Subject: 814 / Hyperlight ??]
From: Paul
Date: 12/9/1999, 11:52 AM
To: zz

Howard Wilkinson wrote:

Anybody know what the rotary engine refered to as an "814" used in the
Sorrell Hyperlite featured in this month's Experimenter is??
Described as being 75 Hp and weighing in at 115 lbs.... The pictures
show it as a twin rotor engine.  Plugs are on the left as installed in
the aircraft, exhaust on the right.  Looks to be all aluminum.

    Is this an NSU or Sachs rotary of some kind???    I was also
curious about the Suzuki motor cycles introduced in about '76 or '77
...The RE5.... I never heard much about the..... are they a viable
power plant in the 50 hp range??

                                                H.W.

These are the specs of the actual engine used in the
Hyperlite.

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


  


-- Paul Lamar The Aircraft Rotary Engine Newsletter. Powered by Linux. http://home.earthlink.net/~rotaryeng/ http://www.linux.org

wancc3.jpg