LCR - 814 TG ti

 

 

LCR 814 Twin-Rotor Aircraft Engine

 

 

Model

LCR - 814 TG ti

Design

twin rotor fuel injected engine, electronic ignition

Dim. [inch’s] L x W x H
l x w x h

15.24 x 11.735 x 10.92
13.28 x 7.11 x 7.25

Weight [lbs] Engine
Drive
Electric system

77.16
14.33
9.92

Performance at speed

80 HP @ 6500 RPM
75 HP @ 6000 RPM

Torque at speed

90 Nm @ 4000 RPM

Displacement

814 cm³

BSFC

.49 lbs/hp/hr

Fuel

unleaded gasoline / Mogas (ROZ 92) or 100LL 1:80-mixture (premix)

Lubrication

standard-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 specification

Engine equipment with electric starter, generator, air-filter, engine management system with twin spark ignition

Optional

Nirosta exhaust muffler, radiator, 3:1 or 2:1 HDT cog-belt reduction drive