US20010022084A1 - Device for limiting the speed of an exhaust-gas turbocharger - Google Patents
Device for limiting the speed of an exhaust-gas turbocharger Download PDFInfo
- Publication number
- US20010022084A1 US20010022084A1 US09/785,683 US78568301A US2001022084A1 US 20010022084 A1 US20010022084 A1 US 20010022084A1 US 78568301 A US78568301 A US 78568301A US 2001022084 A1 US2001022084 A1 US 2001022084A1
- Authority
- US
- United States
- Prior art keywords
- boost pressure
- speed
- pressure sensor
- induction pipe
- compressor
- 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.)
- Granted
Links
- 230000006698 induction Effects 0.000 claims abstract description 18
- 230000003595 spectral effect Effects 0.000 claims abstract description 11
- 238000002485 combustion reaction Methods 0.000 claims description 4
- 238000001914 filtration Methods 0.000 claims 1
- 238000001228 spectrum Methods 0.000 abstract description 2
- 230000006378 damage Effects 0.000 description 2
- 230000003247 decreasing effect Effects 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
Images
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
- F02B37/00—Engines characterised by provision of pumps driven at least for part of the time by exhaust
- F02B37/12—Control of the pumps
- F02B37/18—Control of the pumps by bypassing exhaust from the inlet to the outlet of turbine or to the atmosphere
-
- 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
- F02B2039/168—Control of pump parameters to improve safety thereof the rotational speed of pump or exhaust drive being limited
-
- 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
Definitions
- the present invention relates to a device for limiting the speed of an exhaust-gas turbocharger of an internal combustion engine, a pressure sensor measuring the boost pressure (supercharging pressure) on the pressure side of a compressor of the turbocharger arranged in the induction pipe of the engine, and provision being made for means which reduce a preselected setpoint boost pressure when the speed (rotational speed) reaches a maximum permissible value.
- the boost pressure is controlled in a known manner by comparing a setpoint boost pressure resulting from the driver's command to an actual boost pressure measured by a boost pressure sensor in the induction pipe.
- a boost pressure sensor is used which detects the speed of the compressor in the induction pipe.
- the turbocharger By comparing the measured supercharger speed to a threshold value which corresponds to maximum permissible speed value, it can determine whether the turbocharger reaches a critical speed range and act upon the boost pressure control correspondingly. From the mentioned MTZ it follows that the boost pressure in the induction pipe is always adjusted to programmed values which were determined in standard atmosphere. With increasing altitude and, consequently, dropping pressure, therefore with decreasing air density, the demanded setpoint boost pressure is only attained by increasing the supercharger speed. To this end, the wastegate of the turbocharger is closed to a greater degree and, consequently, the turbine is charged with a larger quantity of exhaust gas. Using an atmospheric pressure sensor, the setpoint boost pressure preselected by the boost pressure control can be lowered in the case of dropping ambient pressure, thereby also allowing the supercharger speed to be limited below its maximum permissible value.
- An object of the present invention is to provide a device for limiting the speed of an exhaust-gas turbocharger, the device neither requiring a speed sensor for the supercharger speed nor an atmospheric pressure sensor.
- the mentioned objective is achieved by providing a bandpass filter which filters out a spectral component from the output signal of a boost pressure sensor existing in the induction pipe, the spectral component appearing in the signal spectrum of the boost pressure sensor when the air column in the induction pipe is set into a vibration which develops when the compressor of the turbocharger rotates at the maximum permissible speed.
- a criterion for limiting the supercharger speed below its maximum permissible value is derived from the output signal of a boost pressure sensor which exists anyway.
- a speed sensor and an atmospheric pressure sensor can be dispensed with.
- a correcting element exists which compares the spectral component delivered by the bandpass filter to a threshold value and, in the case that the threshold value is exceeded, generates a correction signal which reduces the preselected setpoint boost pressure.
- the boost pressure sensor is expediently a piezoelectric sensor since a piezoelectric element responds to vibrations of the air column in the induction pipe in a very sensitive manner.
- FIGURE shows a schematic representation of an internal combustion engine having an exhaust-gas turbocharger and a control unit limiting the supercharger speed.
