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From what I understand, the low power to weight ratio of diesel
engines has been the main limiting factor for their adoption into small planes (and passenger cars for that matter). The reason for the high weight as it was explained to me was that the high compression used for an auto-ignition type engine required strong, and thus heavy castings to withstand the pressures. So these days you see diesels fitted with forced induction systems, which apparently makes them more peppy (e.g. the 90hp VW 1.9L TDI). But doesn't this more powerful charge being introduced by the forced induction system, just require again, a heavier engine to withstand the more powerful explosion? Or to put in in converse, if the same engine could have withstood the more powerful charge, couldn't they have built it lighter in the first place and used a conventional induction system? For now lets ignore the altitude power normalization aspect for aircraft operation. |
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So these days you see diesels fitted with forced induction systems,
which apparently makes them more peppy (e.g. the 90hp VW 1.9L TDI). Check out the RPMs at which the various diesel engines develop their power (I don't have any numbers in front of me, so I'll let you do the web search). That's part of the answer. Ed Wischmeyer |
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Jay wrote:
From what I understand, the low power to weight ratio of diesel engines has been the main limiting factor for their adoption into small planes (and passenger cars for that matter). The reason for the high weight as it was explained to me was that the high compression used for an auto-ignition type engine required strong, and thus heavy castings to withstand the pressures. So these days you see diesels fitted with forced induction systems, which apparently makes them more peppy (e.g. the 90hp VW 1.9L TDI). But doesn't this more powerful charge being introduced by the forced induction system, just require again, a heavier engine to withstand the more powerful explosion? Or to put in in converse, if the same engine could have withstood the more powerful charge, couldn't they have built it lighter in the first place and used a conventional induction system? For now lets ignore the altitude power normalization aspect for aircraft operation. Having spent years behind the big wheels, power to weight is probably on the bottom of my list for not having a diesel in a small vehicle of any type. Your burning kerosene there, so the pistons have to take their time to give those long carbon chains time to burn down. The engines I sat on top of usually ran between 1800 and 2100 RPM, were slow to rev up, and shook like a crack whore. Anything that shook like that would tear an airplane apart, and would be very uncomfortable in a passenger car. -- http://www.ernest.isa-geek.org/ "Ignorance is mankinds normal state, alleviated by information and experience." Veeduber |
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Ernest Christley wrote in news:TLtAb.79227
: Having spent years behind the big wheels, power to weight is probably on the bottom of my list for not having a diesel in a small vehicle of any type. We're getting way off-topic for this group, but if you're at all interested, test-drive a VW (Golf, Jetta, Bettle) TDI some time. Not rockets by any means, but they're reasonably peppy. At idle, you can tell it's a diesel, but when it's moving, it's quieter than the gas engine (due to lower revs). I'd think it's a bad candidate for aircraft use because of power/weight, but it's great for a car (which is why I drive one). |
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