Honda GX25 flies...on Big Bee
#26
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From: Unk,
I got a GX25 to examine and found a few interesting things I'll pass along.
The intake and exhaust valves have the head diameter as the units in the GX31 but with smaller stems(more flow for same head diameter with smaller stem)
The discharge area of the intake valve is greater than the port runner ( straight section immediately after carb)
The throat area (directly under vavle head)also has greater area than intake port,this suggests that port runner be opened to 10.5mm (.413") to improve flow.This would let the engine breath as much as the valve opening will allow with stock cam.
Ideally the smallest area in intake tract would be discharge area of valve,with the port leading to this somewhat larger to insure that port velocity is increasing as it flows towards valve.
With a .413 port the throat area under valve would still have a larger area than runner,so to maintain the decreasing port area as it gets closer to valve,the ideal port runner diameter in this case would be .453" (29/64") The next size up in carb would probably need to be used.IE 12.2 mm
The exhaust port is already in the correct configuration I wouldn't touch it,except for some blending (just round sharp edge not recontour port) of the inside corner at runner and throat intersection.Same blending for intake.
Stock port is .377" diameter,with a .256 restriction in intake, these intake restrictions serve to limit rpm as there is no mechanical or ignition rpm regulation.
They also limit power available.
Larger ports work better at higher rpm levels,and may not be suitable for lower rpm applications such as the range aircraft are using.
I am not suggesting using these modifications just sharing what I have found on the GX25.
The intake and exhaust valves have the head diameter as the units in the GX31 but with smaller stems(more flow for same head diameter with smaller stem)
The discharge area of the intake valve is greater than the port runner ( straight section immediately after carb)
The throat area (directly under vavle head)also has greater area than intake port,this suggests that port runner be opened to 10.5mm (.413") to improve flow.This would let the engine breath as much as the valve opening will allow with stock cam.
Ideally the smallest area in intake tract would be discharge area of valve,with the port leading to this somewhat larger to insure that port velocity is increasing as it flows towards valve.
With a .413 port the throat area under valve would still have a larger area than runner,so to maintain the decreasing port area as it gets closer to valve,the ideal port runner diameter in this case would be .453" (29/64") The next size up in carb would probably need to be used.IE 12.2 mm
The exhaust port is already in the correct configuration I wouldn't touch it,except for some blending (just round sharp edge not recontour port) of the inside corner at runner and throat intersection.Same blending for intake.
Stock port is .377" diameter,with a .256 restriction in intake, these intake restrictions serve to limit rpm as there is no mechanical or ignition rpm regulation.
They also limit power available.
Larger ports work better at higher rpm levels,and may not be suitable for lower rpm applications such as the range aircraft are using.
I am not suggesting using these modifications just sharing what I have found on the GX25.
#27
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From: Independence,
KY
ORIGINAL: BajaBob
The discharge area of the intake valve is greater than the port runner ( straight section immediately after carb)
The throat area (directly under vavle head)also has greater area than intake port,this suggests that port runner be opened to 10.5mm (.413") to improve flow.This would let the engine breath as much as the valve opening will allow with stock cam.
Ideally the smallest area in intake tract would be discharge area of valve,with the port leading to this somewhat larger to insure that port velocity is increasing as it flows towards valve.
With a .413 port the throat area under valve would still have a larger area than runner,so to maintain the decreasing port area as it gets closer to valve,the ideal port runner diameter in this case would be .453" (29/64") The next size up in carb would probably need to be used.IE 12.2 mm
The discharge area of the intake valve is greater than the port runner ( straight section immediately after carb)
The throat area (directly under vavle head)also has greater area than intake port,this suggests that port runner be opened to 10.5mm (.413") to improve flow.This would let the engine breath as much as the valve opening will allow with stock cam.
Ideally the smallest area in intake tract would be discharge area of valve,with the port leading to this somewhat larger to insure that port velocity is increasing as it flows towards valve.
With a .413 port the throat area under valve would still have a larger area than runner,so to maintain the decreasing port area as it gets closer to valve,the ideal port runner diameter in this case would be .453" (29/64") The next size up in carb would probably need to be used.IE 12.2 mm
#28
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From: Unk,
The port runner is a straight shot to the throat area.just take a reamer and ream the port runner,the area directly under valve head doesn't need any work.Technically the runner should be tapered,its easier to continue with straight sided port wall.It can be tapered with a tapered reamer but you need to grind the tip of it back to get the opening at the intersection the diameter you want.
