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2 Stroke reliability

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imacdog

Well-known member
Joined
Mar 12, 2005
Posts
4,196
For those experienced with ultralights, what are your opinions on operating 2-stroke engines? I am looking into the possibility of a larger 2-seat ultralight-style sport plane and am wondering what the advantages and disadvantages are. Do all 2-strokes need to run on premixed oil, or do some have separate oil tanks? I am trying to decide if it would be worth the peace of mind to invest in a more expensive 4-stroke like a Rotax 912, over a Rotax 582. Thanks for any advice.
 
2-stroke engines are a blast. They're Lightweight, simple, and produce tons of power compared to your typical putt-putt 4-stroke.

Most modern 2-stroke application will use oil-injection, eliminating the need to pre-mix.

The problem though, is that they typically do not last a long, nor are as reliable as a typical 4-stroke. They also consume far more fuel/oil in a given amount of time, and therefore are more expensive to operate. Given these facts, the price of a 2-stroke engine may seem like a good deal, but once you buy a 4-stroke, you can be assured of longer engine life and reduced operating costs.

It will come down to personal preference. The only reason 2-strokes are still around is because they are lighter and more powerful than 4-strokes. This makes them ideal for snowmobiles, watercraft, and ultralights, where power/weight can be an issue. Buy a 2-stroke it you enjoy instant and plentiful power when you open the throttle. Buy a 4-stroke if you want reliability/fuel efficiency.
 
2-strokes have an annoying habit of self-destructing when run lean (siezing or burning holes in pistons). Jetting is problematic. Oil injection is problematic. Go with a 4 stroke for piece of mind...
 
Thanks, I'll keep that in mind. I fly large RC planes with 2-stroke engines with electronic ignition, and so far they have been extremely reliable. I'll start looking around at the different four-strokes, such as the Rotax and Jaribus, if I can find them. Reliability is especially important to me and I'm willing to sacrafice power-weght to have the more reliable choice.
 
ackattacker said:
2-strokes have an annoying habit of self-destructing when run lean (siezing or burning holes in pistons). Jetting is problematic. Oil injection is problematic. Go with a 4 stroke for piece of mind...

Ultralight 2-strokes, Sound like a pissed off weedwacker.
 
The two stroke offers some exceptional advantages for certain applications, such as areas in which weight is a concern in light aircraft. Reliability is a tradeoff, as is longevity...but the modern two stroke such as a Hirth is also a lot less expensive to overhaul and maintain.

Many airport rescue vehicles run two stroke; it isn't just for chain saws. The rapid acceleration and light weight is a great advantage, as is size and simplicity.

Modern alloys and metal treatment have reduced the expansion and siezing problems, as well as wear issues that plagued older two strokes.
 
Avbug is right, with respect to the weight issue. However, if you're buying an aircraft where a bit more weight isn't that much of a factor, the extra horsepower and reliability might be worth it.
I'm considering some UL 's, and I'll choose a 912 (or 912S). Why? 300 hour vs 1500 hour TBO is one reason. And while many of us might sell our ultralight after 300-500 hours, I believe the 912 UL will hold the value better. Would you rather buy a 500 hr 2-stroke, with 100 hours to go until TBO? Or a 500 hour 4-stroke with 1000 hours until TBO?
I'm not an expert, but I think if I pay the extra for the 4-stroke up front, then I'll pay less in the long run.
 
Four stroke is no gaurantee of reliability; I've had more than a few failures ranging from lifted cylinder heads to catastrauphic engine failures in four stroke engines...more engine failures behind four stroke piston engines ranging from small four cylinder powerplants to large radials, than any other type of engine. Once a two stroke starts running, it's operation is very simple and straightforward.

No oil system to fail in many. No valves to fail in many. Dirt simple carburetion, dirt simple fuel system. Increadibly simple in construction, easy to work on. No timing to worry about. Lightweight...and as far as fuel efficiency, far more efficient than a four stroke engine. For the power produced vs. fuel consumed...the two stroke walks away from the four stroke. That two stroke fires every time the piston cycles. The power response is faster, crisper, more immediate

Two strokes do have their drawbacks, to be sure, from noise to the fact that the engine doesn't burn as much of it's fuel charge...it gets more power out of it pound for pound and gets it faster, but it also spits out unburned fuel and usually oil with it...it's messier. You generally need to mix the fuel and oil when fueling.

