Hi,
The meaning of hybrid is in fact noting more than 2 engines –electric or ‘whatever’- working together (or separated) as need demands.
In this case it’s a pair of gasoline engines designed and used for their proper purpose.
In my point of view, airplanes are born to use hybrids as they have two (by user) defined power levels. One is take off and the other is chosen cruise speed.
An ordinary 4-stroke engine, doing his job on full throttle is not bad at all, burning 1/5 liter for each HP an hour. Problem starts when operating at “economical” cruise where the engine operates in bad conditions, burning up to 3/5 liter / HP/hour.
Main reasons for this are pump losses and a no longer correct compression rate.
( for this reason they ignite the fuel faster).
Theoretic solution is rather simple: use a 4-stroke at full throttle delivering enough power
for your pre-chosen cruise. For my Ultra Light this is 15 HP at 110 km/h. (take off power = 50 HP)
The only trouble is taking off… and here we need another engine to help the ‘cruise’ engine.
In my case the cruise engine is a strongly modified 4-stroke 250cc Honda CRF delivering 15 HP @4700 rpm and the ‘take off help’ engine is an unmodified 2-stroke Honda CR engine, 56 HP @12000 rpm. Both engines can work separately, driving a single propeller.
Before this all started I was already a huge fan of the long EZ, we even have here a team EZ’s flying demo’s on air shows (the REVA patrouille/France).
It’s not that I absolutely want to build one, buying an EZ is an option too.
Replacing the installed engine with an ‘hybrid’ is the goal, cutting fuel costs in two - or
flying twice as far.
Regards Johan