- FIGURE shows an internal combustion engine 1 having an induction pipe 2 and an exhaust duct 3 .
- a turbine 4 of a turbocharger is located which is mechanically coupled to a compressor 5 arranged in induction pipe 2 .
- turbine 4 in exhaust duct 3 is bridged by a bypass 6 accommodating a controllable valve 7 .
- Valve 7 is driven by an actuator 8 .
- a boost pressure sensor 9 is located whose output signal Id is fed to a control unit SE.
- Boost pressure signal Id is applied to the input of a low pass filter TPF at whose output a mean actual boost pressure Idi freed from all disturbances appears.
- a boost pressure controller LDR e.g., a PD or PI or PID controller
- a bandpass filter BPF is provided in control unit SE, output signal Id of boost pressure sensor 9 being fed to the bandpass filter in parallel to low-pass filter TPF.
- Boost pressure sensor 9 also detects vibrations in the air column in the induction pipe resulting from the rotational movement of compressor 5 .
- the frequency of these vibrations depends on the speed of compressor 5 ; in particular, if boost pressure sensor 9 is a piezoelectric sensor it responds in a very sensitive manner to the vibrations of the air column in the induction pipe which are generated by the compressor. These vibrations manifest themselves in the form of high-frequency signal components which are superimposed upon sensor signal Id.
- bandpass filter BPF is to be designed such that only those spectral components snv appear at its output which are due to vibrations of the air column in induction pipe 2 which develop when compressor 5 rotates at the maximum permissible speed.
- Output signal snv of bandpass filter BPF is fed to a correcting element KG.
- This correcting element KG compares signal snv to a threshold value which is calculated such that when it is exceeded by spectral component snv filtered out from boost pressure signal Id, it can be reliably assumed that filtered out spectral component snv has been generated by a speed of compressor 5 reaching the maximum permissible value. So if correcting element KG detects the maximum permissible supercharger speed in this manner, it emits a correction signal ldk. In logic element V 1 , this correction signal ldk is subtracted from setpoint boost pressure Ids.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Supercharger (AREA)
Abstract
A device for limiting the supercharger speed which makes do without a speed sensor or an atmospheric pressure sensor has a bandpass filter which filters out a spectral component from the output signal of a boost pressure sensor arranged in the induction pipe of the engine, the spectral component appearing in the signal spectrum of the boost pressure sensor when the air column in the induction pipe is set into a vibration which develops when the compressor of the turbocharger rotates at the maximum permissible speed.
Description
- The present invention relates to a device for limiting the speed of an exhaust-gas turbocharger of an internal combustion engine, a pressure sensor measuring the boost pressure (supercharging pressure) on the pressure side of a compressor of the turbocharger arranged in the induction pipe of the engine, and provision being made for means which reduce a preselected setpoint boost pressure when the speed (rotational speed) reaches a maximum permissible value.
- When designing an exhaust-gas turbocharger and its control, care must be taken that the supercharger speed does not exceed a maximum permissible value. As can be gathered from “MTZ Motortechnische Zeitschrift” [Motor Engineering Journal] 53 (1992), 10, pages 454-462, the boost pressure is controlled in a known manner by comparing a setpoint boost pressure resulting from the driver's command to an actual boost pressure measured by a boost pressure sensor in the induction pipe. For monitoring the supercharger speed, usually a speed sensor is used which detects the speed of the compressor in the induction pipe. By comparing the measured supercharger speed to a threshold value which corresponds to maximum permissible speed value, it can determine whether the turbocharger reaches a critical speed range and act upon the boost pressure control correspondingly. From the mentioned MTZ it follows that the boost pressure in the induction pipe is always adjusted to programmed values which were determined in standard atmosphere. With increasing altitude and, consequently, dropping pressure, therefore with decreasing air density, the demanded setpoint boost pressure is only attained by increasing the supercharger speed. To this end, the wastegate of the turbocharger is closed to a greater degree and, consequently, the turbine is charged with a larger quantity of exhaust gas. Using an atmospheric pressure sensor, the setpoint boost pressure preselected by the boost pressure control can be lowered in the case of dropping ambient pressure, thereby also allowing the supercharger speed to be limited below its maximum permissible value.
