FR2941267B1 - Procede et dispositif de determination de la pression en amont d'une turbine d'un turbocompresseur de suralimentation d'un moteur thermique. - Google Patents

Procede et dispositif de determination de la pression en amont d'une turbine d'un turbocompresseur de suralimentation d'un moteur thermique.

Info

Publication number
FR2941267B1
FR2941267B1 FR0950396A FR0950396A FR2941267B1 FR 2941267 B1 FR2941267 B1 FR 2941267B1 FR 0950396 A FR0950396 A FR 0950396A FR 0950396 A FR0950396 A FR 0950396A FR 2941267 B1 FR2941267 B1 FR 2941267B1
Authority
FR
France
Prior art keywords
turbocharger
turbine
determining
pressure before
thermal motor
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 - Fee Related
Application number
FR0950396A
Other languages
English (en)
Other versions
FR2941267A1 (fr
Inventor
Laurent Fontvieille
Angelo Nicolas D
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.)
Renault SAS
Original Assignee
Renault SAS
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
Priority to FR0950396A priority Critical patent/FR2941267B1/fr
Application filed by Renault SAS filed Critical Renault SAS
Priority to PCT/FR2009/052524 priority patent/WO2010084255A1/fr
Priority to JP2011546901A priority patent/JP2012515874A/ja
Priority to US13/145,872 priority patent/US20120016602A1/en
Priority to RU2011134850/06A priority patent/RU2011134850A/ru
Priority to CN2009801580745A priority patent/CN102356222A/zh
Priority to EP09803861A priority patent/EP2379860A1/fr
Priority to KR1020117019391A priority patent/KR20110105873A/ko
Publication of FR2941267A1 publication Critical patent/FR2941267A1/fr
Application granted granted Critical
Publication of FR2941267B1 publication Critical patent/FR2941267B1/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F02B39/00—Component parts, details, or accessories relating to, driven charging or scavenging pumps, not provided for in groups F02B33/00 - F02B37/00
    • F02B39/16—Other safety measures for, or other control of, pumps
    • 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
    • F02D—CONTROLLING COMBUSTION ENGINES
    • F02D41/00—Electrical control of supply of combustible mixture or its constituents
    • 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
    • F02D41/00—Electrical control of supply of combustible mixture or its constituents
    • F02D41/02—Circuit arrangements for generating control signals
    • F02D41/14—Introducing closed-loop corrections
    • F02D41/1438—Introducing closed-loop corrections using means for determining characteristics of the combustion gases; Sensors therefor
    • F02D41/1444—Introducing closed-loop corrections using means for determining characteristics of the combustion gases; Sensors therefor characterised by the characteristics of the combustion gases
    • F02D41/1448—Introducing closed-loop corrections using means for determining characteristics of the combustion gases; Sensors therefor characterised by the characteristics of the combustion gases the characteristics being an exhaust gas pressure
    • F02D41/145—Introducing closed-loop corrections using means for determining characteristics of the combustion gases; Sensors therefor characterised by the characteristics of the combustion gases the characteristics being an exhaust gas pressure with determination means using an estimation
    • 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
    • F02D41/02—Circuit arrangements for generating control signals
    • F02D41/18—Circuit arrangements for generating control signals by measuring intake air flow
    • 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
    • F02B39/00—Component parts, details, or accessories relating to, driven charging or scavenging pumps, not provided for in groups F02B33/00 - F02B37/00
    • F02B39/16—Other safety measures for, or other control of, pumps
    • F02B2039/162—Control of pump parameters to improve safety thereof
    • F02B2039/166—Control of pump parameters to improve safety thereof the fluid pressure in the pump or exhaust drive being limited
    • 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
    • F02B37/013—Engines characterised by provision of pumps driven at least for part of the time by exhaust with exhaust-driven pumps arranged in series
    • 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
    • F02B37/16—Control of the pumps by bypassing charging air
    • F02B37/162—Control of the pumps by bypassing charging air by bypassing, e.g. partially, intake air from pump inlet to pump outlet
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02D—CONTROLLING COMBUSTION ENGINES
    • F02D2200/00—Input parameters for engine control
    • F02D2200/02—Input parameters for engine control the parameters being related to the engine
    • F02D2200/04—Engine intake system parameters
    • F02D2200/0402—Engine intake system parameters the parameter being determined by using a model of the engine intake or its components
    • 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
FR0950396A 2009-01-22 2009-01-22 Procede et dispositif de determination de la pression en amont d'une turbine d'un turbocompresseur de suralimentation d'un moteur thermique. Expired - Fee Related FR2941267B1 (fr)

Priority Applications (8)

Application Number Priority Date Filing Date Title
FR0950396A FR2941267B1 (fr) 2009-01-22 2009-01-22 Procede et dispositif de determination de la pression en amont d'une turbine d'un turbocompresseur de suralimentation d'un moteur thermique.
JP2011546901A JP2012515874A (ja) 2009-01-22 2009-12-14 熱機関の過給ターボチャージャのタービンの上流の圧力を測定する方法及び装置
US13/145,872 US20120016602A1 (en) 2009-01-22 2009-12-14 Method and device for determining the pressure upstream from the turbine of a supercharging turbocharger of a thermal engine
RU2011134850/06A RU2011134850A (ru) 2009-01-22 2009-12-14 Способ и устройство определения давления на входе турбины турбокомпрессора наддува теплового двигателя
PCT/FR2009/052524 WO2010084255A1 (fr) 2009-01-22 2009-12-14 Procede et dispositif de determination de la pression en amont d'une turbine d'un turbocompresseur de suralimentation d'un moteur thermique
CN2009801580745A CN102356222A (zh) 2009-01-22 2009-12-14 确定热发动机涡轮增压机的涡轮机上游压力的方法和设备
EP09803861A EP2379860A1 (fr) 2009-01-22 2009-12-14 Procede et dispositif de determination de la pression en amont d'une turbine d'un turbocompresseur de suralimentation d'un moteur thermique
KR1020117019391A KR20110105873A (ko) 2009-01-22 2009-12-14 열 엔진의 슈퍼차지 터보과급기의 터빈 상류측의 압력을 판단하는 방법 및 장치

