The ULPower engine is a completely new engine. It looks like some of its collegues (it actually is a boxer engine), but the detailled finishing and the electronic injection make it unique.
A lot of engineering has been done to make the engine robust, simple, easily reachable for technical interventions, powerful, economical, ecologically sound and elegant. High quality components and special attention to engineering details puts the ULPower engine in a class of its own.
The following is a list of the ULPower engine standard design features, all included at no additional cost.
Electronic engine management and multi point fuel injection standard - no more danger of carburettor icing and the associated power loss of heating intake air; You get better overall power and efficiency especially if you fly in large variations of weather conditions and altitudes. The pilot doesn't need to make manual adjustments to the fuel mixture to obtain good fuel efficiency. This isn't necessary on your car - why should it be necessary in your aircraft?
The Engine Control Unit (ECU) uses high quality electronic components, electrical connections and wiring of the highest aviation quality (Tefzel). The wiring loom conductors are resistant to high temperatures, with each conductor completely and individually shielded in the wiring harness. The ECU has several in-built safety features which will allow the engine to continue to run (possibly with reduced power) even if some sensors fail, relay false data and/or wiring connections break. (For further information on the ECU see ECU Reliability and ECU Redundancy in the FAQ section.)
Automatic altitude and air temperature compensation for optimal fuel and power efficiency - no need to change the fuel mixture settings for a richer or leaner burn depending on your flight condition or altitude.
The colder the engine, the richer the fuel mixture will be. Accidental flooding of the engine is very unlikely and starting in very cold weather conditions will always be much easier than with carburettor engines.
High security connections between crankshaft and alternator/starter ring gear. The primary load path between the alternator flange and the crankshaft is transferred by the friction caused by the clamping force between the vertical mating surfaces of the inside of the flange and the end of the crankshaft. As a backup we have flat mating surfaces between the back end of the crankshaft and the inside of the alternator flange. The bolt responsible for the clamping force is largely over dimensioned and has thread which is opposite to the direction of the rotation of the engine. In the extremely unlike case that all pretension would be lost, the flat mating surfaces would continue to transfer the rotational motion of the crankshaft to the alternator. The bolt could not loosen itself out of the crankshaft through vibrations because it would have to unscrew faster than the crankshaft speed because of the opposite thread. We haven't used a Nordlock washer for the alternator flange because we feel we have enough security already built in to this fixture.
UL Power use a spline connection to mouth the propellor flange to the crankshaft. A large single bolt and a Nordlock washer ensure that the propellor flange is safe connected.
radial loading forces on the front shell bearing and also acts as the thrust bearing in either tractor or pusher configurations. This thrust bearing can be replaced without the dismantling the engine casing.


