Re: Engine options for my Q1


Kerri & Mark <ksm@...>
 

- 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 [cm] 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 [cm] 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

Leon and Peter this is the specs that the company is displaying this would
power a Q1 very nicely not quite enough for a larger craft??

Mark

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