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0950396A FR2941267B1 (fr) 2009-01-22 2009-01-22 Procede et dispositif de determination de la pression en amont d'une turbine d'un turbocompresseur de suralimentation d'un moteur thermique.

Publications (2)

Publication Number Publication Date
FR2941267A1 FR2941267A1 (fr) 2010-07-23
FR2941267B1 true FR2941267B1 (fr) 2011-01-21

Family

ID=41100501

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0950396A Expired - Fee Related FR2941267B1 (fr) 2009-01-22 2009-01-22 Procede et dispositif de determination de la pression en amont d'une turbine d'un turbocompresseur de suralimentation d'un moteur thermique.

Country Status (8)

Country Link
US (1) US20120016602A1 (fr)
EP (1) EP2379860A1 (fr)
JP (1) JP2012515874A (fr)
KR (1) KR20110105873A (fr)
CN (1) CN102356222A (fr)
FR (1) FR2941267B1 (fr)
RU (1) RU2011134850A (fr)
WO (1) WO2010084255A1 (fr)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP5684668B2 (ja) * 2011-08-02 2015-03-18 株式会社豊田中央研究所 内燃機関の制御装置
FR2980525B1 (fr) * 2011-09-26 2013-08-30 Renault Sa Procede et systeme de diagnostic d'un groupe motopropulseur a deux turbocompresseurs etages.
EP2846027A1 (fr) * 2013-09-10 2015-03-11 Delphi International Operations Luxembourg S.à r.l. Procédé pour déterminer la pression de collecteur d'échappement
US9617931B2 (en) 2014-04-07 2017-04-11 MAGNETI MARELLI S.p.A. Method to control a supercharged internal combustion engine provided with a turbocharger by means of an estimation of the average power delivered by the turbine of the turbocharger
CN106599698B (zh) 2015-10-19 2019-09-20 腾讯科技（深圳）有限公司 一种加密图片、解密图片的方法和装置
US11053875B2 (en) 2016-02-10 2021-07-06 Garrett Transportation I Inc. System and method for estimating turbo speed of an engine
DE102017122932A1 (de) * 2016-10-12 2018-01-18 FEV Europe GmbH Verfahren zum Bestimmen eines Drehmoments einer Turbine mit einer variablen Geometrie
CN115292946B (zh) * 2022-08-15 2023-09-05 中国航发沈阳发动机研究所 一种基于变比热计算的高压涡轮效率评估方法及装置

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6067800A (en) * 1999-01-26 2000-05-30 Ford Global Technologies, Inc. Control method for a variable geometry turbocharger in a diesel engine having exhaust gas recirculation
DE19948136A1 (de) * 1999-10-07 2001-04-12 Volkswagen Ag Verfahren zur Bestimmung eines Abgasgegendruckes an einer Turbine
DE19963358A1 (de) * 1999-12-28 2001-07-12 Bosch Gmbh Robert Verfahren und Vorrichtung zur Steuerung einer Brennkraftmaschine mit einem Luftsystem
FR2853693B1 (fr) * 2003-04-09 2006-06-23 Renault Sa Procede d'estimation de la pression des gaz en amont d'une turbine de moteur a combustion interne suralimente et dispositif de commande d'un tel moteur
JP4356072B2 (ja) * 2004-07-09 2009-11-04 株式会社デンソー ターボチャージャを備えた内燃機関の制御装置
EP1741895B1 (fr) * 2005-07-05 2010-03-03 Magneti Marelli S.p.A. Procédé et dispositif de régulation de la vitesse d'un turbocompresseur pour moteur à combustion interne
DE102006042872B4 (de) * 2006-09-13 2010-02-25 Ford Global Technologies, LLC, Dearborn Verfahren zur Bestimmung des Abgasgegendrucks stromaufwärts einer Turbine eines Abgasturboladers
FR2910059A1 (fr) * 2006-12-19 2008-06-20 Renault Sas Procede d'estimation de la pression des gaz d'echappement en amont d'une turbine de turbocompresseur
US7469577B2 (en) * 2007-03-02 2008-12-30 Detroit Diesel Corporation Method of diagnosing turbochargers for internal combustion engines
IT1401825B1 (it) * 2010-09-27 2013-08-28 Magneti Marelli Spa Metodo di controllo della velocita' di un motore a combustione interna sovralimentato mediante un turbocompressore

Also Published As

Publication number Publication date
FR2941267A1 (fr) 2010-07-23
KR20110105873A (ko) 2011-09-27
RU2011134850A (ru) 2013-02-27
JP2012515874A (ja) 2012-07-12
EP2379860A1 (fr) 2011-10-26
WO2010084255A1 (fr) 2010-07-29
CN102356222A (zh) 2012-02-15
US20120016602A1 (en) 2012-01-19

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Effective date: 20130930