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A Simple Auto Engine Conversion
"Jim Logajan" wrote in message
.. . Ron Wanttaja wrote: On Tue, 26 Aug 2008 21:07:46 -0700 (PDT), " wrote: everyone says "ooh -- auto...dangerous" but no one can explain exactly why. 1. Ignition systems with insufficient redundancy. 2. PSRU failures. 3. Difficulty in implementing efficient liquid cooling systems. But doesn't the Rotax 912 have reduction gearing and liquid cooling? It is getting put into an awful lot of aircraft models - particularly LSAs. That's true, and the biggest annoyance (of which I am aware) is that they have increased the recommended "idle" speed to increase the service life of the PSRU--which is of the spur gear type. I don't know whether any of the belt or chain type PSRU installations have a similar requirement. As to cooling: there were a lot of liquid cooled aircraft engines in WWII, but the the aircraft they in which they were installed looked a lot different from their air cooled counterparts. Peter |
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A Simple Auto Engine Conversion
On Wed, 27 Aug 2008 16:11:51 -0500, Jim Logajan wrote:
Ron Wanttaja wrote: On Tue, 26 Aug 2008 21:07:46 -0700 (PDT), " wrote: everyone says "ooh -- auto...dangerous" but no one can explain exactly why. 1. Ignition systems with insufficient redundancy. 2. PSRU failures. 3. Difficulty in implementing efficient liquid cooling systems. But doesn't the Rotax 912 have reduction gearing and liquid cooling? It is getting put into an awful lot of aircraft models - particularly LSAs. Certainly, and my data shows that the Rotax 912, in homebuilts at least, has a safety record pretty much equal to that of traditional certified engines. My posting was an attempt to answer the OP's question on why some people believe auto engine conversions are dangerous. The three items I mentioned are in the top four causes of auto-engine failures. Looking at my 1998-2006 homebuilt accident database and comparing fixed-wing applications, the rate of occurrence of ignition system problems is four times higher for auto conversions than traditional engines. And the traditional engines had no cases of PSRU or cooling failure. I believe it's possible to convert an auto engine and achieve reliabilities equal to that of a traditional certified engine. It's just that the accident reports show that many people can't achieve that goal. It's basically the same people installing the Continentals as the Subarus, or the Rotax 912s and the Fords. But the average builder seems to have less problems getting the Lyconts and Rotaxen to be reliable. Ron Wanttaja |
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A Simple Auto Engine Conversion
On Aug 26, 11:14*pm, Ron Wanttaja wrote:
On Tue, 26 Aug 2008 21:07:46 -0700 (PDT), " wrote: everyone says "ooh -- auto...dangerous" but no one can explain exactly why. 1. Ignition systems with insufficient redundancy. 2. PSRU failures. 3. Difficulty in implementing efficient liquid cooling systems. Ron Wanttaja i heard the e racer had an inflight engine fire and eventually the designer through in the towl on auto engines. anyone remember why? |
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A Simple Auto Engine Conversion
On Aug 27, 7:01*pm, "
wrote: On Aug 26, 11:14*pm, Ron Wanttaja wrote: On Tue, 26 Aug 2008 21:07:46 -0700 (PDT), " wrote: everyone says "ooh -- auto...dangerous" but no one can explain exactly why. 1. Ignition systems with insufficient redundancy. 2. PSRU failures. 3. Difficulty in implementing efficient liquid cooling systems. Ron Wanttaja i heard the e racer had an inflight engine fire and eventually the designer through in the towl on auto engines. *anyone remember why? Sure do. "From: Dorothy Dickey Sent: Monday, January 24, 2000 8:46 PM To: Young, Ryan Subject: Engines for E-racers There is nothing wrong with the Buick engine it's just that I no longer favor auto engines for aircraft applications. This is because it is not possible to achieve equivalent reliability and performance of an aircraft engine for the same or less money... So why do it? Shirl" Remember, this is a guy who designed an airplane around an auto conversion, and devoted serious time, money, and twice, almost his life to making this idea work. If you think you can do better, step right up. This whole thread smacks of TROLL, but you can read what more of what I think, along with the E-Racer guy (Shirl Dickey), and a little from the Belted Air Power reduction guy (Jess Myers) he http://users.lmi.net/~ryoung/Sonerai/BOP.htm You can also search this newsgroup for anything by Corky Scott, and watch his chronicle. He never flew his auto engine conversion, after working on it for years. |
