EP3555448A1 - Verfahren zur prüfung der dichtheit eines kraftstofftanksystems einer brennkraftmaschine - Google Patents
Verfahren zur prüfung der dichtheit eines kraftstofftanksystems einer brennkraftmaschineInfo
- Publication number
- EP3555448A1 EP3555448A1 EP17811952.5A EP17811952A EP3555448A1 EP 3555448 A1 EP3555448 A1 EP 3555448A1 EP 17811952 A EP17811952 A EP 17811952A EP 3555448 A1 EP3555448 A1 EP 3555448A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- compressor
- air line
- internal combustion
- combustion engine
- scavenging air
- 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
- 238000002485 combustion reaction Methods 0.000 title claims abstract description 71
- 239000002828 fuel tank Substances 0.000 title claims abstract description 58
- 238000000034 method Methods 0.000 title claims abstract description 30
- 238000012360 testing method Methods 0.000 title claims abstract description 15
- 238000007789 sealing Methods 0.000 title abstract 5
- 239000000446 fuel Substances 0.000 claims abstract description 79
- 239000003570 air Substances 0.000 claims description 86
- 230000002000 scavenging effect Effects 0.000 claims description 77
- 239000012080 ambient air Substances 0.000 claims description 18
- 238000003745 diagnosis Methods 0.000 claims description 6
- 238000011144 upstream manufacturing Methods 0.000 claims description 6
- 230000007613 environmental effect Effects 0.000 claims description 5
- 238000004891 communication Methods 0.000 claims description 3
- 239000012530 fluid Substances 0.000 claims description 3
- 238000010926 purge Methods 0.000 abstract description 17
- 238000013022 venting Methods 0.000 abstract description 7
- 239000007789 gas Substances 0.000 description 68
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical class [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 24
- 238000009423 ventilation Methods 0.000 description 8
- 238000011010 flushing procedure Methods 0.000 description 5
- 238000010586 diagram Methods 0.000 description 4
- 238000013461 design Methods 0.000 description 3
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000001704 evaporation Methods 0.000 description 2
- 238000001914 filtration Methods 0.000 description 2
- 230000010354 integration Effects 0.000 description 2
- 238000011068 loading method Methods 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 230000003213 activating effect Effects 0.000 description 1
- 230000004913 activation Effects 0.000 description 1
- 239000010725 compressor oil Substances 0.000 description 1
- 125000004122 cyclic group Chemical group 0.000 description 1
- 239000002283 diesel fuel Substances 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000011156 evaluation Methods 0.000 description 1
- 230000008020 evaporation Effects 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 230000008929 regeneration Effects 0.000 description 1
- 238000011069 regeneration method Methods 0.000 description 1
- 238000001179 sorption measurement Methods 0.000 description 1
- 238000009834 vaporization Methods 0.000 description 1
- 230000008016 vaporization Effects 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D41/00—Electrical control of supply of combustible mixture or its constituents
- F02D41/0025—Controlling engines characterised by use of non-liquid fuels, pluralities of fuels, or non-fuel substances added to the combustible mixtures
- F02D41/003—Adding fuel vapours, e.g. drawn from engine fuel reservoir
- F02D41/0032—Controlling the purging of the canister as a function of the engine operating conditions
- F02D41/0035—Controlling the purging of the canister as a function of the engine operating conditions to achieve a special effect, e.g. to warm up the catalyst
- F02D41/0037—Controlling the purging of the canister as a function of the engine operating conditions to achieve a special effect, e.g. to warm up the catalyst for diagnosing the engine
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M25/00—Engine-pertinent apparatus for adding non-fuel substances or small quantities of secondary fuel to combustion-air, main fuel or fuel-air mixture
- F02M25/08—Engine-pertinent apparatus for adding non-fuel substances or small quantities of secondary fuel to combustion-air, main fuel or fuel-air mixture adding fuel vapours drawn from engine fuel reservoir
- F02M25/0809—Judging failure of purge control system
- F02M25/0818—Judging failure of purge control system having means for pressurising the evaporative emission space
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M25/00—Engine-pertinent apparatus for adding non-fuel substances or small quantities of secondary fuel to combustion-air, main fuel or fuel-air mixture
- F02M25/08—Engine-pertinent apparatus for adding non-fuel substances or small quantities of secondary fuel to combustion-air, main fuel or fuel-air mixture adding fuel vapours drawn from engine fuel reservoir
- F02M25/089—Layout of the fuel vapour installation
-
- 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
Definitions
- the invention relates to a method for testing the tightness of a fuel tank system of an internal combustion engine
- Fuel tank systems for internal combustion engines of motor vehicles regularly have a vent line, which makes it possible to relieve an increasing pressure in the fuel tank of the tank system due to, for example, at high ambient temperatures evaporating fuel to the environment. Due to emission regulations, no fuel vapors should enter the environment as far as possible. This is prevented by integrating into the vent line a fuel vapor filter, usually in the form of an activated carbon filter, which absorbs the fuel vapors.
