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Jerid Sutton Daniel Smith. Spirit Aerosystems Final Review. To prove an already employed analysis tool, improve it, or create new analysis tools for joints and fasteners. In doing this we would predict load distribution through the fasteners in the joint.
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Jerid Sutton Daniel Smith Spirit Aerosystems Final Review
To prove an already employed analysis tool, improve it, or create new analysis tools for joints and fasteners. In doing this we would predict load distribution through the fasteners in the joint. • Being able to predict load transfer at a fastener could be very useful to a stress analyst. Concept Goal
Design Test Concepts • Load Distribution • Fastener arrangement and spacing has a major effect on the distribution of a load
If the fastener is bigger in diameter it attracts more of the load In a flexible joint the first fastener transfers the most load Fastener configuration effects load distribution Load Transfer Theory
Aluminum (2024-T3) • ½” to 2” total joint thickness • Fasteners • Bolts and Nuts (Hi-Loks) • Rivets • 3/16” to 3/8” diameters • Materials – titanium, A-286 Steel, Nickel Alloy Spirit Design Considerations
Availability of testing equipment • Using Aluminum 2024-T1 1/8” and 3/16” Plate • Blind Rivets • 3/16” Diameter • Aluminum • Stainless Steel • Titanium Team Design Considerations
Nut and Bolt Combination • ¼”-3/16” Diameter • Stainless Steel • Grade 8 • Grade 6 Team Design Considerations
Standard Tension Tests • 11,000 lb Maximum Tensile Force • Software • Pro-Mechanica FEA • ALGOR FEA PSU Testing Capabilities
Search ASTM standards for tension testing procedures Predict stress in predetermined specimen using stress and strain Verify testing device by comparing results to predicted ultimate strength of the specimen Standard Test Procedure
1040 Cold-drawn Steel • Stress = Force/Area • Sample Calculation • 6,250 lb/(.25in X .5in) = 50,000 psi • Compare with Pro-Mechanica Analysis Results Calculation Comparison
Two partial dog-bone specimen held together by inline rivets Requires Spirit to assemble the specimen Surface finish has to be capable of adhering a strain gage Riveted joint concept
Measured every specimen cut out and scrapped anything that was not within .1” of tolerance Some holes that were drilled didn’t properly line up so those parts were scrapped as well When parts were cut out and drilled we had to debur edges so there were no sharp corners for safety reasons Tolerance and quality issues
Yield Strength or 2024 = 47000psi YS = F/6x[d2/4] 47000 = F/6x(.250)2/4 F = 14,628lbs to shear rivets The Zwick tensile test machine can only go to 10,000lbs safely so it is not possible to break the specimen here. Rivet shear strength calculation
Fundamentally, all strain gages are designed to convert mechanical motion into an electronic signal. A change in capacitance, inductance, or resistance is proportional to the strain experienced by the sensor. If a wire is held under tension, it gets slightly longer and its cross-sectional area is reduced. This changes its resistance (R) in proportion to the strain sensitivity (S) of the wire's resistance. Strain Gage Fundamentals
At this point we have a few excel programs from Spirit but need their assistance in manipulating them to work with our results. The excel program supplied by Spirit is made to correspond with many different numbers of fasteners and we do not know yet how to get it to calculate the load at only 3. Interpretation of Results