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![]() "Capt. Geoffrey Thorpe" The Sea Hawk At Wow Way D0t C0m wrote in message news:N6adnXfOAtwpgHXanZ2dnUVZ_sWdnZ2d@wideopenwest .com... "Dale Scroggins" wrote in message ... ... 1. Most diesels wear more slowly than gas engines. The fuel is a better lubricant than gasoline is, and the combustion products are a bit more benign. Except, of course, for the particulates. Particulates are hell on bearings, and lungs, and... NOx tends to run higher and isn't usually clasified as "benign" The specific comparison I had in mind was a current-production piston aircraft engine burning 100LL, compared to a current-production automotive diesel engine. Given a choice of the lead compounds that collect within and are emitted by the gasser, and the low levels of particulates deposited and emitted by a current-production automotive diesel, I'd prefer the particulates. As to oxides of nitrogen, given that current production gas aviation engines run with advanced ignition timing, have no EGR, and operate at elevated EGT most of the time, I doubt a current production auto diesel would produce more NOx, and would likely produce less. I'm open to numbers, if you have them. Again, my comparison was between current diesels and current gas aircraft engines, not current automotive gas engines. 5. Automatic mixture control. "mixture control is irrelevent" would be a more accurate statement. For a turbodiesel, "automatic mixture control" is a more accurate statement. Mixture control is quite relevent, and automatically managed. 7. Lower fire risks. Not really. Hmm. So the dozens of induction fires (some of which caused substantial damage) that I've witnessed over the years are just as likely with a diesel engine? And all the extra precautions we followed over the years when fueling and defueling avgas (or mogas), compared to jetA, were a waste of time? 10. Props are more efficient at lower RPMs, usually. Diesels have torque to turn props slow in cruise, like a turboprop (1800-1900 RPM), giving maybe another 5% efficiency gain, and a quieter cabin to boot. Depends on how the engine was designed, not how the fuel is ignited. Hmm again. So the burn characteristics of the fuel, the ability to inject additional fuel after initiation of combustion, and the surplus of available oxygen have no impact on engine torque curves? Given time, I can think of more. Please note that gas engines were abandoned decades, nay, scores of years ago in other transportation sectors. It will be the same in aviation if the weight difference shrinks enough. Well, there's the problem, isn't it. Making a light weight diesel that will last. Note: I'm not suggesting that diesels are a bad idea - they do have there advantages. But, let's not over sell... Wasn't the prospect of a relatively light weight diesel available to homebuilders the point of this thread? No one knows if Subaru's diesel will match the durability of a current-production avgas engine. However, newer diesel injection methods have helped reduce internal engine forces, so durable, light diesel engines are on the horizon. What do you see as the advantages of diesel aircraft engines? DS |
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"Dale Scroggins" wrote in message
... "Capt. Geoffrey Thorpe" The Sea Hawk At Wow Way D0t C0m wrote in message news:N6adnXfOAtwpgHXanZ2dnUVZ_sWdnZ2d@wideopenwest .com... ... Hmm. So the dozens of induction fires (some of which caused substantial damage) that I've witnessed over the years are just as likely with a diesel engine? Probably not, since there is no fuel in the induction system. 10. Props are more efficient at lower RPMs, usually. Diesels have torque to turn props slow in cruise, like a turboprop (1800-1900 RPM), giving maybe another 5% efficiency gain, and a quieter cabin to boot. Depends on how the engine was designed, not how the fuel is ignited. Hmm again. So the burn characteristics of the fuel, the ability to inject additional fuel after initiation of combustion, and the surplus of available oxygen have no impact on engine torque curves? On the contrary. The inabilty to mix the fuel with the air is the reason that typical diesel torque curves flatten out at low speeds - a gas engine can better use the air and generates more torque at the higher speeds. So the TENDANCY is to select bore/stroke ratio's and displacements that favor lower speeds in diesels. But there are lots of exceptions. .. Wasn't the prospect of a relatively light weight diesel available to homebuilders the point of this thread? No one knows if