Engine tuning
This commit is contained in:
parent
9ab1d18989
commit
5b98c62dbb
@ -29,25 +29,32 @@ DisablePropellerControls =1
|
||||
DisableAutopilotControls=1
|
||||
|
||||
[TURBINEENGINEDATA]
|
||||
fuel_flow_gain=1
|
||||
//KH From 1, as per SDK warning
|
||||
fuel_flow_gain=0
|
||||
low_idle_n1=24.2
|
||||
low_idle_n2=62.9
|
||||
inlet_area=9.92
|
||||
rated_N2_rpm=11055
|
||||
static_thrust=61960
|
||||
//KH From 61960 (ideal) as per EASA TCDS for CF6-80C2D1F 5min limit
|
||||
static_thrust=60690
|
||||
reverser_available=1
|
||||
reverser_mach_controlled=0
|
||||
afterburner_available=0
|
||||
afterburner_throttle_threshold=0
|
||||
ThrustSpecificFuelConsumption=0.362
|
||||
//KH From .362, WikiP lists .3 to .344
|
||||
ThrustSpecificFuelConsumption=0.344
|
||||
use_commanded_Ne_Table=1
|
||||
use_corrected_N2_from_FF_table=1
|
||||
use_n2_to_n1_table=1
|
||||
use_old_fuelflow_simvar=1
|
||||
n2_to_n1_table=0:0:0.85,0:0:0,10:1.1:1,20:2.7:2.4,30:5.7:4.7,40:11.1:9.78,50:16.35:14.9,64.5:25.34:25.39,70:38:37.16,80:59.2:58.56,90:80.4:79.96,99.6:110.75:110.5,105:112:112
|
||||
mach_0_corrected_commanded_ne_table=0:1:5.42,0:64:64.5,0.143:69.214:69.857,0.286:74.428:75.214,0.429:79.642:80.571,0.572:84.856:85.928,0.715:90.07:91.285,0.858:95.284:96.642,1:100.5:102
|
||||
mach_hi_corrected_commanded_ne_table=0.88:1:5.42,0:66:67.5,0.143:71.143:72.571,0.286:76.286:77.642,0.429:81.429:82.713,0.572:86.572:87.784,0.715:91.715:92.855,0.858:96.858:97.926,1:102:103
|
||||
corrected_n2_from_ff_table=0:17,0.0099:63.7,0.01:70,0.017:77.6,0.021:80,0.033:84.77,0.048:88.88,0.083:93,0.088:99.3,0.09:106.5
|
||||
//KH Compared the ini A300 to the original in Excel. Constructed based on the shape. Increased its max values to those in the TCDS
|
||||
n2_to_n1_table=0:0:0.85,0:0:0,10:1:1,20:2:2,30:4:4,40:9:9,50:14:14,64.5:25.34:25.34,70:29:29,80:41:41,90:68:68,100:102:102,112.5:117.5:117.5
|
||||
//KH Adjusted to being linear but with >100 as max
|
||||
mach_0_corrected_commanded_ne_table=0:1:5.42,0:64:64.5,0.143:70.6495:71.2925,0.286:77.299:78.085,0.429:83.9485:84.8775,0.572:90.598:91.67,0.715:97.2475:98.4625,0.858:103.897:105.255,1:110.5:112
|
||||
//KH Adjusted to being linear but with >100 as max
|
||||
mach_hi_corrected_commanded_ne_table=0.88:1:5.42,0:66:67.5,0.143:73.15:74.5785,0.286:80.3:81.657,0.429:87.45:88.7355,0.572:94.6:95.814,0.715:101.75:102.8925,0.858:108.9:109.971,1:116:117
|
||||
//KH Compared the ini A300 to the original in Excel. Constructed based on the shape
