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#1
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I am involved with the building of a velocity, and questions are flying
around about propeller choice. For in-flight adjustable, we are limited at this time to an electric control, such as MT or IVO. Cost is pushing our options in this area towards the IVO. I have heard of some vibration/resonance probs with certified engines (i believe it was a lycoming, but dont know specifics).. And one emailer has mentioned when they used the engine on a mazda powered a/c they were limited to 170 mph with the IVO but got 213 mph with a cruise wood prop. I am looking for any other experiences.. good bad or otherwise regarding the IVO inflight adjustable props (particularly in the 200 hp range). Experiences with any other electrically controlled props that can handle 200-220 hp would be welcome too.. but the MT is probably outside my price range.. Dave |
#2
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![]() "Dave S" wrote in message ink.net... I am involved with the building of a velocity, and questions are flying around about propeller choice. For in-flight adjustable, we are limited at this time to an electric control, such as MT or IVO. Cost is pushing our options in this area towards the IVO. I have heard of some vibration/resonance probs with certified engines (i believe it was a lycoming, but dont know specifics).. And one emailer has mentioned when they used the engine on a mazda powered a/c they were limited to 170 mph with the IVO but got 213 mph with a cruise wood prop. I am looking for any other experiences.. good bad or otherwise regarding the IVO inflight adjustable props (particularly in the 200 hp range). Experiences with any other electrically controlled props that can handle 200-220 hp would be welcome too.. but the MT is probably outside my price range.. Dave Dave, Robert and Valerie Harris of "The EZ Hangar" tested some props for IVO on Long-EZ's. They found that the IVO's could handle the O-320s ok but they could not hold up to the beating a prop takes from a O-360 (180 or 200hp). If you are running a six cylinder such as the Contenintal O-360 or the Franklin, things might be different. Suggest you call Robert. I am sure he would be glad to talk with you about their experiment. 901-475-3686 Rick Pellicciotti |
#3
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And one emailer has mentioned when they used the engine on a mazda
powered a/c they were limited to 170 mph with the IVO but got 213 mph with a cruise wood prop. One of the parameters of a propeller is the "helix angle." To give a muddled explanation, think of the propeller as "screwing" its way through the air. At really high forward speeds, the propeller needs a lot of twist to maintain a constant angle of attack along the entire blade. At lower forward speeds, it needs much less twist. If you have a prop with a low speed helix angle and start trying to take it too fast, not all parts of the prop will be pulling their weight equally. When you're checking your potential props, ask about helix angle. The 170 vs 213 MPH sounds like that could be a big part of it. For example, on light twins, apparently the prop blades have helix angles set for about 100 - 120 MPH. This is so they will have some single engine climb performance. A single, on the other hand, might have the helix angle selected for cruise. Ed Wischmeyer |
#4
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"Dave S" wrote in message
ink.net... .. . . I am looking for any other experiences.. good bad or otherwise regarding the IVO inflight adjustable props (particularly in the 200 hp range). Experiences with any other electrically controlled props that can handle 200-220 hp would be welcome too.. but the MT is probably outside my price range.. The EAA has a lot of knowledge in this field. I suggest you contact Aviation Information Services, 920-426-4821, for information. Mostly, all you'll get here is anecdotal data and/or uninformed opinion. Or mebbe a hard time. ;o) Rich S. |
#5
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In article . net, Dave S
writes: I am involved with the building of a velocity, and questions are flying around about propeller choice. For in-flight adjustable, we are limited at this time to an electric control, such as MT or IVO. Cost is pushing our options in this area towards the IVO. I have heard of some vibration/resonance probs with certified engines (i believe it was a lycoming, but dont know specifics).. And one emailer has mentioned when they used the engine on a mazda powered a/c they were limited to 170 mph with the IVO but got 213 mph with a cruise wood prop. I am looking for any other experiences.. good bad or otherwise regarding the IVO inflight adjustable props (particularly in the 200 hp range). Experiences with any other electrically controlled props that can handle 200-220 hp would be welcome too.. but the MT is probably outside my price range.. Dave Please, please, please do a substantial amount of research on all the problems associated with the IVO Prop before making a decision. I don't have first hand experience but from what I have read and heard from some very knowledgable sources in the industry it is a prop to be avoided, especially for the 200 - 220 hp engines. I am sorry but I have not kept any of the various reports and data on the prop because I eliminated it from my list a long tim ago. One thing to look at though is that micky-mouse foil tape inspection required for that prop. Bob Reed www.kisbuild.r-a-reed-assoc.com (KIS Builders Site) KIS Cruiser in progress...Slow but steady progress.... "Ladies and Gentlemen, take my advice, pull down your pants and Slide on the Ice!" (M.A.S.H. Sidney Freedman) |
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I'll second the factual notion.