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A Simple Auto Engine Conversion
wrote in message ... I was thumbing through a catalog from Speedway Motors. They advertise a magneto-type distributor. Assuming you didn't come across a thrashed race engine with magnetos, couldn't someone put together an engine worthy of aircraft use, by simply 1) ordering an aftermarket engine with fuel injection, such as the chevy "RamJet" crate engine, 2) adding a dry sump lubrication system to it (not too strange addition to high perf cars nowadays), and 3)-adding the magneto from Speedway. Use direct drive to keep the RPM low and reliability high. I doubt that today's hi perf crate engines lack the torque to turn a prop at 1:1. If this is unsafe, specifically why? I know someone could fly within 100 miles of a t-storm and have the static electricity play with the ignition system, but stop a magneto? If you were struck with lightning, your auto-engine might stop, but then your resin might burn and melt, leaving you with some loose fiberglass to negotiate a crash. Point I'm making is, experimental planes near t-storms have bigger probs to worry about, don't they? BTW, that magneto appears to be offered just for big and small block chevy's. Aside from that, the models they carry are "nostalgia engines"...1950 hemis, flat head fords and the like. Another caveat: they cost $1100...but even with that and a $1200 dry sump system, we are still way under the cost of an O-540. OEM automotive engines are not usually designed to develop enough horsepower at direct drive RPMs, to justify their finished weight, after including the complete radiator, pump and coolant. Especially when compared to their traditional aircraft counterparts. Selection of an all aluminum small block, with all the lightweight and high strength aftermarket parts can easily begin approaching the cost of a good used aircraft engine, and still leave a lot of engineering to cost money or build time, increase complexity and question reliability. There is also still a question of resale value of the finished aircraft. Lots of factors besides magnetos and dry sump systems. Why do you feel a dry sump is necessary? |
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A Simple Auto Engine Conversion
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A Simple Auto Engine Conversion
a dry sump isn't absolutely necessary...neither is fuel
injection....neither is a magneto. just a good way to hedge your bets. say your're in the mountains, it's stormy, and you have turbulence. no matter what Gs or static you are subjected to, the engine would get a steady supply of oil, fuel and electricity. i know resale value is diminished and the public perception is not good. i'm just trying to understand the specific technical reasons why. all i hear is that 1-auto engines MUST have psru and 2-therefore turn high/spooky rpm continuously. then i fail to hear of any case where a conversion project stumbles for lack of a psru. everyone who dares to run direct is glad, and most of us agree there is nothing scary about driving all day, every day, at 2900 rpm with a car engine. you won't get 100% hp, but a camshaft and dual plane intake change could help with that. the rotaries need a lot of rpm to make decent power. so much that the propeller is spinning too fast. i'm aware of this, but the plug and ply magnetos i'm referring to are not avail for rotaries. maybe aircraft engines have dual spark plugs...each cylinder fed by two independent magnetos..is that the case? is that the safety measure lacking in auto conversions? aside from the "psru myth", the dual plugs are all i can think of. On Aug 25, 9:13*pm, "Ramsey" @##@.^net wrote: wrote in message ... I was thumbing through a catalog from Speedway Motors. *They advertise a magneto-type distributor. *Assuming you didn't come across a thrashed race engine with magnetos, couldn't someone put together an engine worthy of aircraft use, by simply 1) ordering an aftermarket engine with fuel injection, such as the chevy "RamJet" crate engine, 2) adding a dry sump lubrication system to it (not too strange addition to high perf cars nowadays), and 3)-adding the magneto from Speedway. *Use direct drive to keep the RPM low and reliability high. I doubt that today's hi perf crate engines lack the torque to turn a prop at 1:1. If this is unsafe, specifically why? I know someone could fly within 100 miles of a t-storm and have the static electricity play with the ignition system, but stop a magneto? If you were struck with lightning, your auto-engine might