PTU CASE DRAIN FILTER MODULE
PTU Filter Modules
Figure 3
PTU PRESSURE FILTER
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E. Left EDP Pressure Switch
(1) The left EDP pressure switch, which controls left EDP low pressure indication, also turns on the PTU if left EDP pressure drops below approximately 1275 psi. (Ref 29-11-00 for EDP pressure switch location and more information.)
3. Operation
_________
A. Functional Description (Fig. 5)
(1) Automatic Operation
(a) In automatic (normal) operation, 28 volt dc power is provided through the PTU manual switch OFF position to the left engine-out relay No. 2. This relay closes if power is lost in the left engine. If the right engine is still running, power is routed to the PTU control valve through the right engine-out relay No. 4 and the PTU ON relay. If the left engine is running, but the left EDP pressure drops below approximately 1275 psi, 28 volt dc power is routed through the left EDP pressure switch, right engine-out relay NO. 4, and PTU ON relay to the PTU control valve. The valve motor drives the PTU control valve to the open position. This supplies right system pressure to operate the PTU hydraulic motor which drives the pump.
HYDRAULIC LINE
VALVE POSITION INDICATOR AND MANUAL OVERRIDE ARM
VALVE VALVE
ACTUATOR MOTOR
PTU Control Valve
Figure 4
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COMPUTER TO LEFT SUPPLY
HYDRAULIC
SYSTEM
RETURN
Power Transfer Unit System Schematic
Figure 5
28V DCL BUS
P11
LEGEND
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(b) 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址:757 AMM 飞机维护手册 液压 CHAPTER 29 - HYDRAULIC POWER 2(121)