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Author Topic: Unstable bellcranks >< self centering bellcranks  (Read 763 times)

Offline Paul Van Dort

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Unstable bellcranks >< self centering bellcranks
« on: February 02, 2026, 01:54:22 PM »
Another thought about bellcrank design. Usually, at least in my aircraft, the holes for the bellcrank pivot and the leadout connections are aligned. Some very successful models have the leadout connections slightly further (e.g., 1 cm) towards the leadout guide. This creates a kind of overhang on the bellcrank similar as on the handle. This would provide extra inherent stability to the model itself. These pilots then fly with a handle with minimal overhang. I can understand it, but I prefer the overhang on the handle so I can play with that parameter without having to adjust my model. I have handles with varying degrees of overhang. A lot of overhang in calm conditions. Little overhang in heavy winds.
It's clear that in strong winds with higher speeds, in loopings, a large overhang requires more steering force. You have to twist harder against the centrifugal force. Much less twisting with zero overhang, but still clearly noticeable because the pivoting is not on the handle, but rather on the wrist. I assume a selfcentering bellcrank is not helping here either.
If you follow this line of thinking, namely that strong winds make steering more difficult, why not destabilize the bellcrank by shifting the leadout connections on the bellcrank, towards the other side relative to the pivot? It seems to me that in such a case, the extra centrifugal force from the wind/speed could help you fly the figures with less steering effort. In lighter winds, you could compensate for the instability with a handle with more overhang. I did not find any experiments with this kind of setups on this forum..

Offline Howard Rush

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Re: Unstable bellcranks >< self centering bellcranks
« Reply #1 on: February 02, 2026, 04:46:58 PM »
Having bellcrank arms bent away from the circle center might be beneficial.  Tim Just reported that Phil Granderson's Olympic had such a bellcrank and had a great control feel.  Bellcrank arms bent away from the circle center would counter the effect of control surface aerodynamic hinge moment, but bellcrank arms bent in either direction would cause the controls to deflect as a function of total line tension.  This would make the airplane more sensitive to mistrim and could make it hard to fly accurately in turbulence.  https://stunthanger.com/smf/engineering-board/self-centering-ciphering/#google_vignette reply #4 compares hinge moment to bellcrank moment due to centrifugal force.  This is an ideal case.   More realistic would be to add some extra force (from excess tip weight, for example) and see what happens to the bellcrank bend angle curves.

Another problem that might occur when trying to compensate for control surface aerodynamic hinge moment with bent bellcrank arms is that those red and yellow lines on the PDF at the bottom of Reply #4 referenced in the previous paragraph might be really crooked.  That could make the combination of the the bellcrank-bend and hinge moment have a lumpy slope, causing particularly low stunt scores. 

edited to fix reference to pdf
« Last Edit: February 05, 2026, 01:22:15 AM by Howard Rush »
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Offline Dave Hull

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Re: Unstable bellcranks >< self centering bellcranks
« Reply #2 on: February 03, 2026, 02:58:58 AM »
Here is the bellcrank from the Granderson Olympic, after its demise. It looks pretty much like a stock J.Roberts crank like the C-25 that Brodak sells. The installation was nicely done. No question that the plane was flying very well in Tim's hands....

Dave

Offline Howard Rush

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Re: Unstable bellcranks >< self centering bellcranks
« Reply #3 on: February 03, 2026, 12:00:58 PM »
The JCT is always very
Innovative and contrary.
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Offline Dave Hull

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Re: Unstable bellcranks >< self centering bellcranks
« Reply #4 on: February 03, 2026, 08:13:10 PM »
Howard,

You have to remember to teach your new initiates to the JCT not to do combat with the ground! Flying an Oly is stunty stuff...and the ground should not be a tactic, even if they are feeling "contrary"...

The Divot

Offline Paul Van Dort

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Re: Unstable bellcranks >< self centering bellcranks
« Reply #5 on: February 04, 2026, 12:55:21 AM »


Another problem that might occur when trying to compensate for control surface aerodynamic hinge moment with bent bellcrank arms is that those red and yellow lines on file:///C:/Users/hmrus/Downloads/Stunt%20Plane%20Control%20Geometry%208%20SC%20Bellcrank%204-3.pdf might be really crooked.  That could make the combination of the the bellcrank-bend and hinge moment have a lumpy slope, causing particularly low stunt scores.

Thank you for the feedback. The pdf appears to be on your C-drive. I don't think it is accessible by me.

Offline Steve Helmick

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Re: Unstable bellcranks >< self centering bellcranks
« Reply #6 on: February 04, 2026, 01:17:30 PM »
The last SIG bellcrank introduced was of the self-centering or non-self-centering type, depending on whether it was installed correctly or incorrectly. I believe it was designed by Mike Pratt, who also designed the Primary Force and many other good stunt designs. On the Primary Force plans, the bellcrank is one of those, and it's shown installed "reversed", i.e., de-stablizing. The link shows a picture, now on the Brodak site. I'm not sure if this is the only 4" B.C. that Brodak sells. Steve
https://brodak.com/sig-4-nylon-bellcrank.html 
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Offline Howard Rush

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Re: Unstable bellcranks >< self centering bellcranks
« Reply #7 on: February 05, 2026, 01:16:04 AM »
Thank you for the feedback. The pdf appears to be on your C-drive. I don't think it is accessible by me.

