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#1
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![]() Stuart How many blades on the prop? Variable pitch? What Stuart balancer are you using? Is it nose wheel or tail dragger? It's a 2 blade metal prop (Sensenich) and I am using the spectrum mode of a Smart Avionics PB-1 balancer to look at the vibration spectrum. As I am actually the manufacturer of the PB-1, I believe it to be trustworthy! The spectrum display very clearly shows big peaks at 0.5 and 3.5 crank speed and not much elsewhere. A previous post suggested re-indexing the prop and that sounds like it's worth trying. What I really would like to find out is if there are any known engine problems that can give rise to that particular vibration frequency. Mark |
#2
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I am unaware of anything within a 4 cyl opposed engine that would
theoretically that would give anything at the 3.5 harmonic. I think you might be looking at a non-linearity in the mount (is it a dynafocal or a straight conical mouint?) or in the transducer(s) mounting. I'd guess the 3.5 order output to be comparatively insignificant compare to the 0.5 harmonic as far as human discomfort is concerned. Do try the prop indexing thing. Let us know the results. Good luck & THX |
#3
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![]() Thanks for the reply, Sorry, off the top of my head, I don't know what kind of engine mount it is. I shall ask the aircraft's owner. Checking the transducer mounting is a good idea even if it only removes another unknown from the equation. What I should have done at the time was vary the RPM more and see how the 3.5 order vibration magnitude changed. That surely would have indicated whether it was a resonance at a particular RPM. What's nagging at me is the magnitude of the 3.5 order vibration. 0.5 IPS equates to quite a lot of acceleration at that frequency and acceleration means force! Mark |
#4
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Checking the transducer mounting is a good idea even if it only
removes another unknown from the equation - Maybe your xdcr mount is resonant at the 3.5 harmonic? Change the RPM & see what the measurments show. What's nagging at me is the magnitude of the 3.5 order vibration. 0.5 IPS equates to quite a lot of acceleration at that frequency Its still only 1/4 g approx. Not that much for a piece of cheap machinery.......! |
#5
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Also - check the prop blade resonant frequency in the flapping mode
without the engine running, hitting it at a tip with the tip of your index finger. You might be able to hear it with your ear. |
#6
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("nrp" wrote)
Also - check the prop blade resonant frequency in the flapping mode without the engine running, hitting it at a tip with the tip of your index finger. You might be able to hear it with your ear. Oh good. You formed my question for me. I was wondering if there were any old tricks/shortcuts used back in WWI or WWII? Or even in the old barnstorming days - out next to someones ...barn? Not perfect fixes, but 'half-way to the wall' solutions. Montblack |
#7
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Its kinda interesting to critically watch the rotational plane of a
brightly lit (daylight) propeller against a dark background, as someone else varies the engine RPMs. I've seen the blade tips move like 1/2 inch out of plane at certain bad rpms. |
#8
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nrp wrote:
Its kinda interesting to critically watch the rotational plane of a brightly lit (daylight) propeller against a dark background, as someone else varies the engine RPMs. I've seen the blade tips move like 1/2 inch out of plane at certain bad rpms. Or a variable speed party strobe... Sheds an interesting light on things like that. Richard |
#9
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Possible reasons for out of balance are
propeller static balance bad or engine mounts bad. |
#10
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![]() Bingo! I have just determined that the strip of metal I used to mount the sensor to the front of the engine has a resonant frequency (with the sensor attached (of course)) around 95 HZ which is very close to the frequency of the spike I was seeing. I think that solves the mystery of the 3.5 crank vibration. Many thanks to those who replied, I learnt something today! Mark |
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