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Jesii Doyle 1/17/2008 Internal Structure, Mounting Materials Initial Mounting Materials Research. Mounting Materials – Initial Research. Structures. Future Work. Approximate material required Maximum mounting loads. Mounting Materials – Initial Research. Strength/Cost
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Jesii Doyle1/17/2008Internal Structure, Mounting MaterialsInitial Mounting Materials Research AAE 450 Spring 2008
Mounting Materials – Initial Research AAE 450 Spring 2008 Structures
Future Work • Approximate material required • Maximum mounting loads Mounting Materials – Initial Research • Strength/Cost • Al 6061-T6 54.72 MPa/$ • Strength/Weight • Ti 6Al-4V 876 MPa/kg • Recommended Material – Al 6061-T6 AAE 450 Spring 2008 Structures
Backup Slides • Material Properties and Cost Research AAE 450 Spring 2008 Structures
Backup Slides • Strength/$ and Strength/kg Calculation AAE 450 Spring 2008
Backup Slides • References: “6Al-4V Titanium Sheet and Plate,” Titanium Joe, December 2007. [http://www.titaniumjoe.com/6al4v%20sheet.htm. Accessed 1/15/2008.] “Carbon Fiber – Structural,” Metals and Materials, The Robot Marketplace, December 2007. [http://www.robotmarketplace.com/marketplace_ carbonfiber_struc.html. Accessed 1/15/2008.] “Carbon matrix composite, Carbon/carbon, Three-directional orthogonal, Shape,” Engineered Materials Handbook, Vol. 1, Composites, ASM International, 1987. “Properties,” Pultruded Products, Strongwell, January 2008. [http://www.strongwell.com/PDFfiles/Extren/EXTREN%20Properties.pdf. Accessed 1/16/2008.] Setlak, Stanley J., “Aluminum Alloys; Cast,” Aerospace Structural Metals Handbook, Purdue University, Indiana, 2000. AAE 450 Spring 2008
Backup Slides • References (cont.): Setlak, Stanley J., “Titanium Alloys; Cast,” Aerospace Structural Metals Handbook, Purdue University, Indiana, 2000. “Suggested List Prices,” EXTREN: Fiberglass Structural Shapes & Plate, Strongwell, November 2006. [http://www.peabodyconcealment.com/ sitebuildercontent/sitebuilderfiles/StrongwellExtrenPrices.pdf. Accessed 1/15/2008.] AAE 450 Spring 2008