Repairing large cracks and reversing fatigue damage in structural metals

被引:26
|
作者
Fisher, Charles R. [1 ]
Henderson, Hunter B. [2 ]
Kesler, Michael S. [2 ]
Zhu, Pingping [3 ]
Bean, Glenn E. [4 ]
Wright, M. Clara [5 ]
Newman, John A. [6 ]
Brinson, L. Catherine [7 ]
Figueroa, Oscar, III [8 ]
Manuel, Michele, V [8 ]
机构
[1] Naval Surface Warfare Ctr, Carderock Div, 9500 MacArthur Blvd West, Bethesda, MD 20817 USA
[2] Oak Ridge Natl Lab, 1 Bethel Valley Rd, Oak Ridge, TN 37830 USA
[3] Fiat Chrysler Automobiles, 800 Chrysler Dr, Auburn Hills, MI 48326 USA
[4] Aerosp Corp, 2310 E El Segundo Blvd, El Segundo, CA 90245 USA
[5] NASA, John F Kennedy Space Ctr, Kennedy Space Ctr, FL 32899 USA
[6] NASA, NASA Langley Res Ctr, 1 Nasa Dr, Hampton, VA 23666 USA
[7] Northwestern Univ, 2145 Sheridan Rd,Tech A214, Evanston, IL 60208 USA
[8] Univ Florida, 100 Rhines Hall,POB 116400, Gainesville, FL 32611 USA
基金
美国国家科学基金会; 美国国家航空航天局;
关键词
Self-healing; Thermodynamics; Design; Metal-matrix composite; Shape-memory alloy; DESIGN;
D O I
10.1016/j.apmt.2018.07.003
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Self-healing materials represent a paradigm shift from traditional materials development, enabling intrinsic repair of functionality (such as strength) after a catastrophic failure as opposed to part replacement. Several healing mechanisms have been demonstrated in polymeric and ceramic materials, but few in metallic systems. This study demonstrates a novel liquid-assisted self-healing metal-matrix composite (MMC) designed to be capable of over 90% strength recovery after a healing cycle. The aluminum (A1)-based matrix is reinforced with continuous nickel-titanium (NiTi) shape-memory alloy (SMA) reinforcements. Using a tailored heat treatment for healing, a paired effect of crack closure from the SMA reinforcement and partial liquefaction of the matrix occurs. These effects result in a compressive force across the crack surface, and, coupled with increased diffusion rates from the liquefied matrix, produces consolidation and healing in the composite structure. This work provides experimental and computational evidence for the healing mechanism under both tensile and fatigue conditions. (C) 2018 The Authors. Published by Elsevier Ltd.
引用
收藏
页码:64 / 68
页数:5
相关论文
共 50 条
  • [41] Fatigue damage of structural materials IV
    Vasudevan, AK
    Nicholas, T
    Stepp, D
    Paris, PC
    INTERNATIONAL JOURNAL OF FATIGUE, 2003, 25 (9-11) : 789 - 789
  • [42] Structural Aspects of Fatigue Damage.
    Gouzou, J.
    Revue M. Mecanique, 1974, 20 (01): : 21 - 24
  • [43] METALS AND ALLOYS AT ELEVATED TEMPERATURES (STARTER CRACKS BY A RESONANCE FATIGUE TECHNIQUE)
    ACHTER, MR
    SMITH, HH
    SHAHINIA.P
    REPORT OF NRL PROGRESS, 1965, (AUG): : 23 - &
  • [44] Crossing grain boundaries in metals by slip bands, cleavage and fatigue cracks
    Pineau, Andre
    PHILOSOPHICAL TRANSACTIONS OF THE ROYAL SOCIETY A-MATHEMATICAL PHYSICAL AND ENGINEERING SCIENCES, 2015, 373 (2038):
  • [45] FATIGUE CRACK GROWTH OF BONDLINE CRACKS IN STRUCTURAL BONDED JOINTS
    BRUSSAT, TR
    CHIU, ST
    JOURNAL OF ENGINEERING MATERIALS AND TECHNOLOGY-TRANSACTIONS OF THE ASME, 1978, 100 (01): : 39 - 45
  • [46] Experimental investigation of structural system capacity with multiple fatigue cracks
    Zhang, Kaihua
    Collette, Matthew
    MARINE STRUCTURES, 2021, 78
  • [47] Identification of large structural damage
    Mak, PS
    Law, SS
    PROCEEDINGS OF IMAC-XIX: A CONFERENCE ON STRUCTURAL DYNAMICS, VOLS 1 AND 2, 2001, 4359 : 1628 - 1634
  • [48] Study on life and path of fatigue cracks in multiple site damage plates
    Seifi, Rahman
    Ghadimian, Oshin
    Ranjbaran, Milad
    INTERNATIONAL JOURNAL OF FATIGUE, 2015, 80 : 449 - 458
  • [49] ESTIMATING INITIATION TIMES OF SECONDARY FATIGUE CRACKS IN DAMAGE TOLERANCE ANALYSIS
    BRUSSAT, TR
    FATIGUE OF ENGINEERING MATERIALS AND STRUCTURES, 1983, 6 (03): : 281 - 292
  • [50] An experimental investigation on collective damage of short fatigue cracks for a stainless steel
    Hong, YS
    Zheng, XH
    Liu, N
    PROGRESS IN MECHANICAL BEHAVIOUR OF MATERIALS (ICM8), VOL 1: FATIGUE AND FRACTURE, 1999, : 53 - 56