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9/20/2015Group 13
Final Presentation
By: Brendan Keane, Logan McCall, Reggie Scott, Mark Swain
Instructor: Dr. Nikhil Gupta
Sponsor: Dr. Philip Flater (Air Force Research Laboratory Eglin AFB)
Advisor: Dr. Simone Hruda
9/20/2015
Group 13 Speaking:
1 of 27 Final Presentation
 Introduction
 Design and Analysis
 Prototype Testing
 Project Management
 Conclusion
Overview
Reginald Scott
Group 13 Speaking:
2 of 27 Final Presentation
9/20/2015
 Current torsion tester at the
Air Force Research
Laboratory (AFRL) Munitions
Directorate at Eglin AFB is
approximately 5 meters in
length
 Small sample geometries
result in inaccuracy and
inefficiency
Introduction
Figure 2.1: Existing Torsion Machine
“DISTRIBUTION A: Approved for public release, distribution unlimited. (96ABW-2014-1649)”
Reginald Scott
Group 13 Speaking:
3 of 27 Final Presentation
9/20/2015
 Small specimens are a
result of original plate
stock dimensions
 Specimens tested:
 Aluminum 2024
 Titanium 64
Specimen Geometry
Original plate stock
Blank removed
Sample machined
Figure 3.1: Specimen production
Dimension Measurement (mm)
Total Length 58.4
Gauge Length 12.7
Width 14.3
Inner Diameter 9.09
Fillet Radius 27.9
Grip Length 20
Table 3.1: Specimen dimensions
“DISTRIBUTION A: Approved for public release, distribution unlimited. (96ABW-2014-1649)”
Reginald Scott
Group 13 Speaking:
4 of 27 Final Presentation
9/20/2015
 Maximum torque output: 100Nm
 Machine must fit in an area (footprint) of 1m2
 Monotonic (one direction) free-end torsion loading
 Free end must allow for axial motion
 Compatible with measurement equipment used by AFRL
 Budget - $2,000
Design Requirements
Reginald Scott
Group 13 Speaking:
5 of 27 Final Presentation
9/20/2015
Goal Statement:
Design a more effective way of testing small specimens in
free-end torsion
Design Requirements
Reginald Scott
Group 13 Speaking:
6 of 27 Final Presentation
9/20/2015
DIC (Digital Image Correlation)
“DISTRIBUTION A: Approved for public release, distribution unlimited. (96ABW-2014-1649)”
Figure 6.2 Example DIC use in torsion
sample
Figure 6.1 DIC setup at Eglin AFRL
Brendan Keane
Group 13 Speaking:
7 of 27 Final Presentation
9/20/2015
 Current method used by
AFRL to measure applied
stress:
 Strain gage placed on
elastic bar
 Use shear modulus
relationship to output
stress
Load Measurement
Figure 7.1: Stress vs. strain plot showing the
shear modulus relationship
G =
𝜏
𝛾
Brendan Keane
9/20/2015
Group 13 Speaking:
8 of 27 Final Presentation
Torsion Tester
Load Generation
Manual Power
Motor & Transmission
Load Application Gripping Mechanism
Load Measurement Compatibility
Linear Motion Friction Reduction
Frame
Material Selection
User Safety
Breakdown of Design
Brendan Keane
9/20/2015
Group 13 Speaking:
9 of 27 Final Presentation
Load Generation
Design Cost Weight Accuracy Complexity Maintenance Variability Total
Weight Factor 0.25 0.05 0.25 0.1 0.1 0.25
(1) Crank System 5 3 1 5 5 1 2.9
(2) Hydraulic 1 1 5 1 1 5 3
(3) AC Motor 3 3 5 3 3 5 4
(1) (2) (3)
Brendan Keane
9/20/2015
Group 13 Speaking:
10 of 27 Final Presentation
Load Application
Design Cost Weight Reliability Complexity Variability Total
Weight Factor 0.25 0.15 0.3 0.1 0.2
(1) 3-Jaw Chuck 5 5 5 3 5 4.8
(2) 4-Jaw Chuck 3 5 5 3 1 3.5
(3) Self-Aligning
Vise
3 1 3 5 5 3.3
(4) Collet 5 5 5 3 1 4
(1) (2) (3) (4)
Brendan Keane
9/20/2015
Group 13 Speaking:
11 of 27 Final Presentation
Linear Motion
Design Cost Weight Durability Complexity Total
Weight Factor 0.4 0.2 0.2 0.2
(1) 4 Rail Ball
Bearing Guide
1 2 1 1 1.4
(2) 2 Track Roller
Bearing Guide
3 5 5 5 4.2
(3) 2 Rail Ball
Bearing Guide
5 5 3 3 4.2
(1) (2) (3)
Brendan Keane
9/20/2015
Group 13 Speaking:
12 of 27 Final Presentation
Frame
 Design Considerations:
 Strength
 Machinability
 Weight
 Cost
 Material Selection:
 Steel
Figure 12.1: Frame design
Brendan Keane
