Anhang B - Materialreferenzen

Anzeigen der Materialdatenreferenzen

Unidirektionale Lagen

7740G30-500 Graphite

Tomblin, J., McKenna, J., Ng, Y., and Raju, S., "B-Basis Design Allowables for Epoxy-Based Prepreg - Fiberite Graphite unitape G30-500 12K/7740." Advanced General Aviation Transport Experiments, Sep. 2001.

T700/Epoxy

Xiong J et al. Fabrication and crushing behavior of low density carbon fiber composite pyramidal truss structures. Compos Struct (2010), doi:10.1016/j.compstruct.2010.03.010

AS4-3501-6

Soden, P.D., Hinton, M.J., und Kaddour, A.S.: "Lamina Properties, Lay-up Configurations and Loading Conditions for a Range of Fibre-Reinforced Composite Laminates", Composites Science and Technology, Vol. 58, 1011-1022, 1998.

AS4_3502

MIL-HDBK-17-2F: "Department of Defense Handbook: Composite Materials Handbook", U.S. Army Research Laboratory, Materials Directorate, Aberdeen Proving Ground, MD

AS4_8552

Mehrere Quellen:

Portela, Pedro, et al.: "Analysis of Morphing, Multi Stable Structures Actuated by Piezoelectric Patches", Computers and Structures, Vol. 86, Ausgabe 3–5, 347-356, 2008.

"HexPly 8552 Epoxy Matrix", Produktdatenblatt (Veröffentlichung FTA 072b), Hexcel Composites, Stamford, Connecticut, März 2007

Boron/5505

Mayes JS. Micromechanics based failure analysis of composite structural laminates. Naval Surface Warfare Center, Carderock Division Report, NSWCCD-65-TR-1999/15, September 1999.

E-Glass/Epoxy

Zwben, C., "Static Strength & Elastic Properties", Mechanical Behavior & Properties of Composite Materials, Delaware Composites Design Encyclopedia, Vol. 1, Technomic Publishing, Lancaster PA, S. 66-69, (1989).

Eglass21xK43Gevetex-LY556

HM Graphite/Epoxy

HTS150_TC250

"TC250 Resin System", Produktdatenblatt, TenCate Advanced Composites USA, Inc., Morgan Hill, CA., überarbeitet März 2007

IM7_5250-4

Mehrere Quellen:

"CYCOM 5250-4 Prepreg System", Produktdatenblatt , Cytec Engineered Materials, Anaheim, CA

Kim RY, Rice BP, Donaldson SL. Microcracking in composite laminates under thermal environments: 150 to −196 °C. Proceedings of the 47th SAMPE international symposium. Long Beach, CA: SAMPE; 2002. p. 833-42.

IM7_8551-7

Kaddour, A.S., und Hinton, M.J.: "Instructions to Contributors of the Second World-Wide Failure Exercise (WWFE-II): Part (A)"

IM7_8552

Mehrere Quellen:

Makeev, A., Seon, G., und Lee, E., "Failure Predictions for Carbon/Epoxy Tape Laminates with Wavy Plies", Journal of Composite Materials, Article in Press, 2009.

"HexPly 8552 Epoxy." Product Data Sheet, Hexcel Corporation, Dublin, CA.

Anmerkung: - Der Wert S22 wurde basierend auf ähnlichen Kohlenstoff-/Epoxidsystemen geschätzt.

IM7-977-2

Welsh, J.S., Mayes, J.S., und Biskner, A.C.: "Experimental and Numerical Failure Predictions of Biaxially-Loaded Quasi-Isotropic Carbon Composites", 16th International Conference on Composite Materials, Kyoto, Japan, 2007.

IM7-977-3

Mehrere Quellen:

Smith, J.G., Jegley, D.C. und Siochi, E.J., "Hypervelocity Impact Testing of IM7/977-3 with Micron-Sized Particles." Proceedings of 51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Orlando, FL, April 2010.

"CYCOM® 977-3 Epoxy Resin System", Cytec Engineering Materials, www.cytec.com (März 2012)

Kevlar-49/Epoxy

"Data Manual For Kevlar 49 Aramid", E.I Dupont de Nemours & Co., Inc., (Mai 1986).

LM Graphite/Epoxy

"Hercules Prepreg Tape Materials Characterization Data Package," Hercules Composites Products Group, (Februar 1989).

S-2 Glass/Epoxy

"S-2 Glass Fiber", Owens-Corning Fiberglass Corporation, Pub. Nr. 15-PL-16154, (März 1990).

