US20010054287A1 - Charged internal combustion engine - Google Patents

Charged internal combustion engine Download PDF

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Publication number
US20010054287A1
US20010054287A1 US09/836,787 US83678701A US2001054287A1 US 20010054287 A1 US20010054287 A1 US 20010054287A1 US 83678701 A US83678701 A US 83678701A US 2001054287 A1 US2001054287 A1 US 2001054287A1
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United States
Prior art keywords
internal combustion
combustion engine
fact
identified
engine based
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.)
Abandoned
Application number
US09/836,787
Inventor
Patric Hoecker
Stefan Munz
Jens-Wolf Jaisle
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.)
BorgWarner Inc
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BorgWarner Inc
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 BorgWarner Inc filed Critical BorgWarner Inc
Assigned to BORGWARNER, INC. reassignment BORGWARNER, INC. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: HOECKER, PATRIC, JAISLE, JENS-WOLF, MUNZ, STEFAN
Publication of US20010054287A1 publication Critical patent/US20010054287A1/en
Priority to US10/455,537 priority Critical patent/US6920755B2/en
Priority to US10/455,536 priority patent/US6889503B2/en
Priority to US10/455,542 priority patent/US6920756B2/en
Abandoned legal-status Critical Current

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    • 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
    • F02B39/02Drives of pumps; Varying pump drive gear ratio
    • F02B39/08Non-mechanical drives, e.g. fluid drives having variable gear ratio
    • F02B39/10Non-mechanical drives, e.g. fluid drives having variable gear ratio electric
    • 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
    • F02B37/04Engines with exhaust drive and other drive of pumps, e.g. with exhaust-driven pump and mechanically-driven second pump
    • 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
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M26/00Engine-pertinent apparatus for adding exhaust gases to combustion-air, main fuel or fuel-air mixture, e.g. by exhaust gas recirculation [EGR] systems
    • F02M26/02EGR systems specially adapted for supercharged engines
    • F02M26/08EGR systems specially adapted for supercharged engines for engines having two or more intake charge compressors or exhaust gas turbines, e.g. a turbocharger combined with an additional compressor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N3/00Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust
    • F01N3/08Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous
    • F01N3/10Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous by thermal or catalytic conversion of noxious components of exhaust
    • F01N3/24Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for rendering innocuous by thermal or catalytic conversion of noxious components of exhaust characterised by constructional aspects of converting apparatus
    • F01N3/30Arrangements for supply of additional air
    • F01N3/32Arrangements for supply of additional air using air pump
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B29/00Engines characterised by provision for charging or scavenging not provided for in groups F02B25/00, F02B27/00 or F02B33/00 - F02B39/00; Details thereof
    • F02B29/04Cooling of air intake supply
    • F02B29/0406Layout of the intake air cooling or coolant circuit
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M26/00Engine-pertinent apparatus for adding exhaust gases to combustion-air, main fuel or fuel-air mixture, e.g. by exhaust gas recirculation [EGR] systems
    • F02M26/13Arrangement or layout of EGR passages, e.g. in relation to specific engine parts or for incorporation of accessories
    • F02M26/14Arrangement or layout of EGR passages, e.g. in relation to specific engine parts or for incorporation of accessories in relation to the exhaust system
    • F02M26/16Arrangement or layout of EGR passages, e.g. in relation to specific engine parts or for incorporation of accessories in relation to the exhaust system with EGR valves located at or near the connection to the exhaust system
    • 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

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)
  • Exhaust-Gas Circulating Devices (AREA)

Abstract

The invention concerns a charged internal combustion engine with at least one stage of charging by a turbocharger.
The invention is characterized by the fact that at least one supplemental compressor is connected parallel to or in series with the turbocharger, where the supplemental compressor has a drive independent form the working medium cycle of the internal combustion engine.