9/20/2015
Group 13 Speaking:
13 of 27 Final Presentation
Concept Evolution
Brendan Keane
9/20/2015
Group 13 Speaking:
14 of 27 Final Presentation
Figure 5.1: CAD representation of design
Design Overview
Logan McCall
Steel Shaft
32”
13”
Group 13 Speaking:
15 of 27 Final Presentation
9/20/2015
 Vendor: Grainger
 Rpm: 18
 Gear ratio: 95:1
 Max torque: 116 Nm
 Weight: 26 lbs
Load Generation: AC Gearmotor
Figure 15.1: AC Gearmotor
Logan McCall
Group 13 Speaking:
16 of 27 Final Presentation
9/20/2015
 Vendor: Automation
Direct
 Single phase input, three
phase output
 Digital keypad
 Forward and reverse
 Expandable
Motor Control: VFD
Variable Frequency Drive (VFD)
Figure 16.1: VFD keypad
Logan McCall
Group 13 Speaking:
17 of 27 Final Presentation
9/20/2015
 Vendor: LittleMachineShop
 Weight: 6.4 lbs
 Outer diameter: 3.94 in (10 cm)
 Inner diameter: 1.02 in (2.59 cm)
Load Application: 6-Jaw Chuck
Figure 17.1: 6 Jaw Chucks holding specimen
Logan McCall
9/20/2015
Group 13 Speaking:
18 of 27 Final Presentation
Load Measurement
 Coupler material: Al 6061
 Coupler properties
 Shear modulus: 26 GPa
 Shear strength: 76 MPa
 Outer diameter: 1.75 in (4.45 cm)
 Inner diameter: 0.75 in (1.90 cm)
Figure 18.1: FEA performed on coupler
showing strain developed under a
simulated load
Logan McCall
Group 13 Speaking:
19 of 27 Final Presentation
9/20/2015
 Vendor: Grainger
 ½ inch steel rails
 Slot design to ensure
alignment
Linear Motion: 2 Rail Ball Bearing Guide
Figure 19.1: Linear guide system
Logan McCall
9/20/2015
Group 13 Speaking:
20 of 27 Final Presentation
Frame Design
 Steel frame
 Shape: hollow square
shaped cross-section
 Dimensions:
 1/8 in inner supports –
304 stainless steel
 1/8 in outer frame –
low carbon 1015 steel
Figure 20.1: CAD drawing of frame (bottom view)
Logan McCall
9/20/2015
Group 13 Speaking:
21 of 27 Final Presentation
Final Design
Logan McCall
9/20/2015
Group 13 Speaking:
22 of 27 Final Presentation
Prototype Testing
Mark Swain
9/20/2015
Group 13 Speaking:
23 of 27 Final Presentation
 Tester was successful in breaking
aluminum specimen
 Fracture was at center
 During initial testing, free end chuck had
slight rotation
 Solution: Force fit new connecting
rod into free end
 Cylindrical grips slipped during initial
testing
 Solution: Use hex-grip specimen or
increase friction on cylindrical
specimen
Testing Results
Figure 23.1: Fractured
specimens
Mark Swain
9/20/2015
Group 13 Speaking:
24 of 27 Final Presentation
Budget
44%
25%
18%
10%
3%
Load Generation Load Application
Linear Motion Housing
Miscellaneous
 Budget: $2,000
 Spent: $1,844
 Net: + $156
Mark Swain
9/20/2015
Group 13 Speaking:
25 of 27 Final Presentation
Project Progression
Fall
 Background research
 Design breakdown
 Component research
 Design analysis
 Optimal part selection
 Budget breakdown
 Purchase orders
Spring
 Delivery of parts
 Machining
 Assembly
 Motor/VFD testing
 Prototype testing
 Troubleshooting
 Final assembly
Mark Swain
9/20/2015
Group 13 Speaking:
26 of 27 Final Presentation
Conclusion
 Maximum torque output: 100Nm
 Machine must fit in an area (footprint) of 1m2
 Monotonic (one direction)free-end torsion loading
 Free end must allow for axial motion
 Compatible with measurement equipment used by AFRL
 Budget - $2,000
Mark Swain
9/20/2015
Group 13 Speaking:
27 of 27 Final Presentation
 The team was successfully
designed and
manufactured a tabletop
torsion tester for AFRL
 What we learned:
 Focus on the main
customer requirements
 Consult as many
resources as possible
 Teamwork is essential
 Unforeseen
circumstances
Conclusion
Figure 27.1: Final assembly
Mark Swain
9/20/2015Group 13
9/20/2015
Group 13 Speaking:
29 of 27 Final Presentation
 Carter, B. (2008). Texas Instruments: Op Amp Noise Theory and Applications. Retrieved
September 22, 2014
 Flater, P. (2014). Tabletop Torsion Test. Eglin, FL: Air Force Research Laboratory.
