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Page Title: Figure 1-5. Hydraulic Module, Pump, Lines and Hoses
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Figure 1-4. Engine Air Intake System
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TM-55-1730-229-34 Power Unit Aviation Multi-Output GTED Electrical Hydraulic Pneumatic (AGPU) Wheel Mounted Self-Propelled Towable Manual
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Figure 1-6. Propulsion System

TM 55-1730-229-34
AG 320A0-MME-000
TO 35C2-3-473-2
TM 1730-34/1
control panel) and controls the exciter
voltage is half-wave rectified and ap-
field as required to keep the selected
plied to the generator main dc rotating
output within limits.
field.  The magnitude of the three phase
voltage generated  in the main stator
windings is a function of the ampere
e. Hydraulic  System. The hydrau-
turns of the field windings which is, in
lic system,  figure 1-5,  consists of a
turn, a function of the exciter field
hydraulic pump,  interconnecting lines
The GCU monitors the gen-
excitation.
The
and hoses, and a hydraulic module.
erator ac or dc output (depending upon
hydraulic pump is mounted on an engine
which output is  selected at the AGPU
Hydraulic Module, Pump, Lines and Hoses
Figure 1-5.
1-7

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