Description

  • The invention refers to a charged internal combustion engine based on the precharacterizing portion of [0001] claim 1.
  • Internal combustion engines with turbochargers, as commonly known, use the energy contained in the exhaust and convert it into mechanical energy in an exhaust turbine to power a turbo compressor, which increases the pressure of the air supplied to the internal combustion engine. To accomplish this, turbocharging can occur in one or more steps. [0002]
  • In DE 198 37 978 A1, a two step turbocharging is disclosed, where at least two turbines are attached in the exhaust section, each of which power a turbo compressor. The exhaust turbines are connected in series as high and low pressure level. First, the exhaust flows through the high pressure turbine and then through the low pressure turbine. The charge air is first compressed by the low pressure compressor and then by the high pressure compressor and, in certain cases after cooling by passing through a heat exchanger, is supplied to the fresh gas side of the internal combustion engine. As the RPM of the internal combustion engine is increased, compression is increasingly shifted towards a single stage which occurs exclusively in the low pressure compressor. In comparison to one-step compression, charging is already possible at low engine speeds with such a two-step charging process, but the turbine operation, and therefore indirectly the compressor operation, is limited by the energy contained in the exhaust. That means that the unburned gas conducted into the internal combustion engine can only be compressed a little, especially with lower speeds. Without boost the internal combustion engine creates weak torque, which leads to poor acceleration when used in a motor vehicle. [0003]
  • The invention is concerned with the task of improving an internal combustion engine of the type disclosed in the precharacterizing portion of [0004] claim 1, so that it can generate high torque even at low RPM, and thus making stationary torque available more rapidly at partial load. In doing so, a high charge pressure should build up early on, which can match the requirements of the internal combustion engine.
  • Based on the invention, this task is solved by connecting a supplemental compressor, which has a drive which is independent from the working medium cycle of the internal combustion engine, arranged in parallel or in series with the turbocharger. [0005]
  • In an especially beneficial embodiment, the supplemental compressor is driven by an electric motor, and the supplemental compressor is connected with the turbocharger in series. The supplemental compressor is beneficially arranged upstream of the turbocharger, in front of the turbocharger in the direction of flow. [0006]
  • In a further developed embodiment, a closing or switching means is located between the supplemental compressor and the compressor of the turbocharger. Working with an electronic control device for the electric motor and the closing or switching means and power electronics required to support the electric motor, the supplemental compressor supplements the turbocharger in operational conditions in which the power taken from the exhaust flow is not sufficient or not present. [0007]
  • In a beneficial execution, the supplemental compressor and the compressor of the turbocharger are matched to each other in such a manner, that a comparably wide characteristic diagram or power curve results. The compression ratio of the supplemental compressor and the compression ratio of the turbocharger compressor are multiplied at each operating point. [0008]
  • In a further developed execution, the electric motor is regulated based on the boost pressure output of the turbocharger in relation to the prescribed boost pressure curve, so that the supplemental compressor is switched off when the required boost pressure is reached by the turbocharger. However, a predetermined excess or reserve of the boost pressure may be maintained in unsteady operating phases. [0009]
  • In a special execution, the supplemental compressor and the turbocharger take in air via different intake sections, where the closing-switching means guarantees that the air which is pre-compressed by the supplemental compressor can only flow in the direction of the turbocharger, or when the supplemental compressor of the turbocharger is turned off, cannot conduct air through the supplemental compressor any more. In an advantageous execution of the invention, a charge cooler or heat exchanger is provided between the turbocharger and the internal combustion engine. This decreases the thermal stress of the components on the one hand, and on the other decreases the specific volume of the compressed air which had experienced heating during compression in the supplemental compressor and turbocharger, thus resulting in an increase in specific volume. By cooling and densifying the air, the charged mass of the combustion engine is increased, which results in a considerable increase in power. [0010]
  • Because the powering of the supplemental compressor can be operated independently from the internal combustion engine, a further advantage of the invention is that the supplemental compressor also functions as a secondary air pump to conduct the air in the catalytic converter to increase the conversation rate of the catalytic converter in a cold condition. [0011]
  • Through an appropriate design of the turbine, a decrease in the exhaust gas counterpressure is made possible. The execution of the invention is obviously possible with various structural shapes of turbochargers (turbochargers with waste gate or flap or also a charger with variable turbine geometry). The use of multi-stage turbochargers is as conceivable as the use of several supplemental compressors, where the connection could occur not only in series but also in parallel. Several heat exchangers could also be used beneficially. If needed, the supplemental compressor and the turbocharger can intake from the same intake section. A possible bypass with a switch means makes it possible to detour the exhaust gas side of the turbocharger. In order to reduce the amount of nitrogen oxide emission through the exhausts coming from the internal combustion engine, an exhaust gas recirculation system (EGR) can be used, which draws in an amount of exhaust gas from a engine exhaust conduit to a point upstream from the turbine of the turbocharger, and conducts it into an engine intake conduit ([0012] DE 41 20 055 A1).