- An object of the present invention is to provide a device for limiting the speed of an exhaust-gas turbocharger, the device neither requiring a speed sensor for the supercharger speed nor an atmospheric pressure sensor.
- The mentioned objective is achieved by providing a bandpass filter which filters out a spectral component from the output signal of a boost pressure sensor existing in the induction pipe, the spectral component appearing in the signal spectrum of the boost pressure sensor when the air column in the induction pipe is set into a vibration which develops when the compressor of the turbocharger rotates at the maximum permissible speed. Here, a criterion for limiting the supercharger speed below its maximum permissible value is derived from the output signal of a boost pressure sensor which exists anyway. In this context, a speed sensor and an atmospheric pressure sensor can be dispensed with.
- Accordingly, a correcting element exists which compares the spectral component delivered by the bandpass filter to a threshold value and, in the case that the threshold value is exceeded, generates a correction signal which reduces the preselected setpoint boost pressure.
- The boost pressure sensor is expediently a piezoelectric sensor since a piezoelectric element responds to vibrations of the air column in the induction pipe in a very sensitive manner.
- The FIGURE shows a schematic representation of an internal combustion engine having an exhaust-gas turbocharger and a control unit limiting the supercharger speed.
- The FIGURE shows an internal combustion engine1 having an
induction pipe 2 and an exhaust duct 3. In exhaust duct 3, a turbine 4 of a turbocharger is located which is mechanically coupled to a compressor 5 arranged ininduction pipe 2. To be able to control the boost pressure in the induction pipe, turbine 4 in exhaust duct 3 is bridged by a bypass 6 accommodating a controllable valve 7. Valve 7 is driven by anactuator 8. On the pressure side of compressor 5 ininduction pipe 2, a boost pressure sensor 9 is located whose output signal Id is fed to a control unit SE. Boost pressure signal Id is applied to the input of a low pass filter TPF at whose output a mean actual boost pressure Idi freed from all disturbances appears. A boost pressure controller LDR (e.g., a PD or PI or PID controller) derives a controlled variable wg foractuator 8 of wastegate 7 from the offset did between actual boost pressure Idi and a setpoint boost pressure Ids which depends on the driver's command and, possibly, on other performance quantities of the engine. - As already explained by way of introduction, care must be taken that the turbocharger does not exceed a maximum permissible speed to prevent it from destruction. When operating the vehicle at higher altitudes, the maximum permissible supercharger speed can easily be exceeded since, with increasing altitude and, consequently, dropping ambient pressure, the demanded setpoint boost pressure is only attained by increasing the supercharger speed. In the case of an atmospheric pressure heavily dropping with respect to the standard atmosphere therefore, special care must be taken that the supercharger speed does not exceed the maximum permissible value to prevent the turbocharger from destruction. To this end, a bandpass filter BPF is provided in control unit SE, output signal Id of boost pressure sensor9 being fed to the bandpass filter in parallel to low-pass filter TPF.
- Boost pressure sensor9 also detects vibrations in the air column in the induction pipe resulting from the rotational movement of compressor 5. The frequency of these vibrations depends on the speed of compressor 5; in particular, if boost pressure sensor 9 is a piezoelectric sensor it responds in a very sensitive manner to the vibrations of the air column in the induction pipe which are generated by the compressor. These vibrations manifest themselves in the form of high-frequency signal components which are superimposed upon sensor signal Id. With regard to its frequency passband, bandpass filter BPF is to be designed such that only those spectral components snv appear at its output which are due to vibrations of the air column in
induction pipe 2 which develop when compressor 5 rotates at the maximum permissible speed. - Output signal snv of bandpass filter BPF is fed to a correcting element KG. This correcting element KG compares signal snv to a threshold value which is calculated such that when it is exceeded by spectral component snv filtered out from boost pressure signal Id, it can be reliably assumed that filtered out spectral component snv has been generated by a speed of compressor5 reaching the maximum permissible value. So if correcting element KG detects the maximum permissible supercharger speed in this manner, it emits a correction signal ldk. In logic element V1, this correction signal ldk is subtracted from setpoint boost pressure Ids.
