New Technologies for Military Track Bushing Accelerated

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New Technologies for Military Track Bushing Accelerated
Testing and Evaluation
Scott Gruenberg, Scott Bradley – Keweenaw Research Center,
Michigan Technological University
Stephen Gentner, David Ostberg - TARDEC
25 August 2014
UNCLASSIFIED: Distribution Statement A. Approved for public release
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Outline
• Introduction
• Background
• Track Bushing Architecture
– Single Pin
– Double Pin
•
•
•
•
•
•
MIL-DTL-11891G Appendix A
Double Pin Field Test
Full Pitch Bushing Test Machine
Hall Effect Transducer Technology
Path Forward
Conclusions
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Introduction
• The life expectance of most track systems is governed
by the life of the elastomeric components
• Ground Pads normally fail first – However they are
replaceable on most US track system (exc. T107/M88
Hercules)
• Bushings are the usual cause of failure for most track
systems - only replaceable at a depot level through
rebuild
• Backing Rubber has become a close second
• On Vehicle testing is very expensive compared to lab
tests
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Background
• Laboratory bushing testing developed by TARDEC
decades ago
• Part of MIL-DTL-11891(G) Appendix A
• All Bushing compounds for all track systems (except the
M1) need to be tested per this Specification
• Originally developed to weed out sub-standard
compounds, adhesives, manufacturing process, etc
• Current test is for a single-pin track bushing and is not
representative of the double-pin track used by current
fleet of tracked vehicles
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MIL-DTL-11891 Appendix A
• T130 Long Bushings
• Test simultaneously applies:
– Radial Load of 0-5200 lbs at 64 ± 1 cpm
– Torsional deflection of +15° to -15° at 256 ± 4 cpm
• 75°F Ambient Temperature
• 9 total bushings tested
‒ 8 lowest tests must average > 130,000 radial cycles
‒ None of the 9 can have less than 110,000 radial cycles
‒ .145 inch deflection defined as failure
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MIL-DTL-11891 Appendix A
• T130 Long Bushings
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• Test Machine
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MIL-DTL-11891 Appendix A
• T130 Long Bushings
• Test Machine
“Tensile” Side
This side looks
like it is brand
new
“Compressive” Side
This side experiences the
failure characterized by a
crush zone. No torsional
mode is seen.
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Track Bushing Architecture
• Single Pin Shoe Architecture
3/2 Lattice
Backing Rubber
Center Guide
Octagonal Pin
Grouser
Ground Pad
T 130
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Track Bushing Architecture
• Double Pin Shoe Architecture
Backing Rubber
Pin
Ground Pad
Grouser
Center Guide
T 150
T 161
End Connector
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Double Pin Field Test
• T158LL Bushings
• YPG Test
0 miles
‒ Top new bushings
1000 miles
‒ Bottom worn bushings
‒ 250 mile increments
between samples
2000 miles
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Double Pin Field Test
• T158LL Bushings
• YPG Test
‒ Complete bushing failure
in one track shoe.
‒ Radial Crush zone exists
‒ Torsional failure around
pin circumference also
seen in field test failure
mode
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Full Pitch Bushing Test
Machine
• Servo-hydraulic
• Capable of
testing small
T130 test bores
up full size T107
track shoes
• Programmable
• 30,000 lbs radial
• ± 20° torsional
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Full Pitch Bushing Test
Machine
• Measure and
Records
–
–
–
–
–
–
Radial Load
Radial Displacement
Torsional Angle
Torsional Load
Ambient Temp
Right and Left Shoe
Temp
• Records
– Radial and Torsional
Cycle Count
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Full Pitch Bushing Test
Machine
• Comparison of Edge Effect Crack Initiation
T158LL Outside Doughnut (End Connector Side)
Field Test Sample
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Lab Test Sample
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Full Pitch Bushing Test
Machine
• Comparison of Failure Mode
Field Test Sample
Lab Test Sample
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Full Pitch Bushing Test
Machine
• Comparison of Failure Mode
Abraded Material Found Between Interior Bushings
Field Test Sample
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Lab Test Sample
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Hall Effect Transducer
Technology
Track Pitch Showing the Location of the Hall Effect Sensors
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Hall Effect Transducer
Technology
Schematic of Pin and Track Pitch Showing the Location
of the Magnets and Hall Effect Sensors
Bushing 2
Bushing 6
Bushing 9
Bushing 13
HE1
HE3
HE3
HE1
7
5
3
1
8
HE2
6
HE4
4
HE4
2
HE2
Shoe2
Shoe1
HE1-Top
HE2-Bot
Inboard
Side
HE3-Top
HE4-Bot
HE1-Top
HE2-Bot
HE3-Top
HE4-Bot
Slave
Master
Outboard
Side
Top View
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Hall Effect Transducer
Technology
Schematic of Pin and Track Pitch Showing the Location
of the Magnets and Hall Effect Sensors
Binocular Tube
Track
Block
Track Pin
HE 1 & 3
12
deg
7 Deg
7 Deg
HE 2 & 4
Sensors
Locations
Wedge Bolt
Locking
Feature
Orientation
Magnets
End View
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Hall Effect Transducer
Technology
• T161 Instrumentation
Transducer
Location
Computer
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Data
Acquisition
Boards
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Hall Effect Transducer
Technology
• T161 Data From YPG – Southbound Laguna Paved
Disp (inch)
Sprocket
Road
Wheels
Idler
Sprocket
Rollers
Angle (deg)
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Hall Effect Transducer
Technology
• T161 Data From YPG – Southbound Laguna Paved
– Processed Data From Shoe in Sprocket
– Shows Bending of Pin
Length
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Conclusions
• Failure Mode of the Elastomer Bushing between the
Single Pin MIL-DTL-11891 Test and the T158LL Field
Failures do not Match
• Full Pitch Test Machine Failure Mode does closely match
the Field Failure Mode, however cycle count to mileage
relationship has not been established
• With the addition of the bushing displacement history
from the Hall Effect Shoe incorporated into the Servohydraulic machine, closer correlation should be acheived
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Path Forward
• Characterize TRADOC OpMode Courses at YPG with
T158LL Hall Effect Shoe
• Process Data from Courses and Determine “Damaging
Content” of the Load Case
• Develop Load Profile Data File of “Damaging Content” to
be Run on the New Full Pitch Bushing Test Machine
• Correlate Failure Modes, Cycle to Mileage Relationship,
Etc.
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Questions
???
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