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1

2 KPa 1650

3 1623K 1473K

4 SiC

5 (121%) % 10% 20% 30% 40% 0% 10% 20% 30% 40% (%) (%)

6

7

8

9

10 MPa hr K K5C(HIP) MVS(HIP) Nf (Cycles) 4822 MVS 47XD K5C MVSC max (MPa)

11 TIG torch TP Thermo couple

12 57.8 mm :HPT Shroud Support 761 mm

13 :

14

15 Type R.F.*1 Z bundle 6.4 Y bundle Z bundle Y bundle 4.5

16 CMC 5 0

17

18

19

20 SiC SiC (C or BN)

21 Al O 3 CMC ZrO 2 CMC / mm / N

22 as-sprayed / / / mm / N

23

24

25 Surface Length Mach Number

26

27

28

29 NPR2.5

30

31 400 CMSX-4 TMS L.M.P.= T(20+ log t)/1000 T:Temp/K, t:time/hr Stress /MPa

32

33 CoNiCrAlY 8% YSZ Pt - Al

34

35

36

37

38 Applied stress (MPa) (MPa) Rim Bore 735C 29K 764C

39 (m)

40

41 (hr) ,700sec.(83.2kN) +(83.2kN) +(83.2kN) (78.5kN) +(78.5kN) +(78.5kN) 300sec

42 0.70 Re g= Fine 0.60 Impingement Hole 0.50 Conventional Basic 0.40 Pin Plot: Experment Turbine Blade Line: Prediction 0.30 Film Cooling Hole Cooling Air Flow Ratio Wc/Wg Cooling Effectiveness

43 Minimumdistance 0.5mm Unit volume (1mm1mm) High heat flux region Pin(0.25mm) Film cooling hole(0.4mm) Impingement hole(0.4mm)

44

45

46

47 Radial inflow Radial outflow

48

49 [sec] ag 37%ag ag 50%ag [] [rpm]

50 Vane Blade Disk Guide plate ( a ) Applied to disk front cavity Conventional (Disk front) Decreasing Temperature Advanced (Disk front) () %

51

52 Data bus

53 A/D CPU

54 Blade No. TBC TBC TBC TBC TBC TBC 800C 1200C

55

56

57 K K jj kj U j = F j K K jk kk U U j k F j = F k 1 1 [ K ] [ ] [ ] jk Kjj Kjk U k 1 1 [ K ] [ K ][ K ] [ K ] [ K ][ K ] F k kj kk jk jj kk jk F No.1 No. No (rpm) No (rpm)

58 No.1 No.2 No.3 No.4 No.5

59 #5 BRG () #5 BRG () 3rd 1st

60 ) () (mm) 2 MIL-PRF M50/M50 M50/Si M50/Si (GPa) (GPa)

61

62

63

64

65

66

67 10 Ch4 Ch3 Ch2 Ch1 [] (1650) T () T () []

68

69 1

70 (Hz)

71

72

73

74

75

76

77

78

79

80

81 1.2-1 NOx ANC GT LES AI CO 2 MMC CMC GT CMC TBC

82

83

84

85 ESPR

86 /// SST /

87 NO /// (LPP) SST /

88 MMC,CMC,TiAl MMC,CMC,TiAl /// / SST

89 1.3-5 CMC TiAl CMC SC PM CMC CMC TiAl CMC SC PM CMC TiAl CMC SC PM

90

91 ( 10 ) 14,000 12,000 10,000 8,000 6,000 4,000 2, ,372 bil. 9,931 bil. 12,270 bil ( % ) NYC PAR LAX HKG TYO PAR HKG HNL SIN PAR PAR 1 SIN 2 TYO 3 TYO 4 SIN 5 BKK 6 SIN 7 TYO 8 SYD 9 BOM () SST SST 1,

92

93

94

95

96

97

98

99 Large Eddy Simulation Analysis of a 18 lobe Convoluted Mixer Nozzle

100

2-2 ESPR 1 2 3 P. 6465 4 5 P. 63 6 P.6364 7 P. 6465 8 P. 6567 9 P.6567 10 3CO 2 25% 2 NOx NOx5gkg 1/7 1 3dB 4 11 P.69 ICAO Chapter3 1dB3dB3dB 3dB 450m 15dB 12dB 2000m 12 3dB P. 71 NOx 1kgNOxg 35g/kg-fuel

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[1.1] r 1 =10e j(ωt+π/4), r 2 =5e j(ωt+π/3), r 3 =3e j(ωt+π/6) ~r = ~r 1 + ~r 2 + ~r 3 = re j(ωt+φ) =(10e π 4 j +5e π 3 j +3e π 6 j )e jωt

[1.1] r 1 =10e j(ωt+π/4), r 2 =5e j(ωt+π/3), r 3 =3e j(ωt+π/6) ~r = ~r 1 + ~r 2 + ~r 3 = re j(ωt+φ) =(10e π 4 j +5e π 3 j +3e π 6 j )e jωt 3.4.7 [.] =e j(t+/4), =5e j(t+/3), 3 =3e j(t+/6) ~ = ~ + ~ + ~ 3 = e j(t+φ) =(e 4 j +5e 3 j +3e 6 j )e jt = e jφ e jt cos φ =cos 4 +5cos 3 +3cos 6 =.69 sin φ =sin 4 +5sin 3 +3sin 6 =.9 =.69 +.9 =7.74 [.]

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