stop, but then your resin might burn and melt, leaving you with some loose fiberglass to negotiate a crash. *Point I'm making is, experimental planes near t-storms have bigger probs to worry about, don't they? BTW, that magneto appears to be offered just for big and small block chevy's. *Aside from that, the models they carry are "nostalgia engines"...1950 hemis, flat head fords and the like. *Another caveat: they cost $1100...but even with that and a $1200 dry sump system, we are still way under the cost of an O-540. OEM automotive engines are not usually designed to develop enough horsepower at direct drive RPMs, to justify their finished weight, after including the complete radiator, pump and coolant. Especially when compared to their traditional aircraft counterparts. Selection of an all aluminum small block, with all the lightweight and high strength aftermarket parts can easily begin approaching the cost of a good used aircraft engine, and still leave a lot of engineering to cost money or build time, increase complexity and question reliability. There is also still a question of resale value of the finished aircraft. Lots of factors besides magnetos and dry sump systems. Why do you feel a dry sump is necessary?- Hide quoted text - - Show quoted text - |
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A Simple Auto Engine Conversion
wrote OP: a dry sump isn't absolutely necessary...neither is fuel injection....neither is a magneto. just a good way to hedge your bets. say your're in the mountains, it's stormy, and you have turbulence. no matter what Gs or static you are subjected to, the engine would get a steady supply of oil, fuel and electricity. Morg: I think you are hung up on the features of that overpriced aircraft engine. It is hard to believe that the dry sump will do any better than a good old oil pan, unless you plan on some inverted flight, and if you worried about some turbulence, an oil accumulator would keep oil flow temporarily. Anyway, most aircraft engines do not have dry sumps. Morg: Unless you use a header tank, fuel injection will not guarantee keeping fuel going to run the engine. I do like fuel injection, and there is no reason to not have it, and lots of other reasons to have it, but again, not absolutely necessary unless you are going for an inverted package. Morg: Magnetos over electronic ignition? What breaks down more often, a magneto, or electronic ignition? What is better at making an easy starting engine, running with the spark at the appropriate timing? Magnetos are old hat, so if you want reliable, go with dual pickup, dual coil(s) redundant electronic ignition with a battery supplied emergency backup power source for the ignitions. The not having a dual plug is the only slight trade off, because you can use a two into one spark system to tie the dual ignition to the one plug. OP: i know resale value is diminished and the public perception is not good. i'm just trying to understand the specific technical reasons why. all i hear is that 1-auto engines MUST have psru and 2-therefore turn high/spooky rpm continuously. then i fail to hear of any case where a conversion project stumbles for lack of a psru. Morg: PSRUs have another value over direct drive, in that the prop gyroscopic loads and thrust loads are removed from the crankshaft. They can be MAJOR problems, up to and including broken crankshafts. An example are the Corvair cranks broken (in part) from prop adapters that are too long, with heavy props. With a V-8, you are going to have a heavy prop, and a short adapter will make an unstreamlined cowl. The PSRU also raises the thrust line to get better prop to ground clearance. So yes, those are some reasons a conversion stumbles without a PSRU. Morg: Bottom line, it would be very wise to use some type of extra external bearing to help with soaking up the thrust loads and gyroscopic loads. A PSRU does that for you. The PSRU also gets some more HP so the HP to weight ratio is better. As far as spooky high continuous RPMs go, I think you have been listening to some of the critics of conversions too much. Morg: When have you heard of people being concerned at running a marine auto engine at too high constant RPMs? Never. They run at RPMs that would worry me much more, and faster than most people run airplane conversions. You can choose what drive ratio you want to run. A conversion running at 3,000 RPM is too fast for a prop, but not too fast to make me uncomfortable. I would not worry at running a conversion at 3,800 RPM for extended periods of time. I sure run my boat engine at higher RPMs than that. Morg: In short, I think your concerns about PSRUs are