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#51
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Chevy LS2 and Trans??? any real issues besides weight
Hey stol, question, what is the expected life of the belt in the
redrive? The only real experience i have with belted systems is in the weighing systems we build for our industrial customers. I know belted systems cause and transmit way less vibration to our platforms but their life is far under the chains we used to use. Lucky customers would get maybe 1 or 2 years out of a belt where as the the chains never needed replacing. Miss treated systems would sometimes last 6mos. Still the accuracy in weighing would far offset the cost of replacing the drive belts so everyone is still happy. also what is the cost of a belted redrive ? and where do i get the high capacity belts when they need replacing ? the only website i've read regarding the belted systems seems to indicate belt manufacturers don't like this particular usage of their products thanx MrV |
#52
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Chevy LS2 and Trans??? any real issues besides weight
MrV wrote:
also what is the cost of a belted redrive ? and where do i get the high capacity belts when they need replacing ? the only website i've read regarding the belted systems seems to indicate belt manufacturers don't like this particular usage of their products http://www.beltedair.com |
#53
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Chevy LS2 and Trans??? any real issues besides weight
Can I (or anyone) buy just the redrive? Are prices on the web? I didn't see any list. //////////////////////////////////////////////////////////////////////////////////////////////////////////////// The redrive is a BeltedAir unit I modified to fit on a Ford Block. They are pretty damn stout units and all I needed to do was fabricate a new block plate. I used all the other parts from the Chevy unit. I am sure Jess@ BeltedAir has plenty in stock to fit Chevys. Ben |
#54
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Chevy LS2 and Trans??? any real issues besides weight
Hey stol, question, what is the expected life of the belt in the
redrive? The only real experience i have with belted systems is in the weighing systems we build for our industrial customers. I know belted systems cause and transmit way less vibration to our platforms but their life is far under the chains we used to use. Lucky customers would get maybe 1 or 2 years out of a belt where as the the chains never needed replacing. Miss treated systems would sometimes last 6mos. Still the accuracy in weighing would far offset the cost of replacing the drive belts so everyone is still happy. also what is the cost of a belted redrive ? and where do i get the high capacity belts when they need replacing ? the only website i've read regarding the belted systems seems to indicate belt manufacturers don't like this particular usage of their products thanx MrV //////////////////////////////////////////////////////// Your right, the manufacturers of those belts will ""NOT"" sell you one if you even mention the application is closely related to aviation. Ya just say is for a conveyor system or some other industrial setup. I think the belts are somewhere around 70 bucks. |
#55
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Chevy LS2 and Trans??? any real issues besides weight
well given sea level standard temp i'm looking at ~250hp at 3500 rpm
which from the graphs i've seen translates to about 360-375 lb-ft torque at that point. now the graphs are few and far between but i'm sure i can tweak it to atleast this level. It's that torque that will kill the transmission. No car, especially a 'Vette, needs 360 ft-lb of torque and 3500 RPM to cruise the highway, even at 90 MPH. Torque places a LOT of pressure on gear teeth so that the friction heats them up, and the relatively high RPM just multiplies the heating. And we haven't even discussed bearings yet. All that power in the car gets used to lay a strip of rubber a few feet long perhaps a few dozen times in the car's life. More than that, and the gearing starts to suffer. It's not used for cruising. Dan |
#56
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Chevy LS2 and Trans??? any real issues besides weight
Thielert uses a belt redrive on its *certified* conversion designed
for the 172. Belts are OK. But like gears, they need some sort of flywheel on the engine crankshaft to dampen the power pulses, or the reciprocating lash will destroy them. The prop wants to turn at a constant speed, while the crank lurches between compression and firing strokes, and if the belt or gears are expected to deal with all the difference they soon fail. Flywheels add weight, especially if they do a good job of damping, and the redrive adds weight and more failure points, which is why Continental and Lycoming and Franklin built mostly direct-drive engines with long strokes and large cylinders to get the torque required at lower RPM. Some radials were geared, as were the big V engines, but the cranks were so massive and the cylinders numerous enough that the engine ran smoothly enough without a flywheel. Even a direct-drive engine can have problems with the lurching effect of the crank. Some wood propellers, notably the Fairey-Reed types used on larger recips, had to be regularly checked for proper bolt torque and charring of the wood where it met the crank flanges. Torque pulses were strong enough to cause movement. I liked Geschwender's Hi-Vo chain drive in which lash was minimized by the chain's teeth expanding as they bent around the gears. Much stronger. That engine, I believe, was used in cropdusters like the Pawnee rather successfully. Dan |