I have just stuck with straight ports until I arrive at a diameter that does what I need.
On the GX31 the port starts out at .398 I just picked the next 64th size reamer up from there and opened port in 1/64th increments,testing in between.
I'll take some pics.I have a sketch of the GX31 intake port that will clarify some of this.
The hard part is breaking the sharp edge at the intersection of the runner and throat/pocket. I was able to take a cheap needle file heat it up and bend it at the tip,rifler files would do the job very well also as they are bent.
It takes a little patience, but basically you message the edge with the file.All the work is done from the carburetor side of port so its accessible, tight but you can get in it. A grinder can be used but very carefully,you want to round edge evenly around the intersection,its easy for the tool to drop the bottom of the port floor and groove the edge.
Before anything of significance can be done with a cam this simple modification needs to be done first.By itself opening the intake port helps,you won't see a monstrous gain but roughly a 12% increase in flow will be noticeable.
EDIT:Added the following
I have some pics and a drawing I'm preparing,there are some issues on the GX25 that need close attention to avoid daylighting or breaking out of port runner.
BBriBro Did you get my PM?
I have just stuck with straight ports until I arrive at a diameter that does what I need.
On the GX31 the port starts out at .398 I just picked the next 64th size reamer up from there and opened port in 1/64th increments,testing in between.
I'll take some pics.I have a sketch of the GX31 intake port that will clarify some of this.
The hard part is breaking the sharp edge at the intersection of the runner and throat/pocket. I was able to take a cheap needle file heat it up and bend it at the tip,rifler files would do the job very well also as they are bent.
It takes a little patience, but basically you message the edge with the file.All the work is done from the carburetor side of port so its accessible, tight but you can get in it. A grinder can be used but very carefully,you want to round edge evenly around the intersection,its easy for the tool to drop the bottom of the port floor and groove the edge.
Before anything of significance can be done with a cam this simple modification needs to be done first.By itself opening the intake port helps,you won't see a monstrous gain but roughly a 12% increase in flow will be noticeable.
EDIT:Added the following
I have some pics and a drawing I'm preparing,there are some issues on the GX25 that need close attention to avoid daylighting or breaking out of port runner.
BBriBro Did you get my PM?
#29
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From: New Boston,
NH
The thrust HP Calculator shows that an APC 18x6 will give you 15.4 lbs of static @ 7,000 rpm and will absorb 1.5 hp. This is as close as I could get going on the engine ratings. I think you may not be getting the most out of the engine at 5,200 rpm. The 20x8 is absorbing 1.28 horsepower @ 5,200 rpm. Let us know.
Gis
[quote]Well.... turns out im only putting out about 6 lbs of thrust (fish scale). That explain's the horrible performance on its only flight so far.
Gis
[quote]Well.... turns out im only putting out about 6 lbs of thrust (fish scale). That explain's the horrible performance on its only flight so far.
#30
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From: New Boston,
NH
I was reading about your engine problem. But first I must say you did an excellent job on the plane. I was wondering if when you are inverted if fuel is flooding back on the carb overflow/return line. I did some reading on this since there has been some question about the function of the return line. Honda says that it is a overflow/return line and does not pressurize the tank. If you assembled the tank in the classic manner, when inverted the weight of the fuel on the return vent may restrict the return and flood the engine. Also, did you run the return line back to the tank, is your tank vented? Your high speed starvation sounds like you didn't vent the tank. Something to check...
Gis
[quote] the only "issue" I noticed, was that the engine didn't want to run inverted.
Gis
[quote] the only "issue" I noticed, was that the engine didn't want to run inverted.
#31
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From: Independence,
KY
My tank is vented to the atmosphere, I have the return line (from the primer bulb) blocked off, there is only one line from the clunk to the fuel inlet on the carb. I have leaned it out some and it seems to be better inverted, still not "right" but at least it doesn't try to quit, just loads up a little.
[quote]ORIGINAL: Gismo
Honda says that it is a overflow/return line and does not pressurize the tank................... Also, is your tank vented? Something to check...
Gis
[quote]ORIGINAL: Gismo
Honda says that it is a overflow/return line and does not pressurize the tank................... Also, is your tank vented? Something to check...
Gis
the only "issue" I noticed, was that the engine didn't want to run inverted.
#32
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The GX25 I sold to Willdo in New Zealand was turning my 18-6 Mejzlik about 7500 rpm, about 5 to 700 less than a stock G23.....
