Jet Kart powered by an Air Research TurboJet Converted JFS100-13A (9) / Afterburner Page

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The Reheat Pipe before any modifications have been made.

The distorted exhaust spike shown center is one of the reasons that the reheat tube is going to be stripped down.

A view of one of the very nice fuel injectors.

 
The original nozzle has now been cut off which will now let me remove the exhaust spike assembly and flame holder without obstruction.

The flame holder plate removed.

Exhaust Spike assembly removed. I expect the reason that the cone distorted is because the supports are square to the mount, not allowing for any thermal expansion.

Stainless Steel flange has been mounted.

 
As I am getting a new non-reheat cone made with a 2" nozzle for the JFS100, I thought the old nozzle would be a good starting point for the reheat tube. This has a nozzle diameter of 3 1/2".

I felt the the fuel nozzles were to close to the fuel gutter, so I have reversed them to face forward. Now they are only about 20mm form the turbine wheel, but the gas flow should keep the atomised fuel well away.
 
Temporary igniter plug fitted without its flame guard and also the thermocouple has been moved as far forward as possible.


A view of the fuel nozzles facing forwards. For the next test the exhaust spike will be left removed to make any more adjustments easier.

 
Fuel flow control system for the ReHeat. The fuel comes in from the bottom right and in to the pump, with the valve fully open, the fuel flows back to a Tee piece at the inlet side of the pump, but when you start to close the valve, the fuel is made to flow out of the exit point to the left of the image.

Hmm, have a look at the first ReHeat Test 01, it seems that along with the nozzle necks and the totally un-aerodynamic stator ring, the flame gutter has now moved to the fuel nozzle area, which isn't good at all. You can see the entire reheat pipe glowing red, where it should be just from the flame gutter area backwards.

 
Proof that reheat ignition is occurring further forward than it should. The nozzles will now be rotated 180deg to face backwards.

I have come to the folllowing conclusion: The stator ring used is not appropriate for use in an afterburner system due to the square edges exposed to the gas flow, but would be more than acceptable in a normal turbo jet environment. If I had the time, I could possibly add a cone to smooth the outer air flow and obviously make sure that there was a appropriate exhaust spike fitted to help things along, these I feel would be required for the reheat to function safely, so consequently I have made a decision to stop spending any more time on the afterburner, as there are more pressing projects that I would rather be spending my time on.

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