
The new HR-1 engine |
After my initial
experiences with my first jet engine, I decided to build
a new larger engine. This new engine will be called the
HR-1.
I am trying something
new in that I am bringing in the air in the middle side
of the combustor. On my first engine the air flowed axially
through the combustor, entering one end and leaving the
other. This engine will use an annular combustor in which
the air enters from the side and flows out of one end. The
design is a bit easier to construct and is also more compact
as there is not an excess of pipe to transfer the air from
the compressor to the combustor.

Combustor parts
I started by
constructing the outer combustor housing and plumbing that
will connect the combustor to the turbine and compressor.

Combustor exhaust elbow
The combustor
does not flow directly into the turbine, but instead makes
a 90 degree turn before entering. This was done to make
the whole engine more compact.

End cap flange and air inlet
The air will
enter from the side of the combustor. The offset opening
of the inlet pipe should help to induce a swirl in the combustion
chamber. With the gasses swirling before they enter the
flame tube, it should help to create a vortex of fire that
sits in the center of the flame tube.

Construction stand
This is the stand
that was built to hold the turbo during construction.

Turbo inducer
The inducer on
this turbocharger is much larger than on the previous RayJay
turbo. With the additional mass flow of air there should
be a considerable power gain. The inducer is the area of
the blades that can be seen when looking at the inlet of
the turbocharger.

Combustor to turbine elbow
The additional
length of the the combustor that is added by the bend will
also give more time for the burn process to complete before
the hot gasses enter into the turbine. Hopefully this will
allow the engine to run a bit cooler as well.

Blank pipe for the flame tube
This is the pipe
that will be drilled for the flame tube. It is 4 inches
in diameter.

The flame tube
Once the holes
are drilled, the flame tube is ready to be installed. The
hole sizes and pattern were calculated using Jet Spec Designer.
A copy of the program can be downloaded from my site and
is free of charge to use. Once a flame tube has been properly
calculated and drilled, it appears to be almost a work of
art.

Combustor end plate
The end plate
of the combustor is removable for easy access and maintenance.
It is held on with 8 bolts and sealed in place with high
temperature silicone sealant such as is used in automobile
applications.

The finished engine
Here is the completed
and painted engine on the test stand. Note the size of the
actual turbine and the size of the exhaust pipe that was
used. You can see that the pipe fits the housing but it
is much larger that the actual turbine exducer blades. The
exhaust flange of the turbine is much larger that the actual
turbine blades, since the original application for automobile
use would need to slow down the exhaust gasses and pass
them through a smaller exhaust pipe section.

The engine ready to be tested
The engine is
hooked up to the control panel and ready to run with the
addition of the oil pumps and coolers, along with the fuel
system. Gauges will be used to monitor pressures and temperatures,
in the same way as were used on the original RayJay based
engine.

The control panel
The control panel
contains switches to control the oil and fuel pumps, as
well as the ignition and cooling fan. Directly above the
control panel are two gauges which display the compressor
pressure of the turbo as well as the oil pressure for the
cooling and lubricating oil.

The oil pump assembly
I used a power
steering pump for the oil pump and a 12 volt motor to drive
it. It worked well for a while, however, later in testing
on the jet kart it failed and caused the main bearings of
the turbo to be destroyed. More information can be found
about the jet kart in its own section here on the site.
There is more information
on the development of the HR-1 in the next section which can
be accessed by clicking the link below.
Go
to Section 2
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