 Ilic, M. (2014, October 11). Clamp for centering. Retrieved from GRABCAD:
https://grabcad.com/library/stega-za-centriranje-clamp-for-centering-1
 Lathe Chuck. (2014, October 7). Retrieved from GRABCAD:
https://grabcad.com/library/lathe-chuck-3
 Linear Motion Systems. (2014, September 28). Retrieved from Stock Drive Products:
https://sdp-si.com/eStore/coverpg/linearmotion.htm
References
Mark Swain
9/20/2015
Group 13 Speaking:
30 of 27 Final Presentation
9/20/2015
Group 13 Speaking:
31 of 27 Final Presentation
9/20/2015
Group 13 Speaking:
32 of 27 Final Presentation
Fall Gantt Chart
9/20/2015
Group 13 Speaking:
33 of 27 Final Presentation
Spring Gantt Chart
9/20/2015
Group 13 Speaking:
34 of 27 Final Presentation
Specimen Dimensions
Brendan Keane
Units in inches
9/20/2015
Group 13 Speaking:
35 of 27 Final Presentation
Appendix
9/20/2015
Group 13 Speaking:
36 of 27 Final Presentation
9/20/2015
Group 13 Speaking:
37 of 27 Final Presentation
Part # Part
Name
Description Quantity Unit
Cost
Supplier Cost
Load Generation
6Z404 Motor AC Gear Motor, 18rpm,
TEFC, 208 - 230/460V
1 $601.56 Grainger $601.56
GS2-
10P5
VFD Variable Frequency Drive,
0.5 HP, AC Drive
1 $166.00 Automation
Direct
$166.00
Load Application
2276 Lath
Chuck
6-Jaw, 4" Outer Diameter 2 $174.95 Little
Machine
Shop
$349.90
Linear Motion
2HXB4 Rails 0.5in Thick(Annealed
Shaft, Steel, 0.500in
D,16in)
2 $41.80 Grainger $83.60
2CNL6 Pillow
Blocks
0.5in. (PillowBlock, 0.500
in. Bore, 1.690in L)
4 $41.83 Grainger $167.32
2CNU7 Shaft
Support
0.5in. (Shaft Support,
0.500 in. Bore, 1.625in. H)
4 $25.99 Grainger $103.96
Frame
2HHP8 Motor
Shim
0.75in stock (Bar, Rect.,
Steel, 1018, 3/4 x 1in, 1Ft.
