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#21
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How about a slinger followed by a felt seal? The slinger can be made
from an o-ring. Felt will catch any tramp oil, is cheap, & can run dry. The felt will wear. It's used in many older aircraft wheel bearings (even some newer ones, and it doesn't work that well. It has to be saturated with grease to prevent water uptake, and thereby attracts dust. If it soaked up oil it would become saturated and allow the oil past. Autos and trucks abandoned felt seals in the '40s and '50s. Dan |
#22
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Me,
I am (was) a kit builder. 200hrs PPL, now flying the completed kit 18 months, 84hrs. Guess thats why I am complaining since there was little "bad" vacuum pump info available to me as a builder. I do have a science/engineering background. Hey, I am also a fellow Canuck but living in US now. Wish I had the money back for all things I tried that didn't work out as well. ------------------------------------------------ SQ2000 canard: http://www.abri.com/sq2000 wrote: .... What's your experience?... |
#23
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If the pump ran for the life of the engine TBO, who
would make money on that!!!!! For a sealless drive use a magnetic coupling similar to: http://www.micropump.com/tech_tips/magnetic_drives.asp Reggie |
#24
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It would be nice to use a magnetic coupling, but the power
transfer in these pumps is too much. The mag coupling has been around for years and the vac pump manufacturers would be aware of it. Another problem with magnets: they'd be close to the magnetic compass, being on the back of the engine in most cases, and we have enough trouble with magnetic fields as it is when we go to calibrate compasses. "abripl"'s solution of an electric drive, especially if it's away from the engine, is alright as long as he doesn't intend to fly IFR, unless he has a vacuum-driven turn coordinator. Most TCs are electric, and with attitude and heading gyros relying on an electrical source all attitude info would be lost if the electrical system quit, which they can do at the worst possible times. I haven't yet dealt with the new glass panels, but would hope that they'd have some backup power; the ones I see have peanut gyros in the panel as backups. Dan |
#25
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"abripl"'s solution of an electric drive, especially if it's
away from the engine, is alright as long as he doesn't intend to fly IFR, unless he has a vacuum-driven turn coordinator. Actually it was not a solution for my vaccum pump but I simply went to an electric horizon - removing the vacuum. I only use the electric horizon (plus altimeter and speed ind.) as backup. I use Dynon's EFIS-D10 for my primary flight instruments - and have the necessary IFR certifications. You can see the panel on bottom of http://www.abri.com/sq2000/choices.html |
#26
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Most TCs are electric, and with attitude and heading gyros relying on an
electrical source all attitude info would be lost if the electrical system quit, Oh that. I have a dual battery system and my EFIS-D10 has its own internal backup battery to last an hour. The dual batteries have 40amp-hour total capacity and normal flight current is only about 12A. Read more details at http://www.abri.com/sq2000 |
#27
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MAGNETIC pump drive
From: Date: 23 Sep 2005 08:31:24 -0700 Local: Fri, Sep 23 2005 8:31 am Subject: Problems with Rapco dry vacuum pumps. Dan wrote: It would be nice to use a magnetic coupling, but the power transfer in these pumps is too much. The mag coupling has been around for years and the vac pump manufacturers would be aware of it. Another problem with magnets: they'd be close to the magnetic compass, being on the back of the engine in most cases, and we have enough trouble with magnetic fields as it is when we go to calibrate compasses. Dan ^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^^ http://www.manufacturingcenter.com/d...ustonemore.asp The drives are manufactured by MagnaDrive Corp, Seattle, WA. Suited for motors from 10 to 1000 hp, the company's drives and couplings, according to Ron Woodard, MagnaDrive president and CEO, "also eliminate hard starts and much of the vibration associated with power transfer, allowing M-I/SWACO to redesign their oil centrifuges with fewer control systems and with a smaller footprint." ********************** THEREFORE Dan, Your torque limit is a design / weight problem, not a technology limit. (Reggie) ************************************************** ************************************* http://www.sacskyranch.com/rapco.htm The Edo(or Sigma-Tec) quill-shaft is designed to fail at 100 inch-pounds of torque, whereas Airborne drive takes (250 inch-pounds) to snap . Therefore it's not a lot of torque required, and you would not need the break away coupling as the magnetic field does that.... (Reggie) ************************************************** *********************************** As far as the magnet compass problem Beware of: Alternators, especially permanate magnetic ones. Elecrtic gyro instruments. Too closely placed electric vaccuum pumps and Magnetized steel air frame structure. Reggie |
#28
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You're right. There would be plenty of torque transfer available for
a vacuum pump. Now someone needs to try it. Dan |
#29
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Tim,
Wish you posted this before. I kind of suspected possibly cleaning it but was afraid of messing it up. I sent it back to Rapco who refused to warranty service it but gave me a discount deal on a new replacement pump. Tim Hickey wrote: ..... If you do not hear the vanes fall, they most likely are "hung up" due to some contamination. Open the pump, and clean everything. Put it back together. I use a little silicon seal to act as a gasket on the back joint of the pump. I think that the pumps fail when the vane gets sticky and refuses to slide in and out of the slot in the rotor. I know that the slots in the rotor will wear larger eventually, but I listen to my pump every 25 hours at the oil change and have had to clean the pump twice in the last 250 hours. The pump now has about 800 hours on it. ..... |
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Thread | Thread Starter | Forum | Replies | Last Post |
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