无机材料学报 ›› 2026, Vol. 41 ›› Issue (9): 1157-1177.DOI: 10.15541/jim20250494
• 综述 • 下一篇
黄淦1,2(
), 薛佳祥2(
), 檀财旺1(
), 刘洋2, 张国梁2, 杨正茂3, 陈招科4
收稿日期:2025-12-14
修回日期:2026-02-09
出版日期:2026-09-20
网络出版日期:2026-02-28
通讯作者:
薛佳祥, 教授级高级工程师. E-mail: jiaxiang_xue@163.com;作者简介:黄 淦(2003-), 男, 博士研究生. E-mail: 24B909009@stu.hit.edu.cn
基金资助:
HUANG Gan1,2(
), XUE Jiaxiang2(
), TAN Caiwang1(
), LIU Yang2, ZHANG Guoliang2, YANG Zhengmao3, CHEN Zhaoke4
Received:2025-12-14
Revised:2026-02-09
Published:2026-09-20
Online:2026-02-28
Contact:
XUE Jiaxiang, professor. E-mail: About author:HUANG Gan (2003-), male, PhD candidate. E-mail: 24B909009@stu.hit.edu.cn
Supported by:摘要:
SiC复合包壳因其高比强度、耐中子辐照和抗高温氧化等特性, 有望替代传统锆合金包壳的颠覆性核燃料包壳技术。然而, SiC复合包壳结构复杂, 在服役条件下的力学失效行为尚不明确, 制约了技术迭代与应用。为深入揭示SiC复合包壳损伤机理、预测极端环境下应力开裂风险并推进其工程应用, 需开展系统性的多尺度力学损伤研究。本文围绕核用SiC复合包壳的多尺度力学损伤研究方法进行评述, 涵盖宏观及微纳力学试验, 基于数字图像相关、X射线计算机断层扫描和声发射等技术的原位监测与原位电镜表征, 以及多尺度数值仿真等方面。目前该领域已取得重要进展: 宏观力学测试可有效表征SiC复合包壳的整体力学性能, 多种原位监测技术实现了包壳从表面到内部、从静态到动态的多维损伤演化观测, 微纳力学测试为获取纤维、基体及界面等微区组元的力学参数提供了支撑, 多尺度数值仿真则构建了从微观机制到宏观响应的有效关联与预测桥梁。最后, 本文对该领域未来发展趋势与挑战进行了展望。
中图分类号:
黄淦, 薛佳祥, 檀财旺, 刘洋, 张国梁, 杨正茂, 陈招科. 核用SiC复合包壳多尺度力学损伤研究方法评述[J]. 无机材料学报, 2026, 41(9): 1157-1177.
HUANG Gan, XUE Jiaxiang, TAN Caiwang, LIU Yang, ZHANG Guoliang, YANG Zhengmao, CHEN Zhaoke. Multi-scale Methods for Investigating Mechanical Damage in Nuclear SiC Composite Cladding: A Review[J]. Journal of Inorganic Materials, 2026, 41(9): 1157-1177.
