Commander-List Digest Archive

Mon 10/01/07


Total Messages Posted: 12



Today's Message Index:
----------------------
 
     1. 04:23 AM - Re: Re: Pressure Carburetor? (Matthew J. Hawkins)
     2. 05:43 AM - Re: Re: Pressure Carburetor? (Matthew J. Hawkins)
     3. 09:19 AM - Re: Re: Pressure Carburetor? (BobsV35B@aol.com)
     4. 09:28 AM - Re: Re: Pressure Carburetor? (David Owens)
     5. 09:49 AM - Re: Re: Pressure Carburetor? (Matthew J. Hawkins)
     6. 10:57 AM - Re: Re: Pressure Carburetor? (BobsV35B@aol.com)
     7. 11:10 AM - Re: Re: Pressure Carburetor? (Matthew J. Hawkins)
     8. 05:34 PM - Re: Re: Pressure Carburetor? (Don)
     9. 10:27 PM - Re: Re: Pressure Carburetor? (BobsV35B@aol.com)
    10. 11:00 PM - Official Commander-List FAQ (Frequently Asked Questions) (Matt Dralle)
    11. 11:03 PM - Official Commander-List Usage Guidelines (Matt Dralle)
    12. 11:26 PM - Re: Re: Pressure Carburetor? (Don)
 
 
 


Message 1


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    Time: 04:23:07 AM PST US
    From: "Matthew J. Hawkins" <hawkins@cms.udel.edu>
    Subject: Re: Pressure Carburetor?
    Wow! I had no idea my pressure carburetor question would spur this kind of discussion! It's a good one though - quite important is seems. N2760B is a very basic machine. CHT only on one cylinder for each engine - nothing else. No EGT. No fuel transfer system. Sounds to me like best approach is to run with mixtures "full rich" and let the pressure carb do it's job. Leave mixtures "the stink" alone. Matt -----Original Message----- From: owner-commander-list-server@matronics.com [mailto:owner-commander-list-server@matronics.com] On Behalf Of Bill Bow Sent: Sunday, September 30, 2007 8:05 PM Subject: RE: Commander-List: Re: Pressure Carburetor? --> <bowing74@earthlink.net> This is great! It hasn't "hit the fan" like this since the "Sump-Gate" days of '01. bilbo -----Original Message----- From: owner-commander-list-server@matronics.com [mailto:owner-commander-list-server@matronics.com] On Behalf Of N395V Sent: Saturday, September 29, 2007 8:13 PM Subject: Commander-List: Re: Pressure Carburetor? <airboss@excaliburaviation.com> > HI MILT. I am not picking on you, but need to make one other > correction. Not to worry JB I have a thick skin especially when my espousings are based on science and data. This is quite an important topic for any bathtub commander owner and neededs to be thoroughly discussed. -------- Milt 2003 F1 Rocket 2006 Radial Rocket Read this topic online here: http://forums.matronics.com/viewtopic.php?p=137190#137190


    Message 2


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    Time: 05:43:22 AM PST US
    From: "Matthew J. Hawkins" <hawkins@cms.udel.edu>
    Subject: Re: Pressure Carburetor?
    Jb- Thanks for this! Perfect description of what we're seeing. Left engine (with properly re-built carb) does exactly as you say - rapid c hange in engine operation as you get close to idle/cut-off. Right engine seemed to lean somewhat like a "regular" engine. I'll double-check that th is week. Right engine is the one that always seemed to run rich and foul p lugs too. We'll have a look at this when we can. Glad to hear that when "auto lean" is not working properly the fallback in the design is to lean manually. Ma kes good sense. In the short term, sounds like we just need to be aware of whether or not the auto lean is running properly or not. Good news is that all exhaust pipes are a nice ash grey - no black soot/res idue. Perhaps engines are still bedding in? What's your thought on the wire-type plugs? Matt -----Original Message----- From: owner-commander-list-server@matronics.com [mailto:owner-commander-lis t-server@matronics.com] On Behalf Of yourtcfg@aol.com Sent: Sunday, September 30, 2007 12:54 AM Subject: Re: Commander-List: Re: Pressure Carburetor? HI TYLOR You can generally tell if the autolean is operating by engine performance. If the carb fails, it is designed to fail safe and run super rich. You ca n then manually lean it until it can be repaired. On the Commander, look f or the cyl temps to run the same on both engines, at climb and cruse. To c heck normal operation, set cruse power and slowly lean the carbs manually ( one at a time thank you) The levers should travel about 1/2 way with littl e or no change in engine operation. When the change comes, it should be ve ry quick. It should go from running fine to idle cut-off in a very little travel. Last, check the color of the exhaust pipes. They should be a nice ash gray. jb I do have a questions. Matthew's problem, how do you know the auto lean is working? How do you check it? It sounds like the rebuilt side is working and the old er one may not?