- such tank systems are additionally provided with a scavenging air line, which is connected on the one hand to the fuel vapor filter and on the other hand to the fresh gas train of the internal combustion engine.
- a scavenging air line which is connected on the one hand to the fuel vapor filter and on the other hand to the fresh gas train of the internal combustion engine.
- ambient air can be temporarily supplied via an environmental orifice of the vacuum prevailing in the region of the mouth of the scavenging air line in the fresh gas line
- the purge air line is emptied of fuel vapors still present in it, to prevent these fuel vapors from entering the environment via the fresh gas line.
- the compressor thereby conveys the gases contained in the vent line and also via the fresh gas line via the Fuel vapor filter and the ambient air line into the environment, the fuel vapor filter filters out the fuel vapor.
- a lack of tightness of a ventilation system of a tank system would lead to an uncontrolled escape of fuel vapors into the environment, which should be avoided.
- a tank ventilation system for an internal combustion engine with a fuel tank, a, activated carbon filter, a tank vent valve and at least one check valve is known. Between the tank vent valve and the check valve, a pressure sensor is arranged. To diagnose the tank venting system, a vacuum is set between the tank vent valve and the check valve that is less than the ambient pressure. The set pressure is changed by activating the tank venting valve. The change in the pressure in the line between the tank venting valve and the check valve is measured by means of the pressure sensor and associated with the activation of the tank venting valve. From the correlation of the opening state of
- Tank bleeder valve and the check valve is based on the function of
- Tank vent line, the check valve and the tank vent valve closed In particular, it can also be concluded that the tightness of the tank ventilation system in the section between the tank vent valve and the check valve. However, it is not possible to check the tightness of the remaining sections of the tank ventilation system.
- DE 10 2012 218 933 A1 discloses a method for determining the loading of an activated carbon filter in a tank ventilation system, wherein the tank ventilation system comprises at least a first valve between a fuel tank and the activated carbon filter and at least a second valve between the activated carbon filter and an intake pipe of an internal combustion engine.
- the tank ventilation system comprises at least a first valve between a fuel tank and the activated carbon filter and at least a second valve between the activated carbon filter and an intake pipe of an internal combustion engine.
- the loading of the activated carbon filter with the gas volume can be effected by means of a compressor which is part of a known module for the diagnosis of tank leaks, which is arranged on the side of a ventilation opening of the activated carbon filter and is in fluid communication with the environment via a fresh air filter.
- the invention has for its object to provide an advantageous way to check the tightness of a fuel tank system of an internal combustion engine.
- a method for testing the tightness (at least of a section) of a fuel tank system of an internal combustion engine, in particular an internal combustion engine of a motor vehicle comprises at least one fuel tank, a fuel vapor filter (preferably a sorption filter, in particular an activated carbon filter) in fluid communication with an environmental orifice, a vent line leading from the fuel tank to the fuel vapor filter, one leading from the fuel vapor filter to a fresh gas line of the internal combustion engine Spüllufttechnisch, integrated in the scavenging air, preferably driven by an electric motor
- Compressor i.e., a device for conveying gases
- shut-off valve integrated in the scavenging air line, which is connected between an opening of the scavenging air line in the
- Fresh gas train and the compressor is arranged.
