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时间:2011-03-24 08:43来源:蓝天飞行翻译 作者:admin
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

 A current transformer monitors the current supplied to the electric pump. It transmits this data to the phase unbalance detector. In the event of phase unbalance, the detector unit signals the contactors to open. Thus, the supply of electrical power to the electric pump stops.
 5. Component Description_____________________
 A. Electric Pump 3075GX (Ref. Fig. 005) The electric pump is installed in the Yellow hydraulic bay. The pump includes:
 -an electric motor
 -
a boost pump

 -
a hydraulic pump.


 The electric motor is a conventional induction motor. It operates with a three- phase electric supply of 115 V AC, 400 Hz. It has a blower assembly to help the motor stay cool.
 A temperature switch is installed in the electric motor. If the temperature increases to 162 deg. C (503 deg. F) the switch operates and sends signals to the overhead panel and to the ECAM.
 The boost pump is a centrifugal type impeller. It raises the fluid
 pressure by a nominal 2.1 bar (30 psi) relative to the inlet pressure.
 The hydraulic pump is of the variable-displacement inline type. It has seven pistons. A spool valve compensator controls the displacement of the pump through a yoke and yoke actuating piston.
 Performance:
 -displacement = 4.3 ml/rev.
 -
delivery pressure at zero flow = 206 + 3 - 0 bar (2987 + 43.5 - 0 psi)

 -
delivery pressure at 23 l/min (6.08 US gal/min) = 196 bar (2842 psi)

 -
delivery pressure at 32 l/min (8.45 US gal/min) = 150 bar (2175 psi)

 


 B. Hand Pump 3009GM
 Description of the hand pump is given in 52-36-00. 
R  6. Operation_________ 
R  Operation of the pushbutton switch (P/BSW) 3804GX on overhead panel 40VU 
R  controls the electric pump. When the P/BSW is pressed and released, the ON 
R  light comes on and the electric pump starts. At the same time the lower 
R  display unit (DU) of the ECAM shows the operation of the pump (if the HYD 
R  page is selected). It is also possible to start the electric pump from the 
R  cargo door operating panel (Ref. 52-35-00). In this case, the cargo door 
R  system gets a supply of hydraulic power. 

R  The pump gets its supply of fluid from the reservoir of the Yellow hydraulic 
R  system and pressurizes the system to a nominal pressure of 206 bar (3000 
R  psi). The pump automatically changes its output to match the demands of the 
R  system. When the outlet pressure changes, the compensator moves the yoke 
R  plate by movement of the actuator. This increases or decreases the stroke of 
R  the pistons and thus controls the output of the pump. Some inlet fluid goes 
R  through the hollow drive shaft of the motor to keep the bearings and rotor 
R  cool. 

R  The output from the electric pump goes to the RH thrust reverser and to the 
R  high pressure (HP) manifold. From the HP manifold the supply is sent to all 
R  of the services including the cargo doors. 

R  The current transformer 3807GX and the phase unbalance detector 3808GX 
R  together monitor the operation of the electric motor. If there is a 
R  difference in the current flow of the three phases of the supply to the 
R  motor the current transformer sends a signal. This signal goes to the phase 
R  unbalance detector. The phase unbalance detector then sends signals to 
R  contactors 3805GX and 3806GX which causes them to open. This stops the 
R  supply of electrical power to the motor. At the same time signals are sent 
R  to the ECAM and to the overhead panel. 

R  If the motor of the electric pump overheats, the temperature switch in the 
R  motor sends signals to the ECAM and overhead panel. The message "ELEC OVHT" 
R  appears on the ECAM lower DU and the YELLOW ELEC PUMP/FAULT light comes on. 
R  The applicable messages appear on the STATUS page of the ECAM upper DU. If 
R  the temperature decreases, the warnings stop and a message on the STATUS 
R  page gives the information that the electric pump is available.

 

 Power Supply
 Figure 004

 1EFF : ALL 1 29-24-00Page 7/8 1 1 Feb 01/98 1 1 1CES
1


 Electric Pump
 Figure 005
 1EFF :  ALL  1  29-24-00 Page 9 
1  1  Feb 01/98
 
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