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Logic for Mode Selection
标准号：
AIR5924
标准名称： Guidelines for the Integration of Electronic Engine Control Systems with Transport Category Aircraft Systems
同源图形
Station Definitions
Typical FADEC System
Example of Thrust vs
Normal Mode Thrust S
Altitude Dependent T
Engine Idle Selectio
Example of Multiplie
Thrust Schedule Usin
Thrust Rating Select
Ambient Temperature
Thrust* as a Functio
Moving Thrust Lever
Non-Moving Thrust Le
All Engines Operatin
One Engine Inoperati
Typical Cross-Manifo
Typical Body or Nace
Total Air Temperatur
Non-Aspirated TAT Pr
Engine Inlet Mounted
Typical FADEC Select
Typical Presentation
Typical FADEC Engine
Typical EICAS System
相关图形
for结构的故障树形式
GJB/Z 99-97
系统安全工程手册
FIGURE 3 - Torque Ve
AIR1087B
Aircraft A
FIGURE 9 - Torque Ve
AIR1087B
Aircraft A
Specific Optical Den
AIR1106A
Some Facto
Flow Schematic and S
AIR1191A
Performanc
Flow Schematic and S
AIR1191A
Performanc
Approximate Ventilat
AIR1191A
Performanc
FIGURE 5a. Mixing Co
AIR1191A
Performanc
FIGURE 5b. Mixing Co
AIR1191A
Performanc
FIGURE 5c. Mixing Co
AIR1191A
Performanc