I have personally talked with 4 Ivo-prop flyers. The gentleman with the Long-EZ did have problems with the blades loosening (even with the knurled plates.) I don't remember the engine size but it was a Lycoming 4 cyl. As is mentioned the wing "wake" is a serious concern with any prop that is rear mounted. The other gentleman had no issues with a Ivo on a RV-4 with a Lyc. He was pleased with its performance and did not have any issues with the stainless tape moving. I also talked with a gentleman at Copperstate this year with a Ivo on a Lancair 4P with a 3 rotor Mazda auto-conversion. No problems, but hey a 9 cylinder (equivalent) equivalent engine is gonna be smooth. 300+ dyno horsepower. and the gentleman that owns SDS Electronic Fuel Injection Systems is flying behind a Ivo as well..... I spent a great deal of time finding out the facts behind the IVO and I bought one. Did ya know Warp drive was designed and owned by Ivo as well? I have NEVER found ANYONE that has actually had a Ivoprop fail on them. just my 2 cents. Bart -- Bart D. Hull Tempe, Arizona Check http://www.inficad.com/~bdhull/engine.html for my Subaru Engine Conversion Check http://www.inficad.com/~bdhull/fuselage.html for Tango II I'm building. Paul Lee wrote: Indeed, With all due respect.... "I don't have first hand experience..." Please, Please do "correct" research on the IVO before you make conclusions on rumours. For example N570 has over 570+ hours on a 220hp Franklin with IVO without problems and N6Q has 160+ hrs. Obviously there are successfull high HP IVO uses. Again, its not the horsepower, but the smoothness of the engine. See my other post above. Please try normal objective language instead of using emotional, prejudicial terms like "mickey mouse ... inspection" or "do .... research on ALL THE PROBLEMS .... IVO Prop" - rather than of "do research on problems AND successes of IVO". IVO is quite open and honest to tell you that they will not sell their props for certain engines. osite (RobertR237) wrote in message ... Please, please, please do a substantial amount of research on all the problems associated with the IVO Prop before making a decision. I don't have first hand experience but from what I have read and heard from some very knowledgable sources in the industry it is a prop to be avoided, especially for the 200 - 220 hp engines. I am sorry but I have not kept any of the various reports and data on the prop because I eliminated it from my list a long tim ago. One thing to look at though is that micky-mouse foil tape inspection required for that prop. Bob Reed www.kisbuild.r-a-reed-assoc.com (KIS Builders Site) KIS Cruiser in progress...Slow but steady progress.... "Ladies and Gentlemen, take my advice, pull down your pants and Slide on the Ice!" (M.A.S.H. Sidney Freedman) |
#8
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"Bart D. Hull" wrote
Did ya know Warp drive was designed and owned by Ivo as well? I have NEVER found ANYONE that has actually had a Ivoprop fail on them. just my 2 cents. Bart Bart, I was looking at a Dragonfly that shed it's Ivo prop; I was told to investigate it carefully because last they saw it... "we were waiting for them to arrive we saw a streak on final and as they landed the three blades of the Ivo prop went sailing somewhere." I also heard that there was no good way to assemble and align the prop before mounting it on the engine but rather it had to be built right on the hub with no really good way to align it in all dimensions. You mentioned that stainless steel inspection tape. Seems copper tape was used initially but broke too often. Was switching to steel fixing the symptom or the problem? Comment(s)? Eric I looked on the net for supporting info and found the following (which, granted, is a few years old): ------------------------------------------------------ From: Dennis Jackson Subject: Adjustable Props.. Date: 1997/09/08 Message-ID: References: Reply-To: To: "prof S. A. Campbell" Organization: TMS Newsgroups: rec.aviation.homebuilt prof S. A. Campbell wrote: In article , Dennis Jackson wrote: Can anyone suggest a reasonably low cost in-flight adjustable pitch prop 2or3 blade in the 250-340 h.p. range? Thanks, Mike I say the IVO Magnum prop will kill someone soon if it hasn't already. It is very dependent on careful assembly and constant monitoring to make sure it's not coming apart. It might be OK for ultralight engines but forget it for high horsepower apps. DJ OK DJ, what is your basis for making this claim? Have you owned a Magnum? Do you personally know someone who has