AviCom brochure (pdf) - Saab

AVICOM > MODULAR SYSTEMS
FIXED WING
SYSTEMS
Example of an installation on a fixed wing aircraft:
GIU
RCP
GIU
OIU
CVR UHF/HF
VHF NAV
OIU
NIU
GIU
RCP
SCALABLE SOLUTIONS
AviCom’s modular structure has
scalability and adaptability at its heart.
By making use of distributed networking
architecture we ensure that the system can
be used with a wide variety of platforms.
A series of Line Replaceable Units (LRUs)
mean that individual components can be
added to existing systems. Other benefits
relating to the system’s modularity include:
Powerful Digital Communication Bus
Open system architecture
Simplified and reduced aircraft looms
Programmable HMI
Technical specifications
AviCom installation
Interfaces
• ARINC 429 (high or low speed)
• ARINC 664/AFDX
• RS485 (bi-directional)
• RS422 (bi-directional)
• Audio (bi-directional)
• Analogue to Digital (16 bit)
• MIL-STD-1553B (Bus Controller,
Monitor and Remote Terminal)
• Programmable Discrete ports
• 100 Mb/s Digital Bus
• Gigabit Ethernet
(including VOIP bridge)
• Displays: Colour 320 x 240
(Quarter VGA), 4.1 inch
• Power consumption: 30 W
(nominal) per unit
• Mass: < 2.1 kg per unit
• Size: 127 mm (W) x 86 mm (H)
x 215 mm (D) per unit (maximum)
• Operating temperature: -40°C to +70°C
• Development standards:
– MIL-STD-810E
– MIL-STD-461E
– RTCA D0-160F
– RTCA D0-178B
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