|
||||
corrected_n2_from_ff_table=0:0,0.02:60,0.03:70,0.04:75.7,0.055:81.4,0.07:87.1,0.09:92.8,0.11:98.5,0.13:104.2,0.15:112.5
|
||||
n1_and_mach_on_thrust_table=0:0:0.25:0.39:0.49:0.5:0.67:0.74:0.8:0.82:0.85,0:0:0:0:0:0:0:0:0:0:0,20:0.0554:0.0598:0.0598:0.0598:0.0205:0.0282:0.0404:0.0411:0.0224:0.0297,25:0.0748:0.0704:0.0704:0.1304:0.1291:0.1235:0.1278:0.1262:0.1291:0.0393,30:0.0865:0.0821:0.0821:0.0335:0.0547:0.0847:0.0847:0.1039:0.1039:0.1039,35:0.0964:0.0963:0.0963:0.0425:0.0601:0.0901:0.0901:0.1053:0.1053:0.1053,40:0.1312:0.1134:0.1134:0.1007:0.092:0.102:0.102:0.1156:0.1161:0.1176,45:0.163:0.1278:0.1278:0.13:0.3795:0.4095:0.4095:0.4235:0.4235:0.4235,50:0.1816:0.1448:0.1448:0.1518:0.3853:0.4153:0.4153:0.4389:0.4389:0.4389,55:0.2388:0.1711:0.1632:0.1715:0.3906:0.4206:0.4206:0.442:0.442:0.442,60:0.2726:0.2079:0.1902:0.2076:0.3943:0.4243:0.4243:0.446:0.446:0.446,65:0.3294:0.2532:0.2336:0.2367:0.4002:0.4302:0.4302:0.4542:0.4542:0.4542,70:0.3807:0.3116:0.2786:0.2768:0.409:0.439:0.439:0.4642:0.4642:0.4642,75:0.4477:0.3938:0.3318:0.3282:0.4274:0.4574:0.4574:0.4705:0.4703:0.4706,80:0.5395:0.4915:0.4124:0.4138:0.4321:0.4621:0.4621:0.484:0.4813:0.4805,85:0.6524:0.6349:0.5626:0.5072:0.5044:0.5355:0.5309:0.5785:0.5275:0.5356,90:0.7545:0.7735:0.6998:0.61:0.61:0.6173:0.6574:0.6638:0.6044:0.6297,95:0.8364:0.8395:0.7080:0.6900:0.7010:0.7296:0.8207:0.8673:0.7222:0.7682,103.5:0.9779:0.9811:0.7157:0.7212:0.744:0.7453:0.8651:0.9026:0.9209:0.9312,110:0.9853:1.0945:0.7775:0.83:0.85:0.8257:0.8749:0.9122:0.9322:0.9317,120:0.857:0.9826:0.7877:0.84:0.88:0.8339:0.8818:0.9131:0.9473:0.9404
|
||||
corrected_airflow_table=0:0:0.9,0:0:0,20:4.29:14.08,85:4.62:24,90:5.75:25,95:7.23:27,100:8.36:28,105:9.29:29,120:10.94:30
|
||||
JET_density_on_FF_table=0.000462:28.74,0.000587:32.93,0.000738:35.02,0.000891:29.46,0.001066:31.02,0.001267:32.56,0.001496:34.54,0.0017565:35.11,0.002048:30.8,0.002377:22.55
|
||||
@ -64,10 +71,14 @@ oil_press_tc=0.8
|
||||
oil_press_tuning_constant=1
|
||||
itt_peak_temperature=2141
|
||||
itt_tc=2
|
||||
//KH No scaling
|
||||
itt_tuning_constant=1
|
||||
egt_peak_temperature=1600
|
||||
egt_tc=0.1
|
||||
egt_tuning_constant=0.1
|
||||
//KH 750C Start limit as per EASA TCDS for CF6-80C2D1F
|
||||
egt_peak_temperature=1841
|
||||
//KH Taken from the A300, made sense
|
||||
egt_tc=2
|
||||
//KH No scaling
|
||||
egt_tuning_constant=1
|
||||
fuel_press_max=2376
|
||||
fuel_press_tc=2
|
||||
fuel_press_tuning_constant=1
|
||||
