Wankel aircraft-engine

 
 

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