Reliability...I've had turbine engines come unglued on me in a major way, and a turbine engine is generally considered to be more reliable than a piston engine. Perhaps, and perhaps one can dredge up hour by hour statistics to show which is more reliable, but those statistics mean exactly squat when one is looking at sagebrush and pinion rushing up beneath the wings because the powerplant has failed. It happens.

Modern lightweight two stroke powerplants sell for two reasons; they weigh very little in applications where weight is critical, and they're affordable.

Which will cost you more in the long run? When you overhaul that four stroke, you're going to be spending thousands, if not tens of thousands of dollars. When you overhaul that two stroke, even if it has a shorter TBO interval, you're going to be spending hundreds. If that. If you have money to burn and have the choice, then four stroke is a great choice...it's also got a lot more going on internally to fail. The more there is to fail, the greater the possibility some might say. You decide.
 
avbug said:
For the power produced vs. fuel consumed...the two stroke walks away from the four stroke.
I'm going to disagree with you there. 4 strokes are significantly more fuel efficient in general. I could come up with many examples.

From the wikipedia:

Two-stroke engines have several marked disadvantages that have largely precluded their use in automobiles (although there was some use, such as in historic Saabs and DKWs and until recently in several automobiles produced in the Eastern bloc, including Trabants and Wartburgs, among others) and are reducing their prevalence in the above applications. Firstly, they require much more fuel than a comparably powerful four-stroke engine due to less efficient combustion. The burning oil, and the less efficient combustion, makes their exhaust far smellier and more damaging than a four-stroke engine, thus struggling to meet current emission control laws. They are noisier, partly due to the more penetrating high-frequency buzzing and partly due to the fact that muffling them reduces engine power far more than on a four-stroke engine (high-performance two-stroke engine exhausts are tuned by determining the resonant frequency of the exhaust systems and exploiting it to top-up the fuel air charge just before the cylinder port closes). Finally, they are considered less reliable and durable than four stroke engines
 
The reference you cited applies to automotive applications, and what is automotive is not aeromotive...most of that doesn't apply to the use of a two stroke powerplant in an aircraft...and while a two stroke may consume more fuel, it puts out more power pound for pound than a comparable four stroke motor, with far less moving parts and complexity. The biggest reason we don't see them more is emissions, and that could be solved, too.

Efficiency is quantifiable by many parameters, but when speaking of efficiency, does one speak in terms of miles per gallon, gallons per hour, or one of a dozen other possible frames of reference?

The two stroke is a very efficient way of packaging a lot of power in a lightweight, simple mechanism, and consequently is a very efficient method of powering a light aircraft.
 
I'm not following you avbug. Find me an aeromotive 2-stroke which is more fuel efficient (specific fuel consumption) than it's comparable 4-stroke. (Not counting diesels).

avbug said:
and while a two stroke may consume more fuel, it puts out more power pound for pound than a comparable four stroke motor, with far less moving parts and complexity.
This I agree with. It puts out more power per pound of motor, not per pound of fuel. This may or may not represent an overall weight savings depending upon a lot of factors, mainly how far do you want to go. Reliability is also a much more complex function than simply number of parts. A modern jetliner is very reliable but is incredibly complex.

avbug said:
The biggest reason we don't see them more is emissions, and that could be solved, too.
I wasn't aware general aviation powerplants had to meet any emissions standards, other than maybe noise. A two-stroke burning regular unleaded gas is certainly less damaging to the environment than a 4-stroke burning 100LL, but that's neither here nor there.

avbug said:
Efficiency is quantifiable by many parameters, but when speaking of efficiency, does one speak in terms of miles per gallon, gallons per hour, or one of a dozen other possible frames of reference?
Normally when one is talking about an engine's fuel efficiency, one talks in terms of specific fuel consumption or SFC (lbs fuel per hour per shaft horsepower).

You previously claimed that two stroke engines were able to extract more power from a pound of fuel:

avbug said:
the engine doesn't burn as much of it's fuel charge...it gets more power out of it pound for pound
and:

avbug said:
For the power produced vs. fuel consumed...the two stroke walks away from the four stroke.
I'd just like to see you back up those two statements.
 
Faster response, more torque for the fuel burned. Not having to drive an accessory section, valve train, etc, means more power goes out the crankshaft...in a four stroke engine, a considerable amount of the power produced is used overcoming internal friction and resistance of all the components in the engine. For the same power produced, in a two stroke, more goes to the end user and not the engine, and it is therefore, more efficient.

