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I'm back again,
and this time I have some interesting results for the HR-1A
engine. I did more testing and the engine literally came
apart at the seams! You would think this is a bad thing,
but I'm pretty happy about it actually. The thrust was more
than I expected, and other efficiencies were good as well.
This engine is really putting a smile on my face!

Nozzle on engine for thrust testing
The first thing
I wanted to do was reinstall the thrust nozzle on the engine
so that I would have a better chance of seeing some usable
thrust in the testing. Using a few small tack welds, I attached
the nozzle to the jet pipe on the back of the engine.

Business end of the nozzle
The nozzle is
not that much smaller than the jet pipe itself, but it should
make more thrust for the engine by accelerating the gasses
to an even higher velocity as they leave the pipe. I wasn't
really prepared for the results when I fired up the engine
again, and I assure you that this nozzle makes a big difference!

The outside of the combustor casing
Firstly, this
is the outside of the combustor casing. The paint bubbled
up a bit during testing, on this spot right here. It's pretty
obvious that my weld did not penetrate as good as I had
originally thought. The hot gasses from the combustor were
seeping right through the bad weld and getting under the
paint causing it to bubble. As the engine was shut off,
the paint and combustor cooled and the paint settled back
down to look like this. Hmmm, I didn't notice this after
the first test runs I showed in the video?!?

Weld split on the combustor
Whoa! I certainly
didn't expect this! While running the engine, everything
seemed fine and pressure was good with a very good thrust
output. All of a sudden I heard a loud hissing noise. After
checking the combustor I found the culprit. It was this
area in the photo above which actually measured out to be
a little over an inch long and about 1/32nd of an inch wide.
It is one of the welds of the combustor that had split open!
It isn't a big problem and will be an easy fix. This happened
at 35 PSI of pressure on my combustor boost gauge. The engine
never slowed down, didn't heat up, and only lost about 5
pounds of thrust when this happened.

Flame tube after the test runs
After the test
runs, I disassembled the combustor to check for wear and
heat marks. As you can see on the picture of the flame tube
above, the burn is happening right in the primary to secondary
zone.

Other side of the flame tube
Flipping the
flame tube over shows that we have the same pattern all
the way around. Whoo hoo! This is good news for the engine!
Low exhaust temperatures, plenty of boost, the nozzle on
the jet pipe was whizzing away making a high pitched squeal
that tells me it was choking the flow just right, and to
top it all off it was burning 10 gallons per hour as figured
by the nozzle size, fuel pressure, and consumption from
the tank! This engine is a winner for sure. But what about
thrust you ask? Well read on!

The scale after testing
This is my trusty
scale I use for thrust testing. It has never let me down,
and I check the calibration regularly to make sure it is
still going to give good results. As you can see, it wouldn't
give very good results now! The needle is buried at 42.5
pounds, but that is after it came all the way around and
back down after the run! Here is what happened. The engine
pulled the needle all the way to 50 lbs of thrust, and the
scale kept up. The engine then took it on past 50 lbs on
the scale and stopped reading at 5 lbs (technically at 55
lbs and holding). What is surprising is that the engine
pulled so hard that it stripped the mechanism inside, since
it went over the 55 lbs of thrust! You see, the scale needle
is limited to 55 lbs total, but the mechanics just kept
going round and the gears popped over each other. This is
why the scale would return to a lower point than 0 when
removing all tension from it!. If you take that the scale
must have gone over 55 lbs, then you can calculate how far
by seeing how far it went backwards when returning to zero.
It must have gone over by at least 7.5 pounds! I hope this
is making sense so far to you. Just add the 7.5 lbs to the
55 lbs we know we produced, and you will get 62.5 pounds
of thrust! Not bad for an engine of this size, especially
on only 10 gallons of fuel per hour!
So now the combustor
is being patched, a new scale is on order, and I am getting
everything ready for even more testing. I already know for
sure that the engine is much better than it was before,
and here are the number to prove it!
|
HR-1 engine |
HR-1A engine |
| Thrust |
45 lbs max |
at least
62.5 lbs |
| Combustor
PSI |
38 - 40
PSI |
35 PSI |
| Fuel consumption |
16 GPH |
10 GPH |
| Turbine
outlet temps |
1400 degrees
F |
900 degrees
F |
As you can see,
the difference is like night and day. As soon as I get more
results, I will post them here along with more video if
I get some.
Check back soon
for the newest testing results. As you leave the site, please
remember to support us as the builds are partially funded
by your contributions. Thanks again for stopping by!
Gary Richards
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