Sim: Add cfm56 to pw temporarily so it starts, add old EGT just temporarily
This commit is contained in:
Josh Davidson
parent
c6b8643097
commit
608e06d123
7 changed files with 220 additions and 190 deletions
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@ -276,6 +276,7 @@
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<system file="glass-effect"/>
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<system file="a320-fbw"/>
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<system file="a320-fcs"/>
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<system file="a320-cfm56-5b4-engine-fadec"/>
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<system file="a320-fuel"/>
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<system file="a320-fwc"/>
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<system file="a320-fwc-phases"/>
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@ -2,23 +2,23 @@
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<!-- Copyright (c) 2021 Josh Davidson (Octal450) -->
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<turbine_engine name="PW1127G">
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<turbine_engine name="CFM56-5B4">
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<milthrust> 27075 </milthrust>
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<tsfc> 0.445 </tsfc>
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<bleed> 0.03 </bleed>
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<ignitionn1> 0.6 </ignitionn1>
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<ignitionn2> 22.2</ignitionn2>
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<idlen1> 18.9 </idlen1>
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<idlen2> 59.4 </idlen2>
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<n1spinup> 0.05 </n1spinup>
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<n2spinup> 1.85 </n2spinup>
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<n1startrate> 0.573 </n1startrate>
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<n2startrate> 1.127 </n2startrate>
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<maxn1> 103.8 </maxn1>
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<maxn2> 101.4 </maxn2>
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<augmented> 0 </augmented>
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<injected> 0 </injected>
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<milthrust>27000</milthrust>
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<tsfc>0.445</tsfc>
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<bleed>0.03</bleed>
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<ignitionn1>0.6</ignitionn1>
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<ignitionn2>22.2</ignitionn2>
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<n1spinup>0.05</n1spinup>
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<n2spinup>1.85</n2spinup>
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<n1startrate>0.573</n1startrate>
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<n2startrate>1.127</n2startrate>
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<idlen1>18.9</idlen1>
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<idlen2>59.4</idlen2>
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<maxn1>104.0</maxn1>
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<maxn2>105.0</maxn2>
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<augmented>0</augmented>
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<injected>0</injected>
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<function name="N1SpoolUp">
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<table>
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@ -50,32 +50,32 @@
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</table>
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</function>
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<function name="N2SpoolUp">
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<function name="N2SpoolUp"> <!-- N1 to N2 factor 0.535840188014101 -->
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<table>
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<independentVar lookup="row">/engines/engine[0]/n1</independentVar>
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<tableData>
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24 1.1
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28 2.9
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46 9.7
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68 15.4
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80 19.6
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94 21.4
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103 23.6
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24 0.6
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28 1.6
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46 5.2
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68 8.3
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80 10.5
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94 11.5
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103 12.6
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</tableData>
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</table>
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</function>
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<function name="N2SpoolDown">
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<function name="N2SpoolDown"> <!-- N1 to N2 factor 0.535840188014101 -->
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<table>
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<independentVar lookup="row">/engines/engine[0]/n1</independentVar>
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<tableData>
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24 1.1
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28 2.9
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46 9.7
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68 15.4
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80 19.6
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94 21.4
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103 23.6
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24 0.6
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28 1.6
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46 5.2
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68 8.3
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80 10.5
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94 11.5
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103 12.6
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</tableData>
