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#1
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![]() On 29-Sep-2004, Jim Weir wrote: The question is whether to have a two-channel meter (which complexes up both the design AND the panel space), a single meter switchable between lateral and vertical) or a single meter with the two axes summed together. Hmm... Interesting bit of instrumentation there. My take is that since summing the two axes will involve some trivial electronics, why not add a bit more trivial electronics and have a means to (at least momentarily) individually look at either one axis or the other. I envision a 3-position toggle switch which is spring-loaded to the center ("mixed") position. Toggle to either "side" position will select one or the other axis for an individual reading. -- -Elliott Drucker |
#2
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Jim Weir wrote...
The question is whether to have a two-channel meter (which complexes up both the design AND the panel space), a single meter switchable between lateral and vertical) or a single meter with the two axes summed together. You gotta decide what you're going to do with it and what it's going to tell you in the cockpit. Are your procedures going to be different if one axis reads high and the other reads normal ("Holy cow, lateral vibes are off scale! Good thing it's not vertical!")? Personally I'd think that total vibration (RSS) would be sufficient to indicate a problem that warranted more detailed troubleshooting on the ground. Too much information in the cockpit can be just as bad as not enough. Dave 'standard gauge' Hyde |
#3
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Well if you can produce a Power Density Spectrum, it might be useful for
engine condition monitoring. On my helicopter, I have a two channel device with a photo sensor to give me some idea the crank angle (if I'm checking engine balance) or rotor position if I'm doing a rotor balance. However, I put a scope probe on the out put of the accelerometer and can't find an intelligent signal. I'm told that my processor does a tracking filter based on the RPM derived from the photo sensor output. The sensors that I'm using are the piezoelectric type and the processor integrates their output to derive an "inches per second" or ips reading. I find the vibration analyzer both mandatory and frustrating. I will surely follow any KitPlanes article you produce with your sensors. Good luck. "Jim Weir" wrote in message ... I've come across a marvelously cheap vibration sensor that I want to convert into an engine vibration instrument for a Kitplanes article. The electronics for me is relatively trivial...the mechanics of vibration are a little harder to fathom. From a mechanical engineering point of view on a horizontally opposed engine, there are (as with most things) three axes of freedom -- fore and aft, side to side, and up and down (longitudinal, lateral, vertical). The sensor I have reads two axes, and my hit is that fore-aft is the least interesting vibration mode of the engine. The question is whether to have a two-channel meter (which complexes up both the design AND the panel space), a single meter switchable between lateral and vertical) or a single meter with the two axes summed together. Comments and thoughts from the technonerds amongst us appreciated. (It has nothing, repeat NOTHING to do with the fact that such a meter might have detected a crack in that cylinder WAY BEFORE it departed the engine on the way home from Oshkosh {;-) ) Jim Jim Weir (A&P/IA, CFI, & other good alphabet soup) VP Eng RST Pres. Cyberchapter EAA Tech. Counselor http://www.rst-engr.com |
#4
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Gotta watch the temperatures around those sensors...
Up down left right is what you want to 'see'. http://zone.ni.com/devzone/devzone.n...25684A004EB0F4 "Jim Weir" wrote in message ... I've come across a marvelously cheap vibration sensor that I want to convert into an engine vibration instrument for a Kitplanes article. The electronics for me is relatively trivial...the mechanics of vibration are a little harder to fathom. From a mechanical engineering point of view on a horizontally opposed engine, there are (as with most things) three axes of freedom -- fore and aft, side to side, and up and down (longitudinal, lateral, vertical). The sensor I have reads two axes, and my hit is that fore-aft is the least interesting vibration mode of the engine. The question is whether to have a two-channel meter (which complexes up both the design AND the panel space), a single meter switchable between lateral and vertical) or a single meter with the two axes summed together. Comments and thoughts from the technonerds amongst us appreciated. (It has nothing, repeat NOTHING to do with the fact that such a meter might have detected a crack in that cylinder WAY BEFORE it departed the engine on the way home from Oshkosh {;-) ) Jim Jim Weir (A&P/IA, CFI, & other good alphabet soup) VP Eng RST Pres. Cyberchapter EAA Tech. Counselor http://www.rst-engr.com |
#5
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Jim Weir wrote in message . ..
From a mechanical engineering point of view on a horizontally opposed engine, there are (as with most things) three axes of freedom -- fore and aft, side to side, and up and down (longitudinal, lateral, vertical). Can these things measure rotational vibration, or just linear? Seems to me that the real shaking going on up front is rotational. Being able to measure the vibration in the other 3 axis would be nice. I vote for a combination of switchable/discrete channels and a summation mode. ==================== Leon McAtee |
#6
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I work for Bently, Nevada.
NOTE: This is not a plug for Bently products! Our market is large power generation stations/oil refineries, etc. But the research done at Bently is paralled by none. www.bently.com I could go on for hours spewing information and quoting dissertations and such, but I would recommend reading the ORBIT magazine from the bently website. There is always good information machinery diagnostics. I would also recommend looking at some of the applications for Bently's recip monitors (most of the monitoring is for rotating machines, i.e. generators). There has been a great deal of research in recip recently. You can read some of the product literature, too. In particular, read about the 3500/70M, the 3500/72M, and the 3500/77M. These are recip impulse/velocity monitors, rod position monitors, and cylinder pressure monitors. It's probably way more information than your looking for, but it may come in useful for an article. It's not aviation specific, but more about machinery theory. Bently also offers a machinery diagnostics class, which is pretty good. Adam |
#7
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There is also 4th and 5th degrees of freedom, rotation and torque.