Oh, sorry.  Here it is:
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Offline Motorman

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Re: Unstable bellcranks >< self centering bellcranks
« Reply #8 on: February 05, 2026, 08:53:20 AM »
Just put the holes straight across and go fly.
Wasted words ain't never been heard. Alman Brothers

Offline Ken Culbertson

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Re: Unstable bellcranks >< self centering bellcranks
« Reply #9 on: February 05, 2026, 11:28:42 AM »
I have only had an offset (away from the center) one time and I didn't like it.  It was probably not the bellcrank but I still never did it again.  Have we reached any form of answer here?  Which is in theory better?  My stash of 5" printed bellcranks are shaped to be drilled up to 5 degrees either way.

Ken
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Offline Brett Buck

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Re: Unstable bellcranks >< self centering bellcranks
« Reply #10 on: February 05, 2026, 11:37:55 AM »
I have only had an offset (away from the center) one time and I didn't like it.  It was probably not the bellcrank but I still never did it again.  Have we reached any form of answer here?  Which is in theory better?  My stash of 5" printed bellcranks are shaped to be drilled up to 5 degrees either way.

      I want my system to be neutral. But I note that we all used "straight" bellcranks for years that were unstable to various degrees without even realizing. I think Howard is working up to claim that while the bellcrank forces might be unstable but that when you hook it to a control surface, the system as a whole is stable (since while the bellcrank wants to deviate from center, the torque from the control surfaces is in the opposite direction). That would count on the restoring force from the surfaces to require torque faster for a given angle than the bellcrank provides. I don't know if it is true or not.

     Brett

Offline Jim Svitko

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Re: Unstable bellcranks >< self centering bellcranks
« Reply #11 on: February 08, 2026, 03:40:37 PM »
Like many others, I never realized that "straight" bellcranks (the leadout attachments and the bellcrank pivot on the same line) are unstable.   All of us compensated for it, somehow, and life moved on.  However, when I moved the bellcrank pivot outboard of the leadout connections, level flight was easier to maintain and l noticed less bounce in corners.

But, what is optimum for offsetting the bellcrank pivot?  Where is the neutral point?  With converging leadouts that have the same angle relative to the aircraft centerline, the intersection of lines drawn 90 degrees to the leadouts, thru the leadout connection points, will be the neutral point.  But, what if the leadouts do not have the same angle relative to the aircraft centerline?  I have seen plans where the front leadout has a fair amount of sweep, and the aft leadout is nearly parallel to the wing trailing edge. 

Offline M Spencer

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Re: Unstable bellcranks >< self centering bellcranks
« Reply #12 on: February 09, 2026, 07:41:36 PM »
Id found the negitive offset leadouts , definately , when ' it was blowing ' so the handle was ' loaded up ' -
 ;
That , in rounds , the pulled line had way more load , than the other . SO you let the bottom off the handle do the ' fine toonin ' . i.e. de egging .
as it was way more sensitive & lighter . than the one trying to pull you over .    ;D  ( Bobs ' top & bottom ' control ! )

This thing had a heavy 3/8 thick wall aluminum pushrod . As a ' damper ' . And Ears on the elevator ends . To balance control loads .
Flying light in clean air , there was alost a ' schnick ' ( as it were ) as you ( with familiarity ) threw on or reversed control .
As in ' 8 ' intersections , etc . more dicernable .

As this one never hit the deck , despite flying in 20 / 25 mph winds , at times . And downdrafts & turbulance from trees . I thought it o.k.
Sort of winds that hold it down & delay vertical turn downwind . WHICH brings up ' Tracking ' & ' Groove ' which it'd do . Even on an aft C G .
( High Point of airfoil / AT bellcrank pivot .

So theres a thing .

Flaps & tail were TOUGH  New Guinea Quater grain , so stiff . Tho I thought the elevator horn coulda been stiffer . Re the ' Hold Down ' mentioned .
This thing atb 70 ounces twanged  7 strand steel 18 thou. lines in lower Sq  turns , when you needed two hands ( and golf shoes on the damp field )
and stretched .016 solids discernably . When the gales off November came early . as it were . was .

BUT . the Bellcrank - gave that ' schnick / schnick ' control precision /in ordinary conditions . When the lines wernt stretching .
On the 16s in gales it gave the elastic rubbery feel , under duress ( working hard manouvreing . Did the full schedule nearly all flights )

SO . Ya gotta watch yer rubbery lines arnt attributeinng to your ' control issues ' . Missdiagnoseing darting dodgeing flight as aircraft . When its actually your control wires .

Pitcher offittr , for the reckoid .

« Last Edit: February 09, 2026, 08:20:57 PM by M Spencer »


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