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</table>
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</function>
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@ -86,33 +86,43 @@
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<independentVar lookup="column">atmosphere/density-altitude</independentVar>
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<tableData>
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-10000 0 10000 20000 30000 40000 50000
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0.0 0.0430 0.0458 0.0378 0.0684 0.0619 0.0693 0.0000
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0.2 0.0500 0.0291 0.0205 0.0514 0.0627 0.0629 0.0000
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0.4 0.0040 0.0047 0.0012 0.0412 0.0485 0.0571 0.0000
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0.6 0.0000 0.0000 0.0000 0.0000 0.0316 0.0418 0.0000
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0.8 0.0000 0.0000 0.0000 0.0000 0.0254 0.0368 0.0000
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1.0 0.0000 0.0000 0.0000 0.0000 0.0000 0.0252 0.0000
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0.0 0.0430 0.0458 0.0378 0.0684 0.0819 0.0793 0.0000
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0.2 0.0500 0.0291 0.0205 0.0514 0.0727 0.0729 0.0000
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0.4 0.0040 0.0047 0.0012 0.0412 0.0585 0.0671 0.0000
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0.6 0.0000 0.0000 0.0000 0.0000 0.0416 0.0518 0.0000
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0.8 0.0000 0.0000 0.0000 0.0000 0.0354 0.0468 0.0000
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1.0 0.0000 0.0000 0.0000 0.0000 0.0000 0.0352 0.0000
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</tableData>
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</table>
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</function>
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<function name="MilThrust">
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<table>
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<independentVar lookup="row">velocities/mach</independentVar>
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<independentVar lookup="column">atmosphere/density-altitude</independentVar>
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<tableData>
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-10000 0 10000 20000 30000 40000 50000
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0.0 1.2600 1.0000 0.7400 0.5640 0.3920 0.2710 0.0000
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0.2 1.1710 0.9740 0.6970 0.5360 0.3850 0.2610 0.0000
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0.4 1.1500 0.9570 0.6920 0.5460 0.3870 0.2530 0.0000
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0.6 1.1810 0.9410 0.7210 0.5660 0.3580 0.2180 0.0000
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0.8 1.2290 1.0200 0.7820 0.5570 0.3040 0.1930 0.0000
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0.9 1.2580 1.0200 0.7820 0.5220 0.2710 0.1140 0.0000
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1.0 1.1810 0.9510 0.7210 0.4410 0.1740 0.0450 0.0000
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1.2 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
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1.4 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
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</tableData>
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</table>
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<function name="MilThrust"> <!-- If you change this, make sure you update the table in the engine system file -->
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<product>
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<table>
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<independentVar lookup="row">velocities/mach</independentVar>
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<independentVar lookup="column">atmosphere/density-altitude</independentVar>
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<tableData>
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-10000 0 10000 20000 30000 40000 50000
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0.0 1.2600 1.0000 0.7400 0.5640 0.3920 0.2710 0.0000
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0.2 1.1710 0.9740 0.6970 0.5360 0.3850 0.2610 0.0000
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0.4 1.1500 0.9570 0.6920 0.5460 0.3870 0.2530 0.0000
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0.6 1.1810 0.9410 0.7210 0.5660 0.3580 0.2180 0.0000
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0.8 1.2290 1.0200 0.7820 0.5570 0.3040 0.1930 0.0000
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0.9 1.2580 1.0200 0.7820 0.5220 0.2710 0.1140 0.0000
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1.0 1.1810 0.9510 0.7210 0.4410 0.1740 0.0450 0.0000
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1.2 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
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1.4 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
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</tableData>
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</table>
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<property>fadec/limit/rated-thrust-factor</property>
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<table> <!-- Thrust loss due to reverser angle -->
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<independentVar lookup="row">/engines/engine[0]/reverser-pos-norm</independentVar>
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<tableData>
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0.01 1.00
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1.00 0.65
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</tableData>
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</table>
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</product>
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</function>
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</turbine_engine>
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@ -2,23 +2,23 @@
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<!-- Copyright (c) 2021 Josh Davidson (Octal450) -->
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<turbine_engine name="PW1127G">
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<turbine_engine name="CFM56-5B4">
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<milthrust> 27075 </milthrust>
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<tsfc> 0.445 </tsfc>