SilEglass1200tex-MY750

T300_976

MIL-HDBK-17-2F: "Department of Defense Handbook: Composite Materials Handbook", U.S. Army Research Laboratory, Materials Directorate, Aberdeen Proving Ground, MD

T300-BSL914C

T300_PR319

Kaddour, A.S., und Hinton, M.J.: "Instructions to Contributors of the Second World-Wide Failure Exercise (WWFE-II): Part (A)"

T300/VTM266 2x2 3K Twill Weave

Eigenschaften in der Ebene:

"Composite T300/VTM266 2x2 Twill Prepreg" Product Datasheet, Prospector:Composites, Firehole Composites

Anmerkung: Eigenschaften außerhalb der Ebene und thermische Koeffizienten sind geschätzte Werte.

T800H_3900-2

Mehrere Quellen:

MIL-HDBK-17-2F: "Department of Defense Handbook: Composite Materials Handbook", U.S. Army Research Laboratory, Materials Directorate, Aberdeen Proving Ground, MD

Ogihara, S., Takeda, N., und Kobayashi, A.: "Experimental Characterization of Microscopic Failure Process under Quasi-Static Tension in Interleaved and Toughness-Improved CFRP Cross-Ply Laminates", Composites Science and Technology Vol. 57, 267-275, 1997.

Smith, D., und Dow, M.: "Properties of Three Graphite/Toughened Resin Composites", NASA: NASA Langley Research Center, 1991

UM Graphite/Epoxy

Matrixmaterialien

3501-6 Epoxy: Hinton, M.J., Kaddour, A.S. und Soden, P.D., "Failure Criteria in Fibre Reinforced Polymer Composites: The World-Wide Failure Exercise." Niederlande: ELSEVIER Ltd, 2004. 36-37.
5250-4 RTM: "CYCOM 5250-4 RTM." Produktdatenblatt , Cytec Engineered Materials, Anaheim, CA
Anmerkung: Druck- und Schubfestigkeit sind geschätzte Werte.
5505 Epoxy: Mayes JS. Micromechanics based failure analysis of composite structural laminates. Naval Surface Warfare Center, Carderock Division Report, NSWCCD-65-TR-1999/15, September 1999.
8551-7 Epoxy: Kaddour, A.S., und Hinton, M.J.: "Instructions to Contributors of the Second World-Wide Failure Exercise (WWFE-II): Part (A)"
BSL914C Epoxy: Hinton, M.J., Kaddour, A.S. und Soden, P.D., "Failure Criteria in Fibre Reinforced Polymer Composites: The World-Wide Failure Exercise." Niederlande: ELSEVIER Ltd, 2004. 36-37.
CETEX PEI: "CETEX® PEI." Technical Data Sheet, TenCate Advanced Composites, Almelo, The Netherlands.
Coors Tek PEKK: "CoorsTek PEKK." Technical Data Sheet, IDES Prospector, Laramie, WY.
KT-820 PEEK: "KetaSpire® KT-820." Technical Data Sheet, Solvay Specialty Polymers.
KT-880 PEEK: "KetaSpire® KT-880." Technical Data Sheet, Solvay Specialty Polymers.
LY556 Epoxy: Hinton, M.J., Kaddour, A.S. und Soden, P.D., "Failure Criteria in Fibre Reinforced Polymer Composites: The World-Wide Failure Exercise." Niederlande: ELSEVIER Ltd, 2004. 36-37.
MY750 Epoxy: Kaddour, A.S., und Hinton, M.J.: "Instructions to Contributors of the Second World-Wide Failure Exercise (WWFE-II): Part (A)"
Polyester: "1992 Materials Selector," Materials Engineering, S. 181, (Dezember 1991).
PR-319 Epoxy: Kaddour, A.S., und Hinton, M.J.: "Instructions to Contributors of the Second World-Wide Failure Exercise (WWFE-II): Part (A)"
Anmerkung: Diese Werte werden im Vergleich zu typischen Daten für das gleiche Material, die von anderen Quellen publiziert oder vom Hersteller angegeben werten, als niedrig angesehen.
R-5100 PPSU: "Radel® R-5100." Technical Data Sheet, Solvay Specialty Polymers.
Vinylester: "Chemical Resistance Guide, DOW Derakane Vinylester Resins," DOW Chemical, (Dezember 1996)

Fasermaterialien

AS4 Graphite

Mehrere Quellen:

Hinton, M.J., Kaddour, A.S. und Soden, P.D., "Failure Criteria in Fibre Reinforced Polymer Composites: The World-Wide Failure Exercise." Niederlande: ELSEVIER Ltd, 2004. 36-37.

"AS4 Continuous Carbon Fiber." Product Data Sheet, Hexcel Corporation, Dublin, CA.

Anmerkung: Der Endflächenwert ist geschätzt.

Boron

Herakovich C.T., "Mechanics of Fibrous Composites" New York: John Wiley & Sons, Inc. 1998. ff. 7.

Anmerkung: Elastische Konstanten E₂₂, G₁₂, G₂₃ und Nu₁₂ wurden mit Autodesk Material Manager berechnet.

