Is there any .049 Transfer & Exahaust, BDT, rod length data available?

Has anyone ever tried a high compression/low nitro head with a squish band
~.004" squish clearance.


Something else I have only read about is the glow head coming loose while
running. Seems more likely on a control than a free flight? But on our race
engine things tend to come loose when the engine is detonating, or the piston
is hitting the head

Recently saw a picture of a cracked piston, detonation destroys, preignition melts.
Could an .049 piston crack from detonation?


Bill M.

I both hate and love detonation

roddie wrote:
I also suspect that re-using a head-gasket.. rather than installing a new one, might cause the glow-head to loosen.. due to the used-gasket being
previously squished-thinner. This is just speculation though.. Maybe previously-used head-gaskets become "work-hardened" and loose some of their
ability to keep the head from loosening-up?

I have had similar experience using copper head and base gaskets on
Kawasaki Jet Ski's. Except the part about coming loose, that would be
very bad. The copper gaskets do compress and become "work-hardened."

Copper gaskets are reusable after they have been annealed (heated, then
tossed into water).

roddie wrote:
You can bench-run an engine using a flywheel (rather than a propeller).. but it's wise to provide some cooling for the cylinder.. and a BALANCED-flywheel.
An engine running a flywheel will unwind on the bench.

I'll start a new thread on some of my own recently-discovered info. regarding flywheels for the Cox .049 glow engine.

I am very interested in that, and I may have to many questions.

I thought about pros & cons of an inertia dyno when Oldenginerod mentioned
testing .020 & .010 engines. But the problem I saw was how to get the engine
to a low rpm, and then measure the acceleration. An inertia dyno or tachometer
would be a simple electronics project using your favorite microcontroller and
display.

Perhaps all the engine needs is to momentarily block the air intake and let it
accelerate up, and log the data.


Bill M.

What is the goal of further developing an entirely ancient design? Modern 1/2A make much more power. While it may be interesting to know, I haven't bothered to accurately measure timing, I'm just not sure much more power can be extracted from a TD. I had doubts about the pipe adapter I made for Brad being effective with a blocked exhaust port, but it seems to be working. A few attempts were made at schnuerle TD's, but there is very little information available about performance.

Tight clearances or specific timing require the ability to modify/produce the parts, so there is little out there in that regard. I think a better engien could have been produced using the threaded cylinder arrangement, but it would take a larger diameter overall to get the porting in there. Of course, very small details can have a big influence, so it's hard to say what will work without a lot ideas, testing, and experience to interpret the results.

gkamysz wrote:What is the goal of further developing an entirely ancient design? Modern 1/2A make much more power.
While it may be interesting to know, I haven't bothered to accurately measure timing, I'm just not sure much more power
can be extracted from a TD.

Initially my #1 goal is to find a propeller that holds the engine rpm to 22,000
when it unloads. Because published data suggests that is where peak HP is.

I do find the results of bench racing impressive, but I don't see that as a
reliable engine, and so I would rather fine tune the existing engine to its
nearly stock potential for tuning consistency, with pressure, using a bladder.

Goal #2: Similar performance to #1, but using low nitro, or no nitro like an FAI
engine.

gkamysz wrote:
While it may be interesting to know, I haven't bothered to accurately measure timing

It is interesting, and I would like to see if I can gain any practical knowledge
from it by comparing existing cylinder specs.

gkamysz wrote:
I had doubts about the pipe adapter I made for Brad being effective with a blocked exhaust port, but it seems to be working.

That adapter was the first thing I noticed in 1/2anut's thread. I especially liked the
choice of the adapters inside diameter. It looks very professional.

gkamysz wrote:
A few attempts were made at schnuerle TD's, but there is very little information available about performance.

While researching my Kirn Kraft engines, I spoke to a Cox employee who basically
told me the single exhaust port .049 engines didn't test as well as the original design.

gkamysz wrote:
Tight clearances or specific timing require the ability to modify/produce the parts, so there is little out there in that regard.
I think a better engine could have been produced using the threaded cylinder arrangement, but it would take a larger diameter
overall to get the porting in there. Of course, very small details can have a big influence, so it's hard to say what will work
without a lot ideas, testing, and experience to interpret the results.

I am only interested in the benefits of a tight squish, and working with other cylinders,
within the boundaries of what the threaded cylinder will allow. But for the most part,
I believe the engine to be a well tested engine, and that I would not have any new ideas
that remain untested.

The only other goal is to make a better test stand, but not a complicated test stand
with load cells like they sell for electric motors.


Bill M.

wmazz wrote:

gkamysz wrote:What is the goal of further developing an entirely ancient design? Modern 1/2A make much more power.
While it may be interesting to know, I haven't bothered to accurately measure timing, I'm just not sure much more power
can be extracted from a TD.

Initially my #1 goal is to find a propeller that holds the engine rpm to 22,000
when it unloads. Because published data suggests that is where peak HP is.

I do find the results of bench racing impressive, but I don't see that as a
reliable engine, and so I would rather fine tune the existing engine to its
nearly stock potential for tuning consistency, with pressure, using a bladder.

Goal #2: Similar performance to #1, but using low nitro, or no nitro like an FAI
engine.

gkamysz wrote:
While it may be interesting to know, I haven't bothered to accurately measure timing

It is interesting, and I would like to see if I can gain any practical knowledge
from it by comparing existing cylinder specs.

gkamysz wrote:


I had doubts about the pipe adapter I made for Brad being effective with a blocked exhaust port, but it seems to be working.

