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#1 (permalink) |
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HEXUS.timelord.
Join Date: Jul 2003
Location: In Sunny England
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Radial and Rotary engines
Check these out
![]() RADIAL....the cylinders dont spin..the pistons push the central off-set axle around.... ![]() http://www.aviation-history.com/engines/radial.htm ROTARY.....it ALL SPINS!!!!! Unreal.....all of it goes round and the prop is bolted to it! Can YOU spell inertia and can you spell torque twist ?![]() http://www.aviation-history.com/engi...ary-theory.htm My mind was BLOWN
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#2 (permalink) |
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Muttonheaded
Join Date: Jul 2003
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#4 (permalink) |
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HEXUS.timelord.
Join Date: Jul 2003
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First thing I thought to ask the old boy who we were talking to, was how the hell do ya keep the oil in the engine? Its fed into the centre and the spinning engine makes it slide up the bores ! And I have to tell ya.....these things have NO EXHAUST PIPE!!! You can see the top of the cylinder, and the back of the valve is exposed and when the push rod opens the exhaust valve it vents striaght out.....no manifold at all......and its spinning! Mind boggling! |
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#5 (permalink) |
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No more Mr Nice Guy.
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That old boy also told us how it was a loss oil system. There's no sump, so the oil is kept in a tank and drip fed into the center of the engine. He said that most planes with rotary engines had a valve and flow rate guage so you could control how much oil went in...
Imagine having to force land becuase you'd not run out of fuel but of oil!!! Another thought that struck was planes with rotary engines must have been damn easy to shoot down. A few good shots into the engine, unbalance the thing and it'd just shake itself apart. The guy also reckoned that the rotary engined was only designed to solve to the cooling problem. I reckon he's right too. Their fiendishly complex and tricky to manufacture compared with a radial engine, they don't have any power improvements, but they do mean you could completely cowl the thing to improve aerodynamics and therefore performance. ps. Zak, on the radial, the central axle isn't offset, the big end for the pistons is. (I know its not really a big end, but I mean the thingy which all the pistons are joined to in the middle). |
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#7 (permalink) |
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No more Mr Nice Guy.
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According to all the guys we spoke to, it was essentially just cooling... there were no power improvements and the engine was far more complex. But it did mean you could hae a more aerodynamic plane as the engine could be completely cowled in. The Ju-52 is a good example of a radial engine cooling solution, no cowl at all... the drag on all those cylinders is massive.
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#8 (permalink) |
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Guest
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Seems like both configurations have there downsides, either drag from the cylinder heads being out in the draft for cooling or inertia.
Suprised anyone really used it when there were plenty of inline engines around. |
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#9 (permalink) |
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HEXUS.timelord.
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The radial might be very "draggy" but if I was making my first ever plane and had no idea how to do it, cos it was a first ever, BUT had a choice of power plants, the radial would be my first attempt. It justs BOLTS onto the front.....doesn't need to be "integrated" into the nose, just bolted on ![]() Well, thats a basic version of the truth, BUT it does work like that kind-of! |
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#10 (permalink) |
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Guess from an engineers point of view sticking it on the front makes sense, rather than having a long the fuselage.
Until someone had the idea of putting jets under the wings
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#11 (permalink) |
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HEXUS.timelord.
Join Date: Jul 2003
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Hey....a P39 has the engine BEHIND the pilot and a drive shaft running under his bum, with a canon firing THROUGH the centre of the axle.....so they go in all sorts of places.
BUT, when it boils down to it, when aviation was new, cooling was essential, as was easy maintenance, and the power is really quite good for the era
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