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Post by finiteparts on Jul 17, 2018 20:22:18 GMT -5
Hi Patty,
Good to see the interior of a C30 again. First, I am assuming that you do not want to run this engine again. They are tough to get apart and without the factory tools, you will probably destroy it. The tolerances are so tight that they are easily damaged.
That being said, I have never witnessed the center section coming apart, just the engine dismantled to the state that you have it in. If you are trying to look at the air bearings, just look at the ones on the generator shaft. You won't have a thrust bearing, but you can get the basics of the bearing design from the radial air bearings used on the generator.
If you think about the nut holding the turbine onto the shaft, it has to hold the shaft tight while it is providing enough torque to turn the compressor and make an extra 30kW of generator power...so it is going to be tight! I have often thought that the little hex on the shaft can not be enough metal to hold the shaft still while you are removing the 12 point nut, but like I said before, I have never seen it separated. If you don't plan on running it again, then I would heat the shaft while trying to not heat the turbine to hopefully get the shaft to grow while the turbine stays about the same length, thus removing some of the clamp on the turbine tie-bolt.
Good luck!
Chris
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urbansound
Member
Joined: September 2018
Posts: 43
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Post by urbansound on Sept 29, 2018 12:12:02 GMT -5
Dry ice the shaft and heat the nut from one side only, stay below 600 degrees. This oblongs the nut diameter from the shrinking round shaft diameter.
Use an impact wrench. Static torque likely will not break the tension otherwise. If it's a dead horse, maybe a cut-off wheel is the answer. LOL
The kind of heat that turbine has to deal with plus torsional loads at high RPM / balance would require extreme press fit.
It's possible the turbine to shaft was cryo-mounted in the first place. One would almost expect to find a spline mount to carry the torque demands. Could that possibly be a solid assembly? I can't imagine that much stock removal.
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turbotom
Junior Member
Joined: June 2011
Posts: 58
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Post by turbotom on Oct 7, 2018 16:37:26 GMT -5
To tell from the considerable length of thread of the tie rod that still projects from the nut, I'ld say Capstone use a hydraulic puller to pre-tension the rod and then, after a predefined force is reached, the nut is just screwed home without any considerable torque. After that, the puller is released, voila. No chance to get that nut loose without the proper tool. On many (half-way) recent small turbines, the rotors are assembled that way. The advantage is that no torsional stress is introduced in the tie rod. See my page on disassembly of a T312, scoll down approx. two thirds: www.turbinemuseum.de/Gasturbines/KHD_T312/khd_t312.html . I had to make such a tool in order to disassemble the rotor. The rod on that engine is tensioned with 50kN! On the Capstone, it probably in the ballpark of 10 to 20kN. By the way, thanks for the teardown and the photos. I always wanted to have a peek into one of these engines. Interesting to see Capstone utilized rather "conventional" technology, at least turbomachinery-wise... Also quite peculiar that they trimmed back the exducer of the turbine wheel by a considerable amount. Someone must have screwed this up...
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Post by madpatty on Oct 7, 2018 16:45:10 GMT -5
To tell from the considerable length of thread of the tie rod that still projects from the nut, I'ld say Capstone use a hydraulic puller to pre-tension the rod and then, after a predefined force is reached, the nut is just screwed home without any considerable torque. After that, the puller is released, voila. No chance to get that nut loose without the proper tool. On many (half-way) recent small turbines, the rotors are assembled that way. The advantage is that no torsional stress is introduced in the tie rod. See my page on disassembly of a T312, scoll down approx. two thirds: www.turbinemuseum.de/Gasturbines/KHD_T312/khd_t312.html . I had to make such a tool in order to disassemble the rotor. The rod on that engine is tensioned with 50kN! On the Capstone, it probably in the ballpark of 10 to 20kN. It's strange and quite funny, I was just going through your other thread on Williams WR24 engine when you were reading mine. LOL. Thanks.
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Chuks
Senior Member
Joined: August 2015
Posts: 498
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Post by Chuks on Oct 8, 2018 2:04:30 GMT -5
Is that a 5.6:1 PR in a single stage centrifugal compressor wheel? Billet wheel..? Nice website when you want to know more...
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Post by ingeniero on Oct 26, 2018 23:02:00 GMT -5
Are you going to run this unit again? What kind of controls does it have.
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Post by madpatty on Oct 28, 2018 22:22:08 GMT -5
Are you going to run this unit again? What kind of controls does it have. I don’t think it can run again. Cheers.
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Post by 1000eemonarch on Jan 23, 2020 18:10:58 GMT -5
Why do I fear I'm going down the same road? Just got a Capstone C30 and a C60 to play with, and add to the collection of microturbines with direct-driven alternators...... www.youtube.com/watch?v=0hKs9s_J5ZkI'm going to try to get the C60 running.... For some reason I have a hankering to make a turbine-electric pickup truck
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Post by turboron on Jan 23, 2020 19:59:58 GMT -5
1000eemonarch, very interested in your Capstone project. Did you buy them at auction?
Thanks, Ron
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Post by 1000eemonarch on Jan 23, 2020 20:32:42 GMT -5
1000eemonarch, very interested in your Capstone project. Did you buy them at auction? Thanks, Ron Ebay.... I'll try to take videos how things go. Should be fun to see what's inside, how they run and what I do with them.
I've been thinking about playing with with one of these for a while, but my first hand-on experience.
Thanks, Alex.
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