Institute of internal combustion engines
- Prof. Dr.-Ing. Peter Eilts
Peter Eilts, Lennart Klare, 22.08.2017 Institute of Internal Combustion Engines
Determination of the Service Methane Number
Determination of the Service Methane Number Peter Eilts, Lennart - - PowerPoint PPT Presentation
Institute of internal combustion engines Prof. Dr.-Ing. Peter Eilts Determination of the Service Methane Number Peter Eilts, Lennart Klare, 22.08.2017 Institute of Internal Combustion Engines Outline Knocking Methane Number
Institute of internal combustion engines
Peter Eilts, Lennart Klare, 22.08.2017 Institute of Internal Combustion Engines
Determination of the Service Methane Number
Institute of internal combustion engines
Institute of internal combustion engines
Institute of internal combustion engines
Flame propagation with normal combustion Knocking
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Flame propagation with knocking combustion Knocking
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Cylinder pressure with knocking combustion Knocking
Flame speed ca.10 … 25 m/s 250 … 300 m/s
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Institute of internal combustion engines
Definition of the Methane Number
in a mixture of Methane and Hydrogen which has the same knocking behaviour as the gas to be investigated in a defined test engine under defined
Methane Number
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AVL, MWM and NPL correlation
gas from its composition.
simple manner.
hydrocarbons are considered in more detail. Further the influence on N2 is treated differently.
literature.
the AVL data.
Methane Number
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Measurement of the MN
development of the method, just like the RON and MON can only be measured with a CFR engine.
are different. The result is called the Service Methane Number (SMN).
Methane Number
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Institute of internal combustion engines
Definition of the Service Methane Number
Methane in a mixture of Methane and Hydrogen which has the same knocking behaviour as the gas to be investigated in an arbitrary engine under arbitrary
values.
Service Methane Number
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SMN of NG-Propane-mixtures at different engine speeds Service Methane Number
[1], Fig. 5.14
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Institute of internal combustion engines
displacement of 600 ccm. Compression ratio 12.5:1. Connected to a dynamometer.
degree crank angle)
Engine 1
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displacement of 200 ccm. Compression ratio 12.5:1. Connected to a dynamometer.
degree crank angle)
Engine 2
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Engine 1 and 2, pressure indication
Equipment to measure the pressure in the combustion chamber, intake and exhaust system:
[2]
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Knock detection
[3]
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Knock detection
If the knock ratio reaches a certain value it is a knocking cycle
[3]
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Definition of the knock frequency
The knock frequency ist the percentage of knocking combustion cycles compared to the total number of all combustion cycles in a measured time. It is used to characterize the knocking intensity.
Experimental Setup
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Test gases
Component CH4 C2H6 C3H8 n-C4H10 i-C4H10 n-C5H12 i-C5H12 n-C6H14 N2 CO2 AVL-MN Mix 1
78.80 14.0 3.40 0.90 1.10 0.15 0.15 1.5 59
Mix 2
84.52 12.9 1.50 0.21 0.22 0.03 0.02 0.6 69
Mix 3
91.80 5.70 1.30 0.15 0.17 0.04 0.04 0.8 77
Mix 4
81.69 13.38 3.67 0.27 0.28 0.01 0.01 0.69 65
Mix 5
87.89 7.27 2.92 0.71 0.65 0.10 0.11 0.35 66
Mix 6
95.01 2.62 0.73 0.20 0.15 0.06 0.09 0.22 0.54 0.38 82
Mix 7
97.876 1.00 0.50 0.21 0.18 0.016 0.018 0.2 90
Mix 8
99.68 0.09 0.03 0.01 0.01 0.005 0.005 0.17 98
Mix 9
99.4 0.3 0.3 84
Mix 10
99.6 0.2 0.2 89
Mix11
99.8 0.1 0.1 94
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Institute of internal combustion engines
Boundary conditions
Our test engines do not have this so we varied the charge air pressure pL.
characterised by the point where 50 % of the fuel is burnt (MFB50). These were MFB50 = 8, 10, 12 and 14 °CA aTDCF.
the chosen MFB50. For example for Mix1: 0.226, 0.203, 0.184 and 0.168 MPa.
we had to increase the valve overlap and apply an exhaust pressure higher than the charge air pressure to achieve an internal exhaust gas recirculation which provokes knocking.