Anything is measurable if you have the right equipment and techniques. 15 years ago or so, I met a couple of guys who marketed their services of predictive vibration analysis for very large diesels in the oil patch and marine fields. They could tell you when a valve guide was beginning to wear. They smiled big when asked about their fees. Predictive vibration analysis is well known by turbine aircraft operators. I decided long time ago that its not economically viable for aircraft piston engines. I think that the other techniques of predictive maintenance do just as well. Exception maybe is the front alternator 520. Really, who is goin' to pay for it? The first requirement would be to have a well established baseline for a specific engine. And if one is taking measurments that have nothing to do with cylinder head separation, one would not have to account for the percentages of difference of combustion forces of all the cylinders and the percentage difference in the other factors, like valve spring pressure, that influence the horizontal yawing motion a flat opposed aircraft engine undergoes during normal operations. Another angle to consider could be......how to describe this? .....is to ask what musical note the cylinder rings at. Everything rings at its own frequency and a crack will change it. Good luck Kent Felkins Tulsa Oklahoma 15 years ago or so I talked to some guys who "Jim Weir" wrote in message ... I've come across a marvelously cheap vibration sensor that I want to convert into an engine vibration instrument for a Kitplanes article. The electronics for me is relatively trivial...the mechanics of vibration are a little harder to fathom. From a mechanical engineering point of view on a horizontally opposed engine, there are (as with most things) three axes of freedom -- fore and aft, side to side, and up and down (longitudinal, lateral, vertical). The sensor I have reads two axes, and my hit is that fore-aft is the least interesting vibration mode of the engine. The question is whether to have a two-channel meter (which complexes up both the design AND the panel space), a single meter switchable between lateral and vertical) or a single meter with the two axes summed together. Comments and thoughts from the technonerds amongst us appreciated. (It has nothing, repeat NOTHING to do with the fact that such a meter might have detected a crack in that cylinder WAY BEFORE it departed the engine on the way home from Oshkosh {;-) ) Jim Jim Weir (A&P/IA, CFI, & other good alphabet soup) VP Eng RST Pres. Cyberchapter EAA Tech. Counselor http://www.rst-engr.com |
#8
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Jim Weir wrote in message . ..
I've come across a marvelously cheap vibration sensor that I want to convert into an engine vibration instrument for a Kitplanes article. The electronics for me is relatively trivial...the mechanics of vibration are a little harder to fathom. snip Comments and thoughts from the technonerds amongst us appreciated. sig snip How 'bout comments from an ignorant wrench-bender? Have allegedly repeatedly measured 1st order vibration (referenced to propeller rpm) of both recip and turboprop aircraft engines using a single axis sensor mounted perpendicular to the crankshaft. The indicated amplitude of the vibration was not appreciably affected by the "clocking" of the sensor axis. In short, mounted either near the propeller end (front), or the on the accessory case (rear) it did not matter whether the axis of the sensor was parallel to the cylinders (call it side-to-side), perpendicular to the cylinders (call it up and down), or at any clock angle in between. If this information is not useful, just remember what you paid for it, and where it came from. TC |
#9
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Jim Weir wrote:
I've come across a marvelously cheap vibration sensor that I want to convert into an engine vibration instrument for a Kitplanes article. The electronics for me is relatively trivial...the mechanics of vibration are a little harder to fathom. Jim, I was reading an article on the NASA LARC website which discussed flutter detection techniques. Would it be possible to tag the ailerons with a couple of these babies, then add a "pull-power-and-pull-up" buzzer? -- http://www.ernest.isa-geek.org/ "This is by far the hardest lesson about freedom. It goes against instinct, and morality, to just sit back and watch people make mistakes. We want to help them, which means control them and their decisions, but in doing so we actually hurt them (and ourselves)." |
#10
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Ernest Christley wrote:
Jim Weir wrote: I've come across a marvelously cheap vibration sensor that I want to convert into an engine vibration instrument for a Kitplanes article. The electronics for me is relatively trivial...the mechanics of vibration are a little harder to fathom. Jim, I was reading an article on the NASA LARC website which discussed flutter detection techniques. Would it be possible to tag the ailerons with a couple of these babies, then add a "pull-power-and-pull-up" buzzer? I'm sorry. I didn't give quite enough information as to why the vibration sensor would be beneficial. The study was a review of techniques used to generate flutter. It seems to be a well known fact amoung the engineering types that it is fairly easy to detect the onset of flutter. The vibration is fairly steady state and random, and just before flutter sets in the vibration begins to diverge logritmically (I know that ain't spelt rite). A circuit with a sort of squelch mode would be very useful, especially during initial flight testing. -- http://www.ernest.isa-geek.org/ "This is by far the hardest lesson about freedom. It goes against instinct, and morality, to just sit back and watch people make mistakes. We want to help them, which means control them and their decisions, but in doing so we actually hurt them (and ourselves)." |
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