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On 6 Mar, 11:03, bod43 wrote:
On 5 Mar, 21:57, "Morgans" wrote: snip interesting stuff Maybe someone on uk.rec.motorcycles might have an idea as to the expected life span of a hyabusa engine when operated in a constant load regime, say at 130bhp. You'd need to boost the low and midrange torque to swing a prop, as props rotate relatively slowly, don't they? I think a 'Busa engine would last forever is detuned to 130bhp. A Gold Wing 1500 or 1800 lump might be more suitable, IMHO. |
#2
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Using the patented Mavis Beacon "Hunt&Peck" Technique, "TOG@Toil"
typed On 6 Mar, 11:03, bod43 wrote: On 5 Mar, 21:57, "Morgans" wrote: snip interesting stuff Maybe someone on uk.rec.motorcycles might have an idea as to the expected life span of a hyabusa engine when operated in a constant load regime, say at 130bhp. You'd need to boost the low and midrange torque to swing a prop, as props rotate relatively slowly, don't they? I think a 'Busa engine would last forever is detuned to 130bhp. Depends on the prop, but I would think that gearing down would be the way to go. -- Wicked Uncle Nigel - "He's hopeless, but he's honest" It's important is that last ell. |
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Wicked Uncle Nigel wrote:
Using the patented Mavis Beacon "Hunt&Peck" Technique, "TOG@Toil" typed On 6 Mar, 11:03, bod43 wrote: On 5 Mar, 21:57, "Morgans" wrote: snip interesting stuff Maybe someone on uk.rec.motorcycles might have an idea as to the expected life span of a hyabusa engine when operated in a constant load regime, say at 130bhp. You'd need to boost the low and midrange torque to swing a prop, as props rotate relatively slowly, don't they? I think a 'Busa engine would last forever is detuned to 130bhp. Depends on the prop, but I would think that gearing down would be the way to go. The thing that everyone seems to forget when promoting automotive engines for aircraft is that most piston aero engines have a very hard life. Take-off and climb is full power or very nearly, then they throttle back to cruise at 75% or thereabouts. The only roadgoing vehicles that approach that sort of use are in motorsports, and how long do they last? |
#4
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Wicked Uncle Nigel wrote:
You'd need to boost the low and midrange torque to swing a prop, as props rotate relatively slowly, don't they? I think a 'Busa engine would last forever is detuned to 130bhp. Depends on the prop, but I would think that gearing down would be the way to go. If you're forced to use a higher-revving engine, yes- but gearboxes or belts and cogs introduce problems of their own, which is why a relatively large displacement slow-revving engine (which doesn't need four valves/cylinder, multiple chain drive cams with cam chain tensioners, etc.) makes a lot of sense for aircraft. |
#5
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![]() "bod43" wrote in message ... I have the idea that mechanical failure of the original 4 cyl engines (or any high performance japanese bike engine) is pretty much unheard of but I am not at all sure. It matters little, because now you are making a whole new engine for a totally different application, with no track record and the distinct possibility of new and exciting failure modes. Further, the same can be said about the reiliability for most any automotive engine in its intended application, but the track record of automotive aero conversions is spotty at best. Just thinking outside the box... Since the proposed Hyabusa Flat 8 engine will need a PSRU anyhow; how about two Hyabusa engines put together into a twin-pack? The result would likely weigh a tad more than a simple flat 8, but now you have two known engines combined with twin-engine redundancy. Vaughn |
#6
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On Mar 6, 8:38*am, "vaughn" wrote:
"bod43" wrote in message ... I have the idea that mechanical failure of the original 4 cyl engines (or any high performance japanese bike engine) is pretty much unheard of but I am not at all sure. * *It matters little, because now you are making a whole new engine for a totally different application, with no track record and the distinct possibility of new and exciting failure modes. *Further, the same can be said about the reiliability for most any automotive engine in its intended application, but the track record of automotive aero conversions is spotty at best. Just thinking outside the box... *Since the proposed Hyabusa Flat 8 engine will need a PSRU anyhow; how about two Hyabusa engines put together into a twin-pack? *The result would likely weigh a tad more than a simple flat 8, but now you have two known engines combined with twin-engine redundancy. Vaughn There is little difference between the existing V8 Hyabusa and a flat 8 in terms of bottom end design. The V8 has proved bulletproof @400HP. Pretty much everything learned with the V8 Hyabusa conversion applies to a flat 8. Of course it would need to be geared - torque peak is near 8000 RPM. However, there is a weight trade off. These little screamers, which are more like turbines than tractors, can use a light crank because they use a whole lot of tiny power pulses instead of a few humongous ones to produce power. The Hyabusa is on the extreme opposite end of the power/RPM spectrum from a Lycoming. Weight savings in the crank can be shifted to the PSRU which would be a planetary gearset with maybe 5 planet gears for lots of tooth engagement and strength. The gear ratio would need to be 4 or 5:1 so spur gears or cog belts aren't the best choice since the small gear or cog would be small with too few teeth engaged. A planetary allows large ratios with lots of tooth engagement for strength. Keep in mind how the motorcycle works. The bike has a 6-speed gearbox whereas the airplane engine would have only one. The standard sport bike shift technique, approved by the factory, is to apply a large force to the shift lever and then tap the clutch lever when the rider wants to shift. This results in an instant shift with horrific transient loads suffered by the crank and drive train. An aircraft powerplant would never see this abuse. Why is a flat 8 better than a V8? Mainly a higher thrust line for prop clearance and better ballance. To do that with a V8, it would have to be inverted. |
#7
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bildan wrote:
snip Keep in mind how the motorcycle works. The bike has a 6-speed gearbox whereas the airplane engine would have only one. The standard sport bike shift technique, approved by the factory, is to apply a large force to the shift lever and then tap the clutch lever when the rider wants to shift. I don't think it is, you know. ISTBC of course. -- Catman MIB#14 SKoGA#6 TEAR#4 BOTAFOF#38 Apostle#21 COSOC#3 Tyger, Tyger Burning Bright (Remove rust to reply) 116 Giulietta 3.0l Sprint 1.7 145 2.0 Cloverleaf 156 V6 2.5 S2 Triumph Sprint ST 1050: It's blue, see. www.cuore-sportivo.co.uk |
#8
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![]() "vaughn" wrote in message ... "bod43" wrote in message ... I have the idea that mechanical failure of the original 4 cyl engines (or any high performance japanese bike engine) is pretty much unheard of but I am not at all sure. It matters little, because now you are making a whole new engine for a totally different application, with no track record and the distinct possibility of new and exciting failure modes. Further, the same can be said about the reiliability for most any automotive engine in its intended application, but the track record of automotive aero conversions is spotty at best. Just thinking outside the box... Since the proposed Hyabusa Flat 8 engine will need a PSRU anyhow; how about two Hyabusa engines put together into a twin-pack? The result would likely weigh a tad more than a simple flat 8, but now you have two known engines combined with twin-engine redundancy. Eliminate a lot of question marks with the experimental crank and rods too. |
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