Experimental Procedure
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Mean Effective Pressure) to heat through all components of the engine
6. Measurement of all values
Test procedure
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five minutes
For the analysis the average of 200 combustion cycles is taken. The procedure is repeated three times.
Test procedure
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y = 3E+07e‐1.185x y = 1E+12e‐1.993x y = 4E+10e‐1,79x 1 2 3 4 5 6 7 8 12 12.2 12.4 12.6 12.8 13 13.2 13.4 13.6 13.8 14 Kf [%] MFB50 [°CA]
0,23MPa boost pressure
20170803 20170803.1 20180803.2
MFB50 and knock frequency is obtained.
Evaluation
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Evaluation
MFB50_m(5%KF)=12,99°CA pL_m(5%KF)=0,23MPa
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Evaluation
knocking frequency
pL_m(5%KF)=f(MFB50_m(5%KF))
y = 1.3846e0.0388x 1 1.2 1.4 1.6 1.8 2 2.2 2.4 5 7 9 11 13 15 pL_m(5%KF) [bar] MFB50_m(5%KF) [°CA]
20170803 Mix5
20170803 Mix5
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content.
their methane content. So with all reference gases a diagramm pL vs MN for different MFB50 can be drawn.
Evaluation
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y = 0,0096x + 1,3202 y = 0,0107x + 1,4189 y = 0,0119x + 1,5251 y = 0,0132x + 1,6393 1.8 2 2.2 2.4 2.6 2.8 3 3.2 50 60 70 80 90 100 110 pL_m(5%KF) SMN
pL_SMN
MFB50=8°CA MFB50=10°CA MFB50=12°CA MFB50=14°CA Linear (MFB50=8°CA) Linear (MFB50=10°CA) Linear (MFB50=12°CA) Linear (MFB50=14°CA)
Evaluation
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1.8 2 2.2 2.4 2.6 2.8 3 3.2 50 60 70 80 90 100 110 pL_m(5%KF) SMN
pL_SMN
Evaluation
gas For example: pL(MFB50=8°CA) = 0.1888 MPa SMN = 59.2 pL(MFB50=10°CA) = 0.2040 MPa SMN = 58.1 pL(MFB50=12°CA) = 0.2205 MPa SMN = 57.2 pL(MFB50=14°CA) = 0.2383 MPa SMN = 56.4 MFB50 = 14°CA MFB50 = 12°CA MFB50 = 10°CA MFB50 = 8°CA
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Institute of internal combustion engines
Engine 1 pL-SMN vs. AVL-MN
40 50 60 70 80 90 100 110 40 60 80 100 120 pL‐SMN AVL‐MN
MFB50=8°CA aTDCF
MFB50=8°CA x=y Linear (MFB50=8°CA) 40 50 60 70 80 90 100 110 40 60 80 100 120 pL‐SMN AVL‐MN
MFB50=10°CA aTDCF
MFB50=10°CA x=y Linear (MFB50=10°CA) 40 50 60 70 80 90 100 110 40 60 80 100 120 pL‐SMN AVL‐MN
MFB50=12°CA aTDCF
MFB50=12°CA x=y Linear (MFB50=12°CA) 40 50 60 70 80 90 100 110 40 60 80 100 120 pL‐SMN AVL‐MN
MFB50=14°CA aTDCF
MFB50=14°CA x=y Linear (MFB50=14°CA)
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Engine 2 pL-SMN vs. AVL-MN
40 50 60 70 80 90 100 110 40 60 80 100 120 pL‐SMN AVL‐MN
MFB50=8°CA aTDCF
MFB50=8°CA x=y Linear (MFB50=8°CA) 40 50 60 70 80 90 100 110 40 60 80 100 120 pL‐SMN AVL‐MN
MFB50=10°CA aTDCF
MFB50=10°CA x=y Linear (MFB50=10°CA) 40 50 60 70 80 90 100 110 40 60 80 100 120 pL‐SMN AVL‐MN
MFB50=14°CA aTDCF
MFB50=14°CA x=y Linear (MFB50=14°CA) 40 50 60 70 80 90 100 110 40 60 80 100 120 pL‐SMN AVL‐MN
MFB50=12°CA aTDCF
MFB50=12°CA x=y Linear (MFB50=12°CA)
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Comparison of engine 1 and engine 2
