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#11
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![]() Ian Mitchell wrote: Snip "relevent fact" Don't confuse the issue with facts, they don't want to change an earnestly held pre-concieved notion. Ian Maybe, so. I don't get very excited about ugly airplanes... Now a Pulsar with wing mounted twin 582's? I'm fool enough to think that'd be sweet. Richard |
#12
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("Morgans" wrote)
First of all, let me say, "you are really cruel." [snip] You just love throwing salt into open wounds, dont't you? Shame on you! I had to hurry up, before that sucker closed up! g http://home.att.net/~dannysoar/BelGeddes.htm Rotax, Rotax, Rotax, Rotax, Rotax, Rotax, Rotax, Rotax, Rotax, Rotax... Montblack-hearted-fiend, er, I mean, um ...friend. Me friend. |
#13
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.. The problem with conventional 4 stroke
aircraft engines has been weight, and the need to put them into a bigger heavier airframe. I'm very encouraged by the developement of engines like the HKS and Warner, as they appear to offer a nice blend of light weight/power/reliability. Ian Published performance specs for the HKS: 56HP @5800RPM 4.2gph/.45bsfc. This will require a volumetric efficiency of 110%. Not bad for an engine running at 75% throttle. In fact, not very likely. Published performance specs for the Verner: 63HP(75%) @3750RPM. 2.7gph/.25bsfc Much more reasonable 55% volumetric efficiency with 75% power, but absolutely astonishing fuel efficiency. In fact, not very likely fuel efficiency. Both engines achieve their light weight by running at high rpm with small displacement, and by using Nikasil aluminum cylinders. Which is to say, they are race car engines. Would you rather have a C-85 with 2000 hours TT or a Verner with 600 hours TT? Or a 2 stroke with cast iron cylinders? I would appreciate it if someone would check my numbers and see if they come up with similar results. -- John Kimmel remove x "He's dead, Jim." |
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