Again, efficiency may be quantified in many ways. Specific fuel consumption is only one of them.
 
avbug said:
Faster response, more torque for the fuel burned. Not having to drive an accessory section, valve train, etc, means more power goes out the crankshaft...in a four stroke engine, a considerable amount of the power produced is used overcoming internal friction and resistance of all the components in the engine. For the same power produced, in a two stroke, more goes to the end user and not the engine, and it is therefore, more efficient.

Again, efficiency may be quantified in many ways. Specific fuel consumption is only one of them.
What measurement do you want to use? SFC is what an engineer would deal with when measuring efficiency of an engine. SFC measures power at the crank. SFC includes the loses for internal friction, so if in fact a 2-stroke was more efficient then it would have a lower SFC than a corresponding 4-stroke. But the opposite is the case.

As for "torque", a much misunderstood word, torque and power are very closely linked by a simple formula. Power = Torque x RPM. Since most aircraft 2-strokes and many small aircraft 4-strokes use a reduction gearbox, the final prop RPM's will be similar. Hence two engines with the same power rating will produce the same torque at the same prop RPM. Take a 2-stroke and a 4-stroke, both producing 100hp, both spinning an identical prop at the same speed... and they produce identical torque. One cannot claim that the 2-stroke has more torque, or is extracting more torque per pound fuel.

It is common use to refer to an engine as "torquey" if it is able to produce significant power at low RPM. In this regard 4 strokes hold the clear advantage since they don't have a pronounced power band as most 2-strokes do. Very few people would describe your typical 2-stroke as "torquey". In fact the more appropriate term is "peaky", as in having a pronounced power peak at a certain (usually high) RPM. Tuning a 2-stroke to be "torquey" at low RPM's means trading off peak horsepower (detuning, usually through means of adjusting the exhaust pipe). Many two-stroke powered aircraft owners are familiar with the problem of getting the perfect propeller pitch. Too high a pitch and the aircraft never gets into the powerband for takeoff, resulting in piss-poor takeoff performance. Give it just a little less pitch and all of a sudden the engine gets "on the pipe" and can easily overrev.

I am not trying to knock 2-strokes. They certainly have their applications in aviation. But fuel-efficiency is just not one of them. Nor is "torque". Engine acceleration gives a slight advantage to the 2-stroke, due to the lower rotating intertia, but in practice this is a small effect since the inertia of the propeller is much greater anyway.

Since you claim SFC is not representative of overall efficiency, let's examine a typical installation. I choose the Murphy Renegade as typical of a light sport-plane, on the criteria that I really like it. And it has factory performance specs for 2-stroke and 4-stroke engines.

http://murphyair.com/Product_Info/Renagade/Performance.htm

Using a 2-stroke Rotax 582 (65 hp) the aircraft has an empty weight of "420 to 500" pounds. Lets take the average, 465. Gross weight is 950 lbs, leaving 485 lbs as useful load.

Using a 4-stroke Rotax 912 (80 hp) the aircraft has an empty weight of "460 to 520" pounds. Again use the average, 490. Useful load is now 460 pounds, or 25 pounds less.

So it doesn't look good, our 4-stroke airplane is heavier. So it looks like we won't be able to carry as much. BUT, let's assume we want to fly somewhere 200 miles away. Our 2-stroke version cruises two-up at 75% power at only 72mph, while burning 4.5 gallons per hour (16 mpg). The 4-stroke version cruises two-up at 75% power at 80 mph and only burns 4 gallons per hour in cruise (20 mpg)

Leaving a 30 minute VFR reserve, The two-stroke version requires 14.75 gallons... which is .75 gallons more than it holds. So you can't take the trip at all, while the 4-stroke version only requires 12 gallons and so can make it handily, while burning 16.5 pounds LESS gas, nearly making up for the extra weight of the engine.
 
What measurement do you want to use? SFC is what an engineer would deal with when measuring efficiency of an engine.

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?

Since you claim SFC is not representative of overall efficiency, let's examine a typical installation.

I made no such claim...I did however correctly assert that efficiency may be defined in many ways.

If a finely designed four stroke engine with the inner workings of a swiss watch is too heavy for the structure in which it is targeted, then it just ain't that efficient. Period. Efficient is what is light enough to fit in that aircraft and deliver the power required.

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.

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.
 
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?
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:
Efficient is what is light enough to fit in that aircraft and deliver the power required.
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:
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.
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.

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.

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.
This is all correct... but I would propose that the "point of diminishing return" for overall fuel efficiency is a very light aircraft indeed.
 
