EP0668966B1 - Verfahren zur feststellung von störungen im hochdruckkreis eines hochdruck-kraftstoffeinspritz-systems einer brennkraftmaschine - Google Patents

Verfahren zur feststellung von störungen im hochdruckkreis eines hochdruck-kraftstoffeinspritz-systems einer brennkraftmaschine Download PDF

Info

Publication number
EP0668966B1
EP0668966B1 EP94927543A EP94927543A EP0668966B1 EP 0668966 B1 EP0668966 B1 EP 0668966B1 EP 94927543 A EP94927543 A EP 94927543A EP 94927543 A EP94927543 A EP 94927543A EP 0668966 B1 EP0668966 B1 EP 0668966B1
Authority
EP
European Patent Office
Prior art keywords
pressure
duty cycle
value
control cycles
pump
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 - Lifetime
Application number
EP94927543A
Other languages
English (en)
French (fr)
Other versions
EP0668966A1 (de
Inventor
Paolo Tubetti
Riccardo Buratti
Stefano Maria Borrione
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 EP0668966A1 publication Critical patent/EP0668966A1/de
Application granted granted Critical
Publication of EP0668966B1 publication Critical patent/EP0668966B1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • 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
    • F02D41/30Controlling fuel injection
    • F02D41/38Controlling fuel injection of the high pressure type
    • F02D41/3809Common rail control systems
    • F02D41/3836Controlling the fuel pressure
    • 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
    • F02D41/22Safety or indicating devices for abnormal conditions
    • 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
    • F02D41/20Output circuits, e.g. for controlling currents in command coils
    • F02D2041/202Output circuits, e.g. for controlling currents in command coils characterised by the control of the circuit
    • F02D2041/2024Output circuits, e.g. for controlling currents in command coils characterised by the control of the circuit the control switching a load after time-on and time-off pulses
    • F02D2041/2027Control of the current by pulse width modulation or duty cycle control
    • 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
    • F02D41/22Safety or indicating devices for abnormal conditions
    • F02D41/222Safety or indicating devices for abnormal conditions relating to the failure of sensors or parameter detection devices
    • F02D2041/223Diagnosis of fuel pressure sensors
    • 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
    • F02D41/22Safety or indicating devices for abnormal conditions
    • F02D2041/224Diagnosis of the fuel system
    • 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
    • F02D41/22Safety or indicating devices for abnormal conditions
    • F02D2041/224Diagnosis of the fuel system
    • F02D2041/225Leakage detection
    • 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
    • F02D41/22Safety or indicating devices for abnormal conditions
    • F02D2041/228Warning displays
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D2200/00Input parameters for engine control
    • F02D2200/02Input parameters for engine control the parameters being related to the engine
    • F02D2200/06Fuel or fuel supply system parameters
    • F02D2200/0602Fuel pressure
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02DCONTROLLING COMBUSTION ENGINES
    • F02D2250/00Engine control related to specific problems or objectives
    • F02D2250/31Control of the fuel pressure
    • 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
    • F02D41/30Controlling fuel injection
    • F02D41/38Controlling fuel injection of the high pressure type
    • F02D41/3809Common rail control systems

