dalekh wrote:Tom,
This is a tough topic to get info on. Most of what I am finding is simple overview or theoretical with math mostly outside my "comfort zone"!
I know. I think I'm giving up on trying to figure out if this can work mathematically. I found some equations on a nice NASA site that looked applicable to this.
Well, when I started reading, it went on to say that NASA uses high speed computers to arrive at
approximate solutions to these equations... OK... Time for me to go back to the old tried and true method. Intuition, common sense and trial end error or something.
The most informative piece I've found so far is this PDF:
http://ethesis.nitrkl.ac.in/7/1/sghosh-sarangi.pdf
Which also explains why there is not much information available. It is mostly all proprietary for a very niche market.
I did find this patent application which goes into some detail about air cycle.
http://www.faqs.org/patents/app/20090133431
Two valuable bits of info I gleaned before my eyes glazed over:
1) They are seeking to operate at 80 to 100K RPM!!
Mmm.. yeah, turbines are turbines I guess.
I was just reading something about the Turbo-expanders used for liquefaction of Gases. Some operate up to 1,000,000 RPM.
But we are not trying to liquefy helium so...
These things come in all kinds of sizes from giant industrial turbines to dime size micro-turbines, but they all seem to operate on more or less the same principle, that is, to extract heat/energy from the gas by making the gas (air) do work against some load on the turbine.
2) They are asserting the need for very fine tolerances between the turbine and the housing, here referred to simply as "microscopic" or "minuscule". (Of course, they are not using Tesla turbines and I am wondering the reasons for this? One assumes there are reasons.)
These types of issues will keep me out of the game if they persist. But not to give up yet...
My rational for using a Tesla Turbine is 1) not just easy but actually POSSIBLE for me to build. Any other kind would be pretty much impossible. 2) should be relatively easy to balance 3) Quiet !!!!!
I've seen there are a lot of patents. Not much else. I've been ignoring the patents because, anybody can get a patent these days for any hair brained idea, it doesn't necessarily mean it will work or that the information is accurate IMO.
Personally, I don't think that there is much point in worrying about the turbine.
The sizing of the turbine would depend on how much, if any compressed air can be delivered to it - at what volume and pressure.
I'd start
very cautiously with a simple displacer chamber. Make a few check valves and see if it will pump any air at all.
I say
cautiously because heating up a can that has no piston to relieve the pressure could probably be dangerous. Ultimately this is pumping air into some kind of tank or tube. I don't know what kind of pressure could be built up but generally speaking, any kind of tank that is supposed to hold gas under any pressure has to be specially made, Compressor tanks, propane tanks etc.
I think the best thing for a turbine might just be a regular pneumatic air tool of some sort. At least these are made to run on compressed air and not fly apart, and I know they can produce cold air...
They sell special antifreez, just for that reason.
"pneumatic tools can experience downtime from freezing caused by the formation of ice in and around exhaust ports and valves"
Speedynails
I've seen this happen plenty of times while working in a mechanic shop in Arizona in HOT weather when using various air tools.
I don't really think it matters that much what kind of work the gas does, it just has to be made to do work and then the turbine or whatever would have to be well insulated against the heat of the environment.
Of course, though, I have no real idea what I'm talking about.