    Message 3


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    Time: 09:19:10 AM PST US
    From: BobsV35B@aol.com
    Subject: Re: Pressure Carburetor?
    Good Morning Matt, That may very well be the best answer for you and your airplane. However, may I point out that even fifty years ago there were some who did learn how to operate those engines safely and efficiently by judicious use of the mixture control. May I first ask just what style of Pressure Carburetor your engine has? Does it have an AMC unit? There seems to be a lot of mention about pressure carburetors implying that all pressure carburetors have Automatic Mixture Controls installed. That is definitely NOT true. As was mentioned by Milt, the PS5c is not one that will provide any altitude compensation at all, yet it is probably the most commonly used pressure carburetor in the GA fleet. The designers of the fuel controls had to be people who fully understood the vagaries of engine operation. They knew the difficulties present in trying to get even distributor of fuel and air to each and every cylinder as well as the necessity for each cylinder to be manufactured to close enough tolerances so that the compression of each cylinder was as close as possible to being identical and so that the breathing efficiencies of the intake systems were identical. They then designed a fuel delivery system that would work adequately for engines that were at the edges of acceptability when evaluated for cylinder to cylinder consistencies. Have you ever heard a reference to the "Shaky Jakes", when one is discussing Jacobs Aircraft Engines? The reason they were described as shaky was because the early Jakes had a very simple fuel delivery system that caused the lower cylinders to get a LOT more fuel than the upper ones. Most of the later development of the Jacobs engines were directed toward improving that mixture distribution. Later, more modern, round engines used many schemes to provide better distribution. It was thought by all, that it would be best if the pilot did not have to operate any controls that would affect that mixture. The development of the pressure injection carburetor with an AMC unit was an effort toward simplifying the operation for the pilots of the day. It was never completely successful. The best units that were ever made were those that were fitted to the latest P&W R-2800s and the Curtiss Wright R-3350s which were the engines that powered the last of the piston airline fleet. When those engines were used in four engine long range airplanes, they almost always had flight engineers assigned to operating the engines so that adequate and proper leaning procedures could be used. For short haul airplanes, the pilots normally just used the Auto Lean and Auto Rich functions. On those rare occasions when range or endurance became an important consideration, even we lowly aviators would do a bit of manual leaning. What point am I trying to make? You can do manual leaning of your aircraft even if you don't have the modern equipment, but it takes a much greater understanding of the potential vagaries of the combustion process than is generally made available to we aviators in our basic training. JB mentioned monitoring the tail pipes to ascertain whether or not the mixtures being provided by your fuel delivery unit are adequate. That was, and still is, certainly one of the clues, but there are many others. Attendance at a good engine course such as is provided by The Advanced Pilot's Seminar folks will provide the basics, but they start off by saying there is no reason to try to learn the basics if the airplane is not equipped with modern monitoring devices. Having been an active aviator during the days when such stuff was not available, I do have a few techniques which I can use to make a decision as to whether or not it will be practical to operate at any setting other than full rich. Let's forget about what you are flying now, and consider whatever airplane you used when you were a student pilot. Let's say it was a Piper Cherokee 140. Once you were set up in cruise, you may have been taught to lean the engine until it got rough, then richen until the operations smoothed. You were probably also told not to lean at all below some pre selected altitude. That method has good science behind it! Before you can decide how much fuel is needed for the total engine, you must determine how even the mixture is from cylinder to cylinder. A very easy way to check on that when flying that Cherokee was to monitor the RPM while leaning. If the engine got rough before any RPM drop was noted, the mixture distribution was atrocious. If you were able to get a fifty to sixty RPM drop before any roughness occurred, the mixture distribution was reasonable. As an aside, that DID NOT mean you should operate it with the fifty RPM drop, that was merely a way to check for good distribution. Cessna formerly recommended that the 170 with a fixed pitch propellor be leaned until it encountered a two MPH drop in airspeed. That was a good method of finding a point just barely on the lean side of best power and it would probably have given an EGT reading of about fifty rich of peak had we had EGT gauges back then. For any GA engine being operated at 65 per cent power or less, there is nothing you can do with the mixture control that will hurt the engine, so Cessna's method worked well and was very simple. Back to the Cherokee! If the engine kept operating smoothly all the way until all four cylinders quit running, the mixture distribution was perfect. With a constant speed propellor, the same sort of test can be performed by watching the airspeed. Obviously, the air must be smooth and the pilot capable of holding altitude and attitude very closely while performing the check, but it did, and still does, work quite well. If the distribution is good, you should be able to perceive an increase in power by noting the increase in airspeed as the engine is leaned. Peak airspeed will occur when the engine is developing peak power. That is, it will be getting as much power as is possible from the fuel and air being delivered to the engine. For what it is worth, most small normally aspirated piston engine get their peak power when the mixture is at a point corresponding to an EGT temperature that is approximately eighty degrees Fahrenheit cooler than the peak EGT number and on the rich side thereof. Reason would tell us that the engine will run at it's hottest when the most power is being developed, but tests have shown that to not be true. The CHTs will be hottest when the engine is operated with an EGT set to somewhere around fifty degrees rich of the Peak EGT temperature. If we do not have an engine monitor, we cannot tell precisely where the temperature is being set, but we can evaluate the performance of the airplane. If we lean the engine so that the airplane is going just as fast as it will go with the RPM and manifold pressure being used, the engine will be at the best power mixture setting and it will be just a wee bit richer than the point where the CHTs will be the hottest! This is certainly NOT meant as a primer on how to lean your engine. I just wanted to point out that there is no easy cake recipe style of approach. If you wish to rely on the efficacy of the installed fuel control, that is great, but you should understand the process well enough so that you can determine whether or not your system is working as it was designed to work. That part of the equation is very difficult if you DO NOT have modern engine monitoring equipment. The potential for finding a mechanic with a proper flow bench and all the skill and knowledge to use it well is very slim. It has been ten to fifteen years since I last priced a rebuild on one of those fancy fully automatic carburetors for an Aero Commander, but I was quoted a price of fifteen thousand dollars per carburetor. The owner elected to donate the aircraft to a mechanics school as it was not economically viable to overhaul those units. I have no idea whether or not any alternative carburetors were available for that airplane, but installing a simple PS5c and modern monitoring equipment would have been a lot cheaper alternative. The rub would be whether or not it was FAA approved! Happy Skies, Old Bob AKA Bob Siegfried Ancient Aviator Stearman N3977A Brookeridge Air Park LL22 Downers Grove, IL 60516 630 985-8503 In a message dated 10/1/2007 6:24:06 A.M. Central Daylight Time, hawkins@cms.udel.edu writes: N2760B is a very basic machine. CHT only on one cylinder for each engine - nothing else. No EGT. No fuel transfer system. Sounds to me like best approach is to run with mixtures "full rich" and let the pressure carb do it's job. Leave mixtures "the stink" alone. Matt