40 50 60 70 80 90 100 110 40 60 80 100 120 pL‐SMN AVL‐MN
MFB50=8°CA aTDCF
MFB50=8°CA Engine 2 MFB50=8°CA Engine 1 x=y Linear (MFB50=8°CA Engine 2 ) Linear (MFB50=8°CA Engine 1) 40 50 60 70 80 90 100 110 40 60 80 100 120 pL‐SMN AVL‐MN
MFB50=10°CA aTDCF
MFB50=10°CA Engine 2 MFB50=10°CA Engine 1 x=y Linear (MFB50=10°CA Engine 2) Linear (MFB50=10°CA Engine 1) 40 50 60 70 80 90 100 110 40 60 80 100 120 pL‐SMN AVL‐MN
MFB50=12°CA aTDCF
MFB50=12°CA Engine 2 MFB50=12°CA Engine 1 x=y Linear (MFB50=12°CA Engine 2) Linear (MFB50=12°CA Engine 1) 40 50 60 70 80 90 100 110 40 60 80 100 120 pL‐SMN AVL‐MN
MFB50=14°CA aTDCF
MFB50=14°CA Engine 2 MFB50=14°CA Engine 1 x=y Linear (MFB50=14°CA Engine 2) Linear (MFB50=14°CA Engine 1)
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Institute of internal combustion engines
Institute of internal combustion engines
Institute of internal combustion engines
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[1] FVV (1971): Erweiterung der Energieerzeugung durch Kraftgase. Untersuchungen zur Übertragbarkeit der am CFR-Motor gefundenen Ergebnisse auf andere Motoren - Gültigkeitsbereich der Methanzahl. Teil 3. FVV-Heft 120. Frankfurt / Main. [2] https://www.kistler.com/ [3] KiBox To Go, Typ 2893A mit KiBox Cockpit, Manual
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SMN of NG-Propane-mixtures at different engine speeds Service Methane Number
Source: [1], Fig. 5.13
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Comparison of SMN on the CFR/RDH- and MWM-engine Service Methane Number
Source: [1], Fig. 5.15
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Service Methane Number of NG-Hydrogen-Propane mixtures
Source: [1], Fig. 5.44
Service Methane Number
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Engine 1 and 2, testbed
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1 2 3 4 5 6 7 8 9 10 11 AVL‐MN 59 69 77 65 66 82 90 98 84 89 94 MFB50=8°CA 56.5 71.3 83.1 69 62.6 84.1 92.5 101.9 88.4 93.6 91.5 MFB50=10°CA 54.2 70.1 80.9 67.2 61.1 82.2 90.8 101.7 88 94 92.9 MFB50=12°CA 51.6 69.2 78.8 65.9 59.8 80.9 89.2 102 88.2 95 94.8 MFB50=14°CA 49.8 67.9 76.4 64 58 78.7 87.3 101.6 87.7 95.3 95.9 20 40 60 80 100 120 MN
Comparison pL‐SMN AVL‐MN
Mix
Engine 1 pL-SMN vs. AVL-MN
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Engine 2 pL-SMN vs. AVL-MN
1 2 3 4 5 6 7 8 9 10 11 AVL‐MN 59 69 77 65 66 82 90 98 84 89 94 MFB50=8°CA 50.7 67 75.2 60.4 59.2 80.4 89.6 101.1 88.4 89.5 96 MFB50=10°CA 50.6 67 73.9 60.5 58.1 79.4 89.3 97.8 86.9 88.1 93.1 MFB50=12°CA 50.6 67 72.7 60.5 57.2 78.5 89.1 95.7 85.5 86.8 90.4 MFB50=14°CA 50.7 67.1 71.7 60.8 56.4 77.8 89 93.9 84.3 85.8 88.1 20 40 60 80 100 120 MN
Comparison pL‐SMN AVL‐MN
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1 2 3 4 5 6 7 8 9 10 11 MFB50=8°CA 5.8 4.3 7.9 8.6 3.4 3.7 2.9 0.8 4.1 ‐4.5 MFB50=10°CA 3.6 3.1 7 6.7 3 2.8 1.5 3.9 1.1 5.9 ‐0.2 MFB50=12°CA 1 2.2 6.1 5.4 2.6 2.4 0.1 6.3 2.7 8.2 4.4 MFB50=14°CA ‐0.9 0.8 4.7 3.2 1.6 0.9 ‐1.7 7.7 3.4 9.5 7.8 ‐6 ‐4 ‐2 2 4 6 8 10 12 SMN
Difference SMN Engine 1 ‐ Engine 2