![]() |
If this is your first visit, be sure to check out the FAQ by clicking the link above. You may have to register before you can post: click the register link above to proceed. To start viewing messages, select the forum that you want to visit from the selection below. |
|
|
Thread Tools | Display Modes |
|
#1
|
|||
|
|||
![]()
Corky Scott wrote:
On Fri, 21 Nov 2003 17:41:37 -0600, Big John wrote: Corky Have you enough ammunition on auto engines to stop the nit picking in this group? Both Lyc and Con started life with auto engines G Big John Big John, to the best of my knowledge, I try not to nitpick. I try to present facts as I know them. I believe that there are various auto engines that can be successfully converted and I believe it strongly enough that I'm assembling a Ford V6 in my shop that will be the engine I fly behind. You weren't here when this subject was first aired many years ago, but there were many sceptics... actually that's not a strong enough word. There were some extremely vocal critics of the concept who felt that no auto engine would work in an airplane. One of them was an auto engineer, a guy who used to work for the Chaparal Racing Team with Jim Hall. He was absolutely positive that V configured auto engines would disintegrate (literally) under the stress. He also believed they could not cool because the coolant passages were too small and the cylinders too close together. He was wrong. In order to build a reliable auto conversion, you do have to do your homework. You have to safety wire just about everything that could come off including the oil pan bolts. You have to build using accepted aviation practices. There have been guys who screwed gas or oil lines into the block and then ran them to the firewall. They broke. You can't mount pipes solidly to the block and run them for any distance, prop vibration will eventually crack them. The guy who developed the Ford V6 discovered that the stud that holds the air filter can and will unscrew and drop into the engine, if you don't safety wire it. How did he discover this? Because it did. It was one of the many flights in which he coasted back to the runway. By now, many guys have successfully built and flown the Ford V6. One guy accumulated more than 2,000 hours without anything falling off or failing. Others are in the over a thousand hours hobbs time category. For some reason, success stories like this don't seem to matter to those who feel using an auto engine won't work. I do intend to test run the engine extensively. I'm fabricating an engine test stand along with the engine assembly process. While it's true this doesn't exactly duplicate the stresses encountered during flight, it's the best I can do, and better than just hanging it on the airframe and testing the engine during the very first flight. One thing at a time please. Corky Scott First, I apologize for the delayed posting in the middle of a thread. I can only say that it has been a strange week ... My personal view, not fully substantiated be research, is that most (and possibly all) of the current automotive engines can be successfully converted for aircraft use. However many of them have shortcomings that make them less attractive. I might not bother with an engine that I expect to have significant vibration modes other than torsion. For example; I doubt that I would convert any of the three cylinder engines, even if it had balance shafts, as an inline four could be a much smoother installation. My hypothesis is that the pitch oscillation of the three cylinder, and possibly some of the 90 degree vee six, engines would add stresses to the propeller and PSRU. OTOH, there are a lot of 90 degree vee six engines flying... Probably the best question is not whether an automotive engine can be made reliable; but whether a purpose-built engine is available and competitively priced for the application. For example, Jabiru offers ram air cooled engines of 80 and 120 horsepower; provided that the aircraft is fast enough to use a 60 inch diameter prop. Rotax offers engines with a hybrid cooling scheme... As I recall, Blanton's conversion was originally for glider towing. According to the story I was told, the reduction drive allowed the Ford vee six to produce thrust similar to a much more powerful direct drive aircraft engine--at towing speeds. Unfortunately, the story later circulated that the engine produced mathematically ridiculous amounts of horsepower... So, I may eventually build with an automotive conversion. Or may not. The choice is not "open and shut". Regards, Peter |
#2
|
|||
|
|||
![]()
On Wed, 03 Dec 2003 15:50:52 GMT, Peter Dohm
wrote: As I recall, Blanton's conversion was originally for glider towing. According to the story I was told, the reduction drive allowed the Ford vee six to produce thrust similar to a much more powerful direct drive aircraft engine--at towing speeds. Unfortunately, the story later circulated that the engine produced mathematically ridiculous amounts of horsepower... So, I may eventually build with an automotive conversion. Or may not. The choice is not "open and shut". Regards, Peter Not exactly Peter. Blanton's conversion was for anyone who wanted to use it, fast airplanes or slow. Turns out, one guy who did want to use it belonged to an Aussie glider towing club. His original intent was to see if he could certify the engine in Australia for that purpose. He got the engine and PSRU from Blanton at a time when Blanton was declining in health and mind. The PSRU had a lot of problems and the glider group spent a LOT of time refining the carburation and induction. Eventually they got it right, both with the PSRU and the induction and it's been towing gliders ever since. That was some seven or eight years ago. The engine and PSRU are still going strong and have not been overhauled or required overhaul since they finished their development. They tow gliders in their Pawnee with this engine, which in it's former life, used a Continental O-470. The Ford 3.8 swings the same prop the 0-470 did, at the same prop rpm. The Ford burns SUBSTANTIALLY less fuel than the 0-470 did doing the same operation. There's a very specific reason for this: The typical glider operation involves a takeoff with glider in tow, a climb to 5,000 or so feet, release and return to the airport for another tow immediately. That's all it does, no cross country where the engine would be leaned out for best fuel burn. Under these identical operations, the Ford uses less fuel because once the glider is cast off, the pilot simply closes the throttle to idle and returns to the field with the engine at idle the entire time. When they were using the 0-470, the engine came back under power and also used full rich during the climb to release, which engaged the power valve and used a lot of fuel. As to the mathematically ridiculous amounts of horsepower being reported, there was only one person claiming that, David Blanton, the original developer. He was mistaken. Unfortunately, he had the type of personality that did not allow him to accept criticism or corrections (hmm, sounds like he'd fit right in here :-)). His method of calculating horsepower had him claiming nearly 300 horsepower at sea level for a 232 cid V-6 at 4800 rpm. Without supercharging, that's just not possible. Others have checked their rated power with a dyno and have produced a far more believable 180 to 235. The guy who managed 235 got it by turning the engine at 5300 rpm. That's more than I dare go. Almost all the builders use 4800 as the redline. Blanton also originally specified a 500 cfm two barrel carburator. If you do the math using the standard carb sizing formula from Holley (Engine Size (CID) X Maximum RPM / 3456=CFM) you get 322.222 cubic feet per minute (232x4800/3456). Sure, the 500 CFM carburator will work, after all it did for years, but it's overkill and wastes gas. Those who dared to buck Blanton (because they knew carburation, could apply the formula and realised they were over-carbing) discovered that using a 350 CFM carburator worked just fine, gave equal power but used less fuel. This is not conjecture, this has been reported several times by those who made the switch. One guy reported going from 9 or 10 (can't remember exactly) gallons per hour to 8 gallons per hour. Blanton is gone now, and unfortunately his "take no prisoners" stand in regards the horsepower issue, cost him a lot of credibility before he died. People still remember that issue when the mention of using a Ford V-6 comes up. Corky Scott |
Thread Tools | |
Display Modes | |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
AOPA Stall/Spin Study -- Stowell's Review (8,000 words) | Rich Stowell | Aerobatics | 28 | January 2nd 09 02:26 PM |
Single-Seat Accident Records (Was BD-5B) | Ron Wanttaja | Home Built | 41 | November 20th 03 05:39 AM |
Objective Engine Discussion | Rick Maddy | Home Built | 26 | October 14th 03 04:46 AM |
FS: O-235C1 Lycoming engine (core) | Del Rawlins | Home Built | 0 | October 8th 03 09:46 PM |
Corky's engine choice | Corky Scott | Home Built | 39 | August 8th 03 04:29 AM |