Click here to make tpub.com your Home Page

Page Title: LOCATION AND DESCRIPTION OF MAJOR COMPONENTS
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
CAPABILITIES AND FEATURES
Up
TM-55-2840-254-23-1 Engine Gas Turbine Model T55-L-712 Manual
Next
LOCATION AND DESCRIPTION OF MAJOR COMPONENTS (COnt)

TM 55-2840-254-23
1-9 LOCATION AND DESCRIPTION OF MAJOR COMPONENTS
Get to know your engine. The major components are listed and keyed in the following diagrams.
A
STARTER DRIVE ASSEMBLY. Mounts at the 12-o'clock position on the inlet housing and
provides the mounting pad for the starter. Internally connects to a shaft which is
connected by gearing to the compressor rotor.
B
MAIN FUEL FILTER. Filters fuel prior to delivery to the engine fuel control. Provides a visual
indication when it is close to bypassing its element because of clogging.
C
STARTING FUEL SOLENOID VALVE. Controls fuel flow to the starting fuel primer tube and
start fuel nozzles. Activated by airframe-mounted switch.
D
FLOW DIVIDER. Mounts at the bottom of the combustion section. Divides fuel flow from in-line
fuel filter into primary and secondary flows to the main fuel manifolds.
E
FUEL CONTROL. Mounts on the accessory drive gearbox. Isa hydromechanical device contain-
ing a fuel pump, gas producer and power turbine speed governors, an acceleration
and deceleration control, an air-bleed signal mechanism, and a fuel shutoff valve.
1-5

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