E-Glass

"S-2 Glass Fiber", Owens-Corning Fiberglass Corporation, Pub. Nr. 15-PL-16154, (März 1990).

E-Glas 21 x K43 Gevetex

Hinton, M.J., Kaddour, A.S. und Soden, P.D., "Failure Criteria in Fibre Reinforced Polymer Composites: The World-Wide Failure Exercise." Niederlande: ELSEVIER Ltd, 2004. 36-37.

Anmerkung: Die Werte für die thermische Leitfähigkeit, Dichte und Endfläche sind geschätzt.

High Modulus Graphite

Quelle nicht verfügbar

HTS150

"TC250 Resin System", Product Data Sheet, TenCate Advanced Composites USA, Inc., Morgan Hill, CA., überarbeitet März 2007

Anmerkung: Die Werte basieren auf Autodesk Material Manager-Mikromechanik. Die Werte für Festigkeit, Wärmeleitfähigkeit, Dichte und Endfläche sind geschätzt.

IM7 Carbon

Mehrere Quellen:

Kaddour, A.S., und Hinton, M.J.: "Instructions to Contributors of the Second World-Wide Failure Exercise (WWFE-II): Part (A)"

"IM7 Continuous Carbon Fiber." Product Data Sheet, Hexcel Corporation, Dublin, CA.

Kevlar-49

"Data Manual For Kevlar 49 Aramid", E.I Dupont de Nemours & Co., Inc., (Mai 1986).

S-2 Fiberglass

Mehrere Quellen:

"S-2 Glass Fiber", Owens-Corning Fiberglass Corporation, Pub. Nr. 15-PL-16154, (März 1990).

Kaddour, A.S., und Hinton, M.J.: "Instructions to Contributors of the Second World-Wide Failure Exercise (WWFE-II): Part (A)"

Silenka E-Glass 1200tex

Hinton, M.J., Kaddour, A.S. und Soden, P.D., "Failure Criteria in Fibre Reinforced Polymer Composites: The World-Wide Failure Exercise." Niederlande: ELSEVIER Ltd, 2004. 36-37.

Anmerkung: Die Werte für die thermische Leitfähigkeit, Dichte und Endfläche sind geschätzt.

T300 Carbon

Mehrere Quellen:

Kaddour, A.S., und Hinton, M.J.: "Instructions to Contributors of the Second World-Wide Failure Exercise (WWFE-II): Part (A)"

"T300" Technical Data Sheet No. CFA-001, Toray Carbon Fibers America, Inc., Santa Ana, CA.

T800 Carbon

"T800 Continuous Carbon Fiber." Product Data Sheet, Toray Carbon Fibers America, Inc., Flower Mound, TX.

Anmerkung: Materialeigenschaften basierend auf Autodesk Simulation Material-Mikromechanik geschätzt. Die Endfläche ist geschätzt.

Ultra Modulus Graphite

Quelle nicht verfügbar

Kernmaterialien

Aluminum Alloy Honeycomb: "HexWeb Honeycomb Attributes and Properties." Hexcel Corporation, Dublin, CA. S. 16-17
Aluminum Alloy Flex-Core: "HexWeb Honeycomb Attributes and Properties." Hexcel Corporation, Dublin, CA. ff. 18
Balsa: "The Properties of End-Grain Balsa Core," Baltek Corp., Data file 159, (1990).
FR-3700 LAST-A-FOAM: "LAST-A-FOAM FR-3700 Rigid Foam." Interactive Data Sheet, Gerneral Plastics Manufacturing Company, Tacoma, WA.
FR-6700 LAST-A-FOAM: "LAST-A-FOAM FR-6700 Rigid Foam." Interactive Data Sheet, Gerneral Plastics Manufacturing Company, Tacoma, WA.
Glass HC, 3/16: "Mechanical Properties of Hexcel Honeycomb Materials," Hexcel, Doc. Nr. TSB-120, (1988).
High Density Foam: "Sandwich Core Material Average Physical Properties, Divinycell" Diab-Barracuda, Doc. Nr. 87.03.3000, (1987).
Low Density Foam: "Sandwich Core Material Average Physical Properties, Divinycell" Diab-Barracuda, Doc. Nr. 87.03.3000, (1987).
HRH-10 Aramid Fiber Reinforced Honeycomb: "HexWeb Honeycomb Attributes and Properties." Hexcel Corporation, Dublin, CA. ff. 21

Legierungen

1025 Steel: "Metallic Materials and Elements for Aerospace Vehicle Structures," MILHDBK-5E, Dept. of Defense, (Juni 1987).
6061-T6 Aluminum: "Metallic Materials and Elements for Aerospace Vehicle Structures," MILHDBK-5E, Dept. of Defense, (Juni 1987).
Ti-6Al-4v Titanium: "Metallic Materials and Elements for Aerospace Vehicle Structures," MILHDBK-5E, Dept. of Defense, (Juni 1987).