| Subject: Rotary engine vs piston engine efficiency. BSFC's |
| From: Paul |
| Date: 10/12/1999, 1:35 PM |
| To: zz |
X-Mozilla-Keys:
Z wrote:Not to say that I disagree, but I think that isdefinitely an open question. There aretwo pieces to the overall efficiency equation,first, combustion efficiency, (efficiencyof converting chemical potential energy to heat),second, thermodynamic efficiency(efficiency of converting heat energy tomechanical work).There is no question that rotary engines willnever equal reciprocating engines inthe realm of combustion efficiency, for thereasons others have already stated.However, it is important to remember that thethermodynamic efficiency of the rotaryengine cycle is considerably better than that ofthe piston engine cycle. This was oneof the things which helped spur interest in therotary engine in the first place. Withproperly timed intake and exhaust (allowing fullextraction of the available heat energyduring the expansion phase), the greaterthermodynamic efficiency of the conventionalrotary cycle is more than capable of offsettingthe lower combustion efficiency.If you go beyond this and start talking aboutusing the intake air itself to coolthe rotors and rotor housings, the achievableoverall efficiency of the rotaryconfiguration in fact considerably exceeds thatwhich can be realized in a pistonengine, a fact which the Moeller rotary hasalready demonstrated.
The problem of Wankel bsfc is not combustion efficiency otherwise the emissions would be painfully off scale, The wankel is not a higher efficiency cycle - since it is not a cycle but another way of mechanically implementing the same OTTO cycle as the piston engine so cycle thermal efficiency is tied into the same relationship to expansion( compression) ratio in both cases differing only in heat losses due to the high ratio of combustion chamber surface to volume ratio. The heat lost to the coolant at this point of the cycle is most costly to efficiency. The high exhaust temp is a lot due to the fact of the direct port rather than the cooling of this charge thru the exhaust valve and port of the piston engine - (which is not lost energy to the basic cycle -but. to the next recovery mechanism the turbo) The late burning attributed to the Diesel cycle is a loss of thermal efficiency, which in real operation is compensated by the increased expansion ratio from the high compression ratio associated with the Diesel operation. A somewhat related thought - M. Zoeche complaining about the spark ignited "Diesel" Wankel is that compression ignition is not a part of the theoretical cycle at all - Also - does spark ignition of the heavy fuel with Diesel type direct injection timing negate the meed for "octane"? Vance The Aircraft Rotary Engine Newsletter. Powered by Linux. http://home.earthlink.net/~rotaryeng/ http://www.linux.org