- the parameter of an operating parameter of the compressor (64) or the pressure in at least one section of the scavenging air line (16 ) corresponds, with an associated, this operating state representing setpoint or setpoint range, the one
- Fuel tank system) to perform a test for sufficient tightness by a defined pressure level is generated in the corresponding section of the scavenging air line through the compressor and one or more operating parameters of the compressor, in particular the strength of the electric current applied to a drive motor of the compressor to realize the pressure level will be compared, and / or the thereby adjusting input speed of the compressor, with associated setpoint (s) which, for example, by tests on the same or a similar fuel tank system in a (known) Condition sufficient tightness of the section to be tested have been determined. For certain deviations of the currently determined operating parameters compared to the associated setpoint (range) s can then be concluded that insufficient tightness.
- the compressor in at least a portion of the scavenging air line to carry out a test for sufficient tightness by the compressor with at least one defined operating parameters, for example, a predetermined speed or a predetermined current, operated and in the corresponding section of Spül Kunststofftechnisch the thereby adjusting pressure and / or one / the other of the operating parameters (each) with a
- Setpoint (range) is compared to infer from a possible deviation occurring on an insufficient tightness.
- An additional or even primary function of the compressor may be to ensure purging of the fuel vapor filter when there is no or too little pressure gradient from the ambient pressure to the pressure in the fresh gas train in the region of the mouth of the scavenge air line, so preferably a correspondingly powerful design of
- Compressor is provided.
- an inflow or outflow of gases into or out of the section of the scavenging air line to be tested is possible exclusively by means of or via the compressor .
- the shut-off valve should be closed as completely as possible.
- a defined opening of the shut-off valve can also define the defined operating state of the fuel tank system, which can also be variable, provided for carrying out the method.
- Drive speed of the compressor can be used, one of these parameters is used to define the operating state and the other two parameters or values determined for these parameters are compared with one setpoint or setpoint range.
- an overpressure or negative pressure To operate delivery direction to generate in the then to be tested section, an overpressure or negative pressure.
- This shut-off valve may preferably be kept closed when a check (also) of the between the compressor and the
- Fuel vapor filter lying section of the scavenging air line is performed.
- a fluid-conducting Connection between this section of the scavenging air line on the one hand and the vent line and thus also the fuel tank on the other hand in this case, not only the lying between the compressor and the fuel vapor filter section of the scavenging air line but at the same time in particular the vent line and the fuel tank can be checked for sufficient tightness ,
- a further preferred embodiment of a method according to the invention can be provided for use in an internal combustion engine, in which the scavenging air line is branched, wherein a first opening in the fresh gas line upstream of a in the
- Frischgasstrang integrated serving for charging an internal combustion engine of the internal combustion engine fresh gas compressor and a second mouth of the scavenging air line in the
- Fresh gas train is arranged downstream of the fresh gas compressor.
- the compressor between the branch on the one hand and the first mouth or the second mouth on the other hand be integrated into the scavenging air line. Further preferred is then still provided that even in the branch of the scavenging air, in which the compressor is not integrated, a
- shut-off valves of a fuel tank system to which the method of the invention may be applied may be active (controllable) or passive (i.e.
- Method be provided in an internal combustion engine, in which the fuel vapor filter, an (additional) Tankleckdiagnosemodul , for example, a tank leak diagnosis module, as described in DE 10 2012 218 933 A1, assigned. Then, in particular, it may be provided to check the section of the scavenging air line between the compressor on the one hand and the fuel vapor filter or the tank leak diagnosis module on the other hand and / or the vent line and the fuel tank by means of the tank leak diagnostic module with respect to a sufficient tightness, while (at the same time or offset in time) at least the section between the compressor on the one hand and the mouth of the scavenging air line in the fresh gas line or the interposed shut-off valve on the other hand
- inventive manner is checked for a sufficient tightness. In this way, a mass product available on the market and thus relatively
- inexpensive tank leak diagnostic module can be used to one or more
- a tank leak diagnosis module which may in particular also include an (additional) compressor, provided that an inventively provided, integrated in the scavenging air compressor would be omitted or at least not in shape a piston compressor but in the form of a
- Flow compressor (blower) is formed (because he is then sufficiently gas-permeable even at a standstill).
