Okay! Gotta start somewhere, and I'm a couple months into my current project, a turbojet engine based on the large diesel turbocharger shown below.
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| This is a very large Holset ST-50 turbocharger from a Cummins diesel generator set. |
A gas turbine engine is, very simply, a fan to compress the air, a combustor to burn fuel with the air, and a turbine which is driven by the hot gasses produced by the combustor, and which spins the compressor "fan".
A diesel turbocharger is a radial flow compressor, and a radial flow turbine. Two essential elements of a gas turbine engine. The key components I must add are the combustor, a fuel system, and an oil system to accomodate the fragile turbocharger. Here's what I've got done so far:
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| I've fabricated a stainless steel combustion chamber, an engine frame, and mounted some oil system components so far. |
I'm looking forward to continuing this project, and sharing the ride with as many as who may be interested. :)
Generally, the thickness of the Rotary evaporator is usually equipped with good chemical and physical properties. From here:www.toption-china.com/rotary-evaporator. And it can work under the ordinary or positive pressure.
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