    Message 4


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    Time: 09:28:21 AM PST US
    From: "David Owens" <dowens@aerialviewpoint.com>
    Subject: Re: Pressure Carburetor?
    Hey Chris! How you doin??? Dave Owens here with Aerial Viewpoint... Haven't heard from you since your visit here at Hooks a few years back... Did Dreamcatcher get sold or scrapped??? I heard stories. Looking forward to hearing from you. David Owens Aerial Viewpoint N14AV AC-500A-Colemill


    Message 5


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    Time: 09:49:33 AM PST US
    From: "Matthew J. Hawkins" <hawkins@cms.udel.edu>
    Subject: Re: Pressure Carburetor?
    Bob- That's definitely something I've gleaned from this discussion. All pressur e carbs are NOT created equal. I'll check on exactly what I have and let y ou know. Milt's view seems sound - if it can be leaned - you should do it. No sense in wasting fuel/$$ However, seems like I don't have the engine monitorin g systems to do it accurately or efficiently. Next time we're up on a smooth day we'll try the airspeed method you sugges t below. Your description of manual leaning is exactly what I learned as a student p ilot - and still use on a plane with no EGT. In fact, it's what my pilot w ho flies the Commander was trying to do on the ground when engines were (ap parently) running too rich. Sounds like we need to do it differently with the constant speed prop. Everything ran GREAT on our flight last week - think Summit got the final a djustments right. Good mag checks, not rough running, nice grey ash in the tubes (no black soot). Only question is whether or not the auto lean is w orking on the right engine - and exactly what carbs we have (i.e. should it have auto lean?). The shop that did the final "tweak" on the left carb (and got it right) cha rged us $795. Guess we did OK! Milt sent me Chris Schuermanns PDF file that listed the other two recommend ed shop in case we need for the right engine. We'll see. I'm also going to check to see if we have the black gaskets or the newer or ange. Matt -----Original Message----- From: owner-commander-list-server@matronics.com [mailto:owner-commander-lis t-server@matronics.com] On Behalf Of BobsV35B@aol.com Sent: Monday, October 01, 2007 12:18 PM Subject: Re: Commander-List: Re: Pressure Carburetor? Good Morning Matt, May I first ask just what style of Pressure Carburetor your engine has? Does it have an AMC unit? There seems to be a lot of mention about pressure carburetors implying that all pressure carburetors have Automatic Mixture Controls installed. That is definitely NOT true. > > Let's forget about what you are flying now, and consider whatever airplane you used when you were a student pilot. Let's say it was a Piper Cherokee 1 40. Once you were set up in cruise, you may have been taught to lean the en gine until it got rough, then richen until the operations smoothed. You wer e probably also told not to lean at all below some pre selected altitude. That method has good science behind it! > > With a constant speed propellor, the same sort of test can be performed by watching the airspeed. Obviously, the air must be smooth and the pilot capa ble of holding altitude and attitude very closely while performing the chec k, but it did, and still does, work quite well. If the distribution is good, you should be able to perceive an increase in power by noting the increase in airspeed as the engine is leaned. Peak airs peed will occur when the engine is developing peak power. That is, it will be getting as much power as is possible from the fuel and air being deliver ed to the engine. > > I just wanted to point out that there is no easy cake recipe style of appr oach. If you wish to rely on the efficacy of the installed fuel control, th at is great, but you should understand the process well enough so that you can determine whether or not your system is working as it was designed to w ork. > > It has been ten to fifteen years since I last priced a rebuild on one of th ose fancy fully automatic carburetors for an Aero Commander, but I was quot ed a price of fifteen thousand dollars per carburetor. The owner elected to donate the aircraft to a mechanics school as it was not economically viabl e to overhaul those units. Happy Skies, Old Bob


    Message 6


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    Time: 10:57:06 AM PST US
    From: BobsV35B@aol.com
    Subject: Re: Pressure Carburetor?
    Good Morning Matt, Sounds great! Learning and sharing knowledge is what it is all about. You may well have a pressure carburetor that is not easy to manually lean. After all, that WAS the goal of the folks who designed it. In any case, I urge you to read and study the data that is readily available. A good start is to read John Deakin's articles on general engine management. I doubt if you will find very many folks who have current experience with the fuel controllers on your airplane. It is obvious that JB does have current information because he is so insistent that your particular unit should only be leaned in an emergency. I have no gripe with that philosophy, but I do think it is important that an operator of such a unit be very knowledgeable as to just what it is supposed to be doing. I strongly recommend that you do instrument the engine so that you will be able to ascertain whether or not the automatic controls are doing what they were designed to do! I believe checking it using the airspeed method is quite a bit beyond what you should be doing with your current level of experience and lack of on board monitoring equipment.. Those are highly stressed and sophisticated engines. Treat them gently! Happy Skies, Old Bob AKA Bob Siegfried Ancient Aviator Stearman N3977A Brookeridge Air Park LL22 Downers Grove, IL 60516 630 985-8503 In a message dated 10/1/2007 11:50:32 A.M. Central Daylight Time, hawkins@cms.udel.edu writes: That's definitely something I've gleaned from this discussion. All pressure carbs are NOT created equal. I'll check on exactly what I have and let you know.