#57
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Chevy LS2 and Trans??? any real issues besides weight
On 13 Nov 2005 14:27:10 -0800, "MrV" wrote:
well given sea level standard temp i'm looking at ~250hp at 3500 rpm which from the graphs i've seen translates to about 360-375 lb-ft torque at that point. now the graphs are few and far between but i'm sure i can tweak it to atleast this level. MrV, as others have indicated there are a lot of design issues that make using an auto engine a lot more of an engineering problem than you might think. First and foremost, you really need to rethink the idea of using an auto/truck transmission, even a Corvette tranny. It just doesn't make sense from an engineering standpoint. It's WAY too heavy for the job being required, and you are carrying around extra gears and shafts as dead weight. Not only is it dead weight, it's weight kinda behind the center of gravity. Plus, the gears you would need to use simply are not up to the task of transmitting even 50% power, given that you are talking about an engine capable of putting out 250+. Now that you are talking about adding bearings to support and isolate the propshaft, you are adding yet more weight, this time well behind the center of gravity. Are your wings going to have the ability to swing forward and aft in order to compensate for the different weights of the pilot/passengrs and luggage? There was a guy who tried really really hard to make a go of installing the Buick/Olds 215CID aluminum V8 in the back of a Long E-Z. Look for E-Racer on the internet. He kept blowing them up. Some of the blowups were because he did not research in the hot rod community about the engine. Had he done so he would have learned that you cannot bore the engine out to 300 CID and go racing. That doesn't leave enough material to support the cylinder sleeves. There were many other problems that caused catastrophic engine failure. His name is Shirl Dickey. He finally decided to install a Chevy V-6 and last I heard, he'd yanked it and was using a Lycoming. This is the setup you are talking about, except that you keep insisting you can use an auto transmission too. Driving a prop using a driveshaft has been done successfully before. See Curtiss P-39 Airacobra and P-61 King Cobra. But the driveshaft was MASSIVE, as was the engine (Allison V12). It's admirable to want to build a quiet airplane but it is definately not a trivial matter. Are you an aerodynamics engineer? If not, you should be doing some extremely heavy reading to see what such will take. Ben Haas has a very clean looking auto engine conversion using an auto engine. But he has a racing background and the engine is not a stock unit. He had built a number of engines that raced, prior to attempting to install something in his airplane. In addition, he did not design his airplane, he left that headache to Zenith. Others have mentioned that engineering an auto engine conversion is not a simple task. Designing and building an airplane is REALLY not a simple task. You are suggesting you want to do both. I wish you the best of luck. Corky Scott PS, seeking information from this group is not necessarily a good sign. As Groucho Marx put it, "I would not want to belong to any club that would have me." ;-) PPS, for those who think stock Detroit engines are not up to the task of putting out a continuous 65% power, is it time again for me to post the description of what one auto manufacturer does typically to test it's engines? If you've never read it, you will be agast at the punishment. |
#58
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Chevy LS2 and Trans??? any real issues besides weight
thanx charles it was just an idea to use the auto tranny.
just wondering if it would work so maybe just maybe i would have less engineering work even considering the weight. on a side note: does anyone have any hard numbers on the weight of an Ls2 configured to run? I just spent an hour at an off road shop that is selling me the engine and they say the shipping weight fully configured is less than 300lbs. this is an off road racing optimized ls2 i'm considering purchasing. 2 of us actually picked the thing up. i really don't believe this but these guys build atleast 10 cars per year. btw good info charles. hey can u post those test procedures i would really like to see it for myself |
#59
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Chevy LS2 and Trans??? any real issues besides weight
"Charles K. Scott" wrote PPS, for those who think stock Detroit engines are not up to the task of putting out a continuous 65% power, is it time again for me to post the description of what one auto manufacturer does typically to test it's engines? If you've never read it, you will be agast at the punishment. Yep, it's time, and this time, I'm going to save it, too. There is another thread going somewhere else, about auto engines. It might be over in RAPiloting. -- Jim in NC |
#60
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Chevy LS2 and Trans??? any real issues besides weight
On Mon, 14 Nov 2005 18:36:12 -0500, "Morgans"
