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#1
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.....from R.L. Darling
Mr. Chitwood, I have been following Rick Stitts misadventures for over a year now. I have a RotorWay Exec and a Helicycle helicopter and have two friends with Mini-500's that have the Stitt touch on them. One has had the re-built cones and transmission and the other has the tranny mods done. The first clue we had of improper work was the cones...so sloppy I refused to help the owner reinstall them on the aircraft...then his "re-built trans" locked up. Upon dissassembly , we found the bearings to be thickly encrusted with rust as if they had been submerged in salt water for many years. The other ship has been grounded and I won't know the extent of the damage untill I have a chance to tear it down and inspect it closely. The first ships owner is Mr. Wayne Qualls....he is a knowledgeable pilot and has done his own turbine conversion which has proved successful. I know that he would like to talk to you about Mr. Stitts so he won't mind if I let you have his phone number....he too has been bamboozled out of thousands of dollars that he can not afford. The number is xxxxxxxxxxx...this is in Irving, Texas and believe me....he will welcome your call. I can personally vouch that he sent the parts to Mr. Stitts and personally inspected the trans, and bearings after it locked up ...the tranny had less than 15 minutes on it as it sat in the hanger , unused-full of oil- for several months. I too am in belief that if any of these modified Mini-500's are allowed to fly that we will have multiple fatalities. Please give him a call..... Thanks for keeping people informed... R.L. Darling Dallas, Texas Thanks for the incoming comments. We need to stop this guy before people start dying again. Stitt's turbine startup sequence is WAY wrong. His method will cost you $$$$$ in turbines , as his method guarantees hot starts, or a least unnecessary high temps. D. Chitwood N500XT |
#2
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![]() Thanks for the incoming comments. We need to stop this guy before people start dying again. Stitt's turbine startup sequence is WAY wrong. His method will cost you $$$$$ in turbines , as his method guarantees hot starts, or a least unnecessary high temps. D. Chitwood N500XT Student, and a beginner here...still learning about pistons, but I've seen this term before here...Please explain 'hot starts'. Thanks. p |
#3
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"Peter Maus" wrote in message
Student, and a beginner here...still learning about pistons, but I've seen this term before here...Please explain 'hot starts'. It is a turbine only term, there is no piston engine equivalent. It is when there is too much fuel in the engine or too little air moving through it. Now, for the thorough explanation... Here is a basic distinction between gas turbines and piston engines- piston engines normally use the right amount of air for how much fuel they use. Gas turbines almost always use excess air, sometimes two or three times as much as necessary to burn the fuel. This extra air makes the flame temperature several hundred degrees cooler. In general terms, here is how a gas turbine engine normally starts: 1) First, a starter turns the compressor, accelerating it from zero speed. 2) Ignitors (like spark plugs) fire whenever the starter is turning in most engine designs, and usually once or two sparks per second. 3) Next, above some designated rpm, an exact flow of fuel is introduced. This sprays near the ignitors and usually the flame starts within a few seconds. 4) After the flame starts, the rpm will accelerate even more than with the starter only. 5) Above some designated rpm, approximately idle speed, the starter is not used. It may be disengaged, power removed from it, and either automatically or by the pilot flipping a switch (depending on which design). 6) The engine is now at idle speed (usually above 50% rpm) after a normal start. A hot start may occur for a few main reasons: A weak starter may not turn the engine fast enough. Between (4) and (5), both the flame and starter are required to accelerate the engine to idle speed. With the starter only, the engine can turn up to around 25% of maximum rpm. Without the starter but the flame only, the engine can run at any speed as long as it does not drop below around 40-50% rpm. If it drops below that it will not be able to recover speed eventually stop. So... if the starter is weak, or it drops out at too low an rpm (5), then the engine will not be able to reach idle speed. This is like a car that will almost start but sputters and dies instead. The difference with the gas turbine is that fuel will keep on coming and burning as a turbine winds down over the next several seconds, and may then burn too hot. The engine may also "hang" at an rpm below idle with the flame temperature otherwise acceptable, but that is called a "hung start," not "hot start." Air starters may be weak from too little air spinning them or from being worn out. Electric starters may also wear out, or be weak from a weak aircraft battery just like a car. The oil in the engine may also be cold and thick, which