Hks 700e Aircraft Engine

Hks 700e Aircraft engine

specifications

#Configuration:2 cylinders 4-stroke engine with horizontally opposed cylinders 4 valves per cylinder

#Bore-stoke:85mm - 60mm

#Displacement:680 cc

#Compression ratio:11.3:1

#Power output:56hp (41kW) at 5800 rpm (continuous); 60hp (44kW) at 6200 rpm (3min./take off)

#Torque max:7 kgm at 5000 rpm

#Max RPM:6200 rpm

#cylinders:Nickel ceramic composite coated cylinders

#Pistons:PVD coated piston rings

#Valve gap:Automatic adjustment by hydraulic lifters

#Camshaft:One central camshaft-pushrods-OHV

#Direction of rotation:Counter clockwise (looking from pilot seat, tractor configuration)

#Cooling:Air cooled cylinders.  Oil cooled cylinder heads.

#Lubrication:Dry sump forced lubrication by Trichoid pump, Camshaft driven (pressure pump and scavenge pump equipped)

#Ignition system:Dual CDI (captive discharge ignition)

#Generator output:AC-12 Volts 210 Watts

#Rectifier regulator:Three phase regulator

#Starter:Electric only

#Spark plugs:Denso IK24C11

#Electrode spacing:1.1 mm

#Fuel consumption:Approx. 9 litres per hour at 4750 rpm

#Reduction gear:Integrated with torsional shock absorption