Definitions

  • the present invention relates to a method of diagnosing malfunctioning of the high-pressure circuit of internal combustion engine high-pressure injection systems.
  • the EP-A-501 459 describes a high-pressure injection system.
  • This system comprises a fuel tank, and a high-pressure injector supply circuit in turn comprising several pumps for supplying fuel at high pressure to a manifold in turn supplying a number of injectors.
  • the pump presents a pressure regulating solenoid valve for supplying fuel at a predetermined pressure.
  • a device serves to detect whether or not at least one of the pumps fails. Failure is detected when the pressure quantity patterns do not conform to a predetermined pattern.
  • the US-A-5 241 933 describes a high-pressure injection system. This document proposes the use of upper and lower pressure values for determining malfunction of the system. The upper and lower pressure values depend on the engine speed.
  • the FR-A-2 672 640 propose the use of upper and lower values for the control quantity for determining malfunction of a high pressure fuel supply system.
  • a method of diagnosing malfunctioning of the high-pressure circuit of internal combustion engine high-pressure injection systems comprising a high-pressure pump for supplying fuel at a pressure value controlled by means of control cycles; characterized in that it comprises the- steps of monitoring quantities correlated to the pressure generated by said pump in successive control cycles; comparing the pattern of said quantities in said successive control cycles with reference values; and generating fault signals in the event said pattern fails to present a predetermined relationship with said reference values.
  • FIG. 1 A general description will now be given, with reference to Figure 1, of a high-pressure injection system for internal combustion engines.
  • the system indicated by 1, comprises a tank 2 at atmospheric pressure, connected by a delivery line 5 to a radial-piston pump 6 presenting a pressure regulating solenoid valve (or pressure regulator) 7 connected by drain line 8 to tank 2.
  • a solenoid valve or pressure regulator
  • Manifold 10 feeds the fuel at high pressure along line 11 to a manifold 10 which provides for distributing the fuel to the injectors and damping any fluctuation in pressure caused by the action of the pump and opening of the injectors.
  • Manifold 10 consists of a steel body preferably in the form of a parallelepipedon and in which is formed a cylindrical cavity extending along the length of the manifold and connected to line 11 by a central hole 12.
  • Manifold 10 also presents four holes 13 spaced along the length of the manifold and connected to four high-pressure (up to 1500 bar) supply conduits 14 of four injectors 15 of an engine 16. Each injector 15 is also connected to a conduit 17 for recirculating the fuel (for operating the injector) into tank 2.
  • Manifold 10 is fitted at one end with a known pressure sensor 18.
  • Pressure regulator 7 is conveniently formed as shown in Figure 2, and comprises a body 20 defining a conical seat 21 for a spherical shutter 22.
  • shutter 22 is subjected to the combined force of a spring 24 and a solenoid 25 which cooperates with a core 26 integral with a rod 27 in -turn integral with push rod 23.
  • Shutter 22 separates an inlet conduit 28, connected to the body of pump 6, from an outlet conduit 29, connected to line 8; and varying the current supply to solenoid 25 regulates the force exerted on shutter 22 in the closing direction and, hence, the output pressure of pump 6.
  • Pressure is regulated by supplying solenoid 25 with a current whose duty cycle is modulated at a fixed oscillation frequency (PWM - Pulse Width Modulation - technique) and using a closed regulating loop which takes into account the actual pressure measured by pressure sensor 18, and the desired pressure value.
  • PWM Pulse Width Modulation - technique
  • the method according to the present invention provides for periodically checking operation of the system 1 components, and more specifically for determining: the ability of pump 6 to generate the required pressure; correct tightness of regulator 7; the absence of leakage in the circuit; the presence of injectors locked in the open position; correct operation of the electric circuit controlling regulator 7; and the sensitivity and correct operation of pressure sensor 18.
  • the maximum measured pressure test (block 30) consists in determining the pressure measured by sensor 18 in manifold 10 does not exceed a maximum permissible externally set value, e.g. 1600 bar, in a predetermined number of consecutive checks (e.g. five).
