CRUISE
PRESS ALT: 14000 FT

IAS ~ KTS 170 160 150 140 130
180 170

120 160 110
150 140

100 130
90 120
80 110
70
100 90

60
80

50
70

40
60

30
50
40

20
30
20

10
10
0

0

TRUE AIRSPEED ~ KTS

TORQUE PER ENGINE ~ %
AA0578

DATA BASE:FLIGHT TEST SA
Figure 7-22. Cruise High Drag -Pressure Altitude 14,000 Feet (Sheet 5 of 5)
TM 1-1520-253-10 
CRUISE CLEAN CONFIGURATION PRESS ALT: 16000 FT  CRUISE T700 (2) 16000 FT 
.50oC 3  TOTAL FUEL FLOW ~ 100 LB/HR 4 5 6 7 8 9 10 11  IAS ~ KTS .40oC 12 3  TOTAL FUEL FLOW ~ 100 LB/HR 4 5 6 7 8 9 10 11  12 

130
TRUE AIRSPEED ~ KTS
130
120
110
100
TRUE AIRSPEED ~ KTS

120
110
100
20
20
10
10

10 20 30 40 50 60 70 80 90 TORQUE PER ENGINE ~ % TORQUE PER ENGINE ~ % AA0435
DATA BASE:FLIGHT TEST SA
CRUISE
CRUISE 16000 FT

CLEAN CONFIGURATION T700 (2) PRESS ALT: 16000 FT
.30OC .20OC 
TOTAL F UEL  FLOW  ~ 1 00 LB/HR  IAS ~ KTS  TOTAL FUEL  FLO W ~ 1 00 LB/HR 
3  4  5  6  7  8  9  10 11 12  4 5 6  7  8  9  10  11 12 13 

140

TRUE AIRSPEED ~ KTS
130
120
110
100
130
120
110
100
TRUE AIRSPEED ~ KTS

30
30

10
10

102030405060708090 2030405060708090100 TORQUE PER ENGINE ~ % TORQUE PER ENGINE ~ %
AA0434A

DATA BASIS: FLIGHT TEST
SA

CRUISE  CRUISE 
CLEAN CONFIGURATION  T700 (2) 16000 FT 
PRESS ALT: 16000 FT 

TRUE AIRSPEED ~ KTS
.10oC 0oC
TOTAL FUEL FLOW ~ 100 LB/HR IAS ~ KTS TOTAL FUEL FLOW ~ 100 LB/HR
4 5 6 7 8 910111213 4 5 6 7 8 910111213 170

40
60

60
30
50
50
160 150 140 130
120
110
TRUE AIRSPEED ~ KTS
100
90
80
70
60
50
20
20

20 10
10

10 0
0

0 20 30 40 50 60 70 80 9010020 30 40 50 60 70 80 90100TORQUE PER ENGINE ~ % TORQUE PER ENGINE ~ % AA0433
SA

Figure 7-23. Cruise -Pressure Altitude 16,000 Feet (Sheet 3 of 5)
CRUISE CLEAN CONFIGURATION PRESS ALT: 16000 FT  CRUISE T700 (2) 16000 FT 
10oC 5  TOTAL FUEL FLOW ~ 100 LB/HR 6 7 8 9 10 11 12  13  20oC IAS ~ KTS 4  TOTAL FUEL FLOW ~ 100 LB/HR 5 6 7 8 9 10  11  12 

120
130

130
170 160 150 140 130
110

TRUE AIRSPEED ~ KTS
140
100 140
TRUE AIRSPEED ~ KTS
90

120
120
80110

110
70100

100
60
50
40

60
60
30
20

30 30
20 20
10
1010 00

0

10 2030 40506070 8090 TORQUE PER ENGINE ~ % TORQUE PER ENGINE ~ %
AA0436
SA

Figure 7-23. Cruise -Pressure Altitude 16,000 Feet (Sheet 4 of 5)
CRUISE
CRUISE 16000 FT

CLEAN CONFIGURATION T700 (2) PRESS ALT: 16000 FT
30oC
180 170 160 150 140 130
120 110 100
90
80
70
60
50 40 30 20 10 0 4
10 20

TOTAL FUEL FLOW ~ 100 LB/HR 5 6 7 8910

30 40 50 60 70 TORQUE PER ENGINE ~ %
11
80
IAS ~ KTS 12
170 160 150 140 130 120 110 100 90 80 70 60 50 40 30 20 10 0
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：UH-60Q 直升機技術手冊 直升機操作手冊 2(34)