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The descent is then carried out in managed mode, based on the following MACH/IAS law:
MachECON / IASECON / 250 kt
To minimize overall fuel consumption during flight, a low cost index must be used. As the descent phase is performed at idle thrust, it is advantageous to maximize its duration, from a fuel consumption standpoint. This is achieved at a low descent speed, which depends on the aircraft type (e.g. 250 knots for the A320 family). In any case, the descent speed must remain above green dot.
CI = 0 .
IASECON = Minimum descent speed (depends on A/C type)
On the other hand, a high cost index is required when the overall flight time needs to be reduced for cost reasons. In this case, the descent must be as fast as possible (i.e. at the maximum rate of descent speed). It is obtained at a speed, which is generally limited to VMO – 10 kt in normal operations .
CI = CImax .
IASECON = VMO – 10 kt
2.2.5. Emergency Descent
An emergency descent has to be carried out, in case of a cabin pressurization failure, the aim being to reach FL100 as soon as possible due to oxygen constraints. For this reason, MMO/VMO is the best speed schedule, as it enables the quickest possible rate of descent. This rate can even be increased by extending the airbrakes, if needed (refer to “En route Limitations” chapter).
2.3. FCOM Descent Table
Figure H8 shows an example of an A320 FCOM descent table:
IN FLIGHT PERFORMANCE DESCENT 3.05.30 P 2
SEQ 110 REV 31
R
DESCENT -M.78/300KT/250KT
IDLE THRUST NORMAL AIR CONDITIONING ANTI-ICING OFF ISA CG=33.0% MAXIMUM CABIN RATE OF DESCENT 350FT/MIN
WEIGHT (1000KG) 45 65 IAS (KT)
FL TIME (MIN) FUEL (KG) DIST. (NM) N1 TIME (MIN) FUEL (KG) DIST. (NM) N1
390 16.1 181 102 73.0 17.0 125 103 IDLE 241
370 14.6 152 90 74.0 16.2 121 98 IDLE 252
350 12.9 115 77 75.9 15.6 118 93 IDLE 264
330 11.7 90 69 IDLE 14.9 114 88 IDLE 277
310 11.2 87 65 IDLE 14.3 110 83 IDLE 289
290 10.8 84 61 IDLE 13.7 107 79 IDLE 300
270 10.2 81 57 IDLE 12.9 103 73 IDLE 300
250 9.6 77 53 IDLE 12.1 98 67 IDLE 300
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