Off-axis damage tolerance of fiber-reinforced composites for aerospace systems

被引：21

作者：

Galizia, P. ^{[1
]}

Sciti, D. ^{[1
]}

Saraga, F. ^{[1
]}

Zoli, L. ^{[1
]}

机构：

[1] Natl Res Council Italy, CNR, ISTEC, Inst Sci & Technol Ceram, Via Granarolo 64, I-48018 Faenza, Italy

来源：

JOURNAL OF THE EUROPEAN CERAMIC SOCIETY | 2020年 / 40卷 / 07期

关键词：

Transverse direction; Anisotropic porous ZrB2; Continuous fiber ceramic composites (CFCC); Vickers indentation; Pile-up; MECHANICAL-PROPERTIES; POROUS-MATRIX; FRACTURE-BEHAVIOR; THERMAL-SHOCK; CERAMICS; FABRICATION; MICROSTRUCTURE; RESISTANCE; STRENGTH; MODULUS;

D O I：

10.1016/j.jeurceramsoc.2019.12.038

中图分类号：

TQ174 [陶瓷工业]; TB3 [工程材料学];

学科分类号：

0805 ; 080502 ;

摘要：

Off-axis strength retention of continuous carbon fiber-reinforced dense ZrB2-based ceramics (C-f/ZrB2) after thermal or indentation damage was evaluated. Thermal damage was in-situ induced and characterized by cyclic dilatometric analysis. Indentation damage was induced through Vickers indentation and then characterized by digital microscopy. The investigation of Vickers imprints suggested that residual stresses promoted the material pileup onto the fibers' plane and the appearance of out-of-plane freed fibers (OFF). On the other hand, thermal damage reduced the residual stresses and left inner freed fibers (IFF) that enhanced the elastic response. Finally, the flexural tests on damaged specimens unexpectedly revealed that C-f/ZrB2 kept its load bearing capability either after thermal or indentation damage (in both cases) and showed damage insensitivity although tested in fully matrix-dominated loading configuration (off-axis configuration).

引用

页码：2691 / 2698

页数：8

共 42 条

[21]

Osada T, 2014, WOODH PUB S COMPOS S, P410, DOI 10.1533/9780857098825.2.410

[22] Advanced structural ceramics in aerospace propulsion [J].

Padture, Nitin P. .

NATURE MATERIALS, 2016, 15 (08) :804-809

[23] Transverse and longitudinal coefficient of thermal expansion of carbon fibers at high temperatures (300-2500 K) [J].

Pradere, C. ;

Sauder, C. .

CARBON, 2008, 46 (14) :1874-1884

[24] Design, fabrication and high velocity oxy-fuel torch tests of a Cf-ZrB2-fiber nozzle to evaluate its potential in rocket motors [J].

Sciti, D. ;

Zoli, L. ;

Silvestroni, L. ;

Cecere, A. ;

DiMartino, G. D. ;

Savino, R. .

MATERIALS & DESIGN, 2016, 109 :709-717

[25] Modelling of cracking of the ceramic foam specimen with a central notch under the tensile load [J].

Sevecek, Oldrich ;

Bertolla, Luca ;

Chlup, Zdenek ;

Rehorek, Lukas ;

Majer, Zdenek ;

Marcian, Petr ;

Kotoul, Michal .

THEORETICAL AND APPLIED FRACTURE MECHANICS, 2019, 100 :242-250

[26] Behavior of HfB2-30 vol% SiC UHTC obtained by sol-gel approach in the supersonic airflow [J].

Simonenko, Elizaveta P. ;

Simonenko, Nikolay P. ;

Gordeev, Andrey N. ;

Kolesnikov, Anatoly F. ;

Sevastyanov, Vladimir G. ;

Kuznetsov, Nikolay T. .

JOURNAL OF SOL-GEL SCIENCE AND TECHNOLOGY, 2019, 92 (02) :386-397

[27] Mechanical strength and damage tolerance of highly porous alumina ceramics produced from sintered particle stabilized foams [J].

Tallon, Carolina ;

Chuanuwatanakul, Chayuda ;

Dunstan, David E. ;

Franks, George V. .

CERAMICS INTERNATIONAL, 2016, 42 (07) :8478-8487

[28] Crack-healing in ceramics [J].

Tavangarian, Fariborz ;

Hui, David ;

Li, Guoqiang .

COMPOSITES PART B-ENGINEERING, 2018, 144 :56-87

[29] Concept for a damage-tolerant ceramic composite with ''strong'' interfaces [J].

Tu, WC ;

Lange, FF ;

Evans, AG .

JOURNAL OF THE AMERICAN CERAMIC SOCIETY, 1996, 79 (02) :417-424

[30] Ab-initio modeling and experimental investigation of properties of ultra-high temperature solid solutions TaxZr1-xC [J].

Vorotilo, S. ;

Sidnov, K. ;

Mosyagin, I. Yu ;

Khvan, A., V ;

Levashov, E. A. ;

Patsera, E., I ;

Abrikosov, I. A. .

JOURNAL OF ALLOYS AND COMPOUNDS, 2019, 778 :480-486

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