The engine was untouched except for trimming the excess from the case and removing the flywheel for CD ignition....Can't remember the weight, it's on a thread here somewhere...
Your thrust test shows how really inaccurate the ThrustHp chart is....
The engine was untouched except for trimming the excess from the case and removing the flywheel for CD ignition....Can't remember the weight, it's on a thread here somewhere...
Your thrust test shows how really inaccurate the ThrustHp chart is....
#33
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From: Auckland, NEW ZEALAND
RCIGN,
I make it 3lbs 4oz (with original muffler, RCIGN prop driver and walbro carb, - no prop, no coil).
I'm now fitting a Walbro carb, (trial) and I figured that the pump would still work, with the intake vacuum creating a negative pulse, and then a positive pulse being provided when the inlet valve slams shut, (because the kinetic energy of the mixture builds up a positive pulse, as it keeps on coming into the inlet tract.)
Could this possibly be how the original carb works too? - just a thought, - (open to discussion
).
I agree that the restriction needs to be removed from the inlet tract, - I intend to have a tapered tract between the carb and the port on the engine.
BTW, - All work on the project has ground to a halt here, - I severly damaged my thumb ( at work, - not by a prop!
), and now, they have had to amputate the top half, so that's slowed things down considerably! - I've also got to find a way to use the sticks again!
I make it 3lbs 4oz (with original muffler, RCIGN prop driver and walbro carb, - no prop, no coil).
I'm now fitting a Walbro carb, (trial) and I figured that the pump would still work, with the intake vacuum creating a negative pulse, and then a positive pulse being provided when the inlet valve slams shut, (because the kinetic energy of the mixture builds up a positive pulse, as it keeps on coming into the inlet tract.)
Could this possibly be how the original carb works too? - just a thought, - (open to discussion
).I agree that the restriction needs to be removed from the inlet tract, - I intend to have a tapered tract between the carb and the port on the engine.
BTW, - All work on the project has ground to a halt here, - I severly damaged my thumb ( at work, - not by a prop!
), and now, they have had to amputate the top half, so that's slowed things down considerably! - I've also got to find a way to use the sticks again!
#34
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From: Fairfax, VA
BBriBro,
Nice looking plane! Where did you get the nice lightweight exhaust header? Also, do you think it's possible to cruise at 1/4 oz of fuel per minute with this engine?
Thanks
Jason
Nice looking plane! Where did you get the nice lightweight exhaust header? Also, do you think it's possible to cruise at 1/4 oz of fuel per minute with this engine?
Thanks
Jason
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From: Independence,
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ORIGINAL: JasonF
Where did you get the nice lightweight exhaust header? Also, do you think it's possible to cruise at 1/4 oz of fuel per minute with this engine?
Where did you get the nice lightweight exhaust header? Also, do you think it's possible to cruise at 1/4 oz of fuel per minute with this engine?
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From: Joppa,
MD
Hey BBriBro, do you still have problems with your GX25 sagging at full throttle? Mine is doing that. It acts like it goes lean at full throttle. What I think is happening is that with the throttle all the way open there is not enough engine vacuum left to go through the little passage and make the diaphragm in the carby do its thing.
Charlie
Charlie
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From: Independence,
KY
Actually mine is running good now, Mine was definately going rich, I leaned it a little and it helped the inverted flight. Which carb are you using ?
Oh, and BTW, mine never sagged right side up, it ran fine at all RPMs, only inverted it was giving trouble.
Oh, and BTW, mine never sagged right side up, it ran fine at all RPMs, only inverted it was giving trouble.
ORIGINAL: tango28charlie
Hey BBriBro, do you still have problems with your GX25 sagging at full throttle? Mine is doing that. It acts like it goes lean at full throttle. What I think is happening is that with the throttle all the way open there is not enough engine vacuum left to go through the little passage and make the diaphragm in the carby do its thing.
Charlie
Hey BBriBro, do you still have problems with your GX25 sagging at full throttle? Mine is doing that. It acts like it goes lean at full throttle. What I think is happening is that with the throttle all the way open there is not enough engine vacuum left to go through the little passage and make the diaphragm in the carby do its thing.
Charlie
#39
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From: Independence,
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ORIGINAL: tango28charlie
I'm using the stock carb.
I'm using the stock carb.