unfounded. You can run any speed you want to, and higher than a normal prop speed. You get the other advantages I identified, and get more HP from your heavy engine. You don't have to run at peak HP, but it sure would not hurt to run faster than prop speed. OP: everyone who dares to run direct is glad, and most of us agree there is nothing scary about driving all day, every day, at 2900 rpm with a car engine. you won't get 100% hp, but a camshaft and dual plane intake change could help with that. OP: the rotaries need a lot of rpm to make decent power. so much that the propeller is spinning too fast. i'm aware of this, but the plug and ply magnetos i'm referring to are not avail for rotaries. OP: maybe aircraft engines have dual spark plugs...each cylinder fed by two independent magnetos..is that the case? is that the safety measure lacking in auto conversions? aside from the "psru myth", the dual plugs are all i can think of. I hope I gave you a little to think about. There are companies out there with well engineered, time tested, reliable PSRUs. To me, it is not the myth that would keep me running direct drive, but the desire to get a better powered package, with the isolation of prop loads on a crankshaft that IS NOT DESIGNED to take prop loads. -- Jim in NC |
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A Simple Auto Engine Conversion
On Aug 26, 11:43 pm, "Morgans" wrote:
wrote OP: a dry sump isn't absolutely necessary...neither is fuel injection....neither is a magneto. just a good way to hedge your bets. say your're in the mountains, it's stormy, and you have turbulence. no matter what Gs or static you are subjected to, the engine would get a steady supply of oil, fuel and electricity. You'd better think twice about being in the mountains in stormy weather and turbulence. You'll have other problems besides oil supply. In any case, wet-sump aircraft engines fly in the mountains and turbulence all the time and have no oil issues. It's the weather that kills the flier. Morg: Magnetos over electronic ignition? What breaks down more often, a magneto, or electronic ignition? What is better at making an easy starting engine, running with the spark at the appropriate timing? Magnetos are old hat, so if you want reliable, go with dual pickup, dual coil(s) redundant electronic ignition with a battery supplied emergency backup power source for the ignitions. The not having a dual plug is the only slight trade off, because you can use a two into one spark system to tie the dual ignition to the one plug. The use of 100LL fouls plugs rather often. Two plugs are handy for that, and the extra plug improves power output. OP: i know resale value is diminished and the public perception is not good. i'm just trying to understand the specific technical reasons why. all i hear is that 1-auto engines MUST have psru and 2-therefore turn high/spooky rpm continuously. then i fail to hear of any case where a conversion project stumbles for lack of a psru. Morg: Bottom line, it would be very wise to use some type of extra external bearing to help with soaking up the thrust loads and gyroscopic loads. A PSRU does that for you. The PSRU also gets some more HP so the HP to weight ratio is better. As far as spooky high continuous RPMs go, I think you have been listening to some of the critics of conversions too much. Very good point. Auto cranks were designed for torsion loads only, not thrust or gyroscopic loads, and they tend to break when subjected to such loads. Morg: When have you heard of people being concerned at running a marine auto engine at too high constant RPMs? Never. They run at RPMs that would worry me much more, and faster than most people run airplane conversions. You can choose what drive ratio you want to run. A conversion running at 3,000 RPM is too fast for a prop, but not too fast to make me uncomfortable. I would not worry at running a conversion at 3,800 RPM for extended periods of time. I sure run my boat engine at higher RPMs than that. Marine engines have a couple of advantages that aircraft conversions do not: A ready supply of cold coolant, and a drive system that doesn't apply and thrust or gyroscopic loads on the crank. Running an auto engine at or near max power settings, like we do in boats or airplanes, generates huge amounts of waste heat that autos don't when they're cruising unless they're pulling heavy trailers, in which case a trailer-towing package becomes necessary. This includes much larger cooling capacity. Autos typically cruise at around 25-30% power, boats and airplanes at 65-80%. I have experience with both marine and aircraft liquid-cooled conversions, and