  • a pressure in excess of the maximum permissible value indicates the following types of fault: a shift in the setting of sensor 18 (measuring error); or regulator 7 locked in the closed position (a fault on the regulator preventing or greatly reducing pressurized fuel flow from conduit 28 to conduit 29 of regulator 7).
  • the minimum measured pressure test (block 31) consists in determining the measured pressure does not fall below a minimum permissible value in a predetermined number of consecutive checks, e.g. five.
  • the minimum permissible value varies according to engine speed, as shown by curve-B in Figure 4; and a pressure below the minimum permissible value indicates the following types of fault: an injector locked in the open position; a fault on the pump (fails to ensure the required fuel flow); leakage in the circuit; or a shift in the sensor setting.
  • the increase in the minimum permissible value alongside engine speed is important for detecting the presence of an injector locked in the open position, in that, at high engine speed, even with an injector locked in the open position, pressure may fail to fall below values which are acceptable and correspond to efficient operation at low engine speed.
  • Testing of the duty cycle controlling the pressure regulator consists in determining the duty cycle (percentage measurement) does not exceed a predetermined maximum value K2 (e.g. 97%) or fall below a predetermined minimum value K1 (e.g. 2%) in a predetermined number of consecutive checks (e.g. five for the maximum and 25 for the minimum value).
  • a duty cycle repeatedly in excess of the maximum value means the measured pressure in this period is permanently below the reference value of the system controlling the regulator, and indicates the same faults as the minimum pressure test as well as, possibly, malfunctioning of the electric circuit regulating the duty cycle.
  • a repeatedly low duty cycle value means the measured pressure is permanently in excess of the reference value of the system controlling the regulator, and indicates a shift in the setting of sensor 18 or overtightness of regulator 7.
  • Figures 5A, 5B and 5C show the pressure curve (dotted line) and duty cycle curve (continuous line) in three different conditions following locking of the injector at cycle 2 of the engine. More specifically, Figure 5A relates to a high-pressure condition, in which case, the fault is detected on the basis of the duty cycle remaining repeatedly in excess of the predetermined limit; Figure 5B relates to a medium-pressure condition, in which case, the fault is again detected on the basis of the excessively high duty cycle value, though more slowly than in Figure 5A; and Figure 5C relates to a low-pressure condition, in which case, the fault is detected by detecting too low a pressure value a given number of times.
  • the measured pressure/duty cycle congruency test exploits the relationship between the duty cycle (or more specifically the effective current supplied to regulator 7) and the pressure measured in manifold 10, which relationship is as shown by curve C in Figure 6 which shows reference pressure PR as a function of effective current. Since curve C varies within certain limits according to the regulator used, reference value PR is assigned an upper and lower tolerance value T (e.g. 300 bar) to give two curves D1, D2 defining a given acceptance range.
  • T e.g. 300 bar
  • the congruency test consists in determining the duty cycle value of the current supply to solenoid valve 7 according to conveniently proportional-integral algorithms and as a function of actual measured pressure and required pressure (the latter calculated as provided for, e.g. on the basis of engine parameters as described in a further patent application filed by the present Applicant).
  • the reference value PR corresponding to the determined duty cycle is determined; and a check is made to determine whether the value of the pressure measured by sensor 18 corresponds to reference value PR within the given tolerance (i.e. whether the measured pressure value falls within the given tolerance range).
  • a pressure value outside the given range in a given number of consecutive checks substantially indicates a shift in the setting of sensor 18 in that, the congruency test being slower than the others, other types of fault are generally detected earlier.
  • the method described thus provides, in a straightforward, reliable manner, for indicating otherwise undetectable faults in the hydraulic circuit - such as locking of an injector in the open position - by detecting extraneous factors unrelated to faults resulting in a transient variation in circuit control quantities.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
  • Combined Controls Of Internal Combustion Engines (AREA)