That adapter was the first thing I noticed in 1/2anut's thread. I especially liked the
choice of the adapters inside diameter. It looks very professional.

gkamysz wrote:
A few attempts were made at schnuerle TD's, but there is very little information available about performance.

While researching my Kirn Kraft engines, I spoke to a Cox employee who basically
told me the single exhaust port .049 engines didn't test as well as the original design.

gkamysz wrote:


Tight clearances or specific timing require the ability to modify/produce the parts, so there is little out there in that regard.
I think a better engine could have been produced using the threaded cylinder arrangement, but it would take a larger diameter
overall to get the porting in there. Of course, very small details can have a big influence, so it's hard to say what will work
without a lot ideas, testing, and experience to interpret the results.

I am only interested in the benefits of a tight squish, and working with other cylinders,
within the boundaries of what the threaded cylinder will allow. But for the most part,
I believe the engine to be a well tested engine, and that I would not have any new ideas
that remain untested.

The only other goal is to make a better test stand, but not a complicated test stand
with load cells like they sell for electric motors.


Bill M.

Bill M.: I took some data back in 2015 comparing the crankshaft length and the crankcase inside length, comparing a regular crackshaft-crankcase compared to a #2 stamped on the engine mounts. There were several questions about users who were having issues when the 2 were mixed. Long crankshaft in a short case and short crank in a long case. I came across your post looking for my old data. i will edit and repost when i find the correct title. I thought it was "medallion and Tee Dee crankshaft and medallion data", but not yet.  more later.

>>>>>edited 8-4-20 8:40p/m. PST to add correct title of "Cox Tee Dee Crankcase and Crankshaft data" which also included Medallion CC and CD data from 2015 to today. >>>>>edit over

maybe not what you were looking for, but, search "Cox Tee Dee crankcase and crankshaft data" in the search box to left above latest topics. You will have to go to page 2 for 2015 data. It may have updated to todays post.

Hope it is helpful to someone.

happydad      

Here for posterity I will post one of my flights with a tuned pipe.
Engine cylinder is a TD .051 no tampering with timing.



Nano X speed plane / Cox TD .051 / Profi .8cc Tuned Pipe / APC 4.3 x 5.5N
Last two passes are the best peak: 28,181 rpm / 147mph PS / 143mph doppler pass
Now the fastest Cox TD .051 3ch RC plane on You Tube.

Best static 21,962 rpm / 7.2oz thrust / 115 mph pitch speed / Pipe length tuned to 7.5" MRP
.144 hp - 108w  / stock piston /cylinder and crank.

25" span 75 sq. in. wing / 8.1oz RTF / Temp 87F,  dry, winds 7 - 12 mph.
25% nitro / 20% oil  / SPI engine / No pressure tap. Fast burn rate 1oz fuel tank.
2 shims used.  

Kamtechnik turbo plug adapter & prototype manifold / header O.S. RP7 Gold turbo plug.
No mods to cylinder, piston or crank. 1/2A Fitz fuel. Many attributes all contributing to
the top speed thru design / size / weight and quality Kamtechnik engine components.

1/2A Nut wrote:Here for posterity I will post one of my flights with a tuned pipe.
Engine cylinder is a TD .051 no tampering with timing.



Nano X speed plane / Cox TD .051 / Profi .8cc Tuned Pipe / APC 4.3 x 5.5N
Last two passes are the best peak: 28,181 rpm / 147mph PS / 143mph doppler pass
Now the fastest Cox TD .051 3ch RC plane on You Tube.

Best static 21,962 rpm / 7.2oz thrust / 115 mph pitch speed / Pipe length tuned to 7.5" MRP
.144 hp - 108w  / stock piston /cylinder and crank.

25" span 75 sq. in. wing / 8.1oz RTF / Temp 87F,  dry, winds 7 - 12 mph.
25% nitro / 20% oil  / SPI engine / No pressure tap. Fast burn rate 1oz fuel tank.
2 shims used.  

Kamtechnik turbo plug adapter & prototype manifold / header O.S. RP7 Gold turbo plug.
No mods to cylinder, piston or crank. 1/2A Fitz fuel. Many attributes all contributing to
the top speed thru design / size / weight and quality Kamtechnik engine components.

1/2A Nut: did you fly the rocket? did you get really dizzy watching a plane go round and round at 147MPH?  

that is fast. did you use a cradle or how did you hold onto the ?  Oh, RC, how did you even see the rocket go bye?

happydad

The trick is to have the space to line up the plane to fly fast passes in front of the cam.
No TX cradle just keep your eyes on it and time will slow down, having a throttle on
the engine makes warm up easy. The engine ran well and shows what's possible with
the stock timing with a FIRE confiq. no stumbling at full throttle.

1/2A Nut wrote:The trick is to have the space to line up the plane to fly fast passes in front of the cam.  
No TX cradle just keep your eyes on it and time will slow down, having a throttle on
the engine makes warm up easy. The engine ran well and shows what's possible with
the stock timing with a FIRE confiq. no stumbling at full throttle.

 

I had a hard time seeing the “rocket” when it was in the distance, but could hear it, then it came from behind, beside you and WOW, the noise, the feeling of it rushing by.

   Thanks I’ll sit in the bleachers ot in my tank when you fly it.
  Is the plane one of those specially made from Europe? I have seen the name before.

Happydad