MOTORES WANKEL

Description:

- single or twin rotor rotary piston engine - liquid cooled housing - charge-cooled rotor - roller-bearing - "tric-injection" fuel injection system  - engine management system - dual electronic ignition - generator - electric starter  - cogbelt reduction drive

Aircraft-engine LCR - 407 SGti

Modell	LCR - 407 SGti
Design	single rotor injected engine
Dim. [mm] L x W x H                  l x w x  h	481 x 462 x 430 404 x 280 x 285
Weight [kg] Engine                    Drive                                   Elektric system	25,0 6,5 3,5
Performance [kW(hp)] at speed [rpm]	27 (37) 6000
Torque [Nm] at speed [rpm]	42 4500
Displacement [cm³]	407
BCFC [g/kWh]	300
Fuel	unleaded gasoline / Mogas (ROZ 92) or 1:80-mixture (premix)
Lubrication	standart-2-stroke-oil (API-TC)
Ignition unit	WANKEL tric-injection with engine management system
electric starter	12 V / 900 W
Generator	14 V / 200 W
Standard specifikation	Engine equipment with electric starter, generator, airfilter, engine management system with twin spark ignition
Optional	nirosta exhaust muffler, radiator, 3:1 HDT cogbelt reduction drive

Aircraft engine LCR - 814 TGti

Modell	LCR - 814 TGti
Design	twin rotor injected engine
Dim. [mm] L x W x H                  l x w x  h	600 x 462 x 430 523 x 280 x 285
Weight [kg] Engine                    Drive                    Elektric system	35,0 6,5 4,5
Performance [kW(hp)] at speed [rpm]	55 (75) 6000
Torque [Nm] at speed [rpm]	90 4000
Displacement [cm³]	814
BCFC [g/kWh]	300
Fuel	unleaded gasoline / Mogas (ROZ 92) or 1:80-mixture (premix)
Lubrication	standart-2-stroke-oil (API-TC)
Ignition unit	WANKEL tric-injection with engine management system
electric starter	12 V / 900 W
Generator	14 V / 200 W
Standard specifikation	Engine equipment with electric starter, generator, airfilter, engine management system with twin spark ignition
Optional	nirosta exhaust muffler, radiator, 3:1 HDT cogbelt reduction drive