had problems with them? If so, with what engine? A number of people have tried putting them on O-360 and IO-360's with decidedly mixed results, but if you stay aware from these engines, I have heard nothing but good things about the Magnum. Are you just ranting, or do you have real information? Steve Steve: I guess I might as well drop the whole enchilada and get it over with. Wait just a minute while I put on my asbestos underwear. I am not a mechanical engineer, so my opinions should only be given the weight they deserve, but I do speak from experience and know two people personally who have had similar experiences with the Magnum prop, both RV builders using 160 hp Lycs. This discussion is also taking place on the RV-List so you can get more opinions there (http://www.matronics.com). At least I am not alone in my opinions. I am glad to say that I have not heard of any fatalities due to this prop and I have seen a couple of them flying so maybe Ivo has solved the problems but I still remain skeptical. Anyway, after my experiences I became concerned about others use of this prop and wrote a warning letter to other RV builders. Here is the letter I sent at that time to Ken Scott at Van's Aircraft who published an edited version in the RVator. 11/22/95 Ken: Here's a little writeup on my adventures with the Ivoprop Magnum propellor. If you could use it in the Rvator then feel free. I think something should be published as a warning. This prop is not safe. I installed an Ivoprop Magnum model MR-68-2 on my RV-4 with a Lycoming IO320-B1X 160 hp engine (the X means that I changed the sump to fit the RV-4). This prop is a 2 blade 68 inch dia ground-adjustable carbon fiber unit that has steel torsion rods that run lengthwise in the blades that can be twisted with a cam to adjust pitch. Each blade is a separate piece held on by two hub bolts and separated by spacers which are held under the two remaining bolts. The prop can also be set up as a three-blade in which case no spacers are used. I had heard that some people have experienced structural failures with this prop (of course not until I bought one) so naturally I was concerned but figured I could put a few hours on the prop without worry. Wrong. Before I started the engine, I received a factory directive to install tell-tale copper tape strips across the prop root junctions. This tape will break if there is any movement of the blades. I ran the prop on the ground for approx 10 minutes and then flew two times about 15 minutes each. At no time did the engine speed exceed 2400 RPM, therefore power to the prop was limited to no more than 135 HP. Upon ground runup I found that the tape had broken on all joints. I then checked the bolt torque and retaped the joints. The engine was again run up and 3 of the 4 joints failed again. After retorqueing and taping the airplane was flown (first flight by Mike Seager) for about 15 minutes, landed, and found all four joints broken. Retorqued, retaped, flew again (me this time) for about the same amount of time with the same results. I then removed the prop and I found that the prop blades showed friction burning on the surfaces around the bolt lugs with a residue of black (carbon?) dust around the area. The hub and front spinner plate showed similar rubbing and residue where in contact with the prop blades. While I like the basic idea of a ground or in-flight adjustable propellor, I think this design is flawed in that there is too much leverage at the base of the propellor for the clamping forces of the two bolts to hold. Taking measurements on the hub, bolts, and prop bolt barrels, I found that the bolts measured 0.496 o.d. and the hub and prop barrels were 0.500 i.d., thus leaving about .004 inches slop in the fit. This allows enough movement to overcome the clamping friction. If this were a zero tolerance fit, it might work. I would be more comfortable with extended bolts barrels that were a zero tolerance fit into the hub holes. The only thing preventing rotation of the propeller blades with engine power pulses is the friction between the blade and hub on one side and blade and spinner plate on the other. Perhaps this arrangement is reliable with shorter blades and smaller engines such as 2-stroke engines on ultralights, but it is insufficient on larger engines with heavier power pulses and the larger and longer blades necessary with higher power. There is simply too much inertia in the blade and too much leverage on the small base at the hub. The blades will work back and forth with each power stroke. Another area of