Improving Gas Turbine Engine Control System

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5.4 Figure 5-6. Example of Engine Simulation Deck Output Risks and Benefits Compared to CurrentProcess Min AMNude Arptod -266 -94,7 4-14973 -21 1016 r0 Mn SW)D 150,0 KIU PWa Mn P4m M Pn Mn P4* PA PA~. Mn Mn Mn Mr MPMn PAr Mr 14n Mn P4* PA Mn Mr Mn Ma Pwt Mn Mn PA Mn 5W0D 1000 150,0 101 046 970 00 43,4 15,2 KI1 6.4 47.6 4155 18 01 -116 910 5000 100 74,2 SIDJO 00 22 54 Mn !50 600 00 223 00 76 697 69 593 14.. 4G 65. 4 23 1 CIL 121 40 122 486 59,. -39 472 160 18.7 33331 33000 MD)00 100 0 74 100 6017 D0 523 00 9 60 45 -31.7 3000 M 4ODD0 29 7 00 326 114 00 40 40 9. ,flib High R,70-f SPftw E..n*.n Purusnem paamr I 7,5 64 01 A 62 7 72.5 F5.2 636 214 709 00 19 4 00 9497 a-9,3 65 707 69 695 E5 366 486 53 442 17A 3E630 010 375487 50 621 414 100 0 100.0 152.0 100.2 79,1 00 19 00 22.0 S0 B. 1 0.0 22161.9 00 12. 99 4..7 51.0 00 21 0 0 21-7 00 40 00 4 7 .49.0 4?J 10330 10000 500 1@330 100,0 10110 i1001,,0 1(3300 150 0 10000 9721 23320 1010 74 12.6 -3.30 45.0 149 5.0 86 -2.0 45 46 3A5 2flfl) 2CT00 2403m00a0 3M3 1300 33330 101 74b4 74 7 22 6 S0 79 -99 5611 35. .32..80 I6C0Y30 11 7 16 4 60 0 79 59 9 5<4 i Arl A"Load Act #2 Lqg Burn Iow Feet Perceni Percent Percert Prtent Percen ReraenTi Paeint Percent F tgq 100 600 I0 1000 AN F ow 00 26 -3.2 500 528 00 105 522 -78 1920 100 255 S7 .66 00 19 46 4 300 50.0 90 00 31 112 3 -17,1 150 0 10.0 101.7 5.7 40 10 1920 56 316 13.1 2 6 27 4 4 24 6 5,4 4.5 -s7 4 .ic2 -17.7 -11.2 -12 ;j31 43000 43000 8429 5)000 10.0 60 60000 1000 53000 150 0 86 150.0 13'2 110 7.7 00 5 -24.- 60 -0 7 6 -25 9 -11 0 19 5 4)000 50 65.5 5:3 00 22 76 4.7 -11.7 .34 76 5 20 6193 00 0 44 90 00 .9 47 105 90 95 10 43 As stated in the business case analysis (see section 5.2.6), a good potential exists for reduced program cost by invoking the GTA development concept. At the very least, the first 115 7 6 4,4 533 47.6 .j5,F .2&4 -44 0

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