- this can be associated with disadvantages.
- this may be a pressure-resistant design of the fuel vapor filter and / or the integration of a further shut-off valve or other constructive measures, the flushing of the
- the method according to the invention can be used, in particular, in a fuel tank system of an internal combustion engine which includes an internal combustion engine operated according to the Otto principle because the fuel used for the operation of such internal combustion engines is relatively volatile (in particular compared to diesel fuel), which does not only the special need for tank ventilation but also a test of the tightness of the fuel tank system is justified.
- the term "fuel vapor filter” does not mean that it has to filter the volatile fuel in gaseous form. Rather, the fuel can already (partially) be condensed out again during the filtering.
- Fuel tank system of an internal combustion engine
- FIG. 2 shows in two diagrams the curves of the pressure in a section of the scavenging air line of an internal combustion engine according to FIG. 1 to be inspected for sufficient tightness and the current intensity and the input speed of the compressor used for the pressure generation at a defined leakage in comparison to the corresponding curves at the best possible tightness of the same section of the scavenging air duct;
- Fig. 3 a slightly modified to the fuel tank system according to FIG. 1
- Embodiment of a likewise suitable for carrying out a method according to the invention fuel tank system of an internal combustion engine.
- Fig. 1 shows a fuel tank system of an internal combustion engine.
- This comprises a fuel tank 10, which is connected via a vent line 12 with a fuel vapor filter 14, which may be formed in particular in the form of an activated carbon filter or at least one such.
- the fuel vapor filter 14 is further connected via a scavenging air line 16 to a fresh gas line 18 of the internal combustion engine, wherein the scavenging air line 16, starting from a branch 20 in two branches 22, 24, of which a first branch 22 in the fresh gas line 18 upstream (with respect
- the fresh gas compressor 28 is part of an exhaust gas turbocharger, which further comprises an exhaust gas turbine 30, which is integrated in an exhaust line 32 of the internal combustion engine.
- Combustion chambers 34 are used to move in the cylinders 36 longitudinal axial movable guided piston 38. These movements of the piston 38 (not shown) with the interposition of connecting rods in a rotational movement of a crankshaft translated (not shown), wherein the leadership of the piston 38 via the connecting rods by means of the crankshaft simultaneously to a cyclic reciprocating movement of the piston 38 leads.
- the resulting during combustion of the fresh gas-fuel mixtures in the combustion chambers 34 exhaust gas is discharged through the exhaust line 32 and flows through the exhaust gas turbine 30, resulting in a
- Turbine impeller is transmitted by means of a shaft 40 to a compressor impeller (not shown) of the fresh gas compressor 28, whereby the fresh gas compressor 28 provides for a compression of fresh gas via the fresh gas line 18 to the internal combustion engine 26 supplied fresh gas.
- the fuel vapor filter 14 of the fuel tank system stands with respect to the
- Vent line 12 and the scavenging air line 16 opposite side via an ambient air line 42 with an integrated (first) shut-off valve 44 with the environment in gas-conducting connection, to which the ambient air line 42 forms an environmental mouth 62.
- the first shut-off valve 44 is controllable by means of a control device 48 (for example the engine control of the internal combustion engine), i. this can be actively opened or closed.
- a basically known tank leak diagnostic module 46 can also be integrated into the ambient air line 42, in which case the first shut-off valve 44 can also be an integral part of the tank leak diagnosis module 46.
- the fuel tank 10 is partially filled with liquid fuel, wherein a portion of this fuel is vaporized, so that in the fuel tank 10 and fuel in the gaseous state is present.
- vaporization of fuel in the fuel tank 10 is enhanced by a relatively high temperature of the fuel, which is particularly the case at comparatively high ambient temperatures.