    Message 7


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    Time: 11:10:30 AM PST US
    From: "Matthew J. Hawkins" <hawkins@cms.udel.edu>
    Subject: Re: Pressure Carburetor?
    Good advise! Burning a bit of extra fuel won't hurt me too badly in the sh ort term. Matt -----Original Message----- From: owner-commander-list-server@matronics.com [mailto:owner-commander-lis t-server@matronics.com] On Behalf Of BobsV35B@aol.com Sent: Monday, October 01, 2007 1:56 PM Subject: Re: Commander-List: Re: Pressure Carburetor? I believe checking it using the airspeed method is quite a bit beyond what you should be doing with your current level of experience and lack of on bo ard monitoring equipment.. Those are highly stressed and sophisticated engi nes. Treat them gently! Happy Skies, Old Bob


    Message 8


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    Time: 05:34:08 PM PST US
    From: "Don" <dongirod@bellsouth.net>
    Subject: Re: Pressure Carburetor?
    Bob; I used to sit sideways in a Connie running R-3360 Turbo compound engines, but its been a long time. My question is this, since you remember more about those things, I recall being told some where that aircraft engines use approximately 25% of their fuel for cooling. At what point in leaning do we get to where we save fuel, but shorten the engine life? And where is the crossover point. Thanks, Don ----- Original Message ----- From: BobsV35B@aol.com To: commander-list@matronics.com Sent: Monday, October 01, 2007 12:18 PM Subject: Re: Commander-List: Re: Pressure Carburetor? Good Morning Matt, That may very well be the best answer for you and your airplane. However, may I point out that even fifty years ago there were some who did learn how to operate those engines safely and efficiently by judicious use of the mixture control. May I first ask just what style of Pressure Carburetor your engine has? Does it have an AMC unit? There seems to be a lot of mention about pressure carburetors implying that all pressure carburetors have Automatic Mixture Controls installed. That is definitely NOT true. As was mentioned by Milt, the PS5c is not one that will provide any altitude compensation at all, yet it is probably the most commonly used pressure carburetor in the GA fleet. The designers of the fuel controls had to be people who fully understood the vagaries of engine operation. They knew the difficulties present in trying to get even distributor of fuel and air to each and every cylinder as well as the necessity for each cylinder to be manufactured to close enough tolerances so that the compression of each cylinder was as close as possible to being identical and so that the breathing efficiencies of the intake systems were identical. They then designed a fuel delivery system that would work adequately for engines that were at the edges of acceptability when evaluated for cylinder to cylinder consistencies. Have you ever heard a reference to the "Shaky Jakes", when one is discussing Jacobs Aircraft Engines? The reason they were described as shaky was because the early Jakes had a very simple fuel delivery system that caused the lower cylinders to get a LOT more fuel than the upper ones. Most of the later development of the Jacobs engines were directed toward improving that mixture distribution. Later, more modern, round engines used many schemes to provide better distribution. It was thought by all, that it would be best if the pilot did not have to operate any controls that would affect that mixture. The development of the pressure injection carburetor with an AMC unit was an effort toward simplifying the operation for the pilots of the day. It was never completely successful. The best units that were ever made were those that were fitted to the latest P&W R-2800s and the Curtiss Wright R-3350s which were the engines that powered the last of the piston airline fleet. When those engines were used in four engine long range airplanes, they almost always had flight engineers assigned to operating the engines so that adequate and proper leaning procedures could be used. For short haul airplanes, the pilots normally just used the Auto Lean and Auto Rich functions. On those rare occasions when range or endurance became an important consideration, even we lowly aviators would do a bit of manual leaning. What point am I trying to make? You can do manual leaning of your aircraft even if you don't have the modern equipment, but it takes a much greater understanding of the potential vagaries of the combustion process than is generally made available to we aviators in our basic training. JB mentioned monitoring the tail pipes to ascertain whether or not the mixtures being provided by your fuel delivery unit are adequate. That was, and still is, certainly one of the clues, but there are many others. Attendance at a good engine course such as is provided by The Advanced Pilot's Seminar folks will provide the basics, but they start off by saying there is no reason to try to learn the basics if the airplane is not equipped with modern monitoring devices. Having been an active aviator during the days when such stuff was not available, I do have a few techniques which I can use to make a decision as to whether or not it will be practical to operate at any setting other than full rich. Let's forget about what you are flying now, and consider whatever airplane you used when you were a student pilot. Let's say it was a Piper Cherokee 140. Once you were set up in cruise, you may have been taught to lean the engine until it got rough, then richen until the operations smoothed. You were probably also told not to lean at all below some pre selected altitude. That method has good science behind it! Before you can decide how much fuel is needed for the total engine, you must determine how even the mixture is from cylinder to cylinder. A very easy way to check on that when flying that Cherokee was to monitor the RPM while leaning. If the engine got rough before any RPM drop was noted, the mixture distribution was atrocious. If you were able to get a fifty to sixty RPM drop before any roughness occurred, the mixture distribution was reasonable. As an aside, that DID NOT mean you should operate it with the fifty RPM drop, that was merely a way to check for good distribution. Cessna formerly recommended that the 170 with a fixed pitch propellor be leaned until it encountered a two MPH drop in airspeed. That was a good method of finding a point just barely on the lean side of best power and it would probably have given an EGT reading of about fifty rich of peak had we had EGT gauges back then. For any GA engine being operated at 65 per cent power or less, there is nothing you can do with the mixture control that will hurt the engine, so Cessna's method worked well and was very simple. Back to the Cherokee! If the engine kept operating smoothly all the way until all four cylinders quit running, the mixture distribution was perfect. With a constant speed propellor, the same sort of test can be performed by watching the airspeed. Obviously, the air must be smooth and the pilot capable of holding altitude and attitude very closely while performing the check, but it did, and still does, work quite well. If the distribution is good, you should be able to perceive an increase in power by noting the increase in airspeed as the engine is leaned. Peak airspeed will occur when the engine is developing peak power. That is, it will be getting as much power as is possible from the fuel and air being delivered to the engine. For what it is worth, most small normally aspirated piston engine get their peak power when the mixture is at a point corresponding to an EGT temperature that is approximately eighty degrees Fahrenheit cooler than the peak EGT number and on the rich side thereof. Reason would tell us that the engine will run at it's hottest when the most power is being developed, but tests have shown that to not be true. The CHTs will be hottest when the engine is operated with an EGT set to somewhere around fifty degrees rich of the Peak EGT temperature. If we do not have an engine monitor, we cannot tell precisely where the temperature is being set, but we can evaluate the performance of the airplane. If we lean the engine so that the airplane is going just as fast as it will go with the RPM and manifold pressure being used, the engine will be at the best power mixture setting and it will be just a wee bit richer than the point where the CHTs will be the hottest! This is certainly NOT meant as a primer on how to lean your engine. I just wanted to point out that there is no easy cake recipe style of approach. If you wish to rely on the efficacy of the installed fuel control, that is great, but you should understand the process well enough so that you can determine whether or not your system is working as it was designed to work. That part of the equation is very difficult if you DO NOT have modern engine monitoring equipment. The potential for finding a mechanic with a proper flow bench and all the skill and knowledge to use it well is very slim. It has been ten to fifteen years since I last priced a rebuild on one of those fancy fully automatic carburetors for an Aero Commander, but I was quoted a price of fifteen thousand dollars per carburetor. The owner elected to donate the aircraft to a mechanics school as it was not economically viable to overhaul those units. I have no idea whether or not any alternative carburetors were available for that airplane, but installing a simple PS5c and modern monitoring equipment would have been a lot cheaper alternative. The rub would be whether or not it was FAA approved! Happy Skies, Old Bob AKA Bob Siegfried Ancient Aviator Stearman N3977A Brookeridge Air Park LL22 Downers Grove, IL 60516 630 985-8503 In a message dated 10/1/2007 6:24:06 A.M. Central Daylight Time, hawkins@cms.udel.edu writes: N2760B is a very basic machine. CHT only on one cylinder for each engine - nothing else. No EGT. No fuel transfer system. Sounds to me like best approach is to run with mixtures "full rich" and let the pressure carb do it's job. Leave mixtures "the stink" alone. Matt ------------------------------------------------------------------------- ----- See what's new="_blank">Make AOL Your Homepage. ------------------------------------------------------------------------- ----- 10/1/2007 6:59 PM