This is all correct... but I would propose that the "point of diminishing return" for overall fuel efficiency is a very light aircraft indeed.

Which is precisely what will be using a small two stroke engine, and why this thread is in the ultralight forum.
 
avbug said:
Which is precisely what will be using a small two stroke engine, and why this thread is in the ultralight forum.

I meant so small that it would probably not be able to carry a normal sized person. Even large RC planes show better fuel economy generally with 4-strokes. Show me a design which is capable of using either a modern 2-stroke or modern 4-stroke engine of similar power, and which demonstrates better overall fuel economy with the 2-stroke engine. Use any measure of fuel efficiency you wish.

In order to reach the point of diminishing returns the increased induced drag from the increased weight must offset the improved fuel efficiency of the 4-stroke engine. Because the 4-stroke engine is significantly more efficient, you're going to need a lot of extra drag. I don't think you'll be able to come up with one (although I admit it's a theoretical possibility, if your design operates very far up the back side of the power curve).
 
Also, consider this comparison:

A 60 hp Hirth 2-stroke engine weighs 79 lbs, plus 19 lbs for gearbox, plus radiatior and coolant (about another 10 lbs) for a total of about 108 lbs. At 75% power (45 hp) it burns 3.15 gallons / hour.

A 60 hp HKS 4-stroke engine weighs 108 lbs including gearbox and electric start. Add 7 lbs for the exhaust, 6 lbs for oil tank and cooler, and 3 liters of oil (about 6 lbs) and you get a total system weight of 127 lbs. At 75% power (45 hp) it burns 2.38 gallons per hour.

So in this example the 4-stroke installation weighs 19 lbs more but burns 76% of the fuel per hour. In order for the overall aircraft efficiency to be equivalent that 19 pound weight penalty would have to cause a 25% increase in total airframe drag.

Not saying it's impossible, just not very likely...
 
Take it a step further...the weight may mean that the engine can't be mounted on the airframe at all...efficiency is entirely dependent upon perspective.
 
Does anyone else remember the "Car and Driver" contest a few years back where they were gonna give away a POS "Trabby" to the winner?

Someone from the EPA read the article and the agency prompty seized the car and crushed it. :)

I'm not joking...apparently it was imported illegally and wasn't even close to meeting US emission standards.
 
I had a german friend who owned a Trabant. One person could lift the back of the car off the ground.

He crashed it into a ditch and the car didn't have a scratch. With the plastic body, a crash either did no damage or broke the car in half. No middle ground.

A man stops his Trabant at a garage and says: "Two windscreen wipers for my Trabant". The garage owner thinks for a moment, then replies "OK, that's a fair deal".
 
Avbug,

Not withstanding small, kit-type aircraft, why does nearly every single piston-engine airplane come from the factory with 4-stroke engines?

Answer: Because they are more reliable, and more fuel-efficient.
 
avbug said:
...more engine failures behind four stroke piston engines ranging from small four cylinder powerplants to large radials, than any other type of engine.

Duh, that's because 4-strokes USED FAR MORE OFTEN than any other type of [piston] engine.
 
Not withstanding small, kit-type aircraft, why does nearly every single piston-engine airplane come from the factory with 4-stroke engines?

Think. How many certificated two-stroke engines are available for use in production aircraft? Have you any idea the cost involved in certificating an engine for production use in normal category or utility category operations with a standard airworthiness certificate?

Answer: Because they are more reliable, and more fuel-efficient.

Good guess, but no.

Duh, that's because 4-strokes USED FAR MORE OFTEN than any other type of [piston] engine

You're responding to a half-quote taken out of context, to make a point. You failed to include the entire quote, which specifically referred to my experiences with engine failures...truth is just as I correctly stated; I've experienced more engine failures on four stroke pistons, ranging from flat norizontally opposed to large radials, than any other type of powerplant...and no, I haven't used four stroke engines far more often than any other type of piston engine. If you're going to quote to make a point, either include the full quote, or ensure you keep it in context.

They also consume far more fuel/oil in a given amount of time, and therefore are more expensive to operate.

Fuel burn is the least expensive part of operating an aircraft engine. On a per hour basis, maintenance accounts for more of the overall engine operating costs than fuel and oil combined, often a lot more.

As for oil consumption...ever run a radial engine?

Given these facts, the price of a 2-stroke engine may seem like a good deal, but once you buy a 4-stroke, you can be assured of longer engine life and reduced operating costs.

