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Re: trantorque gt for rsg motor attachment and maybe electrodes?
Original poster: FIFTYGUY@xxxxxxx
In a message dated 4/4/06 1:16:28 AM Eastern Daylight Time, Dr. Cox writes:
>This sounds like unsafe engineering practice.
I would argue this. Let's do some actual engineering before
condemning anything:
Refer to
<http://fennerdrives.com/keyless_bushings/ttqtech.pdf>http://fennerdrives.com/keyless_bushings/ttqtech.pdf
Let's say our RSG uses a NEMA 56 framed motor. Shaft diameter is
5/8". Let's say we're using a 1 HP motor, and use that figure for the
caluclations, although that's a little on the large side for the
average RSG and we know the HP drops dramatically with the
salient-pole modification. We'll also say typical 1800 RPM motor.
Running torque = 1 * 5750/1800 = 3.2 ft-lbs or 38 in-lbs. Let's
worst-case the starting torque for our synch motor at an extremely
conservative four times that, at 153 in-lbs. Let's get ultra-paranoid
and call it a "heavy shock load" (as the manufacturer would call
"punch presses", "hammer mills", "crushers", "pulverizers", or
"piston compressors" driven by a "multi-cylinder engine"). The
service factor then doubles the torque requirements, in our case to
306 inch-lbs.
Now looking at the specs for the Trantorque "Mini" series, the
smallest construction they offer, the 5/8" shaft size is rated for
450 in-lbs, well over our extremely worst case. The equivalent
"standard" bushing is rated for 1750 in-lbs. Even the "Narrow"
series, for thin rotors (3/8" in "Mini" and 1/2" in "Standard") are
still within the above requirements.
They also make "Non-Transversing" models, which prevent axial
movement while being tightened. This would be great for maintaining
electrode spacing when removing/installing the rotor. And even these
are within our requirements.
Minimum hub diameter for above applications (to resist rotor
breakage from the Trantorque expansion on installation) is also well
within the bounds of good taste for any reasonable RSG rotor -
nobody's running a 3" diameter rotor off a 1 HP motor are they?
In your favor, however, the application data for the Trantorque says:
"Synthetic Mounted Components
Trantorque GT units are not recommended for use with any
component completely constructed of a synthetic material. Most of
these types of materials have a certain amount of creep under load
which will cause loosening over time. A Trantorque GT unit can be
used if the bore of the synthetic component incorporates a
reinforcing metal sleeve."
G-10, "red fiberglass", etc. probably have very low creepage.
After all, they're widely used in critical structural applications
for commercial electrical equipment (and switchgear). Pressing in a
metal bushing would be an easy way to comply with the manufacturer's
recommendations. Not to mention, if creepage is an issue, the
"throughbolts and hub" method would suffer as well. So would the
typical "radial setscrew" method for the flying electrodes.
And my original caveat still stands - lock everything down with
retaining compound.
>It's probably best to use a 3 inch dia. alum. hub with 5-6 equally
>spaced fasteners that extend all the way thru the G-10 and then
>thread into an aluminum "backblock".
One could argue it would be safer engineering practice to
accomplish the same task with fewer parts, thus reducing the
possibilities of failure. In this case the multiple fastening bolts
wouldn't necessarily be redundant, as the loosening or failure of
only one would cause catastrophic failure of the entire system
(off-balance rotor would wobble and crash electrodes).
-Phil LaBudde