Claims (7)

  1. Verfahren zur Feststellung von Störungen im Hochdruckkreis eins Hochdruckkraftstoffeinspritzsystems einer Brennkraftmaschine, wobei der Hochdruckkreis eine Hochdruckpumpe (6) zur Bereitstellung von Kraftstoff unter hohem Druck umfaßt, der in Regelzyklen geregelt wird, wobei das Verfahren die folgenden Schritt umfaßt:
    Überwachung einer Größe, die den Druck charakterisiert, der von der Hochdruckpumpe (6) in aufeinanderfolgenden Regelzyklen gebildet wird,
    Vergleichen des Verhaltens dieser Größe in aufeinanderfolgenden Regelzyklen mit Referenzwerten, Erzeugen eines Fehlersignals, wenn das Verhalten der Größe nicht in einem vorgegebenen Verhältnis zu dem Referenzwert steht,
    daß das Tastverhältnis des Stromes, mit dem das Regelventil (7) versorgt wird verändert wird,
    Messung des von der Hochdruckpumpe erzeugten Drucks, Berechnung des Tastverhältnises des Stromes auf der Basis der Abweichung zwischen dem Sollwert des Druckes und dem gemessenen Druck,
    Bestimmung eines Referenzdruckes auf Grundlage des Tastverhältnises,
    Vergleichen des gemessenen Druckes und des Referenzdruckes und Erzeugen eines Fehlersignales, wenn der gemessene Druck in einer vorgegebenen Anzahl von aufeinanderfolgenden Regelzyklen um mehr als ein Toleranzband von dem Referenzdruck abweicht.
  2. Verfahren nach Anspruch 1, dadurch gekennzeichnet, daß der Referenzdruck aus einem Kennfeld, in dem der Druckwert als Funktion des Tastverhältnises gespeichert ist, ausgelesen wird.
  3. Verfahren nach Anspruch 1, dadurch gekennzeichnet, daß der Druck, der von der Hochdruckpumpe (6) in einem Speicher (10) bereitgestellt wird, gemessen und der gemessene Druck mit einem maximalen Referenzdruck verglichen wird, und ein Fehlersignal gebildet wird, wenn der gemessene Druck den maximalen Referenzdruck in einer vorgegebenen Anzahl von aufeinanderfolgenden Regelzyklen überschreitet.
  4. Verfahren nach Anspruch 1 oder 3, dadurch gekennzeichnet, daß der gemessene Druck mit einem minimalen Referenzdruck verglichen wird und daß ein Fehlersignal erzeugt wird, wenn der gemessene Druck den minimalen Referenzdruck in einer vorgegebenen Anzahl von aufeinanderfolgenden Regelzyklen unterschreitet.
  5. Verfahren nach Anspruch 4, dadurch gekennzeichnet, daß der minimale Referenzdruck abhängig von der Drehzahl der Brennkraftmaschine vorgebbar ist.
  6. Verfahren nach einem der vorhergehenden Ansprüche, wobei die Regelzyklen den Schritt umfaßt, daß das Tastverhältnis des Stroms, mit dem das Regelventil (7) der Hochdruckpumpe (6) versorgt wird, verändert wird, dadurch gekennzeichnet, daß der von der Hochdruckpumpe erzeugte Druck gemessen wird, daß das Tastverhältnisses des Stroms auf der Basis der Abweichung zwischen dem Sollwert des Druckes und dem gemessenen Druckes berechnet wird, das berechnete Tastverhältniss mit einem Minimalwert und einem Maximalwert verglichen wird, ein Fehlersignal erzeugt wird, wenn das Tastverhältnis in einer vorgegebenen Anzahl von aufeinanderfolgenden Regelzyklen nicht in ein Toleranzband fällt, das durch den Minimalwert und den Maximalwert definiert ist.
  7. Verfahren nach Anspruch 1, dadurch gekennzeichnet, daß zur Bestimmung des Referenzdruckes, der Referenzdruck aus einem Kennfeld ausgelesen wird, in dem Druckwert als Funktion des Tastverhältnisses abgespeichert ist.
EP94927543A 1993-09-03 1994-09-02 Verfahren zur feststellung von störungen im hochdruckkreis eines hochdruck-kraftstoffeinspritz-systems einer brennkraftmaschine Expired - Lifetime EP0668966B1 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
ITTO930646 1993-09-03
ITTO930646A IT1261575B (it) 1993-09-03 1993-09-03 Metodo di diagnosi di malfunzionamenti del circuito ad alta pressione di impianti di iniezione ad alta pressione per motori a combustione interna
PCT/EP1994/002922 WO1995006814A1 (en) 1993-09-03 1994-09-02 Method of diagnosing malfunctioning of the high-pressure circuit of internal combustion engine high-pressure injection systems

Publications (2)

Publication Number Publication Date
EP0668966A1 EP0668966A1 (de) 1995-08-30
EP0668966B1 true EP0668966B1 (de) 1998-03-25

Family

ID=11411710

Family Applications (1)

