ackattacker
Client 9
- Joined
- Nov 14, 2004
- Posts
- 2,125
This is not an issue I have debated. Any engine which is not suitable for the intended installation is just that, not suitable. If your intended use cannot tolerate the weight of a 4-stroke engine then your powerplant decision is an easy one. I was addressing your claim that a 2-stroke engine extracts more *power* from *fuel*, otherwise known as "fuel efficiency".avbug said:As the issue is a small engine in an ultralight aircraft, all the numbers don't really mean squat...the point is mute. Efficiency is being able to power an aircraft in this case with a very light engine. You could probably make it happen with a really big engine, heavier structure, carry more fuel, blah, blah, blah...but that would make it...less efficient. Get it?
I would propose that what you are calling efficiency is more akin to "suitability". A 2-stroke may very well be a more suitable engine for certain ultralights. Other ultralights may be designed so that a 4-stroke is equally or more suitable.avbug said:Efficient is what is light enough to fit in that aircraft and deliver the power required.
I'm scratching my head on this one, as I'm not sure what you're getting at. In a constant speed propeller installation, power is torque and torque is power, since RPM is constant. Tell me the RPM and torque on your propeller and I'll tell you the HP of your engine. Tell me the HP your engine is producing and propeller RPM and I'll tell you the torque. I don't need to know the blade angle, airspeed, angle of attack or any of that. It doesn't make any difference if it's 2-stroke, 4-stroke, or turbine - power is power, and power = torque x rpm.avbug said:As for your comments regarding engine RPM and torque, they do not apply, except in a fixed pitch installation for comparitive purposes. Torque becomes an issue in a constant speed, or variable pitch application, which is inclusive of some ultralightor light airplanes utilizing two stroke engines with flexible propellers, or adjustable propellers. As pitch is increased on a propeller (as it is moved toward coarse), more torque is required to generate the same RPM for any given airspeed...torque is more than merely propeller RPM. It must consider propeller loading, which includes other factors such as blade angle and angle of attack, which in flight may be considered a function of pitch and airspeed, among other things.
You are correct that more torque is required to maintain RPM as pitch increases. But that's the same thing as saying more power is required to maintain RPM as pitch increases. It's one and the same. It takes more power to turn a coarser propeller because a coarser propeller is doing more work. In a constant speed application of course the cause/effect is reversed. Adding more power causes the propeller to coarsen, not the other way around.
The point I am driving at is that a 100 hp 2-stroke engine and a 100 hp 4-stroke engine hooked up to indentical constant speed propellers will behave exactly identically and at all airspeeds. They are both inputing to the propeller the same torque and at the same rpm, the propeller can't tell the difference.
This is all correct... but I would propose that the "point of diminishing return" for overall fuel efficiency is a very light aircraft indeed.avbug said:Clearly there's more to the topic. Fact is that for the same size (eg mass, or weight), a two stroke can put out more power, particularly with regard to small light aircooled airplane engines. A heavier four stroke engine will be required to put out more power to sustain the same flight condition, because the aircraft is heavier. In so doing, any comparitive difference in fuel efficiency is lost...the point of diminishing returns has been reached, and one may well find that one burns less fuel with the two stroke as less fuel is required to accomplish the same thing for a given parameter...time, speed, distance, etc.
Exactly what the numbers are will of course, vary with the aircraft and flight conditions (eg, density altitude, operating weight, etc).
Two strokes are cheaper to operate, cheaper to overhaul, cheaper to purchase, lighter, put out more power per pound than compartive four stroke engines of the same mass, are much more simple in construction, more tolerant of change in operation, and in many cases, ideally suited for the light aircraft they power. Getting into the lighter aircraft, a 1/2 vw still can't compete with a typical Hirth or Rotax...and even if you could wrap it up enough to produce the same power, it would be burning considerably more fuel and would have become...you guessed it...less efficient. Including fuel efficient.