- In logic element V2, offset did between corrected, reduced setpoint boost pressure ldsk and actual boost pressure Idi is generated, the offset finally being fed to boost pressure controller LDR. The boost pressure controller then controls wastegate 7 in such a manner that a smaller quantity of exhaust gas is led via turbine 4 of the exhaust-gas turbocharger, thus reducing the speed of the exhaust-gas turbocharger below the maximum permissible value.
- Using the described device, it is achieved, without using a supercharger speed sensor or an atmospheric pressure sensor, that the exhaust-gas turbocharger can indeed be run up to its maximum permissible speed without exceeding it even when traveling at high geographical altitudes.
Claims (3)
1. A device for limiting a speed of an exhaust-gas turbocharger of an internal combustion engine, the turbocharger including a compressor, the device comprising:
a boost pressure sensor measuring a boost pressure on a pressure side of the compressor situated in an induction pipe of the engine, a spectral component appearing in an output signal of the boost pressure sensor when an air column in the induction pipe is set into a vibration which develops when the compressor rotates at a maximum permissible speed; and
a pressure reducing arrangement for reducing a preselected setpoint boost pressure when a rotational speed reaches a maximum permissible value, the pressure reducing arrangement including a bandpass filter for filtering out the spectral component from the output signal of the boost pressure sensor.
2. The device according to , wherein the pressure reducing arrangement further includes a correcting element, the correcting element comparing the spectral component delivered by the bandpass filter to a threshold value and, if the threshold value is exceeded, the correcting element generating a correction signal which reduces the preselected setpoint boost pressure.
claim 1
3. The device according to , wherein the boost pressure sensor is a piezoelectric sensor.
claim 1
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE10007013A DE10007013B4 (en) | 2000-02-16 | 2000-02-16 | Device for limiting the speed of an exhaust gas turbocharger |
DE10007013 | 2000-02-16 | ||
DE10007013.2 | 2000-02-16 |
Publications (2)
Publication Number | Publication Date |
---|---|
US20010022084A1 true US20010022084A1 (en) | 2001-09-20 |
US6378306B2 US6378306B2 (en) | 2002-04-30 |
Family
ID=7631166
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US09/785,683 Expired - Lifetime US6378306B2 (en) | 2000-02-16 | 2001-02-16 | Device for limiting the speed of an exhaust-gas turbocharger |
Country Status (5)
Country | Link |
---|---|
US (1) | US6378306B2 (en) |
JP (1) | JP4739539B2 (en) |
DE (1) | DE10007013B4 (en) |
FR (1) | FR2804999B1 (en) |
GB (1) | GB2359380B (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20080228447A1 (en) * | 2005-07-07 | 2008-09-18 | Renault S.A.S | Device and Method for Processing a Signal of Pressure Measurement of an Internal Combustion Engine Combustion Chamber |
US20100000309A1 (en) * | 2006-06-13 | 2010-01-07 | Continental Automotive Gmbh | Method and device for monitoring an exhaust-gas turbocharger |
US20110023479A1 (en) * | 2009-07-29 | 2011-02-03 | Ford Global Technologies, Llc | Control strategy for decreasing resonance in a turbocharger |
US20140053642A1 (en) * | 2011-04-08 | 2014-02-27 | Willibald Reitmeier | Method and device for measuring the rotational speed of a turbocompressor, and motor vehicle |
US8676534B2 (en) | 2010-06-03 | 2014-03-18 | MAGNETI MARELLI S.p.A. | Method for determining the rotation speed of a supercharger in an internal combustion engine |
US20190234295A1 (en) * | 2018-01-30 | 2019-08-01 | Robert Bosch Gmbh | Device and method for regulating a compressor for an internal combustion engine |
