Table 1 to Paragraph (c)(2) of § 1036.540 -GEM Input for Gear Ratio
Gear No. | Spark-ignition HDE, light HDE, and medium HDE- all duty cycles | Heavy HDE- transient and ftp duty cycles | Heavy HDE- cruise and set duty cycles |
1 | 3.10 | 3.51 | 12.8 |
2 | 1.81 | 1.91 | 9.25 |
3 | 1.41 | 1.43 | 6.76 |
4 | 1.00 | 1.00 | 4.90 |
5 | 0.71 | 0.74 | 3.58 |
6 | 0.61 | 0.64 | 2.61 |
7 | - | - | 1.89 |
8 | - | - | 1.38 |
9 | - | - | 1.00 |
10 | - | - | 0.73 |
Lockup Gear | 3 | 3 | - |
for each vehicle configuration based on the corresponding designated engine speed (fnrefA, fnrefB, fnrefC, fnrefD, or fntest as defined in 40 CFR 1065.610(c)(2) ) at 65 mi/hr for the transient duty cycle and for the 65 mi/hr highway cruise cycle. Similarly, set these parameters based on the corresponding designated engine speed at 55 mi/hr for the 55 mi/hr highway cruise cycle. Use one of the following equations to determine
and ka at each of the defined engine speeds:
Where:
fn[speed] = engine's angular speed as determined in paragraph (c)(3)(ii) or (iii) of this section.
ktopgear = transmission gear ratio in the highest available gear from Table 1 of this section.
vref = reference speed. Use 65 mi/hr for the transient cycle and the 65 mi/hr highway cruise cycle and use 55 mi/hr for the 55 mi/hr highway cruise cycle.
Example for a vocational Light HDV or vocational Medium HDV with a 6-speed automatic transmission at B speed (Test 3 or 4 in Table 3 of this section):
fnrefB = 1870 r/min = 31.17 r/s
kaB = 4.0
ktopgear = 0.61
vref = 65 mi/hr = 29.06 m/s
Table 5 to Paragraph (c)(3) of § 1036.540 - Alternative Fuel-Mapping Cycle-Validation Criteria for Spark-Ignition Gaseous-Fueled Enginesa
Parameter | Speed | Torque | Power |
Slope, a1 | |||
Absolute value of intercept, |a0| | [LESS THAN EQUAL TO]3% of maximum mapped torque | ||
Standard error of the estimate, SEE | [LESS THAN EQUAL TO]15% of maximum mapped torque | [LESS THAN EQUAL TO]15% of maximum mapped power. | |
Coefficient of determination, r2 | [GREATER THAN EQUAL TO]0.700 | [GREATER THAN EQUAL TO]0.750. |
a Cycle-validation criteria apply as specified in 40 CFR 1065.514 unless otherwise specified.
Eq. 1036.540-3
Where:
MC = molar mass of carbon.
wCmeas = carbon mass fraction of fuel (or mixture of fuels) as determined in 40 CFR 1065.655(d) , except that you may not use the default properties in 40 CFR 1065.655(e)(5) to determine [ALPHA], [BETA], and wC. You may not account for the contribution to [ALPHA], [BETA],[GAMMA], and [DELTA] of diesel exhaust fluid or other non-fuel fluids injected into the exhaust.
i = an indexing variable that represents one recorded emission value.
N = total number of measurements over the duty cycle.
n1 = exhaust molar flow rate from which you measured emissions according to 40 CFR 1065.655 .
xCcombdryi = amount of carbon from fuel and any injected fluids in the exhaust per mole of dry exhaust as determined in 40 CFR 1065.655(c) .
xH2Oexhdryi = amount of H2O in exhaust per mole of exhaust as determined in 40 CFR 1065.655(c) .
[DELTA]t = 1/frecord
MCO2 = molar mass of carbon dioxide.
mCO2DEFi = mass emission rate of CO2 resulting from diesel exhaust fluid decomposition over the duty cycle as determined from § 1036.535(b)(9) . If your engine does not utilize diesel exhaust fluid for emission control, or if you choose not to perform this correction, set mCO2DEFi equal to 0.
Example:
MC = 12.0107 g/mol
wCmeas = 0.867
N = 6680
n1 = 2.876 mol/s
n2 = 2.224 mol/s
xCcombdryi 1 = 2.61·10-3 mol/mol
xCcombdryi 2 = 1.91·10-3 mol/mol
xH2Oexh1 = 3.53·10-2 mol/mol
xH2Oexh2 = 3.13·10-2 mol/mol
frecord = 10 Hz
[DELTA]t = 1/10 = 0.1 s
MCO2 = 44.0095 g/mol
mCO2DEF1 = 0.0726 g/s
mCO2DEF2= 0.0751 g/s
Where:
i = an indexing variable that represents one recorded value.
N = total number of measurements over the duty cycle. For batch fuel mass measurements, set N = 1.
mfueli = the fuel mass flow rate, for each point, i, starting from i = 1.
[DELTA]t = 1/'record
'record = the data recording frequency.
Example:
N = 6680
mfuel1 = 1.856 g/s
mfuel2 = 1.962 g/s
'record = 10 Hz
[DELTA]t = 1/10 = 0.1 s
mfueltransient = (1.856 + 1.962+ . . . +mfuel6680) · 0.1
mfueltransient = 111.95 g
by taking the average engine speed measured during the engine test while the vehicle is moving and dividing it by the average vehicle speed provided by GEM. Note that the engine cycle created by GEM has a flag to indicate when the vehicle is moving.
Table 7 to Paragraph (e)(7)(ii) of § 1036.540 -Generic Example of an Output Matrix for Cruise Cycle Vehicle Configurations
Parameter | Configuration | |||||
1 | 2 | 3 | 4 | . . . | n | |
mfuel[cycle] | ||||||
fnengine[cycle] | ||||||
Tengine[cycle] | ||||||
W[cycle] |
40 C.F.R. §1036.540