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<bleed> 0.03 </bleed>
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<ignitionn1> 0.6 </ignitionn1>
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<ignitionn2> 22.2</ignitionn2>
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<idlen1> 18.9 </idlen1>
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<idlen2> 59.4 </idlen2>
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<n1spinup> 0.05 </n1spinup>
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<n2spinup> 1.85 </n2spinup>
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<n1startrate> 0.573 </n1startrate>
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<n2startrate> 1.127 </n2startrate>
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<maxn1> 103.8 </maxn1>
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<maxn2> 101.4 </maxn2>
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<augmented> 0 </augmented>
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<injected> 0 </injected>
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<milthrust>27000</milthrust>
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<tsfc>0.445</tsfc>
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<bleed>0.03</bleed>
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<ignitionn1>0.6</ignitionn1>
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<ignitionn2>22.2</ignitionn2>
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<n1spinup>0.05</n1spinup>
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<n2spinup>1.85</n2spinup>
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<n1startrate>0.573</n1startrate>
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<n2startrate>1.127</n2startrate>
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<idlen1>18.9</idlen1>
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<idlen2>59.4</idlen2>
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<maxn1>104.0</maxn1>
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<maxn2>105.0</maxn2>
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<augmented>0</augmented>
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<injected>0</injected>
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<function name="N1SpoolUp">
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<table>
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@ -50,32 +50,32 @@
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</table>
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</function>
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<function name="N2SpoolUp">
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<function name="N2SpoolUp"> <!-- N1 to N2 factor 0.535840188014101 -->
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<table>
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<independentVar lookup="row">/engines/engine[1]/n1</independentVar>
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<tableData>
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24 1.1
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28 2.9
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46 9.7
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68 15.4
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80 19.6
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94 21.4
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103 23.6
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24 0.6
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28 1.6
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46 5.2
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68 8.3
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80 10.5
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94 11.5
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103 12.6
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</tableData>
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</table>
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</function>
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<function name="N2SpoolDown">
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<function name="N2SpoolDown"> <!-- N1 to N2 factor 0.535840188014101 -->
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<table>
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<independentVar lookup="row">/engines/engine[1]/n1</independentVar>
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<tableData>
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24 1.1
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28 2.9
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46 9.7
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68 15.4
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80 19.6
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94 21.4
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103 23.6
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24 0.6
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28 1.6
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46 5.2
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68 8.3
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80 10.5
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94 11.5
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103 12.6
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</tableData>
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</table>
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</function>
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@ -86,33 +86,43 @@
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<independentVar lookup="column">atmosphere/density-altitude</independentVar>
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<tableData>
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-10000 0 10000 20000 30000 40000 50000
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0.0 0.0430 0.0458 0.0378 0.0684 0.0619 0.0693 0.0000
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0.2 0.0500 0.0291 0.0205 0.0514 0.0627 0.0629 0.0000
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0.4 0.0040 0.0047 0.0012 0.0412 0.0485 0.0571 0.0000
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0.6 0.0000 0.0000 0.0000 0.0000 0.0316 0.0418 0.0000
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0.8 0.0000 0.0000 0.0000 0.0000 0.0254 0.0368 0.0000
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1.0 0.0000 0.0000 0.0000 0.0000 0.0000 0.0252 0.0000
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0.0 0.0430 0.0458 0.0378 0.0684 0.0819 0.0793 0.0000
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0.2 0.0500 0.0291 0.0205 0.0514 0.0727 0.0729 0.0000