图1 压水堆燃料组件[5]与SiC复合包壳的结构示意图
Fig. 1 Schematic diagrams of the structure of the pressurized water reactor fuel assembly[5] and the SiC composite cladding (a) Pressurized water reactor fuel rod bundle assembly[5]; (b) SiC composite cladding tube
图2 SiC复合包壳宏观力学试验示意图[16,23,32,34]
Fig. 2 Schematic diagrams of macroscopic mechanical tests for SiC composite cladding[16,23,32,34] (a) Uniaxial tension[16]; (b) Expansion due compression[23]; (c) Hydraulic burst test[32]; (d) C-ring compression[34]
图3 单/双编织层厚裸SiC管的四点弯曲试验结果及SEM断口形貌[49]
Fig. 3 Four-point bending test results and SEM fracture surfaces of single/double-layer SiC braided tubes[49] (a) Single-layer; (b) Double-layer; (c) SEM fracture surfaces
| Testing method | Core function | Key advantages | Main limitations |
|---|---|---|---|
| Uniaxial tension test | To obtain axial intrinsic mechanical properties (modulus, strength) | Standardized method, direct quantification of axial response | Primarily reflecting axial performance, differing from the actual hoop-stress-dominated stress state |
| Expansion due compression test | To evaluate the hoop strength and failure behavior of tubular specimens | Simple operation, short setup time | Suitable only for short tubes, prone to stress concentration leading to premature local failure |
| Hydraulic burst test | To evaluate the hoop strength and failure behavior of tubular specimens | Fluid medium ensures uniform hoop stress distribution, applicable to tubes of various lengths | Complex operation, high cost, safety risks from seal failure or fluid jetting |
| C-ring compression test | To determine hoop strength, especially suitable for high-temperature testing | Minimal sample requirement, easy implementation, ideal for high- temperature screening | Sensitive to defect distribution due to significant stress concentration |
| Four-point bending test | To assess flexural performance and overall structural integrity | Four-point bending provides a uniform and stable bending stress field | Absence of well-established research and standards for tubular specimens |
表1 宏观力学测试方法简要对比
Table 1 Brief comparison of macro-mechanical testing methods
| Testing method | Core function | Key advantages | Main limitations |
|---|---|---|---|
| Uniaxial tension test | To obtain axial intrinsic mechanical properties (modulus, strength) | Standardized method, direct quantification of axial response | Primarily reflecting axial performance, differing from the actual hoop-stress-dominated stress state |
| Expansion due compression test | To evaluate the hoop strength and failure behavior of tubular specimens | Simple operation, short setup time | Suitable only for short tubes, prone to stress concentration leading to premature local failure |
| Hydraulic burst test | To evaluate the hoop strength and failure behavior of tubular specimens | Fluid medium ensures uniform hoop stress distribution, applicable to tubes of various lengths | Complex operation, high cost, safety risks from seal failure or fluid jetting |
| C-ring compression test | To determine hoop strength, especially suitable for high-temperature testing | Minimal sample requirement, easy implementation, ideal for high- temperature screening | Sensitive to defect distribution due to significant stress concentration |
| Four-point bending test | To assess flexural performance and overall structural integrity | Four-point bending provides a uniform and stable bending stress field | Absence of well-established research and standards for tubular specimens |
图4 DIC计算的SiC包壳表面环向应变εhoop在不同载荷下的图像[60]
Fig. 4 Images of the circumferential strain εhoop on the surface of the SiC cladding calculated by DIC[60] (a) Fault map under 0 N load; (b-d) Strain εhoop measurement results obtained within the elastic range: (b) 2100 N, (c) 2500 N, (d) 2730 N
图5 原位XCT监测下的多涂层SiC复合包壳高温C环压缩失效行为[69]
Fig. 5 Compressive failure behavior of multi-coated SiC composite cladding in high temperature C-ring under in-situ XCT monitoring[69] (a) Meso-structure of the cladding tube showing the multi-layer coating and CMC matrix; (b) Schematic of the in-situ high-temperature C-ring compression test coupled with 3D-XCT imaging; (c) Real-time crack propagation and failure mechanisms at room temperature and 1200 ℃ under different load levels (0.58PU and 0.73PU, where PU is the maximum load applied (peak load))
图6 声发射监测下的三层SiC复合包壳的准静态径向压缩实验[85]
Fig. 6 Quasi-static radial compression experiment of a three-layer SiC composite cladding under acoustic emission monitoring[85] (a) Schematic diagram of the test site; (b) Test equipment and test sample; (c) Schematic diagram of acoustic emission acquisition