requires a stronger starter. The fuel may be turned on too early (3), before the engine is turning fast enough and moving enough air through the engine. So not enough air means too hot a flame. The fuel may take too long ignite even if everything else is functioning correctly (2,3,4). The unlit fuel can collect in the engine over several seconds, then ignite all at once. So too much fuel means too hot a flame. Sometimes the flame may go all the way out the exhaust pipe like the Batmobile, this is referred to as "torching." The engine may malfunction and spray use too much fuel during a start (3). Lastly, the engine may still be hot if it was just running. In this case, you simply have to run the starter for a little longer to blow fresh air through the engine to cool it off before turning on the fuel. So I hope that makes sense. I simplified most of the explanation, tried to make all the theory relevant but provide some real day-to-day examples of causes. Still, it is all more or less true for all gas turbine engines. |
#4
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![]() Jim Carriere wrote: "Peter Maus" wrote in message Student, and a beginner here...still learning about pistons,... but I've seen this term before here...Please explain 'hot starts'. It is a turbine only term, there is no piston engine equivalent. Yes, I realize that. But it comes up so often in my reading. I'm curious, and have not found reasonable explanations. It is when there is too much fuel in the engine or too little air moving through it. Now, for the thorough explanation... Here is a basic distinction between gas turbines and piston engines- piston engines normally use the right amount of air for how much fuel they use. Gas turbines almost always use excess air, sometimes two or three times as much as necessary to burn the fuel. This extra air makes the flame temperature several hundred degrees cooler. Ok. I'm with you, there. Diesels are non stoichiometric as well. Although I wouldn't want to fly one. In general terms, here is how a gas turbine engine normally starts: 1) First, a starter turns the compressor, accelerating it from zero speed. 2) Ignitors (like spark plugs) fire whenever the starter is turning in most engine designs, and usually once or two sparks per second. 3) Next, above some designated rpm, an exact flow of fuel is introduced. This sprays near the ignitors and usually the flame starts within a few seconds. 4) After the flame starts, the rpm will accelerate even more than with the starter only. 5) Above some designated rpm, approximately idle speed, the starter is not used. It may be disengaged, power removed from it, and either automatically or by the pilot flipping a switch (depending on which design). 6) The engine is now at idle speed (usually above 50% rpm) after a normal start. A hot start may occur for a few main reasons: A weak starter may not turn the engine fast enough. Between (4) and (5), both the flame and starter are required to accelerate the engine to idle speed. With the starter only, the engine can turn up to around 25% of maximum rpm. Without the starter but the flame only, the engine can run at any speed as long as it does not drop below around 40-50% rpm. If it drops below that it will not be able to recover speed eventually stop. So... if the starter is weak, or it drops out at too low an rpm (5), then the engine will not be able to reach idle speed. This is like a car that will almost start but sputters and dies instead. The difference with the gas turbine is that fuel will keep on coming and burning as a turbine winds down over the next several seconds, and may then burn too hot. The engine may also "hang" at an rpm below idle with the flame temperature otherwise acceptable, but that is called a "hung start," not "hot start." Air starters may be weak from too little air spinning them or from being worn out. Electric starters may also wear out, or be weak from a weak aircraft battery just like a car. The oil in the engine may also be cold and thick, which requires a stronger starter. The fuel may be turned on too early (3), before the engine is turning fast enough and moving enough air through the engine. So not enough air means too hot a flame. The fuel may take too long ignite even if everything else is functioning correctly (2,3,4). The unlit fuel can collect in the engine over several seconds, then ignite all at once. So too much fuel means too hot a flame. Sometimes the flame may go all the way out the exhaust pipe like the Batmobile, this is referred to as "torching." The engine may malfunction and spray use too much fuel during a start (3). Lastly, the engine may still be hot if it was just running. In this case, you simply have to run the starter for a little longer to blow fresh air through the engine to cool it off before turning on the fuel. So I hope that makes sense. I simplified most of the explanation, tried to make all the theory relevant but provide some real day-to-day examples of causes. Still, it is all more or less true for all gas turbine engines. Thank you. You've been very helpful. This clarifies a lot. Much obliged. p |
#5
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"Jim Carriere" wrote in message ...