  • In an especially beneficial execution of the invention, the supplemental compressor can be incorporated in an assembly of the internal combustion engine. In doing so it is possible to either incorporate only the supplemental compressor into the assembly or also additional components or aggregates, such as the switching and/or closing means in front of and behind the supplemental compressor, if necessary, required throttle means or even the drive for the supplemental compressor. When putting the supplemental compressor in the intake pipe assembly, it is beneficial to integrate the supplemental compressor in the intake pipe or to build it onto the intake pipe. In a further developed execution, the spiral guide around the compressor wheel can be directly formed on the intake pipe. When mounting the supplemental compressor drive at the intake pipe (or at the internal combustion engine or the body), it is beneficial to provide a vibration decoupling fastener in order to mitigate the vibration loads of the internal combustion engine's stimulus. [0013]
  • In another beneficial execution of the invention, the cylinder head assembly contains the supplemental compressor. For this, the supplemental compressor can be integrated or mounted in the cylinder head or in the cylinder head cover. Formation of the spiral guide around the compressor wheel is possible directly on the cylinder head. When mounting the supplemental compressor drive at the cylinder head, vibration decoupling is beneficially executed. [0014]
  • Other beneficial executions of the invention provide for integration or building on the supplemental compressor in/at the air filter casing or also in/at the exhaust train. Here also, in a further developed execution, the spiral guide around the compressor wheel is formed directly at the air filter casing or in the exhaust train, and the supplemental compressor drive is mounted with vibration decoupling. In a further developed execution of the invention, when arranging the components in the exhaust, these are thermally decoupled, i.e. connecting using a flange with minimal heat conducting capabilities or shielding using a heat shield to minimize the temperature stress on the components. [0015]
  • It is beneficial to connect the heat produced by the drive using a coolant circuit corresponding with the supplemental compressor drive to cool the supplemental compressor drive when necessary. [0016]
  • In an especially beneficial execution of the invention, the switching/closing/or throttle means located in front of or behind the supplemental compressor could also be integrated or built into the following components: intake pipe/cylinder head cover/air filter casing/exhaust train. In a further developed execution—if the supplemental compressor is used as a secondary air pump—the secondary air conduit can also be integrated into or mounted into the mentioned components. The same is possible for the exhaust gas recirculation conduit and the engine ventilation. In the same way, it is possible to integrate the on board diagnostic (OBD) monitor and the sensors in the same assemblies. The turbocharger compressor can also be integrated or build into the components in an especially preferred execution. [0017]
  • A very compact and cost-effective construction is achieved with the mentioned executions where the supplemental compressor is integrated in the assemblies of the internal combustion engine, so that, for example, when used in motor vehicles, the supplemental compressor barely requires additional space compared to the conventional internal combustion engines. Because especially short pipes (air, gas and coolant pipes) are used with these integral constructions, waste and leak risks are minimized. [0018]
  • In an especially beneficial execution, the invention includes control of the supplemental compressor. In a first execution, this control is integrated into the internal combustion engine's control. In a further developed form of the invention, the electronic control of the supplemental compressor is separate from the internal combustion engine's control, where especially advantageous parameters of the engine performance conditions represent an input quantity of the control electronics. [0019]
  • In another beneficial execution of the invention, the internal combustion engine's control is split into partial or subcomponent systems, wherein the control of the supplemental compressor is connected to the entire system as a partial system. The individual partial systems communicate with each other using a bus system (CAN-Bus). Benefits of this subdivision are the simple monitoring and programming of the partial system. [0020]
  • In an especially beneficial execution of the invention, the vehicle's entire system is split into partial systems (system islands). The control of the supplemental compressor is incorporated in such a partial system; the partial systems communicate with each other using a bus system (CAN-Bus). An advantage of this execution is the possibility to match the individual systems with each other optimally, so that the primary goal is optimally adjusting the fuel consumption for the power output as currently or instantaneously necessary for the internal combustion engine. Additional advantages are the simple monitoring and programming of the partial systems and the possibility to add additional components of control without great effort.[0021]
  • Preferred executions of the invention are explained in references to the attached drawings. They show in: [0022]
  • FIG. 1 a schematic representation of an internal combustion engine with one-step turbocharging and an supplemental compressor powered by an electric motor in a first execution based on the invention. [0023]
  • FIG. 2 a schematic of an internal combustion engine with simple turbocharging and supplemental compressor with secondary air channels, turbine bypass and exhaust return. [0024]
  • FIG. 3 a schematic of an internal combustion engine with simple turbocharging and supplemental compressor with secondary air channels, turbine bypass and exhaust return, with the supplemental compressor integrated into the intake pipe assembly. [0025]
  • FIG. 4 a schematic of an internal combustion engine with simple turbocharging and supplemental compressor with secondary air channels, turbine bypass and exhaust return, with the supplemental compressor integrated into the cylinder head assembly. [0026]
  • FIG. 5 a schematic of an internal combustion engine with simple turbocharging and supplemental compressor with secondary air channels, turbine bypass and exhaust return, with the supplemental compressor integrated into the air filter casing assembly. [0027]
