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时间:2011-11-27 13:29来源:蓝天飞行翻译 作者:航空

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The following table assuming typical engine fuel flows, shows extra fuel consumption by using one engine instead of the A.P.U. for 1 minute, assuming  maximum electrical load and minimum ECS:
 
Extra fuel when using Engine instead of APU
 
Aircraft Type
 A.P.U. type
 Engine FF kg/hr/eng
 APU FF      kg/hr       
 Extra Fuel for 1 minute
 
A300 GE
 331-250
 520
 150kg
 6kg
 
A310 GE
 331-250
 520
 150kg
 6kg
 
A320 family CFM
 36-300
 300
 105kg
 3kg
 
A330 GE
 331-350
 520
 175kg
 6kg
 
A330 RR
 331-350
 720
 175kg
 9kg
 
A340 CFM
 331-350
 300
 175kg
 2kg
 
A340 RR
 331-600
 480
 275kg
 4kg
 

 
In overall economic terms, the benefits of APU operation are not just confined to fuel usage. The hourly maintenance costs of an APU are cheaper than the  aircraft powerplant, so reducing ground running time on the engines can significantly reduce the operating costs.
 
 
 
 
4.7  AERODYNAMIC DETERIORATION


 
Some of the most severe penalties in terms of fuel consumption are caused by increased drag resulting from poor airframe condition. Normal aerodynamic deterioration of an aircraft over a period of time can include the incomplete retraction of moving surfaces, damaged seals on control surfaces, skin roughness and deformation due to bird strikes or damage caused by ground vehicles, chipped paint, mismatched doors and excessive gaps. Each deterioration incurs a drag increase, and this increased drag is accompanied by increased fuel consumption.
 
This subject is covered fully in the brochure “Getting Hands-On Experience with Aerodynamic Deterioration”. 
 
The following table gives the highest deterioration effect in each category for the three aircraft families as increased sector fuel consumption in Kg, based on typical utilization figures.
 
Category
 Condition
 A300/310
 A320 Family
 A330/340
 
Misrigging
 Slat 15mm
 90
 60
 270
 
Absence of Seals
 Flap (chordwise)
 30
 14
 90
 
Missing Part (CDL)
 Access Door
 50
 13
 
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