@ -86,11 +97,14 @@ min_n2_for_apu_bleed_air_cutoff=50
|
||||
n1_normal_tc=0.5
|
||||
n1_start_max_rate=1
|
||||
n1_start_combustion_max_rate=2
|
||||
idle_fuel_flow=600
|
||||
//KH From 600, used videos from YT as rough basis
|
||||
idle_fuel_flow=1400
|
||||
idle_high_fuel_flow=40
|
||||
min_n2_for_fuel_flow=17
|
||||
high_n1=110
|
||||
high_n2=105
|
||||
//KH From 110 as per EASA TCDS for CF6-80C2D1F
|
||||
high_n1=117.5
|
||||
//KH From 105 as per EASA TCDS for CF6-80C2D1F
|
||||
high_n2=112.5
|
||||
high_fuel_flow=9800
|
||||
mach_influence_on_n1=10
|
||||
fuel_flow_max=10000
|
||||
@ -100,9 +114,12 @@ fuel_flow_controller_d=0.1
|
||||
fuel_flow_controller_iboundary=10
|
||||
fuel_flow_controller_dboundary=100
|
||||
max_torque_protection=0
|
||||
max_n1_protection=110
|
||||
max_n2_protection=100
|
||||
max_egt_protection=2000
|
||||
//KH Disabled
|
||||
max_n1_protection=0
|
||||
//KH Disabled
|
||||
max_n2_protection=0
|
||||
//KH Disabled
|
||||
max_egt_protection=0
|
||||
fuel_flow_max_itt_factor=2
|
||||
fuel_flow_min_itt_factor=0.9
|
||||
n1_cooling_factor=0.01
|
||||
|
||||
BIN
References/MD11 throttle bug.xlsx
Normal file
BIN
References/MD11 throttle bug.xlsx
Normal file
Binary file not shown.
@ -6,192 +6,29 @@
|
||||
],
|
||||
"settings": {
|
||||
"cSpell.words": [
|
||||
"AFSOVRD",
|
||||
"AGNT",
|
||||
"AICE",
|
||||
"ALBD",
|
||||
"ALTN",
|
||||
"ANNUNLT",
|
||||
"AOVHD",
|
||||
"apos",
|
||||
"APPR",
|
||||
"APPRCAP",
|
||||
"APPRFO",
|
||||
"APPRLAND",
|
||||
"APUFIRE",
|
||||
"ARPT",
|
||||
"Asobo",
|
||||
"ATTND",
|
||||
"AUTOBRAKE",
|
||||
"AUTOFLIGHT",
|
||||
"BARO",
|
||||
"BAROSET",
|
||||
"BRTDIM",
|
||||
"CADC",
|
||||
"CADCCAP",
|
||||
"CADCFO",
|
||||
"CALLBACKCODE",
|
||||
"CAPAUX",
|
||||
"CAPTAUX",
|
||||
"CAUT",
|
||||
"CEVENT",
|
||||
"CKPT",
|
||||
"CKPTDOOR",
|
||||
"CKTBK",
|
||||
"CKTBKR",
|
||||
"CLBDES",
|
||||
"clickspot",
|
||||
"Clickspot",
|
||||
"CMCDU",
|
||||
"CMPS",
|
||||
"CONSEQ",
|
||||
"CRGSMK",
|
||||
"DECR",
|
||||
"DEFL",
|
||||
"DIALAFLAP",
|
||||
"DISAG",
|
||||
"DOWNARROW",
|
||||
"DSPY",
|
||||
"ELEC",
|
||||
"ELEVFEEL",
|
||||
"EMER",
|
||||
"ENGMAXPTRRESET",
|
||||
"evac",
|
||||
"EVAC",
|
||||
"EVTMKR",
|
||||
"FADEC",
|
||||
"FIRETEST",
|
||||
"flaperon",
|
||||
"FLAPLIM",
|
||||
"FLIGHTDECK",
|
||||
"FLTCTL",
|
||||
"FLTDIR",
|
||||
"FLTDIRCAP",
|
||||
"FLTDIRFO",
|
||||
"FLTDIROFF",
|
||||
"FLTNO",
|
||||
"FMSCAP",
|
||||
"FMSFO",
|
||||
"FMSSPD",
|
||||
"FOAUX",
|
||||
"FOREAFT",
|
