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时间:2011-09-28 12:39来源:蓝天飞行翻译 作者:航空
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 2.  Component Details
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 A.  Fuel Level Sensor (Fig. 2)
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MAINTENANCE MANUAL


Pressure Fueling System
Figure 1

H42221
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FUEL TANK LEFT MAIN  CENTER FUEL TANK  FUEL TANK RIGHT MAIN  TANK SURGE 
SENSOR FUEL LEVEL BSEE  DOOR AIRPLANE CENTERLINE  SENSOR BSEE FUEL LEVEL 
ELECTRICAL SYSTEMS CARD FILE, P50 
ASEE ELECTRICAL SYSTEMS CARD FILE, P50  SENSOR FUEL LEVEL (EXAMPLE) EJECTOR CONNECTOR ELECTRICAL A CONTROL CARD OF THE FUEL LEVEL SENSOR ELECTRICAL SYSTEMS CARD FILE, P50 
ELECTRICAL CONNECTOR 
REAR SPAR 
FWD  INBD 
B FUEL LEVEL SENSOR 
Figure 2 Pressure Fueling Overfill Protection Components 

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 (1)  
A fuel level sensor attaches to the rear spar of each surge tank. The fuel level sensor has a probe with a small piezo-electric element sealed in the probe and an electrical connector. The probe, which extends into the fuel tank, and the element form an electromechanical circuit. This circuit sets up acoustic vibrations in the probe when 28v dc from the control card for the fuel level sensor energizes the element. With fuel around the probe the circuit frequency decreases. The control card monitors changes in frequency and controls the fueling shutoff valves accordingly.

 B.  
Control Card for the Fuel Level Sensor

 (1)  
A contral card for the fuel level sensor is installed in the electrical systems card file, P50, in the electrical/electronics bay. The control card supplies control logic to protect the fuel system from overfilling during fueling. The control card operates on 28v dc power and supplies drive signals to each fuel level sensor. The fuel level sensors supply frequency outputs back to the control card which controls the refueling valve relays. The frequency level that the control card senses determines whether the control card logic interrupts power to the refueling valve relays.
 
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本文链接地址:757 AMM 飞机维护手册 燃油 CHAPTER 28 - FUEL 2(38)