kilrbee
Chemical
- Sep 2, 2006
- 41
Presently have a turbo that is run off the right side of the map, NE side of the map to be precise. It runs into very low efficiency numbers, and the boatload of heat it is crating is problemeatic. GT40 compressor, with inlet temps of 220F, higher elevations, trying to push 50 lb/min, at 25-29 psig discharge. Temps up to 600 F at discharge. I am planning to evaporate up to 15 gpm using the disturbance potential of the compressor to obtain quasi-isothermal compression. I believe I will reduce discharge temps at least 150 degrees.
I am looking at designing a waternozzle mount, 30mm in front of the compressor. Are there any likely concerns for inducing surge? Anyone with experience with resonance failure of such a device? I have modeled it with 3 radial ribs that appear like an airfoil, center mounted nozzle.
Any feedback appreciated.
I am looking at designing a waternozzle mount, 30mm in front of the compressor. Are there any likely concerns for inducing surge? Anyone with experience with resonance failure of such a device? I have modeled it with 3 radial ribs that appear like an airfoil, center mounted nozzle.
Any feedback appreciated.