    Message 9


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    Time: 10:27:42 PM PST US
    From: BobsV35B@aol.com
    Subject: Re: Pressure Carburetor?
    Good Evening Don, I have never heard that particular number and I believe we would have to better define the terms before we could either disagree or agree with that 25% assertion. As to where does leaning cause additional wear, that is another tough one. Running any engine too lean at high powers will cause big troubles. However running one leaner than optimum at low powers will not hurt it all, but it will burn more fuel per horsepower developed than is possible when the engine is run so as to attain optimum BSFC (Brake Specific Fuel Consumption). I do not know the number used by your airline to lean the Turbo Compound R-3350, but most users utilized a ten percent BMEP drop from the peak BMEP. The procedure used by my airline was as follows. We would first chose a desired BMEP number from the power charts. Just for kicks, let's say that the desired cruise BMEP was 254. We would start out with the mixture in Auto Rich. The mixture would be slowly leaned until the BMEP started to rise. When it went above 254, we would throttle back until it was at 254, then continue to lean until it was steady at 254 and where any further leaning would take the BMEP reading below 254. That procedure determined the peak BMEP (Peak power) for the manifold pressure being used. At that time, we would continue leaning the engine until the BMEP was reading 254 minus 24.5 or approximately 228 BMEP. Once that spot ten percent leaner than peak power was found, the throttle was used to add manifold pressure so as to bring the BMEP back to the desired cruise power. We then checked the manifold pressure to be sure we were still below the maximum allowed manifold pressure for the desired cruise power. Sound familiar? If we leaned the engine further, it would just lose power, but no harm was done. However, if we richened it up a bit, the engine would overheat and it may even go into mild detonation. It needed to be well lean of peak power to cool properly. I don't know if you recall, but there is a shaft on the rear of the engine which connects the two fuel injection controllers together. One unit is for the front row and the other feeds the rear. That shaft would occasionally slip. When that happened, one row would be running substantially leaner than the other. The one that was getting more fuel would be carrying more of the load that was being developed by the engine. That row would burn the valves and sometimes even have holes burned in the pistons while the row which was not getting enough fuel would be running clean and comfortable. The place where any engine is most likely to develop engine problems are when the mixture is at that point where the peak BMEP or peak engine power is being developed. If the engine is run at that same power with a richer than needed fuel mixture, the extra fuel will slow down the rate of burn and move the point of peak combustion pressure to a point where the engine is able to operate relatively cool. That function is what is normally referred to as cooling the engine with fuel and it is how we kept our cool during takeoff and climb regimes! Another way to cool the engine is to cool it with additional combustion air. That is what happens when the engine is run well lean of best power. (Note that I said best power, not Peak EGT. They do NOT occur at the same point) When we leaned that nice big R-3350 ten percent lean of best power, we were running at a mixture that was well lean of the best power point and the engine was being cooled by that surplus combustion air. Normal cruise power for the 3350 was around 55 to 60 percent of rated power. We were really running it quite conservatively. If we richened it without reducing the manifold pressure, we defeated the air cooling effect and it would overheat and cause all sorts of problems. Leaner is cleaner and leaner is cooler. Cleaner and cooler is generally considered to be better, is it not? So, if you want to extend engine life, run it at relatively low power settings and run the mixture on the lean side of best power! Happy Skies, Old Bob AKA Bob Siegfried Ancient Aviator Stearman N3977A Brookeridge Air Park LL22 Downers Grove, IL 60516 630 985-8503 In a message dated 10/1/2007 7:35:20 P.M. Central Daylight Time, dongirod@bellsouth.net writes: Bob; I used to sit sideways in a Connie running R-3360 Turbo compound engines, but its been a long time. My question is this, since you remember more about those things, I recall being told some where that aircraft engines use approximately 25% of their fuel for cooling. At what point in leaning do we get to where we save fuel, but shorten the engine life? And where is the crossover point. Thanks, Don


    Message 10


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    Time: 11:00:29 PM PST US
    From: Matt Dralle <dralle@matronics.com>
    Subject: Official Commander-List FAQ (Frequently Asked Questions)
    Dear Listers, Please read over the Commander-List Frequently Asked Questions (FAQ) below. The complete Commander-List FAQ including the Usage Guidelines can be found at the following URL: http://www.matronics.com/FAQs/Commander-List.FAQ.html Thank you, Matt Dralle Matronics Email List Administrator [ Note: This FAQ was designed to be displayed with a fixed width font such as Courier. Proportional fonts will cause display formatting errors. ] _-*************************************************************************-_ _-* Commander List Co-Sponsored by the Twin Commander Flight Group (TCFG) *-_ _-* *-_ _-* Please see the link below for a welcome message from the TCFG *-_ _-* directory, Jim Metzger. 