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74000
78000
1500 1600 1700 1800 1900 2000 2100 2200
Runway length (m)
MTOW (kg)
D04
TOGA
D08
D12
D16
D20
D24
2007年6月中國民航大學(xué)空管學(xué)院航務(wù)系Page 176
起飛性能Takeoff Performance
§Impact on takeoff performance
50000
54000
58000
62000
66000
70000
74000
78000
1500 1600 1700 1800 1900 2000 2100 2200
Runway length (m)
MTOW (kg)
D04
TOGA
D08
D12
D16
D20
D24
IAE 27000lb
CONF2
Water ¼ inch
All reversers operative
Zp = 0ft, OAT = 10°C, no wind
1800m
59900kg
65500kg
2007年6月中國民航大學(xué)空管學(xué)院航務(wù)系Page 177
起飛性能Takeoff Performance
2007年6月中國民航大學(xué)空管學(xué)院航務(wù)系Page 178
起飛性能Takeoff Performance
2007年6月中國民航大學(xué)空管學(xué)院航務(wù)系Page 179
起飛性能Takeoff Performance
§6 減推力起飛
4、發(fā)動(dòng)機(jī)加力工作
§The bump produces an increased takeoff thrust capability.
2007年6月中國民航大學(xué)空管學(xué)院航務(wù)系Page 180
起飛性能Takeoff Performance
§6 減推力起飛
4、發(fā)動(dòng)機(jī)加力工作
§There is no possibility to set an intermediate
thrust between the basic maximum takeoff thrust
and the bump
§To take benefit of the DMC of lower engines
ratings while having an additional takeoff thrust
capability
2007年6月中國民航大學(xué)空管學(xué)院航務(wù)系Page 181
起飛性能Takeoff Performance
§6 減推力起飛
4、發(fā)動(dòng)機(jī)加力工作
§Various bumps were defined for the early A320
models, as a function of the customers requirements.
§For some latest A320 family models, the bump can
be made available upon request.
§These bumps provide between 6 and 10% more
thrust than the basic takeoff thrust.
A320 Family
2007年6月中國民航大學(xué)空管學(xué)院航務(wù)系Page 182
起飛性能Takeoff Performance
Bump guarded pushbuttons Bump pushbutton with cover open
Bump activation
2007年6月中國民航大學(xué)空管學(xué)院航務(wù)系Page 183
起飛性能Takeoff Performance
§7 復(fù)習(xí)
1、幾種起飛狀態(tài)？
2、FAR對起飛距離的要求？
3、三種性能計(jì)算方法？
4、一發(fā)停車特性曲線？平衡場地長度？
5、出現(xiàn)非平衡場地長度的原因？
6、V1、VR、V2、VMCG、VMBE、VMU的定義？關(guān)系？
7、起飛航跡的分段？
8、雙發(fā)飛機(jī)爬升梯度要求？
9、推導(dǎo)爬升梯度的計(jì)算公式？
10、總梯度與凈梯度的關(guān)系？
2007年6月中國民航大學(xué)空管學(xué)院航務(wù)系Page 184
起飛性能Takeoff Performance
§7 復(fù)習(xí)
11、飛機(jī)越障的要求？
12、三種越障方法的特點(diǎn)、用途？
13、改善爬升能力的措施？
14、改進(jìn)爬升的條件？
15、襟翼對起飛重量的影響？
16、風(fēng)速、溫度、氣壓高度、跑道坡度對起飛重量的影響？
17、起飛重量的限制因素？
18、減推力起飛的目的？條件？方式？
19、靈活溫度的要求？
20、污染跑道起飛采取的措施？
2007年6月中國民航大學(xué)空管學(xué)院航務(wù)系Page 185
起飛性能Takeoff Performance
§7 復(fù)習(xí)
習(xí)題19、25
飛機(jī)性能工程
Airplane Performance Engineering
中國民用航空學(xué)院空中交通管理學(xué)院航務(wù)運(yùn)行管理工程系
Department of Flight Operation,Air Traffic Management College, CAUC
§1 FLIGHT PLAN
1 Fuel Policy
The required fuel quantity for a safe trip along the
planned route is calculated for each flight. Each operator
has its own fuel policy. This policy is based on the
loading of minimum regulatory fuel requirements (FAR
121).
CHAPTER 10 FLIGHT PLAN AND OTHERS
飛機(jī)性能工程
Airplane Performance Engineering
中國民用航空學(xué)院空中交通管理學(xué)院航務(wù)運(yùn)行管理工程系
Department of Flight Operation,Air Traffic Management College, CAUC
§1 FLIGHT PLAN
1 Fuel Policy
1.1 Domestic Operations
CHAPTER 10 FLIGHT PLAN AND OTHERS
飛機(jī)性能工程
Airplane Performance Engineering
中國民用航空學(xué)院空中交通管理學(xué)院航務(wù)運(yùn)行管理工程系
Department of Flight Operation,Air Traffic Management College, CAUC
§1 FLIGHT PLAN
1 Fuel Policy
1.1 Domestic Operations
CHAPTER 10 FLIGHT PLAN AND OTHERS
飛機(jī)性能工程
Airplane Performance Engineering
中國民用航空學(xué)院空中交通管理學(xué)院航務(wù)運(yùn)行管理工程系
Department of Flight Operation,Air Traffic Management College, CAUC
§1 FLIGHT PLAN
1 Fuel Policy
1.1 Domestic Operations
Taxi Fuel. In order to determine this amount, local
conditions at departure and APU consumption should be
taken into account. Taxi fuel is usually a fixed quantity for
an average taxi duration. For the A320 for example, it is
equal to 140 kg (300 lb). This corresponds to a 12-
minute average taxi fuel. Based on statistics or
evaluation, the taxi duration and
taxi fuel may need to be adjusted.
　
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