- the possibility of at least partial pressure equalization with the ambient pressure via the vent line 12 and the fuel vapor filter 14 as well as via the ambient air line 42 is avoided, whereby the fuel vapor filter 14 is avoided. that such pressure equalization leads to the escape of fuel vapors into the environment.
- Such a venting of the fuel tank leads to an increasing saturation of the
- Ambient air is sucked in via the ambient air line 42 and the first, then opened shut-off valve 44 integrated therein. This ambient air flows through the
- Fuel vapor filter 14 in compared to the flow in the venting of
- Fuel tanks 10 opposite flow direction, whereby in the
- Fuel vapor filter 10 absorbed fuel molecules are entrained by the ambient air and entered via the scavenging air line 16 in the fresh gas line 18, whereby this fuel combustion in the combustion chambers 34 of the engine 26 is supplied.
- Such purging of the fuel vapor filter 14 is provided only temporarily and always during operation of the internal combustion engine 26, because only then introduced by the purging of the fuel vapor filter 14 in the fresh gas line 18 fuel can be safely supplied to combustion in the combustion chambers 34.
- Ambient pressure to the pressure in the fresh gas line 18 in the region of the (second) orifice 52 of the second branch 24 of the scavenging air line 16 is often not even a pressure gradient but a pressure increase, because this second orifice 52 in the area between the
- Fresh gas compressor 28 and the internal combustion engine 26 extending charge air path of the fresh gas line 18 is located in which the fresh gas is often present due to the compression by the fresh gas compressor 28 at elevated pressure.
- this second orifice 52 (as close as possible) downstream of a throttle valve 54, it is possible to utilize a pressure reduction effected by the throttle valve 54; However, this pressure reduction is often not sufficient to actually realize a sufficient pressure drop across the scavenging air line 16.
- a check valve 56 is integrated, by which this branch 24 of the scavenging air line 16 is automatically closed when in the region of the second orifice 52, an overpressure in Compared to the located on the other side of the check valve portion of the second branch 24 of the scavenging air line 16 is present.
- an actively activatable (second) shut-off valve 58 by the control device 48 is integrated into the second branch 24 of the purging air line 16.
- shut-off valve 58 it is possible to dispense with the check valve 56 as a result of the arrangement of this shut-off valve 58, provided that the shut-off valve 58 is designed sufficiently overpressure-resistant (ie, this must remain sufficiently tightly closed at the at least temporary overpressures on the side of the charge air section of the fresh gas train 18).
- the first branch of the scavenging air line 22 opens into an upstream of the
- Fresh gas compressor 28 located portion of the fresh gas line 18, wherein in the portion of this branch 22 of the scavenging air line 16 between the fresh gas compressor 28 and this (first) orifice 50, a (third) shut-off valve 60 is integrated, which is arranged as close to the first orifice 50, or preferably in this is integrated.
- Ambient pressure may be present. However, this is not always the case, for example in an operation of a motor vehicle comprising the internal combustion engine with non-operated internal combustion engine (for example due to an automatic start / stop function).
- the fuel tank system of the internal combustion engine also comprises a compressor 64, also referred to as a "flushing pump", which can be in the form of a piston compressor and, for example, as a vane compressor.
- a compressor 64 By operation of this compressor 64 can actively ambient air over the
- Mouth 62 are sucked, which then flows through the fuel vapor filter 14 to the scavenging and via the compressor 64 to the first mouth 50 of the
- Fresh gas via the second orifice 52 from the charge air path of the fresh gas train 18th In a non-supercharged internal combustion engine without fresh gas compressor 28, a scavenging air line 16, which does not include the first branch 22, would be sufficient for scavenging the fuel vapor filter 14. In a supercharged internal combustion engine according to the
- the first branch 22 of the scavenging air line 16 may be necessary, since a rinse over only the second branch 24 is often not possible. Due to the current tendency to highly dethrottle the internal combustion engine 26 of an internal combustion engine, the use of the compressor 64 may be useful or necessary for sufficient purging of the fuel vapor filter 14.
