METHOD OF DETERMINING FUEL EVAPORATION FROM AN ENGINE OIL SUMP
20220333546 · 2022-10-20
Assignee
Inventors
Cpc classification
F02D41/22
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D2200/0608
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D2250/11
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01M2250/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D2250/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D2200/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01M11/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D2200/023
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
G01M15/042
PHYSICS
F02D41/0025
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F02D41/22
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01M11/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A method of determining the total evaporation rate of fuel from an oil sump of an engine comprising: a) defining for said fuel, a plurality (n-1) of zones, each zone comprising a separate temperature range, and corresponding to a particular fuel constituent portion; b) determining or estimating the mass of said particular fuel constituent portion present in the sump for each zone; c) for each zone, determining an evaporation rate based on oil temperature; and the corresponding mass determined in step b); d) summing the evaporation rates for each zone from step c) to provide said total evaporation rate.
Claims
1. A method of determining the total evaporation rate of fuel from an oil sump of an engine comprising: a) defining for said fuel, a plurality (n-1) of zones, each zone comprising a separate temperature range, and corresponding to a particular fuel constituent portion; b) determining or estimating the mass of said particular fuel constituent portion present in the sump for each zone; c) for each zone, determining an evaporation rate based on oil temperature; and the corresponding mass determined in step b); d) summing the evaporation rates for each zone from step c) to provide said total evaporation rate; e) indicating a fault situation of the engine or controlling the engine dependent on the total evaporation rate determined from step d) or a parameter derived thereform.
2. A method as claimed in claim 1 wherein in step c) the determination of evaporation rates assumes that all chemical components of each fuel constituent portion evaporate with same evaporation rate.
3. A method as claimed in claim 1 wherein in step c) the evaporation rate for the zone is determined form the following equation:
4. A method as claimed in claim 1 where one or more zones are selected such that the corresponding temperature ranges are such that the evaporation curve of the fuel is substantially linear within this range.
5. A method as claimed in claim 1 including integrating the total evaporation rate with respect to time to determine the amount of fuel removed from the sump during a time period.
6. A method as claimed in claim 1 including determining the amount of fuel in an oil sump dependent from said determined amount of fuel removed.
7. A method as claimed in claim 6 including determining the amount of fuel in the oil sump dependent additionally on an initial amount of fuel present in an oil sump minus the amount of fuel removed.
8. A method as claimed in claim 6 including determining the amount of fuel in the oil sump dependent additionally on the amount of fuel entering the sump during cranking and/or warm up.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0027] The present invention is now described by way of example with reference to the accompanying drawings in which:
[0028]
[0029]
[0030]
[0031]
[0032]
DESCRIPTION OF THE PREFERRED EMBODIMENTS
[0033] To recap, during the cranking, a mass from the injected fuel will enter in the oil sump.
[0034] So in other words on gasoline engines e.g. and especially with high percentage of ethanol, rich mixture is applied during crank and warm-up phases in the combustion chamber. Only a part depending on the fuel stoichiometry will burn. The rest either evacuates through the exhaust or enters the oil sump through piston walls. Risks with fuel entering the sump mean there is reduced lubrication capability, increased oil level and boil-off phenomena.
Fuel Entering Sump During Cranking
[0035] This mass of fuel entering the sumps during cranking depends on a number of factors: total mass of fuel injected during the cranking event; fuel ethanol percentage; engine temperature (oil or coolant); ambient temperature.
Fuel Entering the Sump During Warm-Up
[0036] During the warm-up, rich mixture is applied to have stoichiometric exhaust. A part from the unburnt fuel enters the oil sump. The mass entering the oil sump can also be regarded as depending on: the mass of unburnt fuel (mass injected x[1-“combustion efficiency”]); ethanol percentage; engine temperature (oil or coolant); ambient temperature; engine load.
[0037] When the oil temperature starts to rise, the fuel contained in the oil starts to evaporate. The vapors will enter the engine through the positive crankcase ventilation valve (PCV) (or blow-by). The PCV is closed under high load but the evaporating phenomena is assumed to be continuous. If boil-off is ignored: there will be mixture (Lambda) control perturbation; false fuel adaptation learning; false diagnostic faults raised; and problems with emission compliance.
[0038]
Invention
[0039] Gasoline is composed from different chemical components that evaporate at different temperatures: Depending on the temperature, a portion of the fuel is available to evaporate. Considering a short driving cycle, the prior art model will reduce the whole modeled fuel in oil whereas the fuel is not available to evaporate. The fuel that enters the oil sump is composed from different chemical components which evaporate at different temperatures. This leads to an evaporation fraction depending on temperature.
[0040] The problem of error in fuel deposit estimation and boil off rate is solved by taking into account the chemical components of fuel that is entering or in the oil sump.
