aae 450 spring 2008 jesii doyle 1/17/2008 internal structure, mounting materials initial mounting...

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AAE 450 Spring 2008 Jesii Doyle 1/17/2008 Internal Structure, Mounting Materials Initial Mounting Materials Research

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Page 1: AAE 450 Spring 2008 Jesii Doyle 1/17/2008 Internal Structure, Mounting Materials Initial Mounting Materials Research

AAE 450 Spring 2008

Jesii Doyle1/17/2008

Internal Structure, Mounting Materials

Initial Mounting Materials Research

Page 2: AAE 450 Spring 2008 Jesii Doyle 1/17/2008 Internal Structure, Mounting Materials Initial Mounting Materials Research

AAE 450 Spring 2008

Mounting Materials – Initial Research

Structures

Strength/Cost

0

20

40

60

Al 6

061-

T6

Al 7

075-

T6

Ti-6

Al-4

V

Fib

ergl

ass

Car

bon/

Car

bon

3-D

irect

iona

lO

rth.

Strength/Cost

(MPa/$)

Strength/Weight

0

200

400

600

800

1000

Al 6

061-

T6

Al 7

075-

T6

Ti-6

Al-4

V

Fib

ergl

ass

Car

bon/

Car

bon

3-D

irect

iona

lO

rth.

Strength/Weight

(MPa/kg)

Page 3: AAE 450 Spring 2008 Jesii Doyle 1/17/2008 Internal Structure, Mounting Materials Initial Mounting Materials Research

AAE 450 Spring 2008

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

Structures

Future Work Approximate material required Maximum mounting loads

Page 4: AAE 450 Spring 2008 Jesii Doyle 1/17/2008 Internal Structure, Mounting Materials Initial Mounting Materials Research

AAE 450 Spring 2008

Backup Slides Material Properties and Cost Research

Structures

MaterialFtu (ksi)

Ftu (MPa)

Fty (ksi) Fty (MPa)Density (g/cm^3)

Cost/kg

Al 6061-T6

38 262 35 241 2.70 $4.41

Al 7075-T6

75 517 65 448 2.80 $17.64

Ti-6Al-4V 139 958 127 876 4.46 $93.59

Fiberglass 30 207 30 207 1.72 $1,121.98

Carbon/Carbon 3-Directional

Orth.

45 310 23 159 1.90 $552.45

Page 5: AAE 450 Spring 2008 Jesii Doyle 1/17/2008 Internal Structure, Mounting Materials Initial Mounting Materials Research

AAE 450 Spring 2008

Backup Slides Strength/$ and Strength/kg Calculation

MaterialFty

(MPa)Cost/kg

Cost (Assume 1kg)

Strength/$ (MPa/$)

Strength/kg (MPa/kg)

Al 6061-T6 241 $4.41 $4.41 54.72 241.32

Al 7075-T6 448 $17.64 $17.64 25.41 448.16

Ti-6Al-4V 876 $93.59 $93.59 9.36 875.63

Fiberglass 207 $1,121.98 $1,121.98 0.18 206.84

Carbon/Carbon 3-Directional

Orth.

159 $552.45 $552.45 0.29 158.99

Page 6: AAE 450 Spring 2008 Jesii Doyle 1/17/2008 Internal Structure, Mounting Materials Initial Mounting Materials Research

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.

Page 7: AAE 450 Spring 2008 Jesii Doyle 1/17/2008 Internal Structure, Mounting Materials Initial Mounting Materials Research

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.]