- FIG. 2 shows, in two diagrams, the (simultaneous) courses on the one hand (upper diagram) of the current intensity I (course lines 68, 70) and on the other hand (lower diagram) of the pressure p (Gradient lines 72, 74) and the input speed n (Gradient lines 76, 78, as a percentage in
- Operating state (defined by the generated for the determination of the setpoint values or setpoint ranges mean pressure p) are compared, whether the then determined values or
- Value curves of these operating parameters have defined deviations from the desired values or setpoint ranges, from which then to a sufficient (no or below a threshold value deviations) or not sufficient (relatively large
- FIG. 3 shows an embodiment of an internal combustion engine in which the
- Fuel tank system compared to that of the internal combustion engine according to FIG. 1 is slightly modified. Specifically, it is provided that in the fuel tank system according to FIG. 1 in the second branch 24 of the scavenging air line 16 integrated second shut-off valve 58 upstream (with respect to the flow through the scavenging air line 16 when flushing the fuel vapor filter 14) of the branch 20 to order. With regard to the described with reference to FIGS. 1 and 2 test of the between the compressor 64 and the first orifice 50 associated third shut-off valve 60 arranged portion of the scavenging air line 16 has changed this
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Examining Or Testing Airtightness (AREA)
- Supplying Secondary Fuel Or The Like To Fuel, Air Or Fuel-Air Mixtures (AREA)
Abstract
Description
Claims
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102016225206.2A DE102016225206A1 (de) | 2016-12-15 | 2016-12-15 | Verfahren zur Prüfung der Dichtheit eines Kraftstofftanksystems einer Brennkraftmaschine |
PCT/EP2017/082114 WO2018108761A1 (de) | 2016-12-15 | 2017-12-11 | Verfahren zur prüfung der dichtheit eines kraftstofftanksystems einer brennkraftmaschine |
Publications (2)
Publication Number | Publication Date |
---|---|
EP3555448A1 true EP3555448A1 (de) | 2019-10-23 |
EP3555448B1 EP3555448B1 (de) | 2020-10-14 |
Family
ID=60654973
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP17811952.5A Active EP3555448B1 (de) | 2016-12-15 | 2017-12-11 | Verfahren zur prüfung der dichtheit eines kraftstofftanksystems einer brennkraftmaschine |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP3555448B1 (de) |
DE (1) | DE102016225206A1 (de) |
WO (1) | WO2018108761A1 (de) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102018111116B4 (de) | 2018-05-09 | 2020-06-18 | Eagle Actuator Components Gmbh & Co. Kg | Anordnung zum Regenerieren eines Aktivkohlefilters |
DE102021202516A1 (de) | 2021-03-15 | 2022-09-15 | Volkswagen Aktiengesellschaft | Verfahren zur Funktionsprüfung eines Kraftstofftanksystems einer Brennkraftmaschine |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE19639116B4 (de) * | 1996-09-24 | 2009-01-15 | Robert Bosch Gmbh | Tankentlüftungseinrichtung für Kraftfahrzeuge |
DE19829423B4 (de) * | 1998-07-01 | 2007-03-22 | Mahle Filtersysteme Gmbh | Einrichtung zur Entlüftung des Kraftstofftanks eines Verbrennungsmotors |
DE10006186C1 (de) * | 2000-02-11 | 2001-06-13 | Bosch Gmbh Robert | Verfahren zur Dichtheitsprüfung eines Tanksystems eines Fahrzeugs |
DE10018441B4 (de) * | 2000-04-13 | 2005-12-29 | Robert Bosch Gmbh | Verfahren und Vorrichtung zur umweltschonenden Dichtheitsprüfung eines Behältnisses |
DE102004030909A1 (de) | 2004-06-25 | 2006-01-19 | Mahle Filtersysteme Gmbh | Tankentlüftungssystem und zugehöriges Betriebsverfahren |
DE102011086946A1 (de) * | 2011-08-18 | 2013-02-21 | Robert Bosch Gmbh | Entlüftungssystem für einen Kraftstofftank |
DE102011084403A1 (de) | 2011-10-13 | 2013-04-18 | Robert Bosch Gmbh | Tankentlüftungssystem und Verfahren zu dessen Diagnose |
DE102012218933A1 (de) | 2012-10-17 | 2014-04-17 | Robert Bosch Gmbh | Verfahren zur Bestimmung der Beladung eines Aktivkohlefilters in einem Kraftstofftankentlüftungssystem |
DE102014216451A1 (de) * | 2014-08-19 | 2016-02-25 | Continental Automotive Gmbh | Kraftstofftanksystem |
DE102014217195A1 (de) * | 2014-08-28 | 2016-03-03 | Continental Automotive Gmbh | Verfahren zur Leckdiagnose in einem Kraftstofftanksystem |
US9771884B2 (en) * | 2014-10-31 | 2017-09-26 | GM Global Technology Operations LLC | System and method for controlling the amount of purge fluid delivered to cylinders of an engine based on an operating parameter of a purge pump |
