Yagis are usually mounted to the mast at the balance point. This is almost
always not the center of the boom length because of the different element
lengths. As a result varying wind forces cause surging rotational force on
the mast and rotator. If you park the antenna with either boom end pointed
into the wind you can protect your antenna and rotator when you are not
operating. In my case the prevailing wind direction is nearly always from
the SSW.
It is possible to add a wind plate to the boom to take care of the
unbalanced wind force. Dick Weber, K5IU has published information on doing
this in Communications Quarterly for spring 1993, summer 1994, and winter
1995.
Dan, N5AR
On Tue, Oct 1, 2013 at 5:39 PM, Mike Reublin NF4L <nf4l@comcast.net> wrote:
> John,
>
> I have no explanation for the slippage, you didn't say if the U-bolts were
> loose. The U-bolts are also available from C.A.T.S. rotor service. I would
> use a lock washer and/or some Loc-Tite (the removable kind).
>
> You could also bend your own from all-thread. I've bought it in the past
> from my local big box store. I think, without any engineering data at all,
> the having threads bearing on the mast would give a slightly better grip.
> Then there's the slipp-nott http://www.tennadyne.com/slipp_nott.htm
>
> Good luck & 73.
> Mike NF4L
>
>
> On Oct 1, 2013, at 8:00 PM, John Becker <johnb3030@comcast.net> wrote:
>
> > My mast has slipped about 30 degrees in the rotor after over four years
> with no slippage. Prior to noticing this I wasn't aware of any recent windy
> days. Before taking corrective action, I'm thinking about why this has
> happened now and how to most likely prevent a future occurrence.
> >
> > The rotor is a HAM-III in a Rohn 25 top section with a Rohn TB-3 thrust
> bearing. The antenna is a KT34-XA mounted two feet above the thrust
> bearing. This antenna has been up since 1981 and mast slippage has occurred
> previously a few times but only when there has been unusually high wind.
> >
> > One of the first things I found is that these rotors apparently use
> non-standard size U-bolts. They are 1/4-20 stainless steel with a 2.25"
> inside dimension. The only source I found for replacements is Hy-Gain, now
> a division of MFJ. I wonder if they are making their own U-bolts? I was
> unable to find anyone else selling 2.25" ID U-bolts smaller than 5/16-18.
> >
> > I looked for the correct torque spec for bolt tightening. For 1/4-20
> stainless, the Standard Dry Torque spec is 75 inch-pounds or 6.25
> foot-pounds. This is for a bolted joint and I wonder if it also applies to
> a U-bolt? I did some testing with a spare rotor, a short piece of mast and
> a torque wrench. I lubricated the threads to prevent thread galling.
> >
> > 75 inch-pounds is not very tight, definitely less than I would have
> tightened them if just going by what feels reasonable to me. I gradually
> increased the torque to 200 inch-pounds, which is the upper limit of my
> smaller torque wrench. I was expecting the U-bolt to fail at less than 200
> inch-pounds but it did not. I left it at 200 inch-pounds for several days
> to see if there would be a delayed failure but it held. However, 200
> inch-pounds feels too tight to me for a 1/4" bolt.
> >
> > Due to the design of the HAM series rotors, the rotor casting contacts
> only the center 1.5" of the 2.25" ID U-bolt. This permits progressive
> tightening of the U-bolt to cause the shape of the U-bolt to distort, going
> from a "U" shape to a rounded "V" shape. It was necessary to tighten the
> nuts on both sides of the U-bolt by roughly 1/8" to increase the torque
> from 75 inch-pounds to 200 inch-pounds.
> >
> > I'm wondering if this distortion of the U-bolt also occurs slowly over
> time, resulting in a gradual loosening of the U-bolt? This could explain
> why mast slippage becomes a problem as time progresses.
> >
> > Another possibility that comes to mind is that the normal stresses that
> occur each time the rotor starts and stops might gradually cause the nuts
> to loosen in the absence of rust to hold them in place. I plan to add
> stainless steel nylon insert lock nuts on top of the standard nuts on the
> U-bolts to prevent this.
> >
> > The U-bolt that had been tightened to 200 inch-pounds was distorted to
> the point that it was very difficult to get it out of the rotor casting.
> There were obvious bends in the threaded portion just below the nuts. This
> is another indication to me that 200 inch-pounds is too tight, and I would
> not have used this U-bolt on my rotor.
> >
> > I decided to continue the experiment by straightening the test U-bolt
> and tightening it with a larger torque wrench until it failed. However, I
> didn't get to the point of using the larger wrench because as I was
> re-tightening it, this time it failed at between 150 and 175 inch-pounds.
> Undoubtedly the operation of straightening it weakened it further than it
> already was, and I don't have another spare U-bolt to sacrifice.
> >
> > There have been discussions of mast slippage on this list in the past,
> but I don't recall anyone discussing the optimum U-bolt tightening torque.
> Possibly I just missed seeing it.
> >
> > Suggestions and discussion about how to alleviate this problem would be
> appreciated. Thanks!
> >
> > 73,
> >
> > John, K9MM
> >
> >
> >
> >
> >
> >
> >
> >
> >
> >
> >
> > _______________________________________________
> >
> >
> >
> > _______________________________________________
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>
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--
Dan Hearn
N5AR
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