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Understanding the Commander-List policies will minimize problems for the Administrator, and will help keep the Commander-List running smoothly for all of us. ****************************************** *** Quick Start Guide to List Features *** ****************************************** There are many features available on the Matronics Email Lists and each one is described in detailed below. However, using the List Navigator you can quickly access the complete set of features available for this List. The List Navigator can be found at the following URL: http://www.matronics.com/Navigator?Commander-List **************************************** *** How to Subscribe and Unsubscribe *** **************************************** Simply go to the Web Page shown below and enter your email address and select the List(s) that you wish to subscribe or unsubscribed from. You may also use the handy "Find" function to determine the exact syntax of your email address as it is subscribed to the List. 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Every year during November I run a low-key, low-pressure "Fund Raiser" where, throughout the month, I ask List members to make a Contribution in any amount with which they are comfortable. I will often offer free gifts with certain contribution levels during the Fund Raiser to increase the participation. The gifts are usually donated by companies that are themselves List members. Your Contributions go directly to supporting the operation of the Lists including the high-speed, business-class Internet connection, server system hardware and software upgrades, and to partially offset the many many hours I spend running, maintaining, upgrading, and developing the variety of services found here. Generally Contributions range from $20 to $100 and are completely voluntary and non-compulsory. I ask only that if person enjoys the Lists and obtains value from them, that they make a Contribution of equal magnitude. Contributions are accepted throughout the year, and if you've just subscribed, feel free to make a Contribution when you've settled in. The website for making SSL Secure Contributions is listed below. There are a variety of payment methods including Visa and MasterCard, PayPal, and sending a personal check. If you enjoy and value the List, won't you make a Contribution today to support its continued operation? http://www.matronics.com/contributions Thank you! Matt Dralle Email List Administrator ****************************************************************************** Commander-List Usage Guidelines ****************************************************************************** The following details the official Usage Guidelines for the Commander-List. You are encouraged to read it carefully, and to abide by the rules therein. Failure to use the Commander-List in the manner described below may result in the removal of the subscribers from the List. Commander-List Policy Statement The purpose of the Commander-List is to provide a forum of discussion for things related to this particular discussion group. The List's goals are to serve as an information resource to its members; to deliver high-quality content; to provide moral support; to foster camaraderie among its members; and to support safe operation. Reaching these goals requires the participation and cooperation of each and every member of the List. To this end, the following guidelines have been established: - Please keep all posts related to the List at some level. Do not submit posts concerning computer viruses, urban legends, random humor, long lost buddies' phone numbers, etc. etc. - THINK carefully before you write. Ask yourself if your post will be relevant to everyone. If you have to wonder about that, DON'T send it. - Remember that your post will be included for posterity in an archive that is growing in size at an extraordinary rate. Try to be concise and terse in your posts. Avoid overly wordy and lengthy posts and responses. - Keep your signature brief. Please include your name, email address, aircraft type/tail number, and geographic location. A short line about where you are in the building process is also nice. Avoid bulky signatures with character graphics; they consume unnecessary space in the archive. - DON'T post requests to the List for information when that info is easily obtainable from other widely available sources. Consult the web page or FAQ first. - If you want to respond to a post, DO keep the "Subject:" line of your response the same as that of the original post. This makes it easy to find threads in the archive. - When responding, NEVER quote the *entire* original post in your response. DO use lines from the original post to help "tune in" the reader to the topic at hand, but be selective. The impact that quoting the entire original post has on the size of the archive can not be overstated! - When the poster asks you to respond to him/her personally, DO NOT then go ahead and reply to the List. Be aware that clicking the "reply" button on your mail package does not necessarily send your response to the original poster. You might have to actively address your response with the original poster's email address. - DO NOT use the List to respond to a post unless you have something to add that is relevant and has a broad appeal. "Way to go!", "I agree", and "Congratulations" are all responses that are better sent to the original poster directly, rather than to the List at large. - When responding to others' posts, avoid the feeling that you need to comment on every last point in their posts, unless you can truly contribute something valuable. - Feel free to disagree with other viewpoints, BUT keep your tone polite and respectful. Don't make snide comments, personally attack other listers, or take the moral high ground on an obviously controversial issue. This will only cause a pointless debate that will hurt feelings, waste bandwidth and resolve nothing. - Occassional posts by vendors or individuals who are regularyly subscribed to a given List are considered acceptable. Posts by List members promoting their respective products or items for sale should be of a friendly, informal nature, and should not resemble a typical SPAM message. The List isn't about commercialism, but is about sharing information and knowledge. This applies to everyone, including those who provide products to the entire community. Informal presentation and moderation should be the operatives with respect to advertising on the Lists. ------- [This is an automated posting.] do not archive