"Peter Maus" wrote in message Student, and a beginner here...still learning about pistons, but I've seen this term before here...Please explain 'hot starts'. It is a turbine only term, there is no piston engine equivalent. It is when there is too much fuel in the engine or too little air moving through it. Hold on for a minute....... It is not a turbine only term! Look in any number of piston engine manuals and especially with fuel injection for "HOT START PROCEDURES". It happens generally with high ambient temperatures when the fuel air mixture ratio is not correct or normal. Each engine will require different procedures according to the manufacturer. Your description for turbines is essentially correct across the board but to say its only for turbines is not correct. Ol Shy & Bashful Now, for the thorough explanation... Here is a basic distinction between gas turbines and piston engines- piston engines normally use the right amount of air for how much fuel they use. Gas turbines almost always use excess air, sometimes two or three times as much as necessary to burn the fuel. This extra air makes the flame temperature several hundred degrees cooler. In general terms, here is how a gas turbine engine normally starts: 1) First, a starter turns the compressor, accelerating it from zero speed. 2) Ignitors (like spark plugs) fire whenever the starter is turning in most engine designs, and usually once or two sparks per second. 3) Next, above some designated rpm, an exact flow of fuel is introduced. This sprays near the ignitors and usually the flame starts within a few seconds. 4) After the flame starts, the rpm will accelerate even more than with the starter only. 5) Above some designated rpm, approximately idle speed, the starter is not used. It may be disengaged, power removed from it, and either automatically or by the pilot flipping a switch (depending on which design). 6) The engine is now at idle speed (usually above 50% rpm) after a normal start. A hot start may occur for a few main reasons: A weak starter may not turn the engine fast enough. Between (4) and (5), both the flame and starter are required to accelerate the engine to idle speed. With the starter only, the engine can turn up to around 25% of maximum rpm. Without the starter but the flame only, the engine can run at any speed as long as it does not drop below around 40-50% rpm. If it drops below that it will not be able to recover speed eventually stop. So... if the starter is weak, or it drops out at too low an rpm (5), then the engine will not be able to reach idle speed. This is like a car that will almost start but sputters and dies instead. The difference with the gas turbine is that fuel will keep on coming and burning as a turbine winds down over the next several seconds, and may then burn too hot. The engine may also "hang" at an rpm below idle with the flame temperature otherwise acceptable, but that is called a "hung start," not "hot start." Air starters may be weak from too little air spinning them or from being worn out. Electric starters may also wear out, or be weak from a weak aircraft battery just like a car. The oil in the engine may also be cold and thick, which requires a stronger starter. The fuel may be turned on too early (3), before the engine is turning fast enough and moving enough air through the engine. So not enough air means too hot a flame. The fuel may take too long ignite even if everything else is functioning correctly (2,3,4). The unlit fuel can collect in the engine over several seconds, then ignite all at once. So too much fuel means too hot a flame. Sometimes the flame may go all the way out the exhaust pipe like the Batmobile, this is referred to as "torching." The engine may malfunction and spray use too much fuel during a start (3). Lastly, the engine may still be hot if it was just running. In this case, you simply have to run the starter for a little longer to blow fresh air through the engine to cool it off before turning on the fuel. So I hope that makes sense. I simplified most of the explanation, tried to make all the theory relevant but provide some real day-to-day examples of causes. Still, it is all more or less true for all gas turbine engines. |
#6
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"Rocky" wrote in message
Hold on for a minute....... It is not a turbine only term! Look in any number of piston engine manuals and especially with fuel injection for "HOT START PROCEDURES". It happens generally with high ambient temperatures when the fuel air mixture ratio is not correct or normal. Each engine will require different procedures according to the manufacturer. OK, I didn't think of that. I have very little piston time- in aircraft anyway... ![]() This is the same term for for apples and oranges though. In a turbine hot start the risk is damaging the engine. In a piston hot start the risks is not starting, right? Like flooding a car engine on a hot summer day, or did I get the wrong idea? Anyway, you learn something new every day, and I'm glad my explanation made sense to Peter Maus. |
#7
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"Jim Carriere" wrote in message ...