  • FIG. 6 a schematic of an internal combustion engine with simple turbocharging and supplemental compressor with secondary air channels, turbine bypass and exhaust return, with the supplemental compressor integrated into the exhaust train assembly. [0028]
  • FIG. 7 a schematic of a control for the supplemental compressor integrated into the engine control. [0029]
  • FIG. 8 a schematic of a control for the supplemental compressor separate from the engine control. [0030]
  • FIG. 9 a schematic of an engine control split into partial systems, including the control of the supplemental compressor as a partial system. [0031]
  • FIG. 10 a schematic of a vehicle entire system split into partial systems, including the control of the supplemental compressor as a partial system.[0032]
  • FIG. 1 shows an [0033] internal combustion engine 1, which on the fresh gas side 2 is connected to the compressor of a turbocharger 3 and a supplemental compressor 4. The supplemental compressor 4 is connected to the turbocharger compressor 3 in series, and arranged, in the flow direction, in front of the turbocharger compressor 3. The supplemental compressor 4 is powered by an electric motor 5. The turbine 7 of the turbocharger is connected to the internal combustion engine 1 on the exhaust side 6. A closing or switching means 8 is arranged between the supplemental compressor 4 and the turbocharger compressor 3. Using the switch means 8, the turbocharger compressor 3 can draw from its own intake area 9 as well as from the supplemental compressor 4. The supplemental compressor 4 draws from the intake area 10. If necessary, two air mass measurers or meters as well as two filters are provided.
  • FIG. 2 shows an internal combustion engine with simple turbocharging and an electrically powered supplemental compressor, where the main design corresponds with FIG. 1. A closing means [0034] 11 is arranged in flow direction behind the supplemental compressor 4, parallel to the closing or switching means 8, with which the mass flow in the secondary air channels 12 can be controlled. A charge cooler 13 is arranged in flow direction behind the turbocharger compressor 3, which cools the fresh compressed gas before entry into the internal combustion engine 1. Operation without turbocharging is possible with a bypass 14, which diverts exhaust gas to the exhaust side of the turbine 7 of the turbocharger. The switching means 15 controls the mass flow, which is conducted on the fresh gas side using the exhaust return 16.
  • FIG. 3 shows an internal combustion engine with all components from FIG. 2. In this execution, the [0035] intake pipe assembly 18 includes the intake pipe 17, a throttle valve 19 and a supplemental compressor 4, arranged sequentially going in the upstream direction. In addition, drive 5 of the supplemental compressor 4 and the switching or throttling means 20 are arranged in front of and behind the supplemental compressor 4 in the intake pipe assembly 18. Supplemental compressor 4 and turbocharger compressor 3 draw raw air from the same intake area 9, in which the air mass meter 21 and air filter 22 are connected.
  • FIG. 4 shows the schematic of an internal combustion engine in which the [0036] cylinder head assembly 23 includes the supplemental compressor 4, its drive 5 and the closing or switching means. Integrating the supplemental compressor 4 and mounting the drive 5 in the or at the cylinder head cover 1.1 is beneficial.
  • FIG. 5 shows the schematic of an internal combustion engine, in which the air [0037] filter casing assembly 24 incorporates the supplemental compressor, its drive 5, the closing or switching means 20 which are arranged in front of the supplemental compressor 4 in flow direction, the air mass measurer 21 and the air filter 22.
  • FIG. 6 shows the schematic of an internal combustion engine, in which the [0038] exhaust train assembly 25 incorporates the supplemental compressor 4, its drive 5, compressor 3 and turbine 7 of the turbocharger, the charge cooler 13 and the closing or switching means 20.
  • FIG. 7 shows the schematic of an internal combustion engine, in which the [0039] control 40 of the supplemental compressor is integrated into the engine control 41.
  • FIG. 8 shows an internal combustion engine with a [0040] control 40 of the supplemental compressor which is separately executed from the engine control 41, where the parameters of the engine operational condition are input quality of the control electronics of the supplemental compressor.
  • FIG. 9 shows the schematic of an engine control split into partial systems, where, for example, the partial system of [0041] control 40 of the supplemental compressor, the control of the partial system 42 of the intake pipe, of the partial system 43 of the injection and the partial system 44 of the air filter are represented. Additional partial systems are indicated. The partial systems communicate with each other using the bus system 45 (CAN-bus).
  • FIG. 10 shows the schematic of a vehicle entire system split into partial systems, where, for example the [0042] partial system 40 of the control of the supplemental compressor, the partial system 46 (drive train), the partial system 47 (ABS), the partial system 48 (chassis), the partial system 49 (passenger compartment) and the partial system 50 for heating are represented. The partial systems communicate with each other using the bus system 45 (CAN-bus).
  • Reference Number List
  • [0043] 1 internal combustion engine
  • [0044] 2 fresh gas side
  • [0045] 3 turbocharger compressor
  • [0046] 4 supplemental compressor
  • [0047] 5 electric motor
  • [0048] 6 exhaust gas side
  • [0049] 7 turbine
  • [0050] 8 switch means
  • [0051] 9 intake area
  • [0052] 10 intake area
  • [0053] 11 closing means
  • [0054] 12 secondary air channels
  • [0055] 13 charge cooler
  • [0056] 14 bypass
  • [0057] 15 adjusting means
  • [0058] 16 exhaust return
  • [0059] 17 intake pipe
  • [0060] 18 intake pipe assembly
  • [0061] 19 throttle valve
  • [0062] 20 switching means
  • [0063] 21 air mass measurer
  • [0064] 22 air filter
  • [0065] 23 cylinder head assembly
  • [0066] 24 air filter casing assembly
  • [0067] 25 exhaust train assembly
  • [0068] 40 controller
  • [0069] 41 engine control
  • [0070] 42 partial system for the intake pipe
  • [0071] 43 partial system for the injection
  • [0072] 44 partial system for the air filter
  • [0073] 45 bus system
  • [0074] 46 partial system for the drive train
  • [0075] 47 ABS
  • [0076] 48 partial system for the chassis
  • [0077] 49 partial system for the passenger compartment
  • [0078] 50 partial system for the heating