    Message 11


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    Time: 11:03:08 PM PST US
    From: Matt Dralle <dralle@matronics.com>
    Subject: Official Commander-List Usage Guidelines
    Dear Listers, Please read over the Commander-List Usage Guidelines below. The complete Commander-List FAQ including these Usage Guidelines can be found at the following URL: http://www.matronics.com/FAQs/Commander-List.FAQ.html Thank you, Matt Dralle Matronics Email List Administrator ****************************************************************************** Commander-List Usage Guidelines ****************************************************************************** The following details the official Usage Guidelines for the Commander-List. You are encouraged to read it carefully, and to abide by the rules therein. Failure to use the Commander-List in the manner described below may result in the removal of the subscribers from the List. Commander-List Policy Statement The purpose of the Commander-List is to provide a forum of discussion for things related to this particular discussion group. The List's goals are to serve as an information resource to its members; to deliver high-quality content; to provide moral support; to foster camaraderie among its members; and to support safe operation. Reaching these goals requires the participation and cooperation of each and every member of the List. To this end, the following guidelines have been established: - Please keep all posts related to the List at some level. Do not submit posts concerning computer viruses, urban legends, random humor, long lost buddies' phone numbers, etc. etc. - THINK carefully before you write. Ask yourself if your post will be relevant to everyone. If you have to wonder about that, DON'T send it. - Remember that your post will be included for posterity in an archive that is growing in size at an extraordinary rate. Try to be concise and terse in your posts. Avoid overly wordy and lengthy posts and responses. - Keep your signature brief. Please include your name, email address, aircraft type/tail number, and geographic location. A short line about where you are in the building process is also nice. Avoid bulky signatures with character graphics; they consume unnecessary space in the archive. - DON'T post requests to the List for information when that info is easily obtainable from other widely available sources. Consult the web page or FAQ first. - If you want to respond to a post, DO keep the "Subject:" line of your response the same as that of the original post. This makes it easy to find threads in the archive. - When responding, NEVER quote the *entire* original post in your response. DO use lines from the original post to help "tune in" the reader to the topic at hand, but be selective. The impact that quoting the entire original post has on the size of the archive can not be overstated! - When the poster asks you to respond to him/her personally, DO NOT then go ahead and reply to the List. Be aware that clicking the "reply" button on your mail package does not necessarily send your response to the original poster. You might have to actively address your response with the original poster's email address. - DO NOT use the List to respond to a post unless you have something to add that is relevant and has a broad appeal. "Way to go!", "I agree", and "Congratulations" are all responses that are better sent to the original poster directly, rather than to the List at large. - When responding to others' posts, avoid the feeling that you need to comment on every last point in their posts, unless you can truly contribute something valuable. - Feel free to disagree with other viewpoints, BUT keep your tone polite and respectful. Don't make snide comments, personally attack other listers, or take the moral high ground on an obviously controversial issue. This will only cause a pointless debate that will hurt feelings, waste bandwidth and resolve nothing. - Occassional posts by vendors or individuals who are regularyly subscribed to a given List are considered acceptable. Posts by List members promoting their respective products or items for sale should be of a friendly, informal nature, and should not resemble a typical SPAM message. The List isn't about commercialism, but is about sharing information and knowledge. This applies to everyone, including those who provide products to the entire community. Informal presentation and moderation should be the operatives with respect to advertising on the Lists. ------- [This is an automated posting.] do not archive