You may not be assured of a longer life; there are no gaurantees. Certainly not reduce operating costs. Operation of an A65 or an 0320 is never going to be as inexpensive as operating a light two stroke, particularly when overhaul costs and maintenance costs are factored in. Not by a long shot.

Now a great deal has been made of my discussion regarding specific fuel consumption, and a lot of effort has gone into disproving my claim that two stroke engines are more fuel efficient. Problem is, I never made any such claim. Nor did I introduce specific fuel consumption. I did say pound for pount the two stroke puts out more power...I didn't say pound for pound of fuel, but pound for pound of engine weight, and that's true.

Engine efficiency is subjective, and pound for pound, dollar for dollar, and on the basis of available selection of powerplants for light aircraft, the two stroke offers more options, lower costs, and more power per pound of engine weight. In that respect, the two stroke is more efficient to the application, and certainly a more suitable choice in many cases. In many, it may be the only choice.

My project, a Sorrell Guppy, was originally run on a 18 hp cushman engine, but with a two stroke reliable hirth, I can stay within the engine weight limits and preserve the balance of the design at 50 hp. It won't cruise much faster, but certainly will climb better, and offers far more advantages than disadvantages for the application.

2-strokes have an annoying habit of self-destructing when run lean (siezing or burning holes in pistons).

So do four stroke engines, particularly with respect to detonation and mixture management. The two stroke is not necessarily any more susceptable, especially considering modern metal alloys and treatments.
 
avbug said:
Now a great deal has been made of my discussion regarding specific fuel consumption, and a lot of effort has gone into disproving my claim that two stroke engines are more fuel efficient. Problem is, I never made any such claim. Nor did I introduce specific fuel consumption. I did say pound for pount the two stroke puts out more power...I didn't say pound for pound of fuel, but pound for pound of engine weight, and that's true.
avbug said:
the engine doesn't burn as much of it's fuel charge...it gets more power out of it pound for pound
I guess I misunderstood this sentence. I assumed "it" was fuel charge. What was "it"?

avbug said:
For the power produced vs. fuel consumed...the two stroke walks away from the four stroke.
I guess I misunderstood this also. I assumed "walks away from" meant "produced more power for the fuel consumed"

avbug said:
Not having to drive an accessory section, valve train, etc, means more power goes out the crankshaft...in a four stroke engine, a considerable amount of the power produced is used overcoming internal friction and resistance of all the components in the engine. For the same power produced, in a two stroke, more goes to the end user and not the engine, and it is therefore, more efficient.
I must have misunderstood this also. You appear to be claiming that the internal friction of a 4-stroke engine makes it less efficient than the 2-stroke. I guess I was wrong.

avbug said:
Faster response, more torque for the fuel burned.
Here I thought you claimed a 2-stroke produced more torque for the fuel burned than a 4-stroke. I guess I misunderstood you there also.
 
I guess I misunderstood this sentence. I assumed "it" was fuel charge. What was "it"?

I guess you did. This happens when we don't seek clarification. Pound for pound, a two stroke engine is generally lighter than a four stroke engine, both due to the materials of construction, and the lack of all the weighty parts that go into a four stroke, such as a valve train, accessory section, etc.

While the two stroke engine disperses more unburned fuel in it's exhaust than a four stroke engine, the fact that it's lighter and the fact that it doesn't need to produce excess power to overcome it's own internal friction, and it needs to make less revoloutions per piston to accomplish the same functions (eg, power stroke is also exhaust stroke) means a smaller, lighter engine produces the same output as a larger heavier engine. Pound for pound, that small two stroke is putting out more power, and it's not wasting it on enternal needs. Less wasted energy means something is operating more efficiently.

I guess I misunderstood this also. I assumed "walks away from" meant "produced more power for the fuel consumed"

That would really depend on the power setting and opeating conditions, as I've described previously...the specific operating conditions do indeed impact the issue. The following link discusses this on a power boat, and the person making the observations notes that at wide open throttle, or full throttle, the four stroke outboard boat engine in his comparison increases in fuel economy enough to offset the cost of the diffference between the engines over a set period of operation...however, he notes that those are not real operating conditions...and under real operating conditions, the two stroke burns less fuel per hour with the same miles per gallon, on the same boat under the same conditions.

http://continuouswave.com/ubb/Forum4/HTML/001019.html

http://continuouswave.com/ubb/Forum4/HTML/001078.html

Bearing in mind that we're talking about small engines, the discussions and arguements become skewed and very greyed when we move into larger engines. Large power equipment, trains, power stations, large generators, cruise ships, rapid response fire engines, etc, use two stroke engines, for good reasons. In many cases, these engines are turbocharged, and may also have valves. However, they still only make one revoloution per piston cycle, and still put out more power for their weight, than a four stroke. These engines put out considerably more power per pound of engine and per cubic inch of displacement, than a four stroke.

