Analisis Estadístico de Motores Turbojet

Nombre 1 P20 SX 2 K-45G2 3 MW 44 4 K-60G2 5 P60 SE 6 Bee 80 7 JetsMut !"-80B 8 MW 54 9 K-80G2 10 Me$%u$& 11 P80 SE 12 K-100G2 13 Me$'( 100XB 14 P100 )X 15 )*++(t 100 16 P90 ),( 17 K-120G2 18 Me$'( M140XB 19 P140 )X 20 K-160G2 21 eet* 160 22 Jet*t P160 23 W$e 160 24 Pe/*sus 25 P180 )X 26 K-180G2 27 K-180G2 28 AM"-450 AM"-450 29 Me$'( M200XB 30 )( 200 31 K-210G2 32 "J20 33 '&us 34 P200 SX 35 M*t 250 36 P300 )X 37 K-310G 38 M 'u/eu/+*u "J"J39 "(t* 40 Jet*t P400)X 41 "J40- G2 42 "BS 400N-J40P 43 N(e 44 "J 80 45 JetBeet'e JetBeet'e 250 250

Distribución Normal

Empuje 24 44.1 45 58.86 63 80 80 80 84.54258 88 97 98 100 100 100 105 117.72 140 142 156.96 160 160 160 167 175 176.5 176.58 200 200 200 206.1 210 230 230 250 300 304.1 350 392 395 395 420 784 900 1225

N N N N N N N N N N N N N N N N N N N N N N N N N N N N N N N N N N N N N N N N N N N N N

0.0008945 #NAME? #NAME? #NAME? #NAME? #NAME? #NAME? #NAME? #NAME? #NAME? #NAME? #NAME? #NAME? #NAME? #NAME? #NAME? #NAME? #NAME? #NAME? #NAME? #NAME? #NAME? #NAME? #NAME? #NAME? #NAME? #NAME? #NAME? #NAME? #NAME? #NAME? #NAME? #NAME? #NAME? #NAME? #NAME? #NAME? #NAME? #NAME? #NAME? #NAME? #NAME? #NAME? #NAME? #NAME?

Peso

UTM

0.35 3.4335 0.7 6.867 0.468 4.59108 0.85 8.3385 0.83 8.1423 0.79 7.7499 0.95 9.3195 0.99 9. 9 .7119 1.304 12.7922 1.4 13.734 1.36 13.3416 1.3 12.753 0.985 9.66285 1.05 10.3005 1 9.81 1.435 14.0774 1.28 12.5568 1.295 12.704 1.58 15.4998 1.46 14.3226 1.3 12.753 1.39 13.6359 1.43 14.0283 2.125 20.8463 1.595 15.647 1.724 16.9124 1.724 16.9124 2.4 23.544 1.53 15.0093 1.78 17.4618 1.65 16.1865 2.1 20 20.601 2.9 28.449 2.53 24.8193 2.28 22.3668 2.63 25.8003 2.6 25.506 3.65 35.8065 3.555 34.8746 3.55 34.8255 3.8 37.278 4 39.24 8.77 86.0337 10.5 103.005 20 196.2

46 "J 100 47 &, Promedio es: e s:(* (*%( %(; ; Est* Est*< et 47 "u$+>et 51 "u$+>et 55 "u$+>et 56 "u$+>et 57 "u$+>et

Me$'( M140XB Me$'( M200XB K-45G2 K-100G2 K-180G2 K-210G2 K-310G

Pe(, 30.3  "J 76 BAB= BAMBA &u'* "S-31M M(%$tu$+ E%'*($  "u$+e%* P(ee M(%$tu$+ ")S18 NP"301 "u$+>et