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0.4 0.0040 0.0047 0.0012 0.0412 0.0585 0.0671 0.0000
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0.6 0.0000 0.0000 0.0000 0.0000 0.0416 0.0518 0.0000
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0.8 0.0000 0.0000 0.0000 0.0000 0.0354 0.0468 0.0000
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1.0 0.0000 0.0000 0.0000 0.0000 0.0000 0.0352 0.0000
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</tableData>
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</table>
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</function>
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<function name="MilThrust">
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<table>
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<independentVar lookup="row">velocities/mach</independentVar>
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<independentVar lookup="column">atmosphere/density-altitude</independentVar>
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<tableData>
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-10000 0 10000 20000 30000 40000 50000
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0.0 1.2600 1.0000 0.7400 0.5640 0.3920 0.2710 0.0000
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0.2 1.1710 0.9740 0.6970 0.5360 0.3850 0.2610 0.0000
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0.4 1.1500 0.9570 0.6920 0.5460 0.3870 0.2530 0.0000
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0.6 1.1810 0.9410 0.7210 0.5660 0.3580 0.2180 0.0000
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0.8 1.2290 1.0200 0.7820 0.5570 0.3040 0.1930 0.0000
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0.9 1.2580 1.0200 0.7820 0.5220 0.2710 0.1140 0.0000
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1.0 1.1810 0.9510 0.7210 0.4410 0.1740 0.0450 0.0000
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1.2 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
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1.4 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
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</tableData>
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</table>
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<function name="MilThrust"> <!-- If you change this, make sure you update the table in the engine system file -->
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<product>
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<table>
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<independentVar lookup="row">velocities/mach</independentVar>
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<independentVar lookup="column">atmosphere/density-altitude</independentVar>
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<tableData>
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-10000 0 10000 20000 30000 40000 50000
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0.0 1.2600 1.0000 0.7400 0.5640 0.3920 0.2710 0.0000
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0.2 1.1710 0.9740 0.6970 0.5360 0.3850 0.2610 0.0000
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0.4 1.1500 0.9570 0.6920 0.5460 0.3870 0.2530 0.0000
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0.6 1.1810 0.9410 0.7210 0.5660 0.3580 0.2180 0.0000
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0.8 1.2290 1.0200 0.7820 0.5570 0.3040 0.1930 0.0000
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0.9 1.2580 1.0200 0.7820 0.5220 0.2710 0.1140 0.0000
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1.0 1.1810 0.9510 0.7210 0.4410 0.1740 0.0450 0.0000
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1.2 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
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1.4 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000
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</tableData>
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</table>
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<property>fadec/limit/rated-thrust-factor</property>
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<table> <!-- Thrust loss due to reverser angle -->
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<independentVar lookup="row">/engines/engine[1]/reverser-pos-norm</independentVar>
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<tableData>
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0.01 1.00
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1.00 0.65
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</tableData>
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</table>
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</product>
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</function>
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</turbine_engine>
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@ -1015,8 +1015,8 @@ input = {
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# EGT
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egt_1: "/engines/engine[0]/egt-actual",
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egt_2: "/engines/engine[1]/egt-actual",
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egt_1_needle: "/ECAM/Upper/EGT[0]",
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egt_2_needle: "/ECAM/Upper/EGT[1]",
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egt_1_needle: "/instrumentation/upper-ecam/egt[0]",
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egt_2_needle: "/instrumentation/upper-ecam/egt[1]",
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# N1 parameters
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EPR_1: "/ECAM/Upper/EPR[0]",
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@ -1428,6 +1428,32 @@
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</table>
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</function>
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</fcs_function>
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<fcs_function name="/instrumentation/upper-ecam/egt[0]">
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<function>
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<table>
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<independentVar lookup="row">/engines/engine[0]/egt-actual</independentVar>
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<tableData>
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0 -90
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500 0
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1000 90
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</tableData>
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</table>
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</function>