L)
1 $9.05 Grainger $9.05
3DRT8 Motor
Baseplate
0.125in Sheet (Flat Stock,
LCS, Hot Rld., 1/8in T,
1Ft. L)
1 $16.49 Grainger $16.49
3DRU7 Free End
Baseplate
0.25in Sheet (Flat Stock,
LCS, Hot Rld., 1/4in T,
1x1 L)
1 $22.59 Grainger $22.59
3DRR5 Long
Support
Tube
0.125in Th (Tubing, Sq,
1015 LCS, 1OD x 1/8in T,
6 Ft. L)
2 $19.71 Grainger $39.42
4YUL5 Small
Thick
Support
0.25in Th (Sq Tube,
304SS, 1 OD Sq x 3/4 ID
Sq 6ft)
1 $47.48 Grainger $47.48
2HHW5 Free End
Stand
1in Stock 1 $25.55 Grainger $25.55
2EYG6 Rod Aluminum 6061, 4in D x
12in L
1 $105.70 Grainger $105.70
8290T15 Rod Unpolished, 1117 Carbon
Steel, 0.75in D x 12in L
1 $7.79 McMaster $7.79
Miscellaneous Costs $98.54
Total Cost $1,844.95

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Group_13_Final_Presentation

  • 1. 9/20/2015Group 13 Final Presentation By: Brendan Keane, Logan McCall, Reggie Scott, Mark Swain Instructor: Dr. Nikhil Gupta Sponsor: Dr. Philip Flater (Air Force Research Laboratory Eglin AFB) Advisor: Dr. Simone Hruda
  • 2. 9/20/2015 Group 13 Speaking: 1 of 27 Final Presentation  Introduction  Design and Analysis  Prototype Testing  Project Management  Conclusion Overview Reginald Scott
  • 3. Group 13 Speaking: 2 of 27 Final Presentation 9/20/2015  Current torsion tester at the Air Force Research Laboratory (AFRL) Munitions Directorate at Eglin AFB is approximately 5 meters in length  Small sample geometries result in inaccuracy and inefficiency Introduction Figure 2.1: Existing Torsion Machine “DISTRIBUTION A: Approved for public release, distribution unlimited. (96ABW-2014-1649)” Reginald Scott
  • 4. Group 13 Speaking: 3 of 27 Final Presentation 9/20/2015  Small specimens are a result of original plate stock dimensions  Specimens tested:  Aluminum 2024  Titanium 64 Specimen Geometry Original plate stock Blank removed Sample machined Figure 3.1: Specimen production Dimension Measurement (mm) Total Length 58.4 Gauge Length 12.7 Width 14.3 Inner Diameter 9.09 Fillet Radius 27.9 Grip Length 20 Table 3.1: Specimen dimensions “DISTRIBUTION A: Approved for public release, distribution unlimited. (96ABW-2014-1649)” Reginald Scott
  • 5. Group 13 Speaking: 4 of 27 Final Presentation 9/20/2015  Maximum torque output: 100Nm  Machine must fit in an area (footprint) of 1m2  Monotonic (one direction) free-end torsion loading  Free end must allow for axial motion  Compatible with measurement equipment used by AFRL  Budget - $2,000 Design Requirements Reginald Scott
  • 6. Group 13 Speaking: 5 of 27 Final Presentation 9/20/2015 Goal Statement: Design a more effective way of testing small specimens in free-end torsion Design Requirements Reginald Scott
  • 7. Group 13 Speaking: 6 of 27 Final Presentation 9/20/2015 DIC (Digital Image Correlation) “DISTRIBUTION A: Approved for public release, distribution unlimited. (96ABW-2014-1649)” Figure 6.2 Example DIC use in torsion sample Figure 6.1 DIC setup at Eglin AFRL Brendan Keane
  • 8. Group 13 Speaking: 7 of 27 Final Presentation 9/20/2015  Current method used by AFRL to measure applied stress:  Strain gage placed on elastic bar  Use shear modulus relationship to output stress Load Measurement Figure 7.1: Stress vs. strain plot showing the shear modulus relationship G = 𝜏 𝛾 Brendan Keane
  • 9. 9/20/2015 Group 13 Speaking: 8 of 27 Final Presentation Torsion Tester Load Generation Manual Power Motor & Transmission Load Application Gripping Mechanism Load Measurement Compatibility Linear Motion Friction Reduction Frame Material Selection User Safety Breakdown of Design Brendan Keane
