Suddenly there is more room at the Seagull’s nest; the wings are gone to the paint shop. They should be back tomorrow and from my own “weight watch maniac’s” view, I can barely wait to see how much the paint has added. Each wing weighed about 26 kg (57 lbs) including all attachments, flaperon and wing tip before painting.

The painted wings will also represent the first really ready parts and a milestone in the whole process.

 

Another milestone is that we now have an engine. Considering possible alternatives of getting it from the Scandinavian Jabiru dealer in Stavanger Norway, made us go for the quickest which was to jump into the car and go pick it up. We made the 2800 km trip in three days with two overnight stops with relatives in Oslo. The shortest route was closed for the winter and the one available was scenic, narrow, much longer and had 53 tunnels between Oslo and Stavanger (yes, we counted them on the way back). There was also an unexpected number of toll plazas that on the return trip, when many of them were closed, rapidly drained our bulk of Norwegian currency. The aftermath of that is still yet to be seen.

 

The Jabiru was immediately hung in place to verify the needs for cowling modifications.

The Rotax PSRU moves the prop shaft up related to the engine cylinders and we were prepared to some interference with the upper engine cowl. That assumption was right but only a slight lifting of the upper cowl AFT part is needed. In all other aspects the Jabiru fits excellent and with a three inch prop shaft extension, the unwanted nose-up CoG. moment caused by the engine, decreases some 15 % compared to the Rotax installation.

 

In Stavanger we also discussed suitable props a lot. The Jabiru dealer Paul, recommended a two bladed light, fixed pitch wooden propeller. Because of the prototype evaluation, we just thought that an adjustable would give us more options in finding the best pitch. We have learned however, that a fixed prop isn’t that expensive and the rpm’s we get with this at different speeds, will still tell us a lot about how improvements should be made.

 

It is maybe a little harder to predict the performance of a pusher like the LN-3 than on a tractor design. Even if the theoretical calculations give you a certain picture, the reality might give you something different. Not necessarily worse, it can also be better.

Experienced people used to be cautious about the fuselage shape up-streams the propeller. If it’s too steep, a premature offset of the air stream will adversely affect the prop efficiency. Since the LN-3 is a tandem with a relatively narrow fuselage, we are on the right side to what available praxis tells. A good pusher installation is actually more efficient than a tractor since the high speed prop wash flows over much less of the airplane surface.

 

Thanks for your interest

Lage

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