Application Number Title Priority Date Filing Date
EP94927543A Expired - Lifetime EP0668966B1 (de) 1993-09-03 1994-09-02 Verfahren zur feststellung von störungen im hochdruckkreis eines hochdruck-kraftstoffeinspritz-systems einer brennkraftmaschine

Country Status (5)

Country Link
EP (1) EP0668966B1 (de)
JP (1) JP3727339B2 (de)
DE (1) DE69409222T2 (de)
IT (1) IT1261575B (de)
WO (1) WO1995006814A1 (de)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2013089621A1 (en) * 2011-12-13 2013-06-20 Scania Cv Ab Device and method for fault detection in a fuel supply system of a motor vehicle
EP2791496A4 (de) * 2011-12-13 2015-12-02 Scania Cv Ab Vorrichtung und verfahren zur fehlererkennung in einem kraftstoffversorgungssystem eines kraftfahrzeugs

Families Citing this family (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5493902A (en) * 1994-03-02 1996-02-27 Ford Motor Company On-board detection of pressure regulator malfunction
US5499538A (en) * 1994-03-03 1996-03-19 Ford Motor Company On-board detection of fuel pump malfunction
DE19521791A1 (de) * 1995-06-15 1996-12-19 Daimler Benz Ag Verfahren zum Erkennen von Betriebsstörungen in einer Kraftstoffeinspritzanlage einer Brennkraftmaschine
DE19534051A1 (de) * 1995-09-14 1997-03-20 Bosch Gmbh Robert Verfahren zum Betrieb einer Kraftstoffeinspritzeinrichtung
DE19547647A1 (de) * 1995-12-20 1997-06-26 Bosch Gmbh Robert Verfahren und Vorrichtung zur Überwachung eines Kraftstoffzumeßsystems einer Brennkraftmaschine
DE19548280A1 (de) * 1995-12-22 1997-06-26 Bosch Gmbh Robert Verfahren und Vorrichtung zur Steuerung einer Brennkraftmaschine
DE19604552B4 (de) * 1996-02-08 2007-10-31 Robert Bosch Gmbh Verfahren und Vorrichtung zur Steuerung einer Brennkraftmaschine
DE19613184C2 (de) * 1996-04-02 1998-01-22 Daimler Benz Ag Verfahren zum Erkennen von Betriebsstörungen in einer Kraftstoffeinspritzanlage
WO1997049909A1 (de) * 1996-06-26 1997-12-31 Robert Bosch Gmbh Verfahren zum betrieb einer kraftstoffeinspritzeinrichtung
DE19634982C2 (de) * 1996-08-29 2002-10-10 Siemens Ag Verfahren zur Überwachung eines Kraftstoffdruckes
DE19703891B4 (de) * 1997-02-03 2008-07-31 Robert Bosch Gmbh Verfahren und Vorrichtung zur Erkennung einer Leckage
DE19726183A1 (de) * 1997-06-20 1998-12-24 Bosch Gmbh Robert Verfahren und Vorrichtung zur Überwachung eines Kraftstoffzumeßsystems
DE19834660A1 (de) * 1998-07-31 2000-02-03 Bosch Gmbh Robert Verfahren und Vorrichtung zur Überwachung eines Kraftstoffzumeßsystems
DE19937962A1 (de) * 1999-08-11 2001-02-15 Bosch Gmbh Robert Verfahren und Vorrichtung zur Steuerung eines Einspritzsystems
DE10031066C2 (de) * 2000-06-26 2002-05-02 Siemens Ag Einspritzanlage für eine Brennkraftmaschine sowie Verfahren zum Betrieb einer Einspritzanlage
IT1321068B1 (it) * 2000-11-14 2003-12-30 Fiat Ricerche Metodo di diagnosi di perdite in un impianto di iniezione a collettore comune di un motore a combustione interna.
DE10146474B4 (de) * 2001-09-21 2005-10-06 Robert Bosch Gmbh Verfahren und Vorrichtung zur Diagnose eines Druckdämpfers
DE10147189A1 (de) 2001-09-25 2003-04-24 Bosch Gmbh Robert Verfahren zum Betreiben eines Kraftstoffversorgungssystems für einen Verbrennungsmotor eines Kraftfahrzeugs
US6715468B2 (en) * 2001-11-07 2004-04-06 Denso Corporation Fuel injection system
DE10259797A1 (de) * 2002-12-19 2004-07-15 Siemens Ag Vorrichtung und Verfahren zum Erkennen von Fehlern in einem Kraftstoffeinspritzsystem
DE102004022115A1 (de) 2004-05-05 2005-11-24 Robert Bosch Gmbh Verfahren zum Einbringen eines Reagenzmittels in einen Abgaskanal einer Brennkraftmaschine und Vorrichtung zur Durchführung des Verfahrens
DE102004037963A1 (de) 2004-08-05 2006-03-16 Robert Bosch Gmbh Prüfverfahren
JP2008516153A (ja) * 2004-10-12 2008-05-15 フォード・オトマティブ・サナイ・アノニム・シルケチ 燃料噴射を監視する方法および装置
JP4746510B2 (ja) * 2006-02-21 2011-08-10 愛三工業株式会社 負荷駆動系の異常診断システムおよび燃料ポンプ制御システム
JP4591390B2 (ja) * 2006-03-27 2010-12-01 株式会社デンソー ポンプ故障診断装置
DE102008024955B3 (de) 2008-05-23 2009-12-24 Continental Automotive Gmbh Verfahren zur Erkennung einer Fehlfunktion eines Raildrucksensors bei einem Common Rail-Einspritzsystem
US8775052B2 (en) 2011-12-15 2014-07-08 GM Global Technology Operations LLC Sensors bias detection for electronic returnless fuel system
DE102016205481A1 (de) * 2016-04-04 2017-10-05 Bayerische Motoren Werke Aktiengesellschaft Verfahren zur Dichtheitsprüfung einer Kraftstoff-Hochdruck-Einspritzvorrichtung
DE102018217327B4 (de) * 2018-10-10 2023-10-12 Vitesco Technologies GmbH Verfahren und Vorrichtung zur Plausibilisierung der Funktionsfähigkeit eines Hochdrucksensors einer Hochdruckkraftstoffeinspritzvorrichtung eines Kraftfahrzeugs

