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 |
| 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 |
| 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 |