CA110I is a small engine suitable for the power requirements of some small and medium-sized unmanned aerial vehicles, with a maximum power of 20KW. It is suitable for aircraft equipment with takeoff weight of 50-100kg, and can work continuously for 300 hours. The engine adopts.Adopts horizontally opposed double-cylinder design with stable engine speed, and small vibration.No completed circuit wiringwith fast disassembled from aircraft.

CA1101 AERO ENGINES Paramete
Displacement: 342mL
Dimension: 305X480X477mm
Dry weight: 13.4kg(No muffler included )
Maximum power: 20/7000kW/(r/min)
kW/kgPower weight ratio: 1.49
Compression ratio: 10.2:1
Start mode:Electrical start
Lgnition: Inductive discharge ignition
Fuel supply mode:EFI
Fuel type: Min, 92 Mogas or Fuel with a 40:1 premix volume ratio
Cooling mode:Water cooling
TBO:300h
External Characteristic Curve

Altitude Characteristic Curve

Application


