diff --git a/PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11F_GE/engines.cfg b/PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11F_GE/engines.cfg index 126b22e..4e8bc96 100644 --- a/PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11F_GE/engines.cfg +++ b/PackageSources/SimObjects/Airplanes/TFDi_Design_MD-11F_GE/engines.cfg @@ -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 diff --git a/References/MD11 throttle bug.xlsx b/References/MD11 throttle bug.xlsx new file mode 100644 index 0000000..61b5851 Binary files /dev/null and b/References/MD11 throttle bug.xlsx differ diff --git a/xkhofmann-tfdidesign-md11-config-tweaks.code-workspace b/xkhofmann-tfdidesign-md11-config-tweaks.code-workspace index 1ac8ada..2e05046 100644 --- a/xkhofmann-tfdidesign-md11-config-tweaks.code-workspace +++ b/xkhofmann-tfdidesign-md11-config-tweaks.code-workspace @@ -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" ] } } \ No newline at end of file