140 N 200 N 44.1 N 98 N 176.5 N 206.1 N 304.1 N

1.295 / 1.53 / 0.7 / 1.3 / 1.724 / 1.65 / 2.6 /

13000 $ 120000 $ 162000 $ 142000 $ 123000 $ 120000 $ 103000 $

Pa(inas para cecar despues E, DE ') $)R$),) DE' ttp5//66 #)N $'R 4)DE ET$ emp! emp! Velocidad Ma "ases Velocidad "ases #lujo aire $onsumo Ralenti "ases de Escape ma combustible sal comb! 30000 $ 640 Q 0.31 /s 37000 $ 720 Q 630 Q 0.38 /s 454 /( 30000 $ 750 Q 2160  0.5 /s 1300 ml/min 47600 $ 750 Q 650 Q 0.25 /s 290 /( 37000 $ 675 Q 600 Q 0.375 /s 450 /( 36000 $ 750 Q 700 Q 0.45 /s 640 /( 30000 $ 875 Q 825 Q 0.66 /s 1020 /( 20000 $ 875 Q 800 Q 1.25 /s 1900 /( 10000 $ 875 Q 800 Q 2.5 /s 3600 /( 40000 $ 730 Q 510 Q 1500  0.24 /s 288 /( 32000 $ 749 Q 520 Q 1461  0.35 /s 440 /( 32000 $ 750 Q 520 Q 1658  0.38 /s 500 /( 33000 $ 750 Q 480 Q 1840  0.45 /s 584 /( 35000 $ 750 Q 475 Q 2160  0.5 /s 980 /( 35000 $ 690 Q 590 Q 1454  0.26 /s 370 /( 80000 $ 690 Q 480 Q 1674  0.0516 /s 90 /( 50000 $ 730 Q 480 Q 1418  0.16 /s 230 /( 35000 $ 700 Q 510 Q 1397  0.25 /s 340 /( $ Q Q  1.7 /s /( $ Q Q  1.47 /s /( $ 780 Q Q  0.78 /s 1230 /( $ Q Q  /s 390 /( 55000 $ 700 Q 500 Q  /s 335 /( 42000 $ 700 Q 500 Q  /s 360 /( 34000 $ 700 Q 500 Q 620 /( 32000 $ 700 Q 500 Q 700 /( 28000 $ 700 Q 500 Q 810 /( 720 Q 30000 $

0.78 /s

$o Es 0.8

38.24 0.173 0.186 0.171 0.152 0.16 0.17 0.18 0.175 0.168 0.112 0.122 0.165

35 1300 /( 0.682 0.78

55000 $ $ 32000 $ 42000 $ 42000 $

176 '( 700 Q 520 Q 650 Q

480 '( 220 '( 360 '(

35000 $ 30000 $

33000 $ 30000 $

700 Q 650 Q 720 Q 650 Q 700 Q

390 /( 550 /( 155 /( 350 /( 545 /( 590 /( 870 /(

sumo ec%&co

'on(itud

Diametro

K/N$

444  285  350  220  264  267  268  524  690  240  293  297  355  365  300  180  245  290  625  512  373  316  221  228  235  300  325  270  320  425  495  1150  610  1220  1000 

197  112  147  100  120  130  147  201  260  97  112  112  132  132  112  60  83  112  272  235  147  121  82  91  102  110  124  130  156  164  250  370  305  535  381 

/$FNRs K/NR$ K/NR$ K/NR$ K/NR$ K/NR$ K/NR$ K/NR$ K/NR$ K/NR$ K/N$ K/N$ K/N$ K/N$ K/N$ K/N$

/$FNRs

// //

$ombustible P$* Jet A1 Ke$s( Pet$'eu Jet A1 Ke$s( Pet$'eu Ke$see - P*$*@ - Jet A1 - JP4 Ke$see /*s Ke$see Ke$see Ke$see Ke$see Ke$see Ke$see Ke$see Ke$see Ke$see JE"-A JE"-A1 JP4 JP8 "S-1 "2 )" JE"-A1 "S-1 )" e$s(et*/*  >et*/*$ 3 s&tet(% 2" t$%&%'e (' $ tu$ 4

4 5 K(/ "e% "u$+(es 5 5 5 5

)ee$e%(* ttD*e$s*%e2003.*$s(+'/.%Psts108B78B18A78A98AC9 ttsD((>ets.$/e0-t-100-/>et%*t160ttD.>et%*t.et%*t.*($e'*etsut.%-%tetu'*et%'u+.%")BHNE-ENGHNESJetsMut-E/(esL2=-JM-M100XBL2

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