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</fcs_function>
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<fcs_function name="/instrumentation/upper-ecam/egt[1]">
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<function>
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<table>
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<independentVar lookup="row">/engines/engine[1]/egt-actual</independentVar>
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<tableData>
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0 -90
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500 0
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1000 90
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</tableData>
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</table>
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</function>
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</fcs_function>
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</channel>
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@ -1223,5 +1223,66 @@
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</input>
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<output>/instrumentation/mk-viii/inputs/discretes/landing-flaps</output>
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</logic>
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<!-- Redo this sh*t later -->
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<filter>
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<name>EGT L</name>
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<type>gain</type>
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<gain>1.0</gain>
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<enable>
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<condition>
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<and>
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<equals>
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<property>/engines/engine[0]/state</property>
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<value>3</value>
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</equals>
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<greater-than-equals>
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<property>/engines/engine[0]/n1-actual</property>
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<property>/fdm/jsbsim/fadec/limit/min-n1</property>
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</greater-than-equals>
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</and>
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</condition>
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</enable>
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<input>
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<expression>
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<table>
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<property>/engines/engine[0]/n1-actual</property>
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<entry><ind> 18.9</ind><dep>434</dep></entry>
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<entry><ind>110.0</ind><dep>620</dep></entry>
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</table>
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</expression>
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</input>
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<output>/engines/engine[0]/egt-actual</output>
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</filter>
|
||||
|
||||
<filter>
|
||||
<name>EGT R</name>
|
||||
<type>gain</type>
|
||||
<gain>1.0</gain>
|
||||
<enable>
|
||||
<condition>
|
||||
<and>
|
||||
<equals>
|
||||
<property>/engines/engine[1]/state</property>
|
||||
<value>3</value>
|
||||
</equals>
|
||||
<greater-than-equals>
|
||||
<property>/engines/engine[1]/n1-actual</property>
|
||||
<property>/fdm/jsbsim/fadec/limit/min-n1</property>
|
||||
</greater-than-equals>
|
||||
</and>
|
||||
</condition>
|
||||
</enable>
|
||||
<input>
|
||||
<expression>
|
||||
<table>
|
||||
<property>/engines/engine[1]/n1-actual</property>
|
||||
<entry><ind> 18.9</ind><dep>434</dep></entry>
|
||||
<entry><ind>110.0</ind><dep>620</dep></entry>
|
||||
</table>
|
||||
</expression>
|
||||
</input>
|
||||
<output>/engines/engine[1]/egt-actual</output>
|
||||
</filter>
|
||||
|
||||
</PropertyList>
|
||||
|
|
|
|||
|
|
@ -139,84 +139,6 @@
|
|||
<output>/ECAM/Upper/EPRylim</output>
|
||||
</filter>
|
||||
|
||||
<filter>
|
||||
<name>EGT 1</name>
|
||||
<type>gain</type>
|
||||
<gain>1.0</gain>
|
||||
<input>
|
||||
<condition>
|
||||
<equals>
|
||||
<property>/options/eng</property>
|
||||
<value>CFM</value>
|
||||
</equals>
|
||||
</condition>
|
||||
<expression>
|
||||
<table>
|
||||
<property>/engines/engine[0]/egt-actual</property>
|
||||
<entry><ind> 0</ind><dep>-90</dep></entry>
|
||||
<entry><ind> 500</ind><dep> 0</dep></entry>
|
||||
<entry><ind>1000</ind><dep> 90</dep></entry>
|
||||
</table>
|
||||
</expression>
|
||||
</input>
|
||||
<input>
|
||||
<condition>
|
||||
<equals>
|
||||
<property>/options/eng</property>
|
||||
<value>IAE</value>
|
||||
</equals>
|
||||
</condition>
|
||||
<expression>
|
||||
<table>
|
||||
<property>/engines/engine[0]/egt-actual</property>
|
||||
<entry><ind> 0</ind><dep>-90</dep></entry>
|
||||
<entry><ind>400</ind><dep> 0</dep></entry>
|
||||
<entry><ind>800</ind><dep> 90</dep></entry>
|
||||
</table>
|
||||
</expression>
|
||||
</input>
|
||||
<output>/ECAM/Upper/EGT[0]</output>
|
||||
</filter>
|
||||
|
||||
<filter>
|
||||
<name>EGT 2</name>
|
||||
<type>gain</type>
|
||||
<gain>1.0</gain>
|
||||
<input>
|
||||
<condition>
|
||||
<equals>
|
||||
<property>/options/eng</property>
|
||||
<value>CFM</value>
|
||||
</equals>
|
||||
</condition>
|
||||
<expression>
|
||||
<table>
|
||||
<property>/engines/engine[1]/egt-actual</property>
|
||||
<entry><ind> 0</ind><dep>-90</dep></entry>
|
||||
<entry><ind> 500</ind><dep> 0</dep></entry>
|
||||
<entry><ind>1000</ind><dep> 90</dep></entry>
|
||||
</table>
|
||||
</expression>
|
||||
</input>
|
||||
<input>
|
||||
<condition>
|
||||
<equals>
|
||||
<property>/options/eng</property>
|
||||
<value>IAE</value>
|
||||
</equals>
|
||||
</condition>
|
||||
<expression>
|
||||
<table>
|
||||
<property>/engines/engine[1]/egt-actual</property>
|
||||
<entry><ind> 0</ind><dep>-90</dep></entry>
|
||||
<entry><ind>400</ind><dep> 0</dep></entry>
|
||||
<entry><ind>800</ind><dep> 90</dep></entry>
|
||||
</table>
|
||||
</expression>
|
||||
</input>
|
||||
<output>/ECAM/Upper/EGT[1]</output>
|
||||
</filter>
|
||||
|
||||
<!--filter>
|
||||
<name>N1 1</name>
|
||||
<type>gain</type>
|
||||
|
|
|
|||
Loading…
Add table
Reference in a new issue