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3301742A1 (de) * 1983-01-20 1984-07-26 Robert Bosch Gmbh, 7000 Stuttgart Sicherheitseinrichtung fuer eine brennkraftmaschine mit selbstzuendung
DE4103840B4 (de) * 1991-02-08 2011-02-10 Robert Bosch Gmbh Fehler-Überwachungsverfahren
JP3033214B2 (ja) * 1991-02-27 2000-04-17 株式会社デンソー 複数の燃料圧送手段による蓄圧式燃料供給方法及び装置と、複数の流体圧送手段を有する機器における異常判断装置
JPH0569374U (ja) * 1992-02-28 1993-09-21 富士重工業株式会社 筒内直噴式エンジンの異常警告装置

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2013089621A1 (en) * 2011-12-13 2013-06-20 Scania Cv Ab Device and method for fault detection in a fuel supply system of a motor vehicle
EP2791496A4 (de) * 2011-12-13 2015-12-02 Scania Cv Ab Vorrichtung und verfahren zur fehlererkennung in einem kraftstoffversorgungssystem eines kraftfahrzeugs

Also Published As

Publication number Publication date
ITTO930646A1 (it) 1995-03-03
IT1261575B (it) 1996-05-23
ITTO930646A0 (it) 1993-09-03
DE69409222D1 (de) 1998-04-30
WO1995006814A1 (en) 1995-03-09
JPH08503053A (ja) 1996-04-02
JP3727339B2 (ja) 2005-12-14
DE69409222T2 (de) 1998-07-16
EP0668966A1 (de) 1995-08-30