Claims (49)

1. Charged Internal Combustion Engine
1.1 with at least one-step charging by a turbocharger,
1.2 identified by the fact that at least one supplemental compressor is connected to the turbocharger parallel or in series;
1.3 the supplemental compressor has a drive independent from the working medium cycle of the internal combustion engine.
2. Internal combustion engine based on
claim 1
, identified by the fact that the additional compressor is powered by an electric motor.
3. Internal combustion engine based on
claim 1
or
2
, identified by the fact that the supplemental compressor is arranged in front of the turbocharger in the flow direction.
4. Internal combustion engine based on one of the
claims 1
to
3
, identified by the fact that there is at least one closing or switching means between the supplemental compressor and the turbocharger.
5. Internal combustion engine based on one of the
claims 1
to
4
, identified by the fact that the turbocharger has a charge cooler attached behind it, or with multi-level charging, at least one charge cooler is connected behind one level.
6. Internal combustion engine based on one of the
claims 1
to
5
, identified by the fact that the turbocharger has a charge cooler attached behind it, or with multi-level charging, at least one charge cooler is connected behind one level.
7. Internal combustion engine based on one of the
claims 1
to
6
, identified by the fact that the supplemental compressor is used as a secondary air pump to draw air in a catalytic converter.
8. Internal combustion engine based on one of the
claims 1
to
7
, identified by the fact that an electric engine which provides power to the supplemental compressor is present.
9. Internal combustion engine based on one of the
claims 1
to
8
, identified by the fact that an electronic control device is present to power the supplemental compressor and the closing or switching means.
10. Internal combustion engine based on one of the
claims 1
to
9
, identified by the fact that the supplemental compressor aids the turbocharger in operational conditions in which the power taken from the exhaust flow is insufficient.
11. Internal combustion engine based on one of the
claims 1
to
10
, identified by the fact that the supplemental compressor is turned off by the turbocharger when the required boost pressure is attained.
12. Internal combustion engine based on one of the
claims 1
to
10
, identified by the fact that the supplemental compressor is used to deliberately increase the boost pressure.
13. Internal combustion engine based on one of the
claims 1
to
12
, identified by the fact that the supplemental compressor and the turbocharger draw from different intake areas.
14. Internal combustion engine based on one of the
claims 1
to
12
, identified by the fact that the supplemental compressor and the turbocharger draw from the same intake area.
15. Internal combustion engine based on one of the
claims 1
to
14
, identified by the fact that the air compressed by the supplemental compressor can only flow in the direction of the turbocharger.
16. Internal combustion engine based on one of the
claims 1
to
15
, identified by the fact that the turbocharger no longer draws from the supplemental compressor, once the supplemental compressor is switched off.
17. Internal combustion engine based on one of the
claims 1
to
16
, identified by the fact that there is at least one supplemental compressor with at least one step is connected in series with turbocharger.
18. Internal combustion engine based on one of the
claims 1
to
16
, identified by the fact that there is at least one supplemental compressor with at least one step is connected parallel with turbocharger.
19. Internal combustion engine based on
claim 2
, identified by the fact that the electric motor is powered by the 12-volt electrical system.
20. Internal combustion engine based on one of the
claims 1
to
19
, identified by the fact that the intake pipe assembly (18) includes the supplemental compressor.
21. Internal combustion engine based on
claim 20
, identified by the fact that the supplemental compressor is integrated in the intake pipe.
22. Internal combustion engine based on
claim 20
, identified by the fact that the supplemental compressor is built is onto the intake pipe.
23. Internal combustion engine based on one of the
claims 1
to
19
, identified by the fact that the cylinder head assembly (23) includes the supplemental compressor.
24. Internal combustion engine based on
claim 23
, identified by the fact that the supplemental compressor (4) is integrated in the cylinder head or cylinder head cover.
25. Internal combustion engine based on
claim 23
