付録 B - 材料リファレンス

材料データのリファレンスを示します。

一方向単層

7740G30-500 グラファイト
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/エポキシ
Xiong J、および他。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. and 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

複数のソース:

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

"HexPly 8552 Epoxy Matrix." Product Data Sheet (Publication FTA 072b), Hexcel Composites, Stamford, Connecticut. March 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-ガラス/エポキシ
Zwben, C., "Static Strength & Elastic Properties", Mechanical Behavior & Properties of Composite Materials, Delaware Composites Design Encyclopedia, Vol. 1, Technomic Publishing, Lancaster PA, pp. 66-69, (1989).
Eglass21xK43Gevetex-LY556
Soden, P.D., Hinton, M.J. and 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.
HM グラファイト/エポキシ
Zwben, C., "Static Strength & Elastic Properties", Mechanical Behavior & Properties of Composite Materials, Delaware Composites Design Encyclopedia, Vol. 1, Technomic Publishing, Lancaster PA, pp. 66-69, (1989).
HTS150_TC250
"TC250 Resin System." Product Data Sheet, TenCate Advanced Composites USA, Inc., Morgan Hill, CA., Revised March 2007.
IM7_5250-4

複数のソース:

"CYCOM 5250-4 Prepreg System." Product Data Sheet, 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. and Hinton, M.J., "Instructions to Contributors of the Second World-Wide Failure Exercise (WWFE-II): Part (A)."
IM7_8552

複数のソース:

Makeev, A., Seon, G. and 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.

注: - S22 の値は、これに似た炭素エポキシ システムに基づいて推定されています。
IM7-977-2
Welsh, J.S., Mayes, J.S. and 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

複数のソース:

Smith, J.G., Jegley, D.C. and 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 (March 2012)

Kevlar-49/エポキシ
"Data Manual For Kevlar 49 Aramid", E.I Dupont de Nemours & Co., Inc., (May 1986).
LM グラファイト/エポキシ
"Hercules Prepreg Tape Materials Characterization Data Package," Hercules Composites Products Group, (February 1989).
S-2 ガラス/エポキシ
"S-2 Glass Fiber", Owens-Corning Fiberglass Corporation, Pub. No. 15-PL-16154, (March 1990).
SilEglass1200tex-MY750
Soden, P.D., Hinton, M.J. and 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.
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
Soden, P.D., Hinton, M.J. and 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.
T300_PR319
Kaddour, A.S. and Hinton, M.J., "Instructions to Contributors of the Second World-Wide Failure Exercise (WWFE-II): Part (A)."
T300/VTM266 2x2 3K 綾織り

面内プロパティ:

"Composite T300/VTM266 2x2 Twill Prepreg" Product Datasheet, Prospector:Composites, Firehole Composites
注: 面外プロパティおよび熱係数の値は推定値です。
T800H_3900-2

複数のソース:

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

UM グラファイト/エポキシ
Zwben, C., "Static Strength & Elastic Properties", Mechanical Behavior & Properties of Composite Materials, Delaware Composites Design Encyclopedia, Vol. 1, Technomic Publishing, Lancaster PA, pp. 66-69, (1989).

母材材料

3501-6 エポキシ
Hinton, M.J., Kaddour, A.S. and Soden, P.D., "Failure Criteria in Fibre Reinforced Polymer Composites: The World-Wide Failure Exercise." The Netherlands: ELSEVIER Ltd, 2004. 36-37.
5250-4 RTM
"CYCOM 5250-4 RTM." Product Data Sheet, Cytec Engineered Materials, Anaheim, CA.
注: 圧縮とせん断の強度は推定値です。
5505 エポキシ
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 エポキシ
Kaddour, A.S. and Hinton, M.J., "Instructions to Contributors of the Second World-Wide Failure Exercise (WWFE-II): Part (A)."
BSL914C エポキシ
Hinton, M.J., Kaddour, A.S. and Soden, P.D., "Failure Criteria in Fibre Reinforced Polymer Composites: The World-Wide Failure Exercise." The Netherlands: 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 エポキシ
Hinton, M.J., Kaddour, A.S. and Soden, P.D., "Failure Criteria in Fibre Reinforced Polymer Composites: The World-Wide Failure Exercise." The Netherlands: ELSEVIER Ltd, 2004. 36-37.
MY750 エポキシ
Kaddour, A.S. and Hinton, M.J., "Instructions to Contributors of the Second World-Wide Failure Exercise (WWFE-II): Part (A)."
ポリエステル
"1992 Materials Selector," Materials Engineering, p. 181, (December 1991).
PR-319 エポキシ
Kaddour, A.S. and Hinton, M.J., "Instructions to Contributors of the Second World-Wide Failure Exercise (WWFE-II): Part (A)."
注: 他の公開された文献や製造メーカーが引用している同一の材料の一般的なデータと比較すると、この文献で示されるデータの値は低いと考えられます。
R-5100 PPSU
"Radel® R-5100." Technical Data Sheet, Solvay Specialty Polymers.
ビニルエステル
"Chemical Resistance Guide, DOW Derakane Vinylester Resins," DOW Chemical, (December 1996)

