akkudakku
New Member
Joined: April 2014
Posts: 4
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Post by akkudakku on Aug 28, 2014 12:32:47 GMT -5
Hey guys, I'm back with a question again.
Have anyone of you ever tried to build a heat recovery system for your engines? From what I understand of the theory of the turbojet/turbo-shaft engines - power is a function of TIT, TIT is increased by burning fuel and PR determines burn efficiency.
So now what happens on a turbo-shaft if we take the hot exhaust and heat up the air coming out of the compressor just before the combustor with some kind of heat exchanger? From what I understand this way we should use less fuel mass/kW.
Another idea that springs to mind is using the hot exhaust to heat up fuel before it reaches the combustion chamber - it would work great with liquid propane or LPG supplying the heat of evaporation and evaporating it 'for free'.
Could systems like this be used to get better specific fuel consumption?
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Post by racket on Aug 28, 2014 16:59:24 GMT -5
Yep, better SFC if you can use some of the "waste" heat .
I haven't heard of any DIY application , probably because we aren't too concerned with fuel burn rates because of the limited run times , its not worth going to all the trouble and expense, we'd spend more on the heat exchanger than we'd ever spend on fuel .
Cheers John
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akkudakku
New Member
Joined: April 2014
Posts: 4
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Post by akkudakku on Sept 3, 2014 14:17:15 GMT -5
What about sequential combustion in free-power gas turbines John?
I know it is actually increasing the fuel consumption, but what would be the result, increased shaft power?
By the way could you recommend a lecture about gas turbines to me (I'm wondering on the thrust -> power estimation and the thermodynamics of power generation on the free-power)?
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Post by racket on Sept 3, 2014 16:31:10 GMT -5
A second combustor can be used to "reheat" the gases before entering the freepower turbine for a bit more power, but it does add a lot more complication and size to the build. As a rough guide, for every pound of thrust we can make from a DIY engine we should be able to produce a horsepower , 100 lbs of thrust = 100 horsepower. Do you have the Thomas Kamp book , if not , purchase it direct from the publishers, gb.trapletshop.com/model-jet-engines-3rd-edition-by-thomas-kamps ...........its the best book for beginners , the thermodynamics for the gas producer can be applied to the freepower Cheers John
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