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Typical Cross-Manifolded Body StaticPressure Sensing Configuration
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
Logic for Mode Selec
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 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
FIGURE 1. Typical To
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Aircraft A
FIGURE 8 - Probe Cal
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Constructi
Line Calibration Cur
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Constructi
Cross Section of Flo
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(R) Coolin
Isometric Cross Sect
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(R) Coolin
TYPICAL CROSS SECTIO
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(R) Electr
TYPICAL WIRING HARNE
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(R) Electr
Typical Turbine Engi
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Methods of
FIGURE 6 - Typical P
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Gas Energy
FIGURE 7 - Typical G
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Gas Energy