Families Citing this family (16)
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DE10160934A1 (en) * | 2001-12-12 | 2003-06-18 | Daimler Chrysler Ag | Regulation of the surge limit of exhaust gas turbochargers |
US7063810B1 (en) * | 2002-11-27 | 2006-06-20 | The United States Of America As Represented By The Secretary Of The Navy | Co-extrusion of energetic materials using multiple twin screw extruders |
DE102004042272A1 (en) * | 2004-09-01 | 2006-03-02 | Robert Bosch Gmbh | Method and device for controlling or regulating the boost pressure of an internal combustion engine |
DE102005022691A1 (en) * | 2005-05-18 | 2006-11-23 | Robert Bosch Gmbh | Method for operating internal combustion engine entails carrying out correction for operating point modelling differently for different operating points of engine |
US7269992B2 (en) * | 2005-06-15 | 2007-09-18 | Honeywell International Inc. | Magnet orientation and calibration for small package turbocharger speed sensor |
US7378721B2 (en) * | 2005-12-05 | 2008-05-27 | Honeywell International Inc. | Chip on lead frame for small package speed sensor |
US7375406B2 (en) * | 2005-12-20 | 2008-05-20 | Honeywell International Inc. | Thermoplastic overmolding for small package turbocharger speed sensor |
CN101082318B (en) * | 2006-05-31 | 2011-09-21 | 卡特彼勒公司 | Turbo-charger control system |
JP4818944B2 (en) * | 2007-01-26 | 2011-11-16 | 日野自動車株式会社 | Turbine protection device |
US7650218B2 (en) * | 2007-09-20 | 2010-01-19 | Cummins Ip, Inc | Apparatus, system, and method for preventing turbocharger overspeed in a combustion engine |
US8272215B2 (en) * | 2008-05-28 | 2012-09-25 | Ford Global Technologies, Llc | Transient compressor surge response for a turbocharged engine |
DE102009020856A1 (en) * | 2009-05-12 | 2010-11-25 | Bosch Mahle Turbo Systems Gmbh & Co. Kg | Charging device i.e. exhaust gas turbocharger, for internal combustion engine of motor vehicle, has control/regulation device operating actuating device for limiting speed during reaching or exceeding pre-defined limiting speed of rotor |
IT1401825B1 (en) * | 2010-09-27 | 2013-08-28 | Magneti Marelli Spa | METHOD OF CHECKING THE SPEED OF AN INTERNAL COMBUSTION MOTOR OVER-POWERED BY A TURBOCHARGER |
FI20115253A0 (en) * | 2011-03-14 | 2011-03-14 | Waertsilae Finland Oy | Operating procedure and exhaust system for an internal combustion engine |
WO2012143997A1 (en) * | 2011-04-18 | 2012-10-26 | トヨタ自動車株式会社 | Control device for supercharged engine |
US8903598B2 (en) | 2013-04-18 | 2014-12-02 | Chrysler Group Llc | Techniques for detecting supercharger belt slip |
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DE2823255C2 (en) * | 1978-05-27 | 1986-07-17 | Robert Bosch Gmbh, 7000 Stuttgart | Device for determining the charging of an exhaust-gas-charged internal combustion engine |
JPS5584817A (en) * | 1978-12-18 | 1980-06-26 | Nissan Motor Co Ltd | Bypass valve for use with exhaust turbocharger of internal-combustion engine |
JPS5710731A (en) * | 1980-06-24 | 1982-01-20 | Honda Motor Co Ltd | Controller for operation characteristic of supercharger of engine |
JPS5815793A (en) * | 1981-07-22 | 1983-01-29 | Ishikawajima Harima Heavy Ind Co Ltd | No-load operation control device of compressor |
JPS6251729A (en) * | 1985-08-30 | 1987-03-06 | Isuzu Motors Ltd | Turbocharger control device for internal combustion engine |
JP2510855B2 (en) * | 1986-02-10 | 1996-06-26 | いすゞ自動車株式会社 | Energy recovery device in vehicle |
DE3605958A1 (en) * | 1986-02-25 | 1987-09-03 | Fraunhofer Ges Forschung | Device for detecting and eliminating separation vibrations on compressor blades |
JPS63108528A (en) * | 1986-10-27 | 1988-05-13 | Teijin Ltd | Magnetic recording medium |