[0041] The inventors have determined that more accurate boil-off estimation can be determined by considering the evaporation curve. In examples the evaporation curve is used and split into a plurality of temperature zones for the oil, where for each zone it is considered that a particular proportion of fuel is evaporated. This is shown in
[0042] So the problem of wrong estimation of fuel evaporating (fuel boil off estimation) from the oil is solved by treating fuel in respect of each of the zones (temperature ranges) referenced above separately, with separate evaporation rates and reducing the amount of evaporated fuel in the fuel boil off rate estimation only with respect to the affected zone(s). Each zone is assumed to correspond to chemical components which evaporates with same evaporation rate.
EXAMPLES
Fuel In Oil Deposit Estimation
[0043] In examples the (mass of) fuel, and thus the mass of fuel that enters the sump, and/or assumed to be in the in the oil sump is considered as comprising a plurality of components, each with different evaporation rates or characteristics depending on the temperature. Thus the mass of fuel is effectively split into a multi-zonal mass and each zone mass is considered separately in terms of determining the amount evaporated or in the sump. For each zone it is assumed that the fuel portion thereof is evaporated at a particular rate dependent on e.g. temperature
[0044]
[0045] Depending on the fuel mixture e.g. ethanol percentage (here it is 10%), then the proportion of the fuel with respect to (in) each zone may be determined or pre-estimated so preset. So all the fuel mass (that is modeled to enter, exist, and/or be evaporated from the oil sump) is allocated in the example to five different zones: So it is assumes that 10% of the fuel is in zone Z1; 30% is in the zone Z2; 20% is in the zone Z3; 30% is in the zone Z4; 10% is in a so called “Residual fuel” zone Z5.
[0046] The zones (defined by temperature ranges) may thus be considered as eluding to component portions of the fuel mix, the fuel mix assumed thus to have (“n”) constituent parts, each constituent part having a different but single evaporation characteristic. The last zone or residual zone may be assumed to remain unevaporated as the temperature of the engine may never reach that where any reasonable evaporation of constituents of that zone occurs.
[0047] The percentage constituent of each zone is calibratable e.g. can be pre-determined foe the methodology depending on fuel type/mixture e.g. ethanol percentage known by ethanol percentage estimation or ethanol sensor. The last zone is considered as residual fuel because the oil will never rarely exceed 140° C. so the quantity of the chemical components that enters in the oil sump will never be evaporated and will stay until oil change. This logic of splitting fuel into multi-zone model is shown in
[0048] Depending on the oil temperature (assumed to be the fuel in oil temperature), the separate the evaporation effect with respect to fuel in each zone can be determined separately (independently) for a boil-off rate estimation.
Fuel Boil-Off Rate Estimation
[0049] Each zone is assumed to content chemical components that follow an Arhenius law to evaporate. Arhenius law is defined by:
[0050] k(T) is the reaction rate s.sup.−1
[0051] R is the gas constant (8.31 J.K.sup.−1.Math.mol.sup.−1)
[0052] T is temperature (in K)
[0053] E is activation energy (in J.Math.mol.sup.−1)
[0054] a is pre-exponential factor or frequency of collision (s.sup.−1)
[0055] K(T) is a reaction rate, multiplied by the mass, you have an evaporation rate (boil-off rate)
[0056] {dot over (m)}=m×K(T). {dot over (m)} is the boil-off rate, m the mass able to boil-off, K(T) reaction rate
[0057] Each zone has and is assumed to have its own pre-exponential factor and activation energy which allow separately each evaporation rate of each zone to be determined.
[0058] Zone 1 evaporates only starting from 35° C. Zone 2 from 54° C., zone 3 from 70° C., zone 4 from 105° C. (for the example of E10).
[0059] To compute the evaporating fuel rate for each zone, the mass of fuel contained in the actual zone is multiplied by the reaction rate for the actual engine temperature.
[0060] Where n is the zone number. So this may be computed a plurality of zones, e.g. preferably this is calculated for each zone, or each zone minus the residual zone where appropriate. So for zone 1 this is:
[0061] In the example, the total evaporating fuel (boil-off rate) is the summation of the four evaporating flows for zones Z1, Z2, Z3, Z4 is as follows:
{dot over (m)}.sub.Boiloff=m.sub.z1+m.sub.z2+m.sub.z3+m.sub.z4
[0062] In the example the evaporating flow is for zone 5 is ignored i.e. assumed to be zero.
[0063]
[0064] In other examples, the total evaporating fuel (boil-off rate) is the summation of the five evaporating flows for zones Z1, Z2, Z3, Z4 and Z5
{dot over (m)}.sub.Boiloff=m.sub.z1+m.sub.z2+m.sub.z3+m.sub.z4+m.sub.z5
[0065] The value of the total (i.e. aggregate) boil-off rate can be used in models to determine the total fuel in the oil, as well as for determining engine control parameters such as injection correction
[0066] For example, a model can be provided similar to that of
[0067] Fuel entering in the sump may be divided into separate masses with respect to each zone in the multi-zone model. The evaporation rate is physical based. Therefore, the model is more accurate and more sensitive to normal driving conditions (short trip without complete warming of oil). Another big advantage of this model is to be able to raise the information to the driver that the quantity of the fuel in the oil is very high and can lead to engine damage if the driver repeats short trip operations.