believe me, the boat is easy to keep cool. Aircraft engines are built with big cooling capacity right from the start. And they're designed to produce large amounts of torque at lower RPM, which means the basic cylinder geometry is different. And they're designed to do all this without weighing as much as a bridge. OP: everyone who dares to run direct is glad, and most of us agree there is nothing scary about driving all day, every day, at 2900 rpm with a car engine. you won't get 100% hp, but a camshaft and dual plane intake change could help with that. You still won't get 100% unless you're at rated redline, which no prop will stand for. Most direct-drive conversions run a much shorter prop to allow a higher RPM (propeller tip speed and centrifugal forces are the concern) and shorter props lose efficiency big time, so performance, especially takeoff and climb, suffer considerably. One horsepower is 33,000 foot-pounds per minute. To get it we do this: Torque x RPM x 6.28 divided by 33,000. RPM is one of the factors, and a PSRU is usually needed to get the engine's RPM up to its designed redline so it'll generate the claimed HP. Anything less represents a loss, which means a heavy, underpowered airplane. OP: maybe aircraft engines have dual spark plugs...each cylinder fed by two independent magnetos..is that the case? is that the safety measure lacking in auto conversions? aside from the "psru myth", the dual plugs are all i can think of. Boy oh boy, are we at that level of expertise? You'd better do a LOT of research here before deciding that you have answers that the rest of us don't. I hope I gave you a little to think about. There are companies out there with well engineered, time tested, reliable PSRUs. To me, it is not the myth that would keep me running direct drive, but the desire to get a better powered package, with the isolation of prop loads on a crankshaft that IS NOT DESIGNED to take prop loads. Yup. Lots of folks have done the work already and found it much more difficult than they imagined when they started out. I wouldn't want to think that I could improve on any of it on a first try. Dan |
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A Simple Auto Engine Conversion
wrote "Morgans" wrote: wrote Ooops, you attributed the following to me, and it was the OP. just a good way to hedge your bets. say your're in the mountains, it's stormy, and you have turbulence. no matter what Gs or static you are subjected to, the engine would get a steady supply of oil, fuel and electricity. End OP quoted paragraph. Morg: When have you heard of people being concerned at running a marine auto engine at too high constant RPMs? Never. They run at RPMs that would worry me much more, and faster than most people run airplane conversions. You can choose what drive ratio you want to run. A conversion running at 3,000 RPM is too fast for a prop, but not too fast to make me uncomfortable. I would not worry at running a conversion at 3,800 RPM for extended periods of time. I sure run my boat engine at higher RPMs than that. Marine engines have a couple of advantages that aircraft conversions do not: A ready supply of cold coolant, and a drive system that doesn't apply and thrust or gyroscopic loads on the crank. Yes, but a well designed and performing cooling system cools all the extra heat an engine can produce. Don't you thinik the P-51 did ok with their cooling system? There are homebuilt auto engines flying all over the place, for over 2,000 hours that do not have a problem dealing with waste heat. The ONLY time they have a problem is if they have to run sitting on the ground, or too long of a taxi. Flying, they cool just fine, after they have all of the bugs out of the cooling system. I will not say that some people have problems, but there are hundreds of people flying car engines that have absolutely NO problems with cooling in the air. As far as the crank loads, that is taken care of with a PSRU. Another non issue. Running an auto engine at or near max power settings, like we do in boats or airplanes, generates huge amounts of waste heat that autos don't when they're cruising unless they're pulling heavy trailers, in which case a trailer-towing package becomes necessary. This includes much larger cooling capacity. Autos typically cruise at around 25-30% power, boats and airplanes at 65-80%. I have experience with both marine and aircraft liquid-cooled conversions, and believe me, the boat is easy to keep cool. And so are water cooled airplane engines, with good cooling systems, and it is not that hard of an issue to deal with. -- Jim in NC |
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