Seems as the engines get smaller and smaller, two stroke is far more efficient for the intended use, and as the engines get larger and larger, two stroke is more efficient and more common in use, than the four stroke. Why do you suppose that is? The larger two stroke engines are diesel engines, and do not experience the environmental issues that face typical light two stroke gasoline engines. Big or small, the two stroke has the potential to produce twice the power for a given RPM than a four stroke.

Simple advances such as loop scavenging also contribute to greatly inproved efficiency, in terms of emissions, fuel consumption, and power in the two stroke engine.

The Wartsila-Sulzer RTA96-C turbocharged two-stroke diesel engine is the most powerful and most efficient piston power plant in the world today and is used in ships. And that is in terms of specific fuel consumption, as well as power vs. weight.

I must have misunderstood this also. You appear to be claiming that the internal friction of a 4-stroke engine makes it less efficient than the 2-stroke. I guess I was wrong.

No, you were correct. But again, that would depend on the engine. If we're talking about small two strokes, then yes, less internal friction and less internal power wasteage...if a 60 hp engine must produce 70 or 80 hp to output that 60 hp, then it's less efficient than an engine which does not need to waste it's power overcoming it's own internal needs.

In theory, a two stroke engine should perform at twice the power output for a given cubic capacity, than a four stroke, though it's often more like half that with current design...about fifty percent more efficient with respect to power output. This is mitigated and brought up with exhaust tuning, induction boosting, etc.

If you really want efficiency, forget either of these engines and go for a wankel engine such as a mazda rotary...which might be described as a "three stroke" or a one-stroke, due to it's continuous power implulse.


Here I thought you claimed a 2-stroke produced more torque for the fuel burned than a 4-stroke. I guess I misunderstood you there also.

Asked and answered, under real world conditions, including the world's most efficient engine...yes.

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.

"horsepower" in aircraft engines is a sales term, but yes, it may be used in a mathematical comparison. However, RPM in operation is not a direct indication of available torque. An engine with a constant speed propeller will experience a torque increase as the RPM decreases as blade angle is increased, as the load is increased on the crank or drive shaft. Two engines producing the same RPM in level flight may not be able to produce the same RPM under a load, such as in a climb. Under a load, one engine may be able to maintain torque, whereas another might lose it. The two stroke engine does better under a load.

A four stroke engine has limitations with respect to RPM and efficiency, as well as operational capability. These range from harmonic issues to detonation issues, to valve float. These are not problems normally asociated with a two stroke powerplant.

Arguements may be made for, or against, and have been for many decades. Much like pitch for power or visa versa, or the subject of downwind turns...it's an unwinnable discussion as both two stroke and four stroke powerplants have their drawbacks and advantages. When discussing both, however, it's important to stay away from nonsensical arguements such as why more aircraft engines are four stroke vs. two stroke, etc...and stick to salient points of interest.

For the subject of the thread, light powerplants in an ultralight aircraft, little option exists beyond any of the excellent two stroke designs available today. Certainly some wonderful advances in four stroke small engines are available such as the Jaiburu and HKS, but even these are more expensive and too heavy for light airplane applications that require engines such as Rotax or Hirth two strokes. Economically, the two strokes win hands-down; they're cheaper to buy, run, maintain, overhaul, and operate.

While a slow evoloution in aircraft piston engines has seen gradual and minimal increases in technology for four stroke installations, we can generally see that we're flying behind powerplants that aren't much more advanced that what powered airplanes in 1930...nearly eighty years later. The technology is there, but won't be utilized in the face of the cost of certification and the very limited aviation market.
 
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As someone who's not a mechanic, and wants minimum hassels with an engine, I'll opt for a Rotax 912 over a 582 (or other two stroke) for any UL-type aircraft I get. With a 1500 hour TBO compared to 300 in the two-strokes, it's worth the extra cost to me.
 
Pound for pound, a two stroke engine is generally lighter than a four stroke engine

Which weighs more, a ton of lead or a ton of cotton?;)

Face it avbug, a two stroke burns more fuel in order to produce the same amount of work.

Two strokes have some efficiencies, but fuel consumption (the generally accepted measure of efficiency) is not one of them.
 

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