繊維材料

AS4 グラファイト

複数のソース:

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

"AS4 Continuous Carbon Fiber." Product Data Sheet, Hexcel Corporation, Dublin, CA.
注: 終端領域の値は推定値です。
ボロン
Herakovich C.T., "Mechanics of Fibrous Composites" New York: John Wiley & Sons, Inc. 1998. pp. 7.
注: 弾性定数 E22、G12、G23、Nu12 は、Autodesk Material Manager を使用して計算しています。
E-ガラス
"S-2 Glass Fiber", Owens-Corning Fiberglass Corporation, Pub. No. 15-PL-16154, (March 1990).
E-Glass 21 x K43 Gevetex
Hinton, M.J., Kaddour, A.S. and Soden, P.D., "Failure Criteria in Fibre Reinforced Polymer Composites: The World-Wide Failure Exercise." The Netherlands: ELSEVIER Ltd, 2004. 36-37.
注: 熱伝導率、密度、終端領域は推定値です。
高弾性グラファイト
ソースはありません。
HTS150
"TC250 Resin System." Product Data Sheet, TenCate Advanced Composites USA, Inc., Morgan Hill, CA., Revised March 2007
注: 値は Autodesk Material Manager のマイクロメカニックスに基づいています。強度、熱伝導率、密度、終端領域は推定値です。
IM7 カーボン

複数のソース:

Kaddour, A.S. and 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., (May 1986).
S-2 ファイバーグラス

複数のソース:

"S-2 Glass Fiber", Owens-Corning Fiberglass Corporation, Pub. No. 15-PL-16154, (March 1990).

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

Silenka E-ガラス 1200tex
Hinton, M.J., Kaddour, A.S. and Soden, P.D., "Failure Criteria in Fibre Reinforced Polymer Composites: The World-Wide Failure Exercise." The Netherlands: ELSEVIER Ltd, 2004. 36-37.
注: 熱伝導率、密度、終端領域は推定値です。
T300 カーボン

複数のソース:

Kaddour, A.S. and 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 カーボン
"T800 Continuous Carbon Fiber." Product Data Sheet, Toray Carbon Fibers America, Inc., Flower Mound, TX.
注: 材料特性は、Autodesk Material Manager のマイクロメカニックスの推定値です。終端領域は推定値です。
超弾性グラファイト
ソースはありません。

コア材料

アルミニウム合金ハニカム
"HexWeb Honeycomb Attributes and Properties." Hexcel Corporation, Dublin, CA. pp. 16-17
アルミニウム合金 Flex-Core
"HexWeb Honeycomb Attributes and Properties." Hexcel Corporation, Dublin, CA. pp. 18
バルサ材
"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. No. TSB-120, (1988).
高密度の泡
"Sandwich Core Material Average Physical Properties, Divinycell" Diab-Barracuda, Doc. No. 87.03.3000, (1987).
低密度の泡
"Sandwich Core Material Average Physical Properties, Divinycell" Diab-Barracuda, Doc. No. 87.03.3000, (1987).
HRH-10 アラミド繊維強化ハニカム
"HexWeb Honeycomb Attributes and Properties." Hexcel Corporation, Dublin, CA. pp. 21

合金

1025 鋼
"Metallic Materials and Elements for Aerospace Vehicle Structures," MILHDBK-5E, Dept. of Defense, (June 1987).
6061-T6 アルミニウム
"Metallic Materials and Elements for Aerospace Vehicle Structures," MILHDBK-5E, Dept. of Defense, (June 1987).
Ti-6Al-4v チタン
"Metallic Materials and Elements for Aerospace Vehicle Structures," MILHDBK-5E, Dept. of Defense, (June 1987).