Title: The GVSU Baja Race Team
1The GVSU Baja
Race Team
- Front Suspension Redesign
Michael R. Olson Michael R. Mulder Paul
Wittkoski Jeremy Pruneau Andrew Tallman Ryan E.
Peer
Jeff A. Blair Dan J. Schwarz Ryan J.
Anderson Chris Dittmer Kevin Mattox Bryan C.
Keefe
2Objectives
Improve Cornering
- Criteria
- Increase negative chamber change from -0.5o to
-1.5o per inch of compression. -
- Justification
- Increased tire angle increases lateral force in
corner as long as contact patch is the same.
3Camber Thrust
For any given slip angle, negative camber
produces higher lateral thrust than zero camber
4Objectives
Improve Cornering
- Criteria
- Decrease center of gravity by 2 inches and
increase track width by 2 inches -
- Justification
- Reduces load transfer and increases cornering
force
5Objectives
Decrease Unsprung Weight
- Definition
- Weight of the suspension that is not supported by
the spring. Approximately 50 of the control
links are included in unsprung weight -
- Criteria
- Decrease A-arm mass by at least 15
-
- Justification
- Increases responsiveness to improve road holding
6Objectives
Decrease Cost
- Criteria
- Decrease overall cost by at least 15.
-
- Justification
- Improve cost report score
- Cost is 10 of the total vehicle score
7Objectives
Meet SAE Rules
- Criteria
- Keep overall width under 64
- Grade five or better fasteners
- All fasteners must be captive (nylon lock nuts,
cottered nut, or safety wired bolts -
8Prototype Characteristics
9Prototype Characteristics
- Camber Change
- Increased negative chamber change from -0.5o to
-1.56o per inch of compression. -
- Mass
- Decreased A-arm mass by 39
-
- Dimensions
- Ride height was set at 10
- Overall vehicle width was set at 62
-
10Prototype Characteristics
- Cost
- Total cost was decreased by 25
-
- Fasteners
- Grade five fasteners and nylon lock nuts were used
11Cost Analysis
- Cost Discrepancy Justification
- SAE cost was determined by a cost per unit mass
method - Purchase cost was based on a cost per unit length
- Not all of the purchased materials were used to
build the prototype -
12Cost Analysis
13Cost Analysis
14(No Transcript)
15Strain Gage Attachment
- UPPER ARM
- Gage 1 Stress in weld
- Gage 2 Axial stress in tube
16Strain Gage Attachment
LOWER ARM Gage 3,4,5 (Rosette) Combined stress
in lower tube Gage 6 Stress near weld
17Strain Gage Attachment
Gage 7,8,9 (Rosette) - check for bending Gage
10 - check for strain caused by the shock
18TEST RESULTS
19Upper A-Arm FEA
- Von Mises Stresses compared
- Maximum stress observed in the ball joint where
tubes are welded - Sharp change in geometry
- Stress riser
20Lower A-Arm
- Maximum stress seen in shock mounting tabs
- Stress appears higher than expected
- Testing did not show a failure
21Final Results
- Initially Used ANSYS
- Ran into Program Limitations
- Rotational Constraints
- Element number
- Used Mechanica for final analysis
- Lower A-Arm analysis indicates failure. However,
physical testing does not support this result.
22Manufacturing
- Tubes
- Prototype
- Manually cut to length
- Notched on mill using hole saw
- Production
- Notching punch and die
- Press or hydraulic operation
23Manufacturing
- Lower ball joint mount
- Prototype
- Cylinder turned on lathe
- Angle cut on mill
- Production
- Cast
-
24Manufacturing
- Shock mount tabs and plate
- Prototype
- Drilled and cut
- Slot cut on mill
- Production
- Stamped
25Manufacturing
- Assembly
- Prototype
- Upper and lower jig built
- Manually TIG welded
- Production
- Automated TIG welding
26Possible Improvements
- Further tubing optimization
- Cross members may be unnecessarily large
- Review lower shock mount design
- FEA was inconclusive
- Further review may be needed to verify the safety
factor
27Design Summary
28Questions