, identified by the fact that the supplemental compressor (4) is built onto the cylinder head or cylinder head cover.
26. Internal combustion engine based on one of the
claims 1
to
19
, identified by the fact that the air filter assembly (24) includes the supplemental compressor (4).
27. Internal combustion engine based on
claim 26
, identified by the fact that the supplemental compressor (4) is integrated in the air filter casing.
28. Internal combustion engine based on
claim 26
, identified by the fact that the supplemental compressor (4) is built onto the air filter casing.
29. Internal combustion engine based on one of the
claims 1
to
19
, identified by the fact that the exhaust assembly (25) includes the supplemental compressor (4).
30. Internal combustion engine based on
claim 29
, identified by the fact that the supplemental compressor is integrated in the exhaust drive.
31. Internal combustion engine based on
claim 29
, identified by the fact that the supplemental compressor (4) is built onto the exhaust drive.
32. Internal combustion engine based on one of the
claims 20
to
31
, identified by the fact that the spiral conduction is formed around the compressor running wheel directly in the component incorporating the compressor.
33. Internal combustion engine based on one of the
claims 20
to
32
, identified by the fact that the drive (5) of the supplemental compressor (4) is mounted vibration decoupling in the assembly which incorporates the supplemental compressor (4).
34. Internal combustion engine based on one of the
claims 1
to
33
, identified by the fact that the drive (5) of the supplemental compressor (4) is attached to the coolant circuit of the internal combustion engine in such a manner that the heat of the drive is dissipated.
35. Internal combustion engine based on one of the
claims 20
to
34
, identified by the fact that the assembly includes the closing or switching means (20) in front of or behind the supplemental compressor (4) includes.
36. Internal combustion engine based on one of the
claims 20
to
35
, identified by the fact that the assembly (12) includes the secondary air channels (12).
37. Internal combustion engine based on one of the
claims 20
to
36
, identified by the fact that the assembly includes the exhaust return (16).
38. Internal combustion engine based on one of the
claims 20
to
37
, identified by the fact that the assembly includes the engine ventilation.
39. Internal combustion engine based on one of the
claims 20
to
38
, identified by the fact that the assembly includes the on board diagnostic monitoring and/or the sensors.
40. Internal combustion engine based on one of the
claims 20
to
39
, identified by the fact that the assembly includes the turbocharger.
41. Internal combustion engine based on one of the
claims 29
to
40
, identified by the fact that the components in or at the exhaust area are thermally decoupled.
42. Internal combustion engine based on one of the
claims 1
to
41
, identified by the fact that the internal combustion engine includes a control of the supplemental compressor.
43. Internal combustion engine based on
claim 42
, identified by the fact that the control of the supplemental compressor is integrated into the internal combustion engine control.
44. Internal combustion engine based on
claim 42
, identified by the fact that the control of the supplemental compressor is separate from the internal combustion engine control.
45. Internal combustion engine based on
claim 44
, identified by the fact that the parameters of the engine operational condition is an input quantity of the control electronics.
46. Internal combustion engine based on
claim 42
, identified by the fact that the control of the supplemental compressor is a partial system in the central the internal combustion engine control.
47. Internal combustion engine based on
claim 46
, identified by the fact that the partial systems are connected to each other with a bus system.
48. Internal combustion engine based on
claim 42
, identified by the fact that the control of the supplemental compressor a partial system of the vehicle system.
49. Internal combustion engine based on
claim 48
, identified by the fact that the partial systems are connected to each other with a bus system.
US09/836,787 2000-05-11 2001-04-17 Charged internal combustion engine Abandoned US20010054287A1 (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
US10/455,537 US6920755B2 (en) 2000-05-11 2003-06-05 Charged internal combustion engine
US10/455,536 US6889503B2 (en) 2000-05-11 2003-06-05 Charged internal combustion engine
US10/455,542 US6920756B2 (en) 2000-05-11 2003-06-05 Charged internal combustion engine