  • 10. 9/20/2015 Group 13 Speaking: 9 of 27 Final Presentation Load Generation Design Cost Weight Accuracy Complexity Maintenance Variability Total Weight Factor 0.25 0.05 0.25 0.1 0.1 0.25 (1) Crank System 5 3 1 5 5 1 2.9 (2) Hydraulic 1 1 5 1 1 5 3 (3) AC Motor 3 3 5 3 3 5 4 (1) (2) (3) Brendan Keane
  • 11. 9/20/2015 Group 13 Speaking: 10 of 27 Final Presentation Load Application Design Cost Weight Reliability Complexity Variability Total Weight Factor 0.25 0.15 0.3 0.1 0.2 (1) 3-Jaw Chuck 5 5 5 3 5 4.8 (2) 4-Jaw Chuck 3 5 5 3 1 3.5 (3) Self-Aligning Vise 3 1 3 5 5 3.3 (4) Collet 5 5 5 3 1 4 (1) (2) (3) (4) Brendan Keane
  • 12. 9/20/2015 Group 13 Speaking: 11 of 27 Final Presentation Linear Motion Design Cost Weight Durability Complexity Total Weight Factor 0.4 0.2 0.2 0.2 (1) 4 Rail Ball Bearing Guide 1 2 1 1 1.4 (2) 2 Track Roller Bearing Guide 3 5 5 5 4.2 (3) 2 Rail Ball Bearing Guide 5 5 3 3 4.2 (1) (2) (3) Brendan Keane
  • 13. 9/20/2015 Group 13 Speaking: 12 of 27 Final Presentation Frame  Design Considerations:  Strength  Machinability  Weight  Cost  Material Selection:  Steel Figure 12.1: Frame design Brendan Keane
  • 14. 9/20/2015 Group 13 Speaking: 13 of 27 Final Presentation Concept Evolution Brendan Keane
  • 15. 9/20/2015 Group 13 Speaking: 14 of 27 Final Presentation Figure 5.1: CAD representation of design Design Overview Logan McCall Steel Shaft 32” 13”
  • 16. Group 13 Speaking: 15 of 27 Final Presentation 9/20/2015  Vendor: Grainger  Rpm: 18  Gear ratio: 95:1  Max torque: 116 Nm  Weight: 26 lbs Load Generation: AC Gearmotor Figure 15.1: AC Gearmotor Logan McCall
  • 17. Group 13 Speaking: 16 of 27 Final Presentation 9/20/2015  Vendor: Automation Direct  Single phase input, three phase output  Digital keypad  Forward and reverse  Expandable Motor Control: VFD Variable Frequency Drive (VFD) Figure 16.1: VFD keypad Logan McCall
  • 18. Group 13 Speaking: 17 of 27 Final Presentation 9/20/2015  Vendor: LittleMachineShop  Weight: 6.4 lbs  Outer diameter: 3.94 in (10 cm)  Inner diameter: 1.02 in (2.59 cm) Load Application: 6-Jaw Chuck Figure 17.1: 6 Jaw Chucks holding specimen Logan McCall
  • 19. 9/20/2015 Group 13 Speaking: 18 of 27 Final Presentation Load Measurement  Coupler material: Al 6061  Coupler properties  Shear modulus: 26 GPa  Shear strength: 76 MPa  Outer diameter: 1.75 in (4.45 cm)  Inner diameter: 0.75 in (1.90 cm) Figure 18.1: FEA performed on coupler showing strain developed under a simulated load Logan McCall
  • 20. Group 13 Speaking: 19 of 27 Final Presentation 9/20/2015  Vendor: Grainger  ½ inch steel rails  Slot design to ensure alignment Linear Motion: 2 Rail Ball Bearing Guide Figure 19.1: Linear guide system Logan McCall
  • 21. 9/20/2015 Group 13 Speaking: 20 of 27 Final Presentation Frame Design  Steel frame  Shape: hollow square shaped cross-section  Dimensions:  1/8 in inner supports – 304 stainless steel  1/8 in outer frame – low carbon 1015 steel Figure 20.1: CAD drawing of frame (bottom view) Logan McCall
  • 22. 9/20/2015 Group 13 Speaking: 21 of 27 Final Presentation Final Design Logan McCall
  • 23. 9/20/2015 Group 13 Speaking: 22 of 27 Final Presentation Prototype Testing Mark Swain
  • 24. 9/20/2015 Group 13 Speaking: 23 of 27 Final Presentation  Tester was successful in breaking aluminum specimen  Fracture was at center  During initial testing, free end chuck had slight rotation  Solution: Force fit new connecting rod into free end  Cylindrical grips slipped during initial testing  Solution: Use hex-grip specimen or increase friction on cylindrical specimen Testing Results Figure 23.1: Fractured specimens Mark Swain
  • 25. 9/20/2015 Group 13 Speaking: 24 of 27 Final Presentation Budget 44% 25% 18% 10% 3% Load Generation Load Application Linear Motion Housing Miscellaneous  Budget: $2,000  Spent: $1,844  Net: + $156 Mark Swain