"Rocky" wrote in message Hold on for a minute....... It is not a turbine only term! Look in any number of piston engine manuals and especially with fuel injection for "HOT START PROCEDURES". It happens generally with high ambient temperatures when the fuel air mixture ratio is not correct or normal. Each engine will require different procedures according to the manufacturer. OK, I didn't think of that. I have very little piston time- in aircraft anyway... ![]() This is the same term for for apples and oranges though. In a turbine hot start the risk is damaging the engine. In a piston hot start the risks is not starting, right? Like flooding a car engine on a hot summer day, or did I get the wrong idea? Anyway, you learn something new every day, and I'm glad my explanation made sense to Peter Maus. Jim As I said, your explanation was essentially good across the board for turbines and I couldn't have said it better ![]() examples of hot starts with turbine and one that resulted in a rapid meltdown of a PT6. I'm glad it wasn't me with my finger on the start!! Most generally the flawed hot start with piston can result in a dead battery, or burning up a starter. I've seen at least one fire started with a starter that got overheated and ignited wires and insulation. In any case, its wise to know the correct procedures for each and important to follow them! Cheers Flyinrock |
#8
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A "hot start" is where you give the turbine engine too much fuel too
soon during the start up or there is fuel left in the engine after the previous shutdown. The power turbine wheel over heats. If the EGT temperature goes past read line then the turbine wheel and other expensive parts MUST be replaced or sometime in the not too distant future the turbine wheel will come apart rapidly. If the hot start is bad enough and exceeds red line it can cost $50K- $1M+ for the engine tear down and parts replacement. On Sun, 04 Jan 2004 03:41:11 GMT, Peter Maus wrote: Thanks for the incoming comments. We need to stop this guy before people start dying again. Stitt's turbine startup sequence is WAY wrong. His method will cost you $$$$$ in turbines , as his method guarantees hot starts, or a least unnecessary high temps. D. Chitwood N500XT Student, and a beginner here...still learning about pistons, but I've seen this term before here...Please explain 'hot starts'. Thanks. p |
#9
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OT to R.L Darling: How is your Helicycle doing?? I saw it at
Waxahatchee...Stu Fields "Dennis Chitwood" wrote in message om... ....from R.L. Darling Mr. Chitwood, I have been following Rick Stitts misadventures for over a year now. I have a RotorWay Exec and a Helicycle helicopter and have two friends with Mini-500's that have the Stitt touch on them. One has had the re-built cones and transmission and the other has the tranny mods done. The first clue we had of improper work was the cones...so sloppy I refused to help the owner reinstall them on the aircraft...then his "re-built trans" locked up. Upon dissassembly , we found the bearings to be thickly encrusted with rust as if they had been submerged in salt water for many years. The other ship has been grounded and I won't know the extent of the damage untill I have a chance to tear it down and inspect it closely. The first ships owner is Mr. Wayne Qualls....he is a knowledgeable pilot and has done his own turbine conversion which has proved successful. I know that he would like to talk to you about Mr. Stitts so he won't mind if I let you have his phone number....he too has been bamboozled out of thousands of dollars that he can not afford. The number is xxxxxxxxxxx...this is in Irving, Texas and believe me....he will welcome your call. I can personally vouch that he sent the parts to Mr. Stitts and personally inspected the trans, and bearings after it locked up ...the tranny had less than 15 minutes on it as it sat in the hanger , unused-full of oil- for several months. I too am in belief that if any of these modified Mini-500's are allowed to fly that we will have multiple fatalities. Please give him a call..... Thanks for keeping people informed... R.L. Darling Dallas, Texas Thanks for the incoming comments. We need to stop this guy before people start dying again. Stitt's turbine startup sequence is WAY wrong. His method will cost you $$$$$ in turbines , as his method guarantees hot starts, or a least unnecessary high temps. D. Chitwood N500XT |
#10
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Dennis Chitwood wrote:
