Betatronics®

PO Box 1288, 2286 S. Industrial, Ann Arbor, MIchigan 48106-1288
voice 734-930-6136

This web site is http://www.beta-aa.com      Our e-mail address is info@beta-a2.com

HOME page ( beta-aa.com/index.html )
AXLE ASSEMBLY page       AXLE PHOTOS page
GEAR RATIO MEASUREMENT page       This is PIN PRELOAD PLOT page
MISCELLANEOUS & UNRELATED INFO page       MISCELLANEOUS PHOTOS page
INFORMATION on Ford Rouge Factory Tours at www.hfmgv.org/rouge/default.asp.
INFORMATION on Betatronics I232, E232, and TIMELOG at www.beta-a2.com.

CNC Communication and Industrial Gaging Equipment
Displacement - Torque - Force - Time Monitoring - Ratio - Backlash - Data Collection
Select Axle Assembly web page at the top for information on gaging. 

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* Axle Assembly --- Pinion Preload Adjust *



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A Pinion Preload Adjust Cycle Plot vs Time.

PA1 --- Pinion Preload Drag Torque vs Time and Corresponding Nut Torque vs Time Plot of a Trio Pinion Preload Adjustment Machine Cycle with an Aluminum Carrier, 1982.

This plot is from a Trio machine with Betatronics gaging equipment controlling the adjustment cycle. This is the first Trio machine that combined the two measurements and was installed in production in early 1982.

In 1972 Betatronics provided the first electronic control of pinion adjustment on a Trio machine installed at Pontiac Motor Div. of GM, and therefore probably any pinion preload adjust machine. Prior to that a force balance air switch was Trio's method. This line ran close to one part every 15 seconds. Two Trio machines were used to meet this thruput. Our initial experiments on line (this was a retrofit to existing machines) produced a lot of rejects and required 4 to 6 operators with impact wrenches to fix our rejects as we worked on parameter development. This equipment used analog circuits to amplify the straingage signal to the 1 volt level, but beyond this all processing was digital, including the threshold limits. This was without a microprocessor because it predated the availability of microprocessors.

The Trio machines support the pinion on a pair of centers, the carrier is free floating on it's bearings and restrained only by a force transducer used to measure the drag torque. This means there are no residual torque errors other than some very small errors in the transducer mechanism. There is an air motor (sometimes hydraulic) that is used to pre-rundown the nut to bring all components in contact with the collapsible spacer. This is done while the pinion is stopped. After pre-rundown the pinion is rotated and two clutches, fast and slow, are used to rotate, thru gearing from the same drive motor, the pinion nut relative to the pinion. Built into the nut driver shaft is a nut torque transducer. The Betatronics gage controls the pre-rundown time, the spindle motor speed, the clutches to achieve the desired pinion drag torque, and finally to test the drag torque and nut torque. Both drag torque and nut torque are compared with preset limits at the end of the cycle to determine if the part is a good part. Note, nut torque can not be controlled in a collapsible spacer application and it will be whatever it will be. Also nut torque is a function of nut angular velocity.

The plot shown above was made 3 Feb 1982 and had no seal because it was easier to assemble and disassemble for testing without the seal. The residual drag torque, about 1/2 #-in, before bearing contact is due to the carrier weight on the inner bearing. This increases just slightly before bearing contact because the outer bearing starts to make contact. With a seal installed this residual drag torque typically would be 3 to 4 #-in higher and more noisy.

In this application the bearings and flange are pre-pressed to contact the collapsible spacer, and the nut is finger started about one thread. The carrier is then loaded into the machine and the cycle started. The carrier is raised and the centers are engaged. A "regulating unit" is brought into the tube bore. The "regulating unit" is the torque transducer, and restrains rotation of the carrier.

The driver that engages the flange or yoke is locked and does not rotate. The clutches are disabled and an air motor rotates the nut thru a one-way clutch until stall. In this particular cycle stall occurs at 4 seconds. The prevailing torque of the crimped nut is about 30 #-ft. You see a gradual buildup to the full engagement of the crimp.

The peak torque at stall is about 140 #-ft and partly due to inertia. The steady state stall is about 120 #-ft. It is important that this stall torque be below the torque to collapse the spacer. Note, if the collapsible spacer is missing, then the unit will lockup from pre-rundown torque.

In a collapsible spacer product the design is such that there is guaranteed endplay at the start of the cycle. This is typically 1/16".

In this application pre-rundown was allocated a fixed 7 seconds, later applications are dynamic. After pre-rundown the pinion driver brake is released. Thus, you see the drag torque go from zero to about 1/2 #-in when the drive motor starts. After a 1 second test for excessive drag torque, someone may have left the collapsible spacer out, fast motor fast clutch is enabled. Here this occurs at 8.1 seconds.

This cycle the nut torque rapidly builds to about 145 #-ft where the spacer starts to collapse. Different individual spacers may have quite different characteristics even though from the same manufacturing batch. This torque gradually builds to about 230 #-ft and then remains approximately constant. During this time the drag torque does not change until bearing contact. After bearing contact drag torque rises at about 12 #-in/sec. This is fast motor fast clutch, 90 rpm for the motor, and about 6 rpm for the nut relative to the pinion.

At a preset threshold the fast clutch turns off and the slow clutch is engaged. Then somewhat higher the fast motor changes to slow motor. Final adjustment is slow motor slow clutch, and here drag torque rises about 3 #-in/sec. When final drag torque threshold is reached both clutches are turned off. A dwell is initiated, then drag torque is checked. Note that this part has almost 3 #-in peak-to-peak variation during the test period. This is primarily roller noise. The part should be tested for drag torque later, just before case is installed, because after banging around, being rotated, and other variations the torque may change, especially with an open cup situation.

This plot is very much an ideal build. A lot of parts do not build this well. There are many different shapes to the nut torque. The drag torque has a lot of noise during adjustment, some that is due to torsional vibration.

During the preload test period at the end of the cycle we check the peak to peak value against a limit, typically 6 #-in. This is to catch very bad bearings, bent stone shields, etc. The peak to peak magnitude is very much affected by the measuring system bandwidth. With a bad oil and a hand torque wrench I have seen peak to peak greater than 50 #-in on an axle with 20 to 25 #-in average torque. A twice per revolution variation may result from ovality, most likely bores. A once per revolution is a parallelism problem. And a variation slower than pinion velocity is most likely a cage problem. See photo P1 on AXLE PHOTOS page.

Total cycle time here is about 38 seconds excluding part loading.

Today, meaning late 90's and on, there is much more nut torque variation from nut to nut because cadmium plated nuts are banned.

Note 1:  If a search engine brings you to this site and you do not know why, then save this page to a file on your computer (under FILE you would use SaveAs) and after saving, then open the file with a word processor and search for the words individually that you used in your search.  For example if the words --- drag torque --- bring up this site and this page of this site, then you would first search for drag or torque and look around those locations.  Pick If_search to return to beginning.

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Copyright ©  2003, 2004, 2005     Gordon A. Roberts     All rights reserved.      050128-1130