Click here to make tpub.com your Home Page

Page Title: Figure 1-4. Engine Compartment
Back | Up | Next

Click here for thousands of PDF manuals

Google


Web
www.tpub.com

Home


   
Information Categories
.... Administration
Advancement
Aerographer
Automotive
Aviation
Construction
Diving
Draftsman
Engineering
Electronics
Food and Cooking
Logistics
Math
Medical
Music
Nuclear Fundamentals
Photography
Religion
   
   

 

Back
Figure 1-3. Electrical and Battery Compartments
Up
TM-55-1730-229-12 Power Unit Aviation Multi-Output GTED Electrical Hydraulic Pneumatic (AGPU) Wheel Mounted Self-Propelled Towable Manual
Next
Engine/Gearcase

TM 55-1730-229-12
TO 35C2-3473-1
1.
DOOR, ACCESS
4.
ENGINE
2.
HYDRAULIC HOSES (STORAGE)
5.
GENERATOR
3.
AIR INTAKE DUCT ASSY
Engine Compartment
C.  Engine/Gearcase. The gas turbine
the engine. Engine exhaust is through
engine (GTE), Fig. 1-8, provides pneuma-
an  exhaust ejector, and out the roof
tic  power,  and shaft power to drive an
through an exhaust flapper.
AC/DC  generator  and  a  hydraulic pump
The  generator  and  pump are mounted on
NOTE
pads on the gearcase. Fuel for operation
of  the  engine  can be supplied from an
tegral  fuel tank or an external source.
tube, items  1 and 2, Fig. 1-8,
Selection  of  fuel source is controlled
are  being replaced with a low
the four-way valve, Fig. 1-1. Once star-
back-pressure exhaust installa-
ted, the engine runs up to 100% governed
tion will be incorporated in a
speed  of 58, 737 rpm, and automatically
83-360D AGPU and on other AGPUs
maintains that speed until shutdown. En-
whenever  replacement  of  the
gine air intake is through an air clean-
current ejector assembly is re-
er/duct assembly, Fig. 1-9 to
quired.

Privacy Statement - Press Release - Copyright Information. - Contact Us