图7 纳米压痕试验示例结果及纤维TEM照片[91]
Fig. 7 Example results of nanoindentation test and TEM images of fibers[91] (a) Nanoindentation illustration; (b) Radial distribution of the inclusions within a fiber; (c) Relationship between hardness and modulus varying with depth; (d) Cross-section of a fiber; (e) Inclusions at the grain boundaries of fibers; (f) EDX linescan signals of C and Si
图9 微柱在微柱压缩试验后的SEM照片[110]
Fig. 9 SEM images of the micro-pillar after micro-pillar compression test[110] (a) Remaining part of the 55° pillar; (b) Top piece removed from the 55° pillar
图10 微柱压缩测量PyC界面层断裂韧性示意图[111]
Fig. 10 Schematic diagrams illustrating the microcolumn compression measurement of the fracture toughness of the PyC interface layer[111] (a, b) Schematic diagrams of microcolumn compression test; (c) Stress state and force balance of typical microcolumn compression structures; (d) Performance of interface layers of different thicknesses
| Testing Method | Core function | Key advantages | Main limitations |
|---|---|---|---|
| Nanoindentation | To measure hardness and elastic modulus of micro-regions (fiber, matrix, etc.) | Relatively simple sample preparation, enabling rapid property mapping via arrays | Susceptible to size effects and matrix constraint effects |
| Push-out/Push-in | To characterize the interfacial shear strength between fiber and matrix | Enabling direct use of bulk samples via push-in technique, avoiding preparation-induced damage | Requiring validation with other techniques due to indirect signal interpretation |
| Micro-pillar compression | To obtain the intrinsic strength and deformation behavior of micro-regions (e.g., interface) | Providing robust data via simple stress state, offering a realistic measure of interfacial bonding | Time-consuming FIB preparation with potential damage and significant size effects |
| Micro-cantilever bending | To measure the fracture toughness of micro-regions (fiber, matrix, etc.) | Enabling direct measurement of fracture toughness parameters | Highly dependent on precise FIB machining, which is complex and time-consuming |
表2 微纳力学测试方法简要对比
Table 2 Brief comparison of micro-/nano-mechanical testing methods
| Testing Method | Core function | Key advantages | Main limitations |
|---|---|---|---|
| Nanoindentation | To measure hardness and elastic modulus of micro-regions (fiber, matrix, etc.) | Relatively simple sample preparation, enabling rapid property mapping via arrays | Susceptible to size effects and matrix constraint effects |
| Push-out/Push-in | To characterize the interfacial shear strength between fiber and matrix | Enabling direct use of bulk samples via push-in technique, avoiding preparation-induced damage | Requiring validation with other techniques due to indirect signal interpretation |
| Micro-pillar compression | To obtain the intrinsic strength and deformation behavior of micro-regions (e.g., interface) | Providing robust data via simple stress state, offering a realistic measure of interfacial bonding | Time-consuming FIB preparation with potential damage and significant size effects |
| Micro-cantilever bending | To measure the fracture toughness of micro-regions (fiber, matrix, etc.) | Enabling direct measurement of fracture toughness parameters | Highly dependent on precise FIB machining, which is complex and time-consuming |
图12 不同水平载荷下的表面裂纹扩展路径SEM照片[125]
Fig. 12 SEM images of surface crack propagation paths under different load levels[125] In unreinforced matrix region: (a) 60 MPa, (b) 65 MPa, (c) 70 MPa; In transverse fiber bundles: (d) 60 MPa, (e) 65 MPa; In longitudinal fiber bundles: (f) 70 MPa
图13 SiCf/SiC复合材料的微观RVE模型与不同加载条件下的累积应变等值线图[133]
Fig. 13 Micro-scale RVE model of SiCf/SiC composite material and the contour maps of cumulative strain under different loading conditions[133] (a) Random fiber distribution; (b) Fiber groups; (c) Matrix groups; (d) Interface groups and contour maps of cumulative strain under different loading conditions; (e) Transverse tension; (f) Transverse compression; (g) Out-of-plane shear
图14 SiC纤维束的RVE模型和三种不同的SiC内外编织结构模型[134]
Fig. 14 RVE model of SiC fiber bundle and three different models of SiC internal and external weaving structures[134] (a) SiC fiber bundle RVE model; (b) Braided structure inside B1; (c) Braided structure outside B1; (d) Braided structure inside B2; (e) Braided structure outside B2; (f) Braided structure inside B3; (g) Braided structure outside B3
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