||||
"FPLN",
|
||||
"FUELUSEDRESET",
|
||||
"FWDAUX",
|
||||
"gltf",
|
||||
"GPWS",
|
||||
"HANDLEREL",
|
||||
"HDGTRK",
|
||||
"HELPID",
|
||||
"hideable",
|
||||
"HORNSHUT",
|
||||
"hstab",
|
||||
"IASMACH",
|
||||
"IDNT",
|
||||
"inbd",
|
||||
"INBD",
|
||||
"INHG",
|
||||
"INHP",
|
||||
"INSTPED",
|
||||
"INTEG",
|
||||
"INTP",
|
||||
"ISDF",
|
||||
"ISFD",
|
||||
"ISOL",
|
||||
"castering",
|
||||
"coef",
|
||||
"daoa",
|
||||
"dboundary",
|
||||
"EASA",
|
||||
"fuelflow",
|
||||
"GENERALENGINEDATA",
|
||||
"htail",
|
||||
"iboundary",
|
||||
"khofmann",
|
||||
"KHOFMANN",
|
||||
"kohlsman",
|
||||
"LECP",
|
||||
"LEFTARROW",
|
||||
"LEFTRELEASE",
|
||||
"LEFTRIGHT",
|
||||
"LEFTSINGLE",
|
||||
"LLIFAIL",
|
||||
"LLIFOFF",
|
||||
"LLOFAIL",
|
||||
"LLOFOFF",
|
||||
"LMCDU",
|
||||
"LODS",
|
||||
"LSIDE",
|
||||
"LTRANS",
|
||||
"LYDA",
|
||||
"LYDAFAIL",
|
||||
"LYDAOFF",
|
||||
"LYDB",
|
||||
"LYDBFAIL",
|
||||
"LYDBOFF",
|
||||
"LYOKE",
|
||||
"MAGTRU",
|
||||
"MAINT",
|
||||
"MANF",
|
||||
"MCDU",
|
||||
"MLDG",
|
||||
"MOUSEDOWN",
|
||||
"MOUSEFLAGS",
|
||||
"MSFS",
|
||||
"NEXTPAGE",
|
||||
"NOSMOKE",
|
||||
"OFST",
|
||||
"OUTB",
|
||||
"outbd",
|
||||
"OUTBD",
|
||||
"OUTFLO",
|
||||
"OVHD",
|
||||
"OVHT",
|
||||
"OVRD",
|
||||
"PAINUSE",
|
||||
"PUSHPULL",
|
||||
"RECP",
|
||||
"REPLNT",
|
||||
"RIGHTARROW",
|
||||
"RLIFAIL",
|
||||
"RLIFOFF",
|
||||
"RLOFAIL",
|
||||
"RLOFOFF",
|
||||
"RMCDU",
|
||||
"RPTG",
|
||||
"RSIDE",
|
||||
"RTRANS",
|
||||
"RYOKE",
|
||||
"scmi",
|
||||
"scmp",
|
||||
"SPDBRK",
|
||||
"splr",
|
||||
"stby",
|
||||
"STBY",
|
||||
"TCAS",
|
||||
"TERROVRD",
|
||||
"tfdidesign",
|
||||
"THNDRSTRM",
|
||||
"TOAPPR",
|
||||
"TOEBRAKE",
|
||||
"TOOLTIPID",
|
||||
"TRFC",
|
||||
"UPARROW",
|
||||
"UPRAUX",
|
||||
"UYDA",
|
||||
"UYDAFAIL",
|
||||
"UYDAOFF",
|
||||
"UYDB",
|
||||
"UYDBFAIL",
|
||||
"UYDBOFF",
|
||||
"VENTDISAG",
|
||||
"VENTOFF",
|
||||
"Vistag",
|
||||
"Vistags",
|
||||
"VORCAP",
|
||||
"VORFO",
|
||||
"VORNDB",
|
||||
"VSFPA",
|
||||
"WHEELDOWN",
|
||||
"WHEELUP",
|
||||
"WNDSHLD",
|
||||
"WXBRT",
|
||||
"XFEED",
|
||||
"XFER",
|
||||
"xkhofmann",
|
||||
"XPNDR",
|
||||
"yokebase"
|
||||
"maxangle",
|
||||
"otherwheel",
|
||||
"propwash",
|
||||
"simvar",
|
||||
"spoileron",
|
||||
"spoilerons",
|
||||
"steeringwheel",
|
||||
"TCDS",
|
||||
"TURBINEENGINEDATA",
|
||||
"vtail",
|
||||
"wingflex",
|
||||
"xkhofmann"
|
||||
]
|
||||
}
|
||||
}
|
||||
Loading…
x
Reference in New Issue
Block a user