DE102015209651B4 (de) * | 2015-05-27 | 2022-08-18 | Robert Bosch Gmbh | Tankentlüftungsanlage und Verfahren zur Diagnose einer Tankentlüftungsanlage |
JP2017203415A (ja) * | 2016-05-11 | 2017-11-16 | 愛三工業株式会社 | 蒸発燃料処理装置 |
-
2016
- 2016-12-15 DE DE102016225206.2A patent/DE102016225206A1/de not_active Withdrawn
-
2017
- 2017-12-11 WO PCT/EP2017/082114 patent/WO2018108761A1/de unknown
- 2017-12-11 EP EP17811952.5A patent/EP3555448B1/de active Active
Also Published As
Publication number | Publication date |
---|---|
DE102016225206A1 (de) | 2018-06-21 |
EP3555448B1 (de) | 2020-10-14 |
WO2018108761A1 (de) | 2018-06-21 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
DE102016210579B4 (de) | Dampfentlüftungssystem für einen verbrennungsmotor | |
WO2019121169A1 (de) | Vorrichtung zum betreiben eines tankentlüftungssystems einer brennkraftmaschine | |
DE102016210570A1 (de) | Tankentlüftungsmodul sowie Brennkraftmaschine mit derartigem Modul | |
EP3077654B1 (de) | Ventileinheit mit spülluftpumpe | |
DE19645382A1 (de) | Tankanlage für ein Fahrzeug mit Verbrennungsmotor | |
EP3092401B1 (de) | Verfahren zur leckdiagnose in einem kraftstofftanksystem | |
WO2015062792A1 (de) | Tankleckdiagnose mit kraftstofftank als druckspeicher | |
DE102018106441A1 (de) | Verfahren zum Betreiben einer Brennkraftmaschine und Brennkraftmaschine | |
DE102017108246A1 (de) | Verfahren zur Leckagebestimmung eines Kurbelgehäuseentlüftungssystems | |
EP2411653B1 (de) | Tankentlüftungsvorrichtung für eine aufgeladene brennkraftmaschine und zugehöriges steuerverfahren | |
EP3555448B1 (de) | Verfahren zur prüfung der dichtheit eines kraftstofftanksystems einer brennkraftmaschine | |
EP1377741B1 (de) | Beheizbare tankleckdiagnoseeinheit insbesondere für kraftfahrzeuge | |
WO2015185303A1 (de) | Aufgeladene brennkraftmaschine | |
EP3533985A1 (de) | Verfahren zum betreiben einer brennkraftmaschine, brennkraftmaschine und kraftfahrzeug | |
EP3559432B1 (de) | Kraftstofftanksystem und verfahren zur prüfung der dichtheit eines solchen kraftstofftanksystems | |
DE102009033451B4 (de) | Verfahren zum Überprüfen der Funktionsfähigkeit eines Ventils in einem Gaskanal einer Brennkraftmaschine sowie Steuervorrichtung | |
DE102017108249B4 (de) | Kurbelgehäuseentlüftungssystem, Verbrennungskraftmaschine und Verfahren zur Leckagediagnose eines Kurbelgehäuseentlüftungssystems | |
WO2020078789A1 (de) | Tankentlüftungsventileinheit | |
DE102016202140A1 (de) | Verbrennungsmotor mit Kurbelgehäuseentlüftung | |
DE102015007059A1 (de) | Vorrichtung zum Überprüfen der Dichtheit eines Tanks, insbesondere für ein Kraftfahrzeug | |
DE10163780B4 (de) | Entgasungseinrichtung für ein Kurbelgehäuse | |
EP4060179A2 (de) | Verfahren zur funktionsprüfung eines kraftstofftanksystems einer brennkraftmaschine | |
DE102016221901A1 (de) | Verfahren zur Steuerung einer Tankentlüftung für einen Kraftstofftank | |
DE102017213868A1 (de) | Verfahren zum Betreiben einer Brennkraftmaschine und Brennkraftmaschine | |
DE102021209762A1 (de) | Verfahren zum Betreiben einer Brennkraftmaschine mit Diagnose eines Tankabsperrventils |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: UNKNOWN |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE INTERNATIONAL PUBLICATION HAS BEEN MADE |
|
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 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE |
|
17P | Request for examination filed |
Effective date: 20190715 |
|
AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: GRANT OF PATENT IS INTENDED |
|
INTG | Intention to grant announced |
Effective date: 20200722 |
|
GRAS | Grant fee paid |
Free format text: ORIGINAL CODE: EPIDOSNIGR3 |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE PATENT HAS BEEN GRANTED |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: FG4D Free format text: NOT ENGLISH |
|
REG | Reference to a national code |
Ref country code: AT Ref legal event code: REF Ref document number: 1323834 Country of ref document: AT Kind code of ref document: T Effective date: 20201015 Ref country code: CH Ref legal event code: EP |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R096 Ref document number: 502017007789 Country of ref document: DE |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: FG4D Free format text: LANGUAGE OF EP DOCUMENT: GERMAN |
|
REG | Reference to a national code |
