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1
4/18/16
• Schedule Updates
• Cross-Slide
– Functional Requirements
– Flexure
– Lead-Screw
– Testing
– Model
2
• Finished
– Cross Slide Assembly
– Testing Cross Slide
– Carriage Machining
– Designing Rest of Lathe
• Behind Schedule
– Structural Tube Machining, Bill’s schedule was
booked
• Potting delayed as a result
• Gantt Chart on Next Slide
3
4
Link to schedule:
https://teamgantt.com/gantt/schedule/?ids=582767#&ids=582767&user=&custom=&company=&hide_complet
ed=false&date_filter=&color_filter=
• Allow for Z-axis misalignment (+1 DOF)
• Allow for human hand movement increments to
produce a x-axis motion of < 50 microns
• Error Allotment </= 7 microns
• Stationary Handle , </= 250 microns linear
movements
• Start Torque </= 4lb-inch (ideal </= 2lb-inch)
• Lifetime =/> 3120 hours (12 hrs/week, 52
weeks/year, 5 years), at 60 rpm for rotary
• Natural Frequency =/> 80Hz
• Withstand: Fx=20lbs, Fy=135lbs, Fz=60lbs,
• Range of Motion =/> 0.3 inches
6
Thrust Bearing
Attachment 0.25” gap
Stabilizers,
cut off when
done with
machining
Carriage
attachment
Threaded
Attachment
Headstock
Clearance
Chuck
Clearance
Added
Protection
Tool Post
Holes
7
3 lb applied
force
8
Mode # Freq (Hertz) X direction Y direction Z direction
1 235.5 0.0021013 0.49048 1.1352e-006
2 315.12 1.2538e-005 6.5322e-007 3.4188e-006
3 346.51 0.010169 4.9037e-005 0.00172
4 388.48 0.041212 4.4115e-005 0.0022115
5 473.01 0.0055886 2.9683e-005 0.00036685
• Custom OMAX path
• Waterjet outlines
• Counter-bore and thread
holes
9
10
For more analysis: https://docs.google.com/spreadsheets/d/1V_9k8njTLzHD-
3Jz04GE_dwqZ0_g9mWqIl43e8NAWQ8/edit#gid=1853057762
12
13
Lifetime: 9000 hours
This is at 150 RPM and 30 lbf thrust
force (maximum load rating at 150
RPM is 65 lbf)
Ball thrust bearings are optimal
because they can tolerate slight radial
forces/misalignment if the lathe is
dropped
• Design: Friction between
aluminum housing and steel
threads was low enough to
meet our functional
requirements
• Obstacle: After assembling, fit
between the lead screw and
housing was too loose
• Solution: opening up the hole
and using a brass bushing
significantly reduced end play
14
can see
the hole
was too
big
15
• Precision lost through
leadscrew torsion instead
of translation of carriage
being translated.
• Negligible x-direction
error (~0.8μm)
• Presence of substantial
torque to turn in both
directions implies no
“play” either.
16
17
• Torque to turn <2lb*in when free, <4lb*in
under maximum load (aka a person).
18
• Tool post deflection tends to be negligible as
we tighten beyond 0.3 turns. (~8lbs applied)
19
20
• Huge errors in x axis(~650 microns), probably
due to loose leadscrew / not actually turning 1
revolution
• Total errors in Y (~13 microns) and Z (~76
microns) coming from wobble
21
• Little angular variation but at constant offset
• Large error from offset (~13 microns)
• Add shims to help adjust angular offset
Thank You
22
Questions?
EXTRA SLIDES
23
• FOS of 1.6 with a 160lb load in the –y
direction
• Deflections of:
– -3.42microns in x (|122N| force)
– -86.4microns in y (|252N| force)
– +5.16 microns in z (|100N| force)
for tool location in FEA when cutting 0.07”
depth of aluminum
24
For more analysis: https://docs.google.com/spreadsheets/d/1V_9k8njTLzHD-
3Jz04GE_dwqZ0_g9mWqIl43e8NAWQ8/edit#gid=1853057762
For more analysis: https://docs.google.com/spreadsheets/d/1V_9k8njTLzHD-
3Jz04GE_dwqZ0_g9mWqIl43e8NAWQ8/edit#gid=1853057762
27
• θ = L T / (J G) = 4E-3 rad
Where:
• J = π D4 / 32 =1.242E-4
• D=0.1886in
• G=11457981psi
• L=1.46in worst case
• T = 4 lb*in worst case
• Lateral loss < 1micron
28
29
30
31
32

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Schedule and Testing Updates for Mini Lathe Project