Subaru's diesel will match the durability of a current-production avgas engine. However, newer diesel injection methods have helped reduce internal engine forces, so durable, light diesel engines are on the horizon. What do you see as the advantages of diesel aircraft engines? Primary advantage is fuel consumption - higher compression, lower pumping losses (minor benifit for aircraft) and reduced heat loss due to the stratified nature of the combustion all help to improve efficiency. Increased fuel density also gives a boost to "miles per gallon" - but for aircraft it's about "miles per pound". Primary disadvantage is power to weight. Diesels are typically smoke limited - they can't use all the air, so the power is limited - that's why turbos are so popular on diesels. The higher combustion pressures also require a heavier block and a heavier bottom end which, well, being heavier, adds weight. Secondary advantage is no ignition system. Secondary disadvantage is a somewhat fussy fuel system (and, with a common rail system, you are just as reliant on electricity as an electronic fuel injected gas engine). Probably less of a problem for aircraft use when compared to small marine applications - do a search on "fuel polishing"... FWIW - look for the press propaganda on Ford's "Eco-Boost" - turbo charged, direct injection, spark ignited gas - looks like they are shooting to get closer to diesel fuel economy without the cost (diesel aftertreatment is REAL expensive at the lower emission standards). Improving power to weight lets them downsize the engine, down size vehicle componants, etc. Of course, one could say that direct injection gasoline has all the disadvantages of both gasoline and diesel engines. ;-) -- Geoff The Sea Hawk at Wow Way d0t Com remove spaces and make the obvious substitutions to reply by mail When immigration is outlawed, only outlaws will immigrate. |
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"Capt. Geoffrey Thorpe" The Sea Hawk At Wow Way D0t C0m wrote in message
... "Dale Scroggins" wrote in message ... "Capt. Geoffrey Thorpe" The Sea Hawk At Wow Way D0t C0m wrote in message news:N6adnXfOAtwpgHXanZ2dnUVZ_sWdnZ2d@wideopenwest .com... ... ... What do you see as the advantages of diesel aircraft engines? Primary advantage is fuel consumption - higher compression, lower pumping losses (minor benifit for aircraft) and reduced heat loss due to the stratified nature of the combustion all help to improve efficiency. Increased fuel density also gives a boost to "miles per gallon" - but for aircraft it's about "miles per pound". Oh, I forgot, they can run on Jet fuel if the injector pump will tolerate it... On the downside, diesel fuel is good for growing algae, dunno about jet fuel - but given the number of hanger queens at the typical airport, I assume we will find out when diesels make a dent in the aircraft market. -- Geoff The Sea Hawk at Wow Way d0t Com remove spaces and make the obvious substitutions to reply by mail When immigration is outlawed, only outlaws will immigrate. |
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![]() "Capt. Geoffrey Thorpe" The Sea Hawk At Wow Way D0t C0m wrote in message news:mLWdneP7Q9QVCXTanZ2dnUVZ_sqinZ2d@wideopenwest .com... Primary advantage is fuel consumption - higher compression, lower pumping losses (minor benifit for aircraft) and reduced heat loss due to the stratified nature of the combustion all help to improve efficiency. Increased fuel density also gives a boost to "miles per gallon" - but for aircraft it's about "miles per pound". Oh, I forgot, they can run on Jet fuel if the injector pump will tolerate it... AFAIK, the newly demanded ultra low sulphur diesel fuel is nasty stuff for the pumps, because the hurriedly implemented refining process also strips lubricants from the fuel. I have no idea whether this will be a continuing problem or whether other processes maintain the lubricity of the fuel. On the downside, diesel fuel is good for growing algae, dunno about jet fuel - but given the number of hanger queens at the typical airport, I assume we will find out when diesels make a dent in the aircraft market. I don't know about the kerosene based jet fuel sold here in the U.S., but some of the foreign stuff is (or at least was) a feeding ground for micro-organisms. The Eastern Airlines L-1011 that went down in the Florida Everglades some years ago was apparently full of the stuff after having been previously refuelled in Israel. BTW, I'm glad someone remembers what a hangar queen is. ;-)) Peter |
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