Aircraft Display Unit

The ADU (Aircraft Display Unit) was designed for an avionics environment (helicopter) as a highly integrated, stand-alone x86 compatible computing system, complete with Pentium MMX class processor, high efficiency power supply, quarter VGA display and solid state storage.

Enclosed in a rugged 1/4-Turn Dzus Rail Enclosure that meets military mounting specification MS25212, the PC/104-Plus (PCI bus)-based unit incorporates Parvus' CPU-1432, 90 Watt Power supply, a Sharp 3.8” 320x240 QVGA Display, CompactFlash SSD, and thermal measurement sensor. Set up is done through three front-panel control buttons and a Power Switch. Pending software development in a Windows CE environment the 3 various buttons can be enabled to serve various functionalities.

The Compact flash slot allows for boot-from-disk functionality along with use as an external memory source.

NOTE: This page showcases a CUSTOM product designed by Parvus for a specific systems engineering project. For more information on how a similar product can be designed to meet your specific requirements, contact Parvus Sales at 801-483-1533 or via email (sales@parvus.com).

FEATURES

Front Panel

Rendering of Inside

ADU Diagram

Back Panel Breakout

Temp Sensor	High/Low Combined Temperature Trigger. Active when temperature is above high setting and stays high until temperature falls below the low setting
Voltage Consumption	9V-12V DC
OS	Windows CE compatible
Navigation	3 programmable touch senstive buttons, 1 power button
SSD	Front-loading CompactFlash slot

Land

Airborne

Maritime

Unmaned

Aircraft Display Unit

Aircraft Display Unit

FEATURES