  • 2. • Schedule Updates • Cross-Slide – Functional Requirements – Flexure – Lead-Screw – Testing – Model 2
  • 3. • Finished – Cross Slide Assembly – Testing Cross Slide – Carriage Machining – Designing Rest of Lathe • Behind Schedule – Structural Tube Machining, Bill’s schedule was booked • Potting delayed as a result • Gantt Chart on Next Slide 3
  • 5. • Allow for Z-axis misalignment (+1 DOF) • Allow for human hand movement increments to produce a x-axis motion of < 50 microns • Error Allotment </= 7 microns • Stationary Handle , </= 250 microns linear movements • Start Torque </= 4lb-inch (ideal </= 2lb-inch) • Lifetime =/> 3120 hours (12 hrs/week, 52 weeks/year, 5 years), at 60 rpm for rotary • Natural Frequency =/> 80Hz • Withstand: Fx=20lbs, Fy=135lbs, Fz=60lbs, • Range of Motion =/> 0.3 inches
  • 6. 6 Thrust Bearing Attachment 0.25” gap Stabilizers, cut off when done with machining Carriage attachment Threaded Attachment Headstock Clearance Chuck Clearance Added Protection Tool Post Holes
  • 8. 8 Mode # Freq (Hertz) X direction Y direction Z direction 1 235.5 0.0021013 0.49048 1.1352e-006 2 315.12 1.2538e-005 6.5322e-007 3.4188e-006 3 346.51 0.010169 4.9037e-005 0.00172 4 388.48 0.041212 4.4115e-005 0.0022115 5 473.01 0.0055886 2.9683e-005 0.00036685
  • 9. • Custom OMAX path • Waterjet outlines • Counter-bore and thread holes 9
  • 10. 10
  • 11. For more analysis: https://docs.google.com/spreadsheets/d/1V_9k8njTLzHD- 3Jz04GE_dwqZ0_g9mWqIl43e8NAWQ8/edit#gid=1853057762
  • 12. 12
  • 13. 13 Lifetime: 9000 hours This is at 150 RPM and 30 lbf thrust force (maximum load rating at 150 RPM is 65 lbf) Ball thrust bearings are optimal because they can tolerate slight radial forces/misalignment if the lathe is dropped
  • 14. • Design: Friction between aluminum housing and steel threads was low enough to meet our functional requirements • Obstacle: After assembling, fit between the lead screw and housing was too loose • Solution: opening up the hole and using a brass bushing significantly reduced end play 14 can see the hole was too big
  • 15. 15
  • 16. • Precision lost through leadscrew torsion instead of translation of carriage being translated. • Negligible x-direction error (~0.8μm) • Presence of substantial torque to turn in both directions implies no “play” either. 16
  • 17. 17 • Torque to turn <2lb*in when free, <4lb*in under maximum load (aka a person).
  • 18. 18 • Tool post deflection tends to be negligible as we tighten beyond 0.3 turns. (~8lbs applied)
  • 19. 19
  • 20. 20 • Huge errors in x axis(~650 microns), probably due to loose leadscrew / not actually turning 1 revolution • Total errors in Y (~13 microns) and Z (~76 microns) coming from wobble
  • 21. 21 • Little angular variation but at constant offset • Large error from offset (~13 microns) • Add shims to help adjust angular offset
  • 24. • FOS of 1.6 with a 160lb load in the –y direction • Deflections of: – -3.42microns in x (|122N| force) – -86.4microns in y (|252N| force) – +5.16 microns in z (|100N| force) for tool location in FEA when cutting 0.07” depth of aluminum 24
  • 25. For more analysis: https://docs.google.com/spreadsheets/d/1V_9k8njTLzHD- 3Jz04GE_dwqZ0_g9mWqIl43e8NAWQ8/edit#gid=1853057762
  • 26. For more analysis: https://docs.google.com/spreadsheets/d/1V_9k8njTLzHD- 3Jz04GE_dwqZ0_g9mWqIl43e8NAWQ8/edit#gid=1853057762
  • 27. 27
  • 28. • θ = L T / (J G) = 4E-3 rad Where: • J = π D4 / 32 =1.242E-4 • D=0.1886in • G=11457981psi • L=1.46in worst case • T = 4 lb*in worst case • Lateral loss < 1micron 28
  • 29. 29
  • 30. 30
  • 31. 31
  • 32. 32

Editor's Notes

  1. Sammi
  2. Tim
  3. Adri
  4. Nhlamulo
  5. Sammi
  6. Cyndia
  7. Cyndia
  8. Sammi
  9. Nhlamulo
  10. Nhlamulo
  11. Adri
  12. Adri
  13. Adri
  14. Tim
  15. Tim
  16. Tim
  17. Tim
  18. Lilly
  19. Lilly
  20. Assembly
  21. Tim