METHOD FOR CALCULATING REACTION HEAT IN AN EXHAUST SYSTEM
20240209767 ยท 2024-06-27
Inventors
- Elke Baeder (Stuttgart, DE)
- Sascha Giese (Ludwigsburg, DE)
- Thomas Zein (Sindelfingen, DE)
- Michael Stein (Loechgau, DE)
- Patrick Thierfelder (Leonberg, DE)
Cpc classification
F01N2900/1631
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N9/005
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N2900/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N2900/0412
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N2900/1411
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N11/005
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N2900/1402
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N2900/0414
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N2900/1621
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N2900/0601
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N2900/1624
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
Abstract
A method for calculating reaction heat in an exhaust system of an internal combustion engine by means of a model, comprising a first model component and a second model component, wherein the first model component refers to a calculation of exhaust components flowing from valves of the internal combustion engine, the second model component relates to the entire exhaust system, and total masses from the first model component are divided along the exhaust system onto the individual components of the exhaust system.
Claims
1. A method for calculating reaction heat in an exhaust system (300) of an internal combustion engine by means of a computer configured with a model (312) having a first model component (10, 314) and a second model component (150, 316), wherein the computer, via the first model component (10, 314), calculates exhaust components flowing from valves of the internal combustion engine, and the computer, via the second model component (150, 316) divides total masses from the first model component (10, 314) along the exhaust system between individual components (302) of the exhaust system (300).
2. The method according to claim 1, wherein the incompletely combusted (rich) exhaust components and air flowing directly into the exhaust system (300) are calculated in a cylinder-specific manner in the first model component (10, 314).
3. The method according to claim 2, wherein the cylinder-specific calculation from the current engine operational variables covers at least one special mode of operation.
4. The method according to claim 3, wherein the at least one special mode of operation is selected from a group consisting of: overrun shut-off, cylinder suppression, half-engine operation, purging, and cylinder balance.
5. The method according to claim 1, wherein the dividing is carried out in the second model component (150, 316) depending on the mass flow rate and the volume of the components (302).
6. The method according to claim 1 wherein, in the second model component (150, 316), a storage of a portion of the residual gases into the catalyst surface is modeled depending on an applied adsorption efficiency.
7. An assembly for calculating reaction heat in an exhaust system (300) configured to perform a method according to claim 1.
8. A non-transitory, computer-readable medium containing instructions that when executed by the computer cause the computer to calculate reaction heat in an exhaust system (300) of an internal combustion engine by means of a model (312) having a first model component (10, 314) and a second model component (150, 316), by calculating, via the first model component (10, 314), exhaust components flowing from valves of the internal combustion engine, and divide, via the second model component (150, 316), total masses from the first model component (10, 314) along the exhaust system between individual components (302) of the exhaust system (300).
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0022]
[0023]
[0024]
[0025]
[0026]
DETAILED DESCRIPTION
[0027] The invention is illustrated schematically in the drawings on the basis of embodiments and is described in detail below with reference to the drawings.
[0028]
[0050] Output variables are control unit signals: [0051] fuel equivalent oxygen mass flow at exhaust valve bank 1 (reference numeral 60), [0052] oxygen mass flow at exhaust valve bank 1 (reference numeral 62),
[0053]
[0054] Input variables are: [0055] calculate function command (reference numeral 110), [0056] engine speed selection (reference numeral 112), [0057] engine speed status=0 (reference numeral 114), [0058] total relative charge without internal residual gas (reference numeral 116), [0059] relative air charge flowing into engine (without inert gas) bank 1 (reference numeral 118).
[0060] Further variables are: [0061] relative fuel charge flowing into engine bank 1 (reference numeral 120), [0062] combustion effectiveness factor engine bank 1 (reference numeral 122), the effectiveness refers here to the chemical conversion efficiency of air and fuel, [0063] relative air charge after combustion (accumulated since the last calculation of the function) bank 1 (reference numeral 124), air or air lean gas components not fully reacted here after combustion, [0064] relative fuel charge after combustion (accumulated since the last calculation of the function) bank 1 (reference numeral 126), fuel or oil gas components not fully reacted here after combustion.
[0065] Output variables are: [0066] fuel equivalent oxygen mass flow at exhaust valve bank 1 (reference numeral 130), [0067] oxygen mass flow at exhaust valve bank 1 (reference numeral 132).
[0068]
[0088] Output variable is a control unit signal: [0089] reaction heat in the elements of the exhaust system, bank 1 (reference numeral 190).
[0090]
[0091] Variables are: [0092] calculation commands 1 to 7 (reference numeral 220), the sequence of calculation, [0093] software class elemental properties in blocks 202, 206, 210 (reference numeral 222). [0094] lean gas mass in the gas of the current element (reference numeral 224), [0095] oil gas mass (oxygen equivalent) in the gas of the current element (reference numeral 226), [0096] data structure in which information on the catalyst surface is present (reference numeral 228), for example, oil and lean gas mass currently stored in the surface, [0097] reaction heat due to storage of lean gas in the catalyst surface (reference numeral 230), [0098] lean gas mass in the gas of the current element after reaction (reference numeral 232), [0099] lean gas mass in the surface of the current element (if a catalyst) after reaction (reference numeral 234), [0100] oil gas mass in the gas of the current element after reaction (reference numeral 236), [0101] oil gas mass in the surface of the current element (if a catalyst) after reaction (reference numeral 238), [0102] reaction heat due to reaction of oil and lean gases (reference numeral 240)
[0103] The model is thus divided into two model components 10, 150 and areas. The first area relates to the calculation of exhaust components flowing out of the valves of the engine. Here, the incompletely reacted exhaust components, as well as the air flowing directly into the exhaust system, are calculated individually for each cylinder. The amount of air, the mixture, and the ignition timing must be observed. By cylinder-specific calculation from the current engine operating variables, special modes of operation, such as overrun shut-off, cylinder suppression, half-engine operation, scavenging, and purging and cylinder balance, are automatically covered.
[0104] Output from the first model range is the sum of the mass flows of the reactive residual gas components across all cylinders of an exhaust bank.
[0105] The second area refers to the entire exhaust system. Here, the total masses from the first model part are distributed along the exhaust system to the individual components, such as manifold, turbocharger, catalytic converter, particulate filter. In catalysts and catalytically coated particulate filters, storage of a portion of the residual gases into the catalyst surface is also modeled depending on an applied adsorption efficiency.
[0106] Because the catalytic surfaces have limited storage capacity, the storage capability values of the individual catalysts are read from the catalytic converter diagnostic functions; alternatively, a fixed value may be specified. The heat generated by the exothermic reaction of storing oxygen in the catalytic surfaces is calculated.
[0107] Depending on the amount of rich and lean portions present in the gas volume and on the surface, the reaction heat is modeled by the reaction of rich and lean exhaust components to carbon dioxide and water depending on an applied reaction efficiency. Unreacted portions from the surface are considered again in the next calculation step. Components remaining in the gas are passed to the subsequent exhaust element.
[0108] Finally, the proportions of heat generated from the adsorption and reaction per exhaust element are added and used to calculate the modeled exhaust temperature in that exhaust element.
[0109] In