014722A1 (de) * 2013-09-05 2015-03-05 GM Global Technology Operations LLC (n. d. Ges. d. Staates Delaware) Verfahren zum Betreiben einer Brennkraftmaschine mit einem Turbolader
DE102015203621A1 (de) * 2015-03-02 2016-09-29 Bayerische Motoren Werke Aktiengesellschaft Zweistufige Abgasturbo-Aufladevorrichtung für eine Brennkraftmaschine
DE102015010047B4 (de) * 2015-08-01 2024-05-02 Audi Ag Verfahren und Steuervorrichtung zum Steuern einer Vorrichtung
IL241683B (en) 2015-09-17 2020-09-30 Israel Aerospace Ind Ltd Multi-serial charger
CN105782141B (zh) * 2016-04-06 2017-10-03 哈尔滨工程大学 一种基于废气利用的二级增压柴油机液压装置及控制方法
US10760478B2 (en) 2016-05-18 2020-09-01 Mitsubishi Heavy Industries Engine & Turbocharger, Ltd. Multi-stage turbo supercharging system
CN106939823A (zh) * 2017-04-26 2017-07-11 哈尔滨工程大学 一种应用于船用低速机废气涡轮的以提高冷却系统效率的开式冷却系统
CN110778391B (zh) * 2019-11-20 2020-12-22 创客帮(山东)科技服务有限公司 一种涡轮机

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JPH0450433A (ja) * 1990-06-20 1992-02-19 Toyota Motor Corp 直列2段過給内燃機関の排気ガス再循環装置
JP3931507B2 (ja) * 1999-11-17 2007-06-20 いすゞ自動車株式会社 ディーゼルエンジンのターボチャージャーシステム
JP2004027897A (ja) * 2002-06-24 2004-01-29 Nissan Motor Co Ltd ターボ過給機の制御装置
US6637205B1 (en) * 2002-07-30 2003-10-28 Honeywell International Inc. Electric assist and variable geometry turbocharger
JP3979294B2 (ja) * 2003-01-22 2007-09-19 トヨタ自動車株式会社 多段ターボチャージャの制御装置
JP4254606B2 (ja) * 2004-04-28 2009-04-15 トヨタ自動車株式会社 内燃機関用多段過給システム
JP4254612B2 (ja) * 2004-05-18 2009-04-15 トヨタ自動車株式会社 内燃機関用多段過給システム及びその設定方法
EP1640598A1 (de) * 2004-09-22 2006-03-29 Ford Global Technologies, LLC, A subsidary of Ford Motor Company Aufgeladene Brennkraftmaschine und Verfahren zur Verbesserung des Emissionsverhaltens einer aufgeladenen Brennkraftmaschine
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DE102004056894A1 (de) * 2004-11-25 2006-06-01 Robert Bosch Gmbh Verfahren und Vorrichtung zur Regelung des Ladedrucks einer Brennkraftmaschine
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Also Published As

Publication number Publication date
BRPI0704864A (pt) 2008-08-12
CN101205829A (zh) 2008-06-25
KR20080058235A (ko) 2008-06-25
JP2008157236A (ja) 2008-07-10
US20080148727A1 (en) 2008-06-26
CA2611215A1 (en) 2008-06-20
EP1936147A3 (en) 2009-04-01
EP1936147A2 (en) 2008-06-25

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