concern is the minimal edge distance of the bolt barrels to the prop base. There does not appear to be any reinforcing around the barrels. How are the barrels anchored into the prop? Are the barrels connected together? If not, then what will prevent the barrels from working loose in the prop and fracturing the base with a resultant loss of a blade? I talked with another RV-4 driver in Kentucky and he experienced the same chafing due to movement of the blades against the hub and in addition found that one bolt barrel was starting to loosen in the hub and the hub had fractured across the base parallel to the barrel. He had put less than 3 hours on the propeller. Another negative is the necessity of leaving the spinner off to facilitate inspection. For aesthetic and aerodynamic reasons this is not an option for me. I called Ivoprop and spoke to Ivo about the situation. He stated that the copper tape was giving false readings and they are now recommending stainless steel tape which will not break so easily!? He said that it was normal for the blades to have some movement at first while seating and then they should stabilize. He said that they have other ideas to make the prop safe but I told him that I was just too much of a chicken to test his theories and was not comfortable flying with his prop. To Ivo's credit, he did not hesitate to offer a refund when I expressed my desire to return the prop even though it was long past the 30 day money-back guarantee period. To sum up, it is my opinion that this design is UNSAFE. Anyone with the Ivoprop Magnum propeller should immediately ground their aircraft and remove the propeller. It is not a matter of IF it will fail, the question is just WHEN will it fail. It is very likely that a fatality will result if a blade suffers a catastrophic failure in flight, as the resulting vibration can and probably will tear the engine from the aircraft. Do not fly with this prop even one more hour! Your pal, Dennis |
#9
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Bart,
One factor that may influence IVO prop success is properly remounting it after removal. The info I got from Johnny at northwest-aero.com - a news post - is that the knurled plates are really needed and that when the prop is removed it should marked and later remounted in exactly same position/orientation it was before. Otherwise the "knurls" do not seat together the same way and they wear off and the prop goes loose and you will likely have problems. "Bart D. Hull" wrote in message ... I'll second the factual notion. .... |
#10
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In article ,
(Paul Lee) writes: Indeed, With all due respect.... "I don't have first hand experience..." Please, Please do "correct" research on the IVO before you make conclusions on rumours. For example N570 has over 570+ hours on a 220hp Franklin with IVO without problems and N6Q has 160+ hrs. Obviously there are successfull high HP IVO uses. Again, its not the horsepower, but the smoothness of the engine. See my other post above. Please try normal objective language instead of using emotional, prejudicial terms like "mickey mouse ... inspection" or "do .... research on ALL THE PROBLEMS .... IVO Prop" - rather than of "do research on problems AND successes of IVO". IVO is quite open and honest to tell you that they will not sell their props for certain engines. Sorry if I offended you but I wouldn't touch that prop with a ten foot pole. I did clearly state that I did not have first hand experience with the prop and simply urged the requestor to do a very complete job of research on the prop before buying one. I will not argue that there are some "successful" installations of the IVO prop, there are and that is an indisputable fact. There have also been many reported problems with the IVO prop which must be totally understood before buying one. The poster did not specifically state which engine he was using only the report HP range. That range is most frequently associated with the Lycoming O-360 and IO-360 engines which according to YOUR OWN post have serious problems with the IVO Prop. Now where the HELL to you get emotional and prejudicial from that. And Yes, I still maintain the foil tape inspection process on the IVO prop is a micky mouse deal. Bob Reed www.kisbuild.r-a-reed-assoc.com (KIS Builders Site) KIS Cruiser in progress...Slow but steady progress.... "Ladies and Gentlemen, take my advice, pull down your pants and Slide on the Ice!" (M.A.S.H. Sidney Freedman) |
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