English French German Italian Portuguese Spanish Swedish
Thursday, 29 September 2011 17:33

Understanding the Ground Adjustable Prop

Written by  Rotax Owner

Keeping it simple and effective for the common setup

Let's discuss prop pitch and how it affects flight characteristics. It can help flight characteristics or it can hinder. I'm often asked; What's the correct prop pitch for a specific plane? There is no single answer as many props are available to us today for Rotax engines and for different fuselages. There are, however, some commonalities and that is where we are headed in this article.

Certain principles do apply in either the 2 stroke or 4 stroke engines, although the numbers will be different, as with most ground adjustable props. This article won't get into all the designs, blade twists, angles, thrusts, shaft powers, etc...etc. Whoa, just thinking about it puts my brain in a tail-spin. We are going to keep it simple and easy to follow. I am going to use the Rotax 912ULS as an example.

Related Videos: Propeller Strike Inspection | Crankshaft Out Of Round Inspection | Crankshaft Distortion Inspection | Preventing Detonation - 4 Stroke

First let's pick a few numbers to keep in the back of our minds for later. We are going to shoot for certain idle rpm, so let's pick 1800 +/- rpm and 5500 + rpm for wide open throttle (WOT), flat and level at your average cruise altitude. It wouldn't make sense to set a prop for sea level when you are at 8,000' msl all the time. Why 5500 rpm as a target? That is the "continuous run" rpm Rotax recommends for the Rotax 912ULS and that rpm can be flown all the time if you chose to do so. Another good reason would be if you were to break a cable or had a throttle control failure. One carb would probably go wide open, as it's supposed to do and then you could advance your throttle and have the other carb go wide open. You could then fly to wherever you needed for hours; shut down and land. Anything over 5500 rpm (i.e. 5600-5800 rpm) would limit you to a 5 minute run time. This is just a little benefit for the 5500 target rpm, but not a determining factor. A prop manufacturer will usually have some instructions for their prop and sometimes a suggested starting point for pitch depending on the engine. Another often asked question is, What should my static rpm be? There is no specific or accurate answer for everyone's engine and prop. The static won't mean much if you only want to fine tune your existing setup. Static is more important for the first run owners or for new prop installation. The static rpm setting is just to get you in the ballpark and then you will need to fine tune it for your specific aircraft while flying WOT at your average altitude. So keeping it simple, you will want to set the pitch on most props to achieve a target with a beginning static (ground run) WOT rpm of around 4950-5100 rpm, but your static rpm may be slightly different depending on what you wanted for a final in flight WOT rpm outcome.

(Note: These next figures are general and yours may vary slightly) To do this properly, you will need to go fly at your average cruise altitude and fly flat and level at WOT for at least 1 minute. Now if your WOT rpm at this time is 5500 rpm and up to 5600 rpm you're probably set up fairly well for your engine, temperatures and fuel economy. If you are up at 5700+ rpm (150-200 rpm which could be high for your circumstances) then you may want to land and add a little pitch (about 1 - 1.25 degrees) back into the prop pitch, which will make it more coarse.

If you already have your prop setup is only turning 5200 rpm WOT flat and level you need to flatten or reduce the pitch approximately 2 degrees to achieve 5500+ rpm. Now you may have some special circumstance like a float equipped aircraft (heavy aircraft) that needs a little better climb, so a climb pitch of 5600-5675 rpm WOT might be warranted. We need to tune our props for the type of flying that we do.

What else does my prop pitch do for me?

Setting the prop pitch excessively coarse (i.e. 5000-5200 rpm WOT) causes excessive stress on engine components and gearbox which may necessitate early maintenance. Having the pitch too coarse will cause higher engine (CHT, EGT) and oil temperatures, excessive fuel consumption, poor climb and decreased cruise speed. Your engine doesn't have the horse power and torque to turn an excessively pitched prop. All piston engines have their limits and the props all have limits, too. So if your engine temps are up and your WOT engine rpm is below 5500 rpm try unloading the engine by reducing the prop pitch. If you have a prop that is too flat then it may climb well, but have a loss in cruise speed and of course engine temps and fuel are affected again.

Your exact numbers may vary some, but you now have a general idea on what to look for and how it may affect your flying and engine. We'll keep this discussion on the root topic of ground adjustable props. Special circumstance rpm settings and constant speed props will warrant discussion in a future article.

One last parting comment: If adjusting prop pitch sounds complicated, it isn't; it usually will only take 30-40 minutes, a couple of wrenches, a prop protractor and/or a level. So take the time to fine tune, your engine will say thank you in improved performance.

Read 3969 times

Comments  

 
0 # prop settingrichard seiders 2011-09-30 22:56
Good article, and glad to see mine is w/i the requested parameters. i wish I could have read this about six mos ago as that's when I learned how to set only after considerble trial and error. One thing I would suggest tho is a digital level with a homemade bracket to attach it to the prop blades to achieve blade settings w/i 1 degree max. difference. This info available on Vans Airforce blog for RV12
Report to administrator
 
 
+3 # Manifold PressureRoger Barlee 2011-09-30 23:35
A great article,and a further comment on the role of manifold pressure in the equation would also be helpful.
Report to administrator
 
 
+3 # eng temps vs RPMClyde Poser 2011-10-01 16:07
It is my understanding that the relationship between EGT/CHT vs engine RPM is a follows:
More Pitch and Lower RPM = higher CHT and lower EGT
Less Pitch and Higher RPM = lower CHT and Higher EGT
The reason for this is because when you increase the pitch you are loading the prop and making the engine work harder. The CHT goes up due to the higher workload and because the piston is moving slower it is pumping less air. Less air means a richer mixture and a lower EGT.
When you decrease the pitch you are unloading the engine and it isn't working as hard. So the CHT is lower. But you are pumping more air and the mixture gets leaner with a higher EGT.
Report to administrator
 
 
+3 # RPM and engine tempsRoger Lee 2011-10-01 22:38
There are a few variables, but generally speaking if you put too much pitch in the CHT, oil & coolant temps rise. When you unload the engine's work load then these temps usually come back down. Part of this is why when we have a ground adjustable prop we look for a balance between loading and unloading the engine which translates directly to performance for that particular aircraft. This is one reason we strive for that 5500-5600 rpm balance area. Keep in mind there are some special circumstances where some pilots need more rpm for the climb performance, but none of us should be down 100+ rpm below 5500. Your engine was designed to run at certain rpms and that is it.
Report to administrator
 
 
0 # simplicityClyde Poser 2011-10-02 02:20
I guess my explanation was too complicated. Thanks Roger for simplfying it.
Report to administrator
 

You need to login to comment.
A Free Registered account or a Subscription account is required to post comments. Sign up HERE

             | 
  • Facebook Page: 171088202915123
  • Twitter: rotaxowner
  • YouTube: rotaxowner