Similar Documents

Publication Publication Date Title
EP0668966B1 (de) Verfahren zur feststellung von störungen im hochdruckkreis eines hochdruck-kraftstoffeinspritz-systems einer brennkraftmaschine
US5715786A (en) Device for detecting leakage in a fuel supply
US11306676B2 (en) Methods and system for diagnosing a high-pressure fuel pump in a fuel system
US5773716A (en) Method and unit for diagnosing leakage of an internal combustion engine high-pressure injection system
EP2188517B1 (de) Kraftstoffeinspritzdüse und kraftstoffeinspritzsystem
KR100413305B1 (ko) 내연기관의연료량조정장치의감시방법및감시장치
US6467466B1 (en) Gas leakage detection and fail-safe control method for gas-fueled internal combustion engine and apparatus for implementing the same
US5816220A (en) Process and device for monitoring a fuel delivery system
US8261605B2 (en) Method and device for controlling a fuel metering system
CN102428264B (zh) 燃料喷射系统中的故障定位
ITMI971554A1 (it) Procedimento e dispositivo per il contrllo di un sistema di iniezione
US6840228B2 (en) Filter processing device for detecting values of common rail pressure and common rail fuel injection control device
KR20100014658A (ko) 셧 오프 밸브의 진단 방법
US4761608A (en) In use position measuring device calibration
US11668262B2 (en) Methods and system for diagnosing a high-pressure fuel pump in a fuel system
JP2000054903A (ja) 燃料調量システムの監視方法および装置
US7171952B2 (en) Method, computer program, control and/or regulation device for operation of an internal combustion engine and fuel system for an internal combustion engine
CN116696566A (zh) 氢气供给系统及方法
CN101466934B (zh) 用于检查燃油喷射系统部件的功能的方法
US20240200504A1 (en) Systems and methods of fuel injection timing drift detection and compensation
US20190136784A1 (en) Method for operating an internal combustion engine, device for the open-loop and closed-loop control of an internal combustion engine, injection system, and internal combustion engine
JP6498000B2 (ja) 圧力センサ故障診断方法及びコモンレール式燃料噴射制御装置
GB2325275A (en) A device for measuring the quantity of fuel supplied to a fuel injection valve of an internal combustion engine
CN108798928B (zh) 共轨式燃料喷射系统中燃料供应的控制方法
JP3752678B2 (ja) 燃料供給装置

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: A1

Designated state(s): DE FR GB IT SE

17P Request for examination filed

Effective date: 19950911

17Q First examination report despatched

Effective date: 19970116

GRAG Despatch of communication of intention to grant

Free format text: ORIGINAL CODE: EPIDOS AGRA

GRAG Despatch of communication of intention to grant

Free format text: ORIGINAL CODE: EPIDOS AGRA

GRAG Despatch of communication of intention to grant

Free format text: ORIGINAL CODE: EPIDOS AGRA

GRAH Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOS IGRA

GRAH Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOS IGRA

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): DE FR GB IT SE

ET Fr: translation filed
REF Corresponds to:

Ref document number: 69409222

Country of ref document: DE

Date of ref document: 19980430

ITF It: translation for a ep patent filed

Owner name: STUDIO TORTA S.R.L.

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

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

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed
REG Reference to a national code

Ref country code: GB

Ref legal event code: IF02

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: SE

Payment date: 20130920

Year of fee payment: 20

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: GB

Payment date: 20130920

Year of fee payment: 20

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: IT

Payment date: 20130926

Year of fee payment: 20

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20131121

Year of fee payment: 20

Ref country code: FR

Payment date: 20130918

Year of fee payment: 20

REG Reference to a national code

Ref country code: DE

Ref legal event code: R071

Ref document number: 69409222

Country of ref document: DE

REG Reference to a national code

Ref country code: GB

Ref legal event code: PE20

Expiry date: 20140901

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DE

Free format text: LAPSE BECAUSE OF EXPIRATION OF PROTECTION

Effective date: 20140903

REG Reference to a national code

Ref country code: SE

Ref legal event code: EUG

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GB

Free format text: LAPSE BECAUSE OF EXPIRATION OF PROTECTION

Effective date: 20140901