#40

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BBri Bro-- just saw this post on your Honda 4-stroke application. What a gorgeous plane! I have been looking at these engines for a while but until now had not really heard how well they worked in a firsthand report. I had e-mailed Dave Carr a while back regarding mounting these engines inverted because of my concern of crankcase oil seepage past the rings in between flying days, as well as how they ran inverted (although I wasn't too worried in that respect due to weedeaters being used that way all the time). His reply was that they would work fine while mounted inverted, but should be stored upright for that reason (seepage past the rings). The fact that he recommends inverted mounting and one of the other posts saying his ran fine inverted suggests an isolated problem with your setup. I don't have any input or suggestions, just an observation. One other observation that I'm sure you're on top of: have you tried a dual pitch prop, like a 20-6/10? There are a couple guys at our field using gas engines in their WWI and WWII warbirds and they say power delivery and performance is better than with a single pitch prop. I don't know their reasoning, but that's their experience. Don't know if it would be different with 2- vs 4-stroke gas. Also don't think it is related to difficulties with inverted operation, but wouldn't a velocity stack smooth out engine operation since there's no cowl to block the slipstream?
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From: Independence,
KY
ORIGINAL: khodges
BBri Bro-- just saw this post on your Honda 4-stroke application. What a gorgeous plane! .................His reply was that they would work fine while mounted inverted, but should be stored upright for that reason (seepage past the rings).
BBri Bro-- just saw this post on your Honda 4-stroke application. What a gorgeous plane! .................His reply was that they would work fine while mounted inverted, but should be stored upright for that reason (seepage past the rings).
#42

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ORIGINAL: BBriBro
Thanks for the compliments, as far as the engine being mounted inverted, Honda says they can be operated and stored inverted, with no limitations. The oil "tank" is round and contains the full quantity of oil, without it "puddling" in the bottom of the piston and cylinder. The only oil you would have that seeped by the rings is whatever was actually on the cylinder walls when you shut it down and stored it, (a very small amount) the actual supply of liquid oil would remain in the "tank" DId you see my pics of the piston? There are several rings, including an oil scraper, I would think it would seal quite well. Even if it didn't look at the old radial aircraft engines, they were known for oil to collect in the bottom cylinders which is why the smoked and coughed so much on startup.
ORIGINAL: khodges
BBri Bro-- just saw this post on your Honda 4-stroke application. What a gorgeous plane! .................His reply was that they would work fine while mounted inverted, but should be stored upright for that reason (seepage past the rings).
BBri Bro-- just saw this post on your Honda 4-stroke application. What a gorgeous plane! .................His reply was that they would work fine while mounted inverted, but should be stored upright for that reason (seepage past the rings).
#43
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From: Joppa,
MD
ORIGINAL: BBriBro
Why would you think the stock carb wouldn't work at full throttle?
Why would you think the stock carb wouldn't work at full throttle?
I would have no reason to think the stock carb wouldn't work at full throttle, other than observing that 1.) The RPM sags at full throttle, and 2.) after a few seconds at full throttle, the fuel level in the primer bulb decreases to nearly zero.
Charlie
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From: KILPEDDERWICKLOW, IRELAND
BBribro,
Well done on the coversion,love the plane looks great.
I have a gx31 that i have started to convert and i want to know where i can get a prop driver thanks.
Petrolhead
Well done on the coversion,love the plane looks great.
I have a gx31 that i have started to convert and i want to know where i can get a prop driver thanks.
Petrolhead
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From: Independence,
KY
ORIGINAL: Petrolhead
BBribro,
Well done on the coversion,love the plane looks great.
I have a gx31 that i have started to convert and i want to know where i can get a prop driver thanks.
Petrolhead
BBribro,
Well done on the coversion,love the plane looks great.
I have a gx31 that i have started to convert and i want to know where i can get a prop driver thanks.
Petrolhead
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From: Independence,
KY
ORIGINAL: av8tor1977
Say BBriBro, what became of your carb experiments? I have a Honda 31cc four stroke that I would like to get a carb for. Recommendations??
Thanks,
AV8TOR
Say BBriBro, what became of your carb experiments? I have a Honda 31cc four stroke that I would like to get a carb for. Recommendations??
Thanks,
AV8TOR
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From: Independence,
KY
ORIGINAL: av8tor1977
Ok, thanks guy. That's WYK-61. Any modifications, or is it a bolt on? It has both hi and low needles right?
Take care,
AV8TOR
Ok, thanks guy. That's WYK-61. Any modifications, or is it a bolt on? It has both hi and low needles right?
Take care,
AV8TOR


