Jan said, as do I, that the internal radii in the transfer ducts should be as large
as possible. In the RSA cylinders the available duct length was used to the max. Lengthening the transfer ducts any further which would have nullified the effect of the larger radii.
Yes, the transfer flow would also be reluctant to stop, but the piston would not give a damn and slam the transfer ports shut regardlessly. That would create a pressure rise in the transfer ducts, but that pressure rise would not wait around till the next transfer opening; it would spread over the crankcase volume. So no compensation for the reluctant initial mass flow into the cylinder and on top of this a higher crankcase pressure after transfer closing, which would hurt the next induction phase.
Fair enough...How about a couple of chambers, mounted off each side of the cylinder at transfer height, short direct ducts to the A, C & D ports. Each chamber has a reed valve fed by a large (enough) passage from the case through holes cut into the bottom of the main B transfer duct. Piston ported to the case and the B transfer, reed valved to the rest
Re the silicon oven mitts: they don't come in engine sizes, but you might use this thermal insulation paint, developed for the Russian space program and liberated by my friend Martijn Stehouwer of Emot Racing (
www.emot.nl). Martijn became twice European classic 50 cc champion using the stuff.
Attachment 331570
Martijn's Site looks great, some really nice gear. Looks like he's not selling the Russian Rocket paint. Pity 'cos it would be perfect for my Ram Jet cooling & propulsion system.
The only flaw with that system is we don't get the thrust until we're already travelling pretty quickly. Needs some fans and stuff to complicate it.
Here's a link to a interesting analysis of an 'oddballish' engine. A Two stroke, compound, uniflow helicopter engine that's as light and powerful and 31% more fuel efficient than the standard turbo jet. http://dtic.mil/dtic/tr/fulltext/u2/a180007.pdf Another great idea that didn't get of the ground. A cynic might think that Rolls Royce & Honeywell could afford more Generals & Senators than the Garrett Turbo Co.
Remember the hinged 'comma' roofs in the transfer ducts that we discussed two years ago? That didn't happen either as you came up with your sliding cylinder solution whilst I got stuck with the problem of how to operate those commas. Now I think that rubber bladders could have been a solution. Keep thinking outside the box Neil
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