Ref country code: NL Ref legal event code: MP Effective date: 20201014 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: PT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210215 Ref country code: RS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20201014 Ref country code: FI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20201014 Ref country code: GR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210115 Ref country code: NO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210114 |
|
REG | Reference to a national code |
Ref country code: LT Ref legal event code: MG4D |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: ES Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20201014 Ref country code: BG Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210114 Ref country code: SE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20201014 Ref country code: PL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20201014 Ref country code: IS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210214 Ref country code: LV Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20201014 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: HR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20201014 Ref country code: NL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20201014 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R097 Ref document number: 502017007789 Country of ref document: DE |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: RO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20201014 Ref country code: SK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20201014 Ref country code: SM Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20201014 Ref country code: EE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20201014 Ref country code: CZ Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20201014 Ref country code: LT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20201014 |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: PL |
|
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 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MC Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20201014 Ref country code: DK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20201014 |
|
REG | Reference to a national code |
Ref country code: BE Ref legal event code: MM Effective date: 20201231 |
|
26N | No opposition filed |
Effective date: 20210715 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: AL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20201014 Ref country code: IE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20201211 Ref country code: IT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20201014 Ref country code: LU Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20201211 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LI Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20201231 Ref country code: SI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20201014 Ref country code: CH Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20201231 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20210214 Ref country code: TR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20201014 Ref country code: MT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20201014 Ref country code: CY Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20201014 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20201014 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: BE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20201231 |
|
P01 | Opt-out of the competence of the unified patent court (upc) registered |
Effective date: 20230523 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: GB Payment date: 20231219 Year of fee payment: 7 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: FR Payment date: 20231226 Year of fee payment: 7 Ref country code: DE Payment date: 20231231 Year of fee payment: 7 |
|
REG | Reference to a national code |
Ref country code: AT Ref legal event code: MM01 Ref document number: 1323834 Country of ref document: AT Kind code of ref document: T Effective date: 20221211 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: AT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20221211 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: AT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20221211 |