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE10023022A DE10023022A1 (en) 2000-05-11 2000-05-11 Supercharged internal combustion engine
DE10023022.9 2000-05-11

Related Child Applications (3)

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US10/455,537 Division US6920755B2 (en) 2000-05-11 2003-06-05 Charged internal combustion engine
US10/455,542 Division US6920756B2 (en) 2000-05-11 2003-06-05 Charged internal combustion engine
US10/455,536 Division US6889503B2 (en) 2000-05-11 2003-06-05 Charged internal combustion engine

Publications (1)

Publication Number Publication Date
US20010054287A1 true US20010054287A1 (en) 2001-12-27

Family

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Family Applications (4)

Application Number Title Priority Date Filing Date
US09/836,787 Abandoned US20010054287A1 (en) 2000-05-11 2001-04-17 Charged internal combustion engine
US10/455,537 Expired - Fee Related US6920755B2 (en) 2000-05-11 2003-06-05 Charged internal combustion engine
US10/455,542 Expired - Fee Related US6920756B2 (en) 2000-05-11 2003-06-05 Charged internal combustion engine
US10/455,536 Expired - Fee Related US6889503B2 (en) 2000-05-11 2003-06-05 Charged internal combustion engine

Family Applications After (3)

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US10/455,537 Expired - Fee Related US6920755B2 (en) 2000-05-11 2003-06-05 Charged internal combustion engine
US10/455,542 Expired - Fee Related US6920756B2 (en) 2000-05-11 2003-06-05 Charged internal combustion engine
US10/455,536 Expired - Fee Related US6889503B2 (en) 2000-05-11 2003-06-05 Charged internal combustion engine

Country Status (4)

Country Link
US (4) US20010054287A1 (en)
EP (1) EP1154133B1 (en)
JP (1) JP2002021573A (en)
DE (2) DE10023022A1 (en)

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DE60114920D1 (en) 2005-12-22
EP1154133A3 (en) 2003-01-02
US20030196436A1 (en) 2003-10-23
US6920755B2 (en) 2005-07-26
DE60114920T2 (en) 2006-07-20
EP1154133A2 (en) 2001-11-14
US20030192313A1 (en) 2003-10-16
DE10023022A1 (en) 2001-11-22
US20030192312A1 (en) 2003-10-16
US6889503B2 (en) 2005-05-10
EP1154133B1 (en) 2005-11-16
JP2002021573A (en) 2002-01-23
US6920756B2 (en) 2005-07-26

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Effective date: 20010330

STCB Information on status: application discontinuation

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