wrote: Yep, it's time, and this time, I'm going to save it, too. There is another thread going somewhere else, about auto engines. It might be over in RAPiloting. -- Jim in NC Ok folks here it is in it's entirety, note, the comments in parenthesis are sometimes mine. I originally posted this some five or six years ago to this group: Max Freeman is the engineer in charge of GM's Premium Engine programs and has written an article for Mick Myal in the latest "Contact!" magazine regarding the development and testing of their new PV6 aluminum 90° bank angle V-6. It's a lot of technical stuff about why they chose this configuration or mechanical design over that, which is why I like it. He also wrote about the kind of developmental testing done on the engine to make sure that customers get an engine they can depend on, and I'd very much like to quote that section in full because it should lay to rest the question of whether auto engines can take the kind of power settings aircraft engines routinely manage. "PERFORMANCE The engine in production form for 1999 develops 215 HP at 5600 RPM and 230 foot pounds of torque at 4400 rpm. As a routine part of an engine development program we tested the engine at full power, maximum RPM. We ran it at 6000 RPM, pulling 215 HP at wide open throttle, for 265 hours. That's a continuous 265 hours of wide open throttle, far worse than autobahn driving, because even on the German Autobahn, you wouldn't be at 6000 RPM. THAT IS A STANDARD DURABILITY TEST. (emphasis mine) We run many engines through this test as a matter of course. Specific development focus is on the crank, pistons, rods, block structure, timing drive wear; we get a lot of full load cycles in a hurry. It isn't necessarily designed to replicate customer driving but to get development answers. Wear and fatigue are accelerated. The test is particularly applicable in proving out dampers and their effectiveness. If the damper is not properly tuned to the engine the crankshaft will inevitably break in that time period. (note, this is evidence you should not discard the stock damper when using the auto engine for aircraft power) A number of other engine tests are utilized. We use a variety of specific tests to accelerate engine wear and to look at fatigue failures. The cyclic endurance test is now called PTED (power train endurance). It closely approximates cyclic durability. The engine is cycled from its torque peak to its horsepower peak, at wide open throttle, then down to idle, then accelerates up to shift points, then back down to the torque peak and then horsepower peak. This test is run for 400 hours. Once again, it's a wide open throttle test for 400 hours. The RPM for this engine, ranged between 4400 and 6000 RPM, back and forth in about a 5 minute cycle. The dyno computer will occasionally bring the engine down to idle, up to 6500 RPM shift points, and then back to the 4400 - 6000 RPM 5 minute cycle. Thermal cycle tests are run to define engine capability under cold weather condition. We run the engine at full throttle at 4000 RPM, bring it down to idle, stop it, switch the coolant valves to drain the hot coolant, pump the chilled coolant from the chiller until the metal temperature stabilizes at 0 degrees F. Frost forms on the outside of the block, as the cold coolant rushes into the engine. When it stabilizes at 0 F, we motor the engine, start it, come to full throttle at 4400 RPM, the valves switch and the coolant temperature starts to climb. It climbs back up to 260 degrees F. It takes 10 -11 minutes to complete one cycle. The engine must pass 600 cycles without any sign of failure. We typically run 1200 cycles and a probe test will run 1600 cycles. That's a (sic) excellent gasket killer test. Head gaskets are the first to fail because of the rapid expansion and contraction. A powertrain endurance test simulates in-vehicle operation. The Ypsilanti plant uses it for testing transmission. We, of course, use it to look at engine performance. The equipment consists of an engine/transmission combination, which sits on a dyno with large steel inertia wheels. The inertia wheels are being driven by the transmission output shaft, just like in a car. They cycle is brutal; the engine is at idle in gear. The engine accelerates wide open to 6200 RPM, upshift occurs, 6200 RPM is reached, upshift occurs to 3rd, 6200 RPM is reached, upshift occurs to 4th, the wheels turn up to 135 MPH depending on the application. The second half of the cycle calls for a closed throttle down to 70 MPH, then wide open throttle with a downshift to 2nd, the engine goes back up to top speed, coasts down so that the transmission selects down to a lower range. The engine is in an overrun condition all the way down to idle; i.e., the engine is being used for braking. That's one cycle. One transmission life cycle is typically 12K - 13K cycles of the above test. We will run an engine through 4 or 5 transmissions. This is a very harsh schedule for the engine, particularly because of the overrun braking. Cylinders and rings suffer the most on this test. We run some idle tests to verify low speed operation. The engine is run at idle for about 2000 hours to make sure of adequate oil flow at idle. We use all those engine tests in addition to fleet tests and extensive vehicle road testing. The customer can be assured that the PV6 engine is a thoroughly tested advanced design that matches or exceeds competing offerings." Corky's comment: I don't believe engine testing for aircraft certification approaches this intensity, duration or severity. |
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