Description
The Omnia Fuel Computer monitors the instant fuel consumption, the estimation of remaining fuel, the endurance and the flight independence (with GPS). It requires 1 or 2 flow measurements for supply and fuel return. Three alarms can be configurated: remaining quantity, minimal endurance and minimal scope. It can also monitors the fuel pressure with a sensor in option.
Fuel flow indicator Remaining quantity indication Burn fuel since the engine start-up
Endurance Remaining distance Remaining fuel estimated for destination
Main characteristics
Included measures:
- Fuel throughput
- Fuel remaining
- Burnt fuel
- Endurance times
- Reserve scope
Interfaces :
- Button with push button
- 2 CAN bus
- Light sensor entry
- USB 2.0 port
- 2 sensors input for fuel throughput
- 1 fuel pressure input for Flybox sensor with an option Cod. 601040
- Can be linked on cluster with other Omnia instruments
Production:
- Solid box in aluminium
- Powder paint
- 100% fabricated and tested with automatic process
Functions:
- Visual alarm on screen
- Alarm output with transistor
- Manual or automatic backlighting dimmer
- Easy software upgrade through the USB port
Technical specifications:
- LCD screen with graphic colors 2,4″ 320 x 240 pixels, with 1000 nits backlighting dimensions 29x18mm.
- Standard set-up 2-1/4" 57mm and 3-1/8" 80mm
- Aluminium box with powder painting
- Dimensions : 68x62x35mm (57), 85x85x40mm (80)
- Weight: 140g. (57"), 230g. (80")
- 2 fuel throughput sensors inputs with amplitude scope: 5-30 Vpp, frequency scope 2Hz-10Khz, min. impetus duration: 50uS
- 1 fuel pressure input: 0-5V
- Power supply tension: 10 ~ 30 V
- GPS input: RS232 RX port
- Power supply: 60 mA (57), 135 mA (80)
- Alarm output with open collector (max 300mA, weak active). This output can also be used to send a tone in the intercom, by using the optional device Flybox code 105899
- Functioning temperature range: -20 ~ +70 °C
- Humidity: 90% max (without condensation)
- Communication through 2 CAN bus
English 
French 