    Message 12


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    Time: 11:26:16 PM PST US
    From: "Don" <dongirod@bellsouth.net>
    Subject: Re: Pressure Carburetor?
    Good Evening Bob; I flew the Connie on the Shuttle Backup out of DCA, and yes it does sound familiar. But that was a long, long time ago,(67) I was in the last class of Connie engineers. I have all three ratings of F/E which with about $ 5 will get you a cup of coffee at most Starbucks. I only slid off the wings ( 14 ft.) twice in the winter snow, now it would break my leg, then it just 'stung' like crazy. I remember we were always happy to get a G as it had gas heaters and we could pre heat the cabin. I was so happy to get out of the wing walking to check the fuel and climbing out on the engine to check the oil, times sure have changed. But your procedures sound familiar, how do you remember all this stuff? My hard drive gets full, and when I left an aircraft, I tried to forget it so I could remember the new aircraft and not get them confused. As to the 25% it is probably just a figure that some one once told me, hanger talk, might be true at one particular power setting, might be false, not sure. I always figured that was part of the reason aircraft engines were not very efficient in a power verses specific fuel consumption. Now that aught to start another discussion! Don ----- Original Message ----- From: BobsV35B@aol.com To: commander-list@matronics.com Sent: Tuesday, October 02, 2007 1:27 AM Subject: Re: Commander-List: Re: Pressure Carburetor? Good Evening Don, I have never heard that particular number and I believe we would have to better define the terms before we could either disagree or agree with that 25% assertion. As to where does leaning cause additional wear, that is another tough one. Running any engine too lean at high powers will cause big troubles. However running one leaner than optimum at low powers will not hurt it all, but it will burn more fuel per horsepower developed than is possible when the engine is run so as to attain optimum BSFC (Brake Specific Fuel Consumption). I do not know the number used by your airline to lean the Turbo Compound R-3350, but most users utilized a ten percent BMEP drop from the peak BMEP. The procedure used by my airline was as follows. We would first chose a desired BMEP number from the power charts. Just for kicks, let's say that the desired cruise BMEP was 254. We would start out with the mixture in Auto Rich. The mixture would be slowly leaned until the BMEP started to rise. When it went above 254, we would throttle back until it was at 254, then continue to lean until it was steady at 254 and where any further leaning would take the BMEP reading below 254. That procedure determined the peak BMEP (Peak power) for the manifold pressure being used. At that time, we would continue leaning the engine until the BMEP was reading 254 minus 24.5 or approximately 228 BMEP. Once that spot ten percent leaner than peak power was found, the throttle was used to add manifold pressure so as to bring the BMEP back to the desired cruise power. We then checked the manifold pressure to be sure we were still below the maximum allowed manifold pressure for the desired cruise power. Sound familiar? If we leaned the engine further, it would just lose power, but no harm was done. However, if we richened it up a bit, the engine would overheat and it may even go into mild detonation. It needed to be well lean of peak power to cool properly. I don't know if you recall, but there is a shaft on the rear of the engine which connects the two fuel injection controllers together. One unit is for the front row and the other feeds the rear. That shaft would occasionally slip. When that happened, one row would be running substantially leaner than the other. The one that was getting more fuel would be carrying more of the load that was being developed by the engine. That row would burn the valves and sometimes even have holes burned in the pistons while the row which was not getting enough fuel would be running clean and comfortable. The place where any engine is most likely to develop engine problems are when the mixture is at that point where the peak BMEP or peak engine power is being developed. If the engine is run at that same power with a richer than needed fuel mixture, the extra fuel will slow down the rate of burn and move the point of peak combustion pressure to a point where the engine is able to operate relatively cool. That function is what is normally referred to as cooling the engine with fuel and it is how we kept our cool during takeoff and climb regimes! Another way to cool the engine is to cool it with additional combustion air. That is what happens when the engine is run well lean of best power. (Note that I said best power, not Peak EGT. They do NOT occur at the same point) When we leaned that nice big R-3350 ten percent lean of best power, we were running at a mixture that was well lean of the best power point and the engine was being cooled by that surplus combustion air. Normal cruise power for the 3350 was around 55 to 60 percent of rated power. We were really running it quite conservatively. If we richened it without reducing the manifold pressure, we defeated the air cooling effect and it would overheat and cause all sorts of problems. Leaner is cleaner and leaner is cooler. Cleaner and cooler is generally considered to be better, is it not? So, if you want to extend engine life, run it at relatively low power settings and run the mixture on the lean side of best power! Happy Skies, Old Bob AKA Bob Siegfried Ancient Aviator Stearman N3977A Brookeridge Air Park LL22 Downers Grove, IL 60516 630 985-8503 In a message dated 10/1/2007 7:35:20 P.M. Central Daylight Time, dongirod@bellsouth.net writes: Bob; I used to sit sideways in a Connie running R-3360 Turbo compound engines, but its been a long time. My question is this, since you remember more about those things, I recall being told some where that aircraft engines use approximately 25% of their fuel for cooling. At what point in leaning do we get to where we save fuel, but shorten the engine life? And where is the crossover point. Thanks, Don ------------------------------------------------------------------------- ----- See what's new at AOL.com and Make AOL Your Homepage. ------------------------------------------------------------------------- ----- 10/1/2007 6:59 PM




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