....from R.L. Darling Mr. Chitwood, I have been following Rick Stitts misadventures for over a year now. I have a RotorWay Exec and a Helicycle helicopter and have two friends with Mini-500's that have the Stitt touch on them. One has had the re-built cones and transmission and the other has the tranny mods done. I've read a bit also. And would very much like to learn more. I'm trying to find information about it. Every time I ask, I get no answers or just emotional angry responces, not facts... Near as I can tell, there was a major "buisness" fall-out, and Rick Stitts, Bill Phillips, Randy Culver, Dean Fetters, Ken Armstrong, and Fred Stewart, and Joe Rinke seem to have all been involved. When ever any of those names comes up, there is more emotion and anger than facts. I am NOT trolling, but I am very aware this is a troll topic. I am seriously trying to study if a Mini-500 can be rebuilt to be safe (defining "safe" in context of experimental aircraft, which it itself is a tough thing to say). The first ships owner is Mr. Wayne Qualls....he is a knowledgeable pilot and has done his own turbine conversion which has proved successful. I know that he would like to talk to you about Mr. Stitts so he won't mind if I let you have his phone number....he too has been bamboozled out of thousands of dollars that he can not afford. The number is xxxxxxxxxxx...this is in Irving, Texas and believe me....he will welcome your call. I would be happy to call, because I am considering a Mini-500 Turbine conversion. And I promise, I'm just trying to figure this thing out. I just started reading about it 2 weeks ago, and haven't found much about rebuilding. Thanks for the incoming comments. We need to stop this guy before people start dying again. Stitt's turbine startup sequence is WAY wrong. His method will cost you $$$$$ in turbines , as his method guarantees hot starts, or a least unnecessary high temps. D. Chitwood N500XT I believe, althought I could be wrong, that I read on Rick Stitt's site that he has found that the hot starts are not the way to go, and he has explained himself turbine starts should be done diffrent. To quote his website: "This is a Turbine T62-2A being installed into a Mini 500. The radiator area has be converted to a main fuel tank. The first conversions done for a mini were direct drive and had one starter to drive the main rotor system and the engine during the start cycle. This system did work but many of the customers didn't like the EGT going over 1300 or 1400 deg F during the start cycle. The next logical step was to install two starters in parallel. This reduced the start temp to 1190 during the start cycle. The Turbine really likes to be started with no load and the following information is how we reduced the start temp to 650 deg F. with hover at 800 deg F." Further, Stitt's site has a comlete list of all the fatals in Mini-500s, and I have read the reports there as well as 9 fatals in the Mini-500 on the http://www.ntsb.gov/NTSB site. (I also read the reports of all 7 fatals in RotorWay Exec's there, but they happened over a longer period of time). I can not find numbers of RotorWay Exec kits sold, I know about 550 Mini-500 kits were sold. I can find no real answer to how many of either of these kits were ever built, or how many hours people have logged in them. MUCH LESS on Turbine Conversions. I'm honestly just trying to research this before I buy, build, or rebuild anything. My big conserns are the weight limits, and the 210 lbs seat limit of the RotorWay, and the 220 lbs seat limit of the HeliCycle are holding me back from going that direction. Any information you or anyone can provide would be greatly appreciated by me at this point. Good, bad, about RotorWay, HeliCycle, Mini-500, or anything, I don't care as long as the information is factual, not emotional or trolls. For referance, here are some good and bad things I have found about the Mini-500 (other than Stitt's site): http://www.moneypit.net/~pratt/ambuilt/helicopter.htm (it may be better to just read NTSB reports insted?) http://www.kitplanes.com/features/su.../mini-500.html (more politics and buisness than air-worthy-ness) http://yarchive.net/air/mini500.html (I found some interesting things here, and would really appreciate if someone could explain the "RHCI puts a fixed elevator on the horizontal stab which is deflected down to compensate for a positive pitching moment in forward flight as the MR system pumps air down." statement to me, I'm really new to learning about helicopters in general, and haven't even begun my flight training). Again, I'm looking for any and all information I can get, hopefully with explinations not just flames. Thanks in advance. |
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