JPH0539726A (en) * | 1991-08-02 | 1993-02-19 | Toyota Motor Corp | Supercharging pressure controller for engine with supercharger |
JP2993264B2 (en) * | 1992-03-10 | 1999-12-20 | トヨタ自動車株式会社 | Supercharge control device for internal combustion engine for vehicles with automatic transmission |
SE500813C2 (en) * | 1993-01-22 | 1994-09-12 | Ase Autotest Ab | Procedure for measuring the engine speed of turbochargers |
CA2149576A1 (en) * | 1994-05-19 | 1995-11-20 | Hideomi Harada | Surge detection device and turbomachinery therewith |
JPH08200082A (en) * | 1995-01-31 | 1996-08-06 | Toyota Motor Corp | Overspeed preventive device of turbocharger |
DE19730578A1 (en) * | 1997-07-17 | 1999-01-21 | Bosch Gmbh Robert | Method and device for protecting a turbocharger |
US6000384A (en) * | 1998-03-06 | 1999-12-14 | Caterpillar Inc. | Method for balancing the air/fuel ratio to each cylinder of an engine |
DE19818124C2 (en) * | 1998-04-23 | 2001-09-13 | Daimler Chrysler Ag | Device for detecting the speed of turbochargers |
-
2000
- 2000-02-16 DE DE10007013A patent/DE10007013B4/en not_active Expired - Fee Related
-
2001
- 2001-01-31 GB GB0102416A patent/GB2359380B/en not_active Expired - Fee Related
- 2001-02-14 JP JP2001037521A patent/JP4739539B2/en not_active Expired - Fee Related
- 2001-02-16 US US09/785,683 patent/US6378306B2/en not_active Expired - Lifetime
- 2001-02-16 FR FR0102130A patent/FR2804999B1/en not_active Expired - Fee Related
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20080228447A1 (en) * | 2005-07-07 | 2008-09-18 | Renault S.A.S | Device and Method for Processing a Signal of Pressure Measurement of an Internal Combustion Engine Combustion Chamber |
US7660703B2 (en) * | 2005-07-07 | 2010-02-09 | Renault S.A.S. | Device and method for processing a signal of pressure measurement of an internal combustion engine combustion chamber |
US20100000309A1 (en) * | 2006-06-13 | 2010-01-07 | Continental Automotive Gmbh | Method and device for monitoring an exhaust-gas turbocharger |
US8291752B2 (en) | 2006-06-13 | 2012-10-23 | Continental Automotive Gmbh | Method and device for monitoring an exhaust-gas turbocharger |
US20110023479A1 (en) * | 2009-07-29 | 2011-02-03 | Ford Global Technologies, Llc | Control strategy for decreasing resonance in a turbocharger |
US8312718B2 (en) | 2009-07-29 | 2012-11-20 | Ford Global Technologies, Llc | Control strategy for decreasing resonance in a turbocharger |
US9243551B2 (en) | 2009-07-29 | 2016-01-26 | Ford Global Technologies, Llc | Control strategy for decreasing resonance in a turbocharger |
US8676534B2 (en) | 2010-06-03 | 2014-03-18 | MAGNETI MARELLI S.p.A. | Method for determining the rotation speed of a supercharger in an internal combustion engine |
US20140053642A1 (en) * | 2011-04-08 | 2014-02-27 | Willibald Reitmeier | Method and device for measuring the rotational speed of a turbocompressor, and motor vehicle |
US9121862B2 (en) * | 2011-04-08 | 2015-09-01 | Continental Automotive Gmbh | Method and device for measuring the rotational speed of a turbocompressor, and motor vehicle |
US20190234295A1 (en) * | 2018-01-30 | 2019-08-01 | Robert Bosch Gmbh | Device and method for regulating a compressor for an internal combustion engine |
US10781744B2 (en) * | 2018-01-30 | 2020-09-22 | Robert Bosch Gmbh | Device and method for regulating a compressor for an internal combustion engine |
Also Published As
Publication number | Publication date |
---|---|
DE10007013A1 (en) | 2001-08-23 |
FR2804999B1 (en) | 2006-08-04 |
US6378306B2 (en) | 2002-04-30 |
FR2804999A1 (en) | 2001-08-17 |
JP2001248454A (en) | 2001-09-14 |
DE10007013B4 (en) | 2009-04-16 |
GB2359380B (en) | 2002-06-19 |
JP4739539B2 (en) | 2011-08-03 |
GB2359380A (en) | 2001-08-22 |
GB0102416D0 (en) | 2001-03-14 |
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