  • 26. 9/20/2015 Group 13 Speaking: 25 of 27 Final Presentation Project Progression Fall  Background research  Design breakdown  Component research  Design analysis  Optimal part selection  Budget breakdown  Purchase orders Spring  Delivery of parts  Machining  Assembly  Motor/VFD testing  Prototype testing  Troubleshooting  Final assembly Mark Swain
  • 27. 9/20/2015 Group 13 Speaking: 26 of 27 Final Presentation Conclusion  Maximum torque output: 100Nm  Machine must fit in an area (footprint) of 1m2  Monotonic (one direction)free-end torsion loading  Free end must allow for axial motion  Compatible with measurement equipment used by AFRL  Budget - $2,000 Mark Swain
  • 28. 9/20/2015 Group 13 Speaking: 27 of 27 Final Presentation  The team was successfully designed and manufactured a tabletop torsion tester for AFRL  What we learned:  Focus on the main customer requirements  Consult as many resources as possible  Teamwork is essential  Unforeseen circumstances Conclusion Figure 27.1: Final assembly Mark Swain
  • 30. 9/20/2015 Group 13 Speaking: 29 of 27 Final Presentation  Carter, B. (2008). Texas Instruments: Op Amp Noise Theory and Applications. Retrieved September 22, 2014  Flater, P. (2014). Tabletop Torsion Test. Eglin, FL: Air Force Research Laboratory.  Ilic, M. (2014, October 11). Clamp for centering. Retrieved from GRABCAD: https://grabcad.com/library/stega-za-centriranje-clamp-for-centering-1  Lathe Chuck. (2014, October 7). Retrieved from GRABCAD: https://grabcad.com/library/lathe-chuck-3  Linear Motion Systems. (2014, September 28). Retrieved from Stock Drive Products: https://sdp-si.com/eStore/coverpg/linearmotion.htm References Mark Swain
  • 31. 9/20/2015 Group 13 Speaking: 30 of 27 Final Presentation
  • 32. 9/20/2015 Group 13 Speaking: 31 of 27 Final Presentation
  • 33. 9/20/2015 Group 13 Speaking: 32 of 27 Final Presentation Fall Gantt Chart
  • 34. 9/20/2015 Group 13 Speaking: 33 of 27 Final Presentation Spring Gantt Chart
  • 35. 9/20/2015 Group 13 Speaking: 34 of 27 Final Presentation Specimen Dimensions Brendan Keane Units in inches
  • 36. 9/20/2015 Group 13 Speaking: 35 of 27 Final Presentation Appendix
  • 37. 9/20/2015 Group 13 Speaking: 36 of 27 Final Presentation
  • 38. 9/20/2015 Group 13 Speaking: 37 of 27 Final Presentation Part # Part Name Description Quantity Unit Cost Supplier Cost Load Generation 6Z404 Motor AC Gear Motor, 18rpm, TEFC, 208 - 230/460V 1 $601.56 Grainger $601.56 GS2- 10P5 VFD Variable Frequency Drive, 0.5 HP, AC Drive 1 $166.00 Automation Direct $166.00 Load Application 2276 Lath Chuck 6-Jaw, 4" Outer Diameter 2 $174.95 Little Machine Shop $349.90 Linear Motion 2HXB4 Rails 0.5in Thick(Annealed Shaft, Steel, 0.500in D,16in) 2 $41.80 Grainger $83.60 2CNL6 Pillow Blocks 0.5in. (PillowBlock, 0.500 in. Bore, 1.690in L) 4 $41.83 Grainger $167.32 2CNU7 Shaft Support 0.5in. (Shaft Support, 0.500 in. Bore, 1.625in. H) 4 $25.99 Grainger $103.96 Frame 2HHP8 Motor Shim 0.75in stock (Bar, Rect., Steel, 1018, 3/4 x 1in, 1Ft. L) 1 $9.05 Grainger $9.05 3DRT8 Motor Baseplate 0.125in Sheet (Flat Stock, LCS, Hot Rld., 1/8in T, 1Ft. L) 1 $16.49 Grainger $16.49 3DRU7 Free End Baseplate 0.25in Sheet (Flat Stock, LCS, Hot Rld., 1/4in T, 1x1 L) 1 $22.59 Grainger $22.59 3DRR5 Long Support Tube 0.125in Th (Tubing, Sq, 1015 LCS, 1OD x 1/8in T, 6 Ft. L) 2 $19.71 Grainger $39.42 4YUL5 Small Thick Support 0.25in Th (Sq Tube, 304SS, 1 OD Sq x 3/4 ID Sq 6ft) 1 $47.48 Grainger $47.48 2HHW5 Free End Stand 1in Stock 1 $25.55 Grainger $25.55 2EYG6 Rod Aluminum 6061, 4in D x 12in L 1 $105.70 Grainger $105.70 8290T15 Rod Unpolished, 1117 Carbon Steel, 0.75in D x 12in L 1 $7.79 McMaster $7.79 Miscellaneous Costs $98.54 Total Cost $1,844.95