Autonomous stimulus triggered self-healing in smart structural composites

被引:51
作者
Norris, C. J. [1 ]
White, J. A. P. [1 ]
McCombe, G. [1 ]
Chatterjee, P. [1 ]
Bond, I. P. [1 ]
Trask, R. S. [1 ]
机构
[1] Univ Bristol, Dept Aerosp Engn, ACCIS, Bristol BS8 1TR, Avon, England
基金
英国工程与自然科学研究理事会;
关键词
FIBER-REINFORCED POLYMER; IMPACT DAMAGE; RESISTANCE;
D O I
10.1088/0964-1726/21/9/094027
中图分类号
TH7 [仪器、仪表];
学科分类号
0804 ; 080401 ; 081102 ;
摘要
Inspired by the ability of biological systems to sense and autonomously heal damage, this research has successfully demonstrated the first autonomous, stimulus triggered, self-healing system in a structural composite material. Both the sensing and healing mechanisms are reliant on microvascular channels incorporated within a laminated composite material. For the triggering mechanism, a single air filled vessel was pressurized, sealed and monitored. Upon drop weight impact (10 J), delamination and microcrack connectivity between the pressurized vessel and those open to ambient led to a pressure loss which, with the use of a suitable sensor, triggered a pump to deliver a healing agent to the damage zone. Using this autonomous healing approach, near full recovery of post-impact compression strength was achieved (94% on average). A simplified alternative system with healing agent continuously flowing through the vessels, akin to blood flow, was found to offer 100% recovery of the material's virgin strength. Optical microscopy and ultrasonic C-scanning provided further evidence of large-scale infusion of matrix damage with the healing agent. The successful implementation of this bioinspired technology could substantially enhance the integrity and reliability of aerospace structures, whilst offering benefits through improved performance/weight ratios and extended lifetimes.
引用
收藏
页数:10
相关论文
共 35 条
[1]   Ways and options for aircraft structural health management. [J].
Boller, C .
SMART MATERIALS & STRUCTURES, 2001, 10 (03) :432-440
[2]   PERSPECTIVES ON WOUND-HEALING IN RESISTANCE TO PATHOGENS [J].
BOSTOCK, RM ;
STERMER, BA .
ANNUAL REVIEW OF PHYTOPATHOLOGY, 1989, 27 :343-371
[3]   THE IMPACT RESISTANCE OF COMPOSITE-MATERIALS - A REVIEW [J].
CANTWELL, WJ ;
MORTON, J .
COMPOSITES, 1991, 22 (05) :347-362
[4]   Visceral pain [J].
Cervero, F ;
Laird, JMA .
LANCET, 1999, 353 (9170) :2145-2148
[5]   Impact on composite structures [J].
Davies, GAO ;
Olsson, R .
AERONAUTICAL JOURNAL, 2004, 108 (1089) :541-563
[6]   Structural health monitoring techniques for aircraft composite structures [J].
Diamanti, K. ;
Soutis, C. .
PROGRESS IN AEROSPACE SCIENCES, 2010, 46 (08) :342-352
[7]   Autonomous materials with controlled toughening and healing [J].
Garcia, Michael E. ;
Lin, Yirong ;
Sodano, Henry A. .
JOURNAL OF APPLIED PHYSICS, 2010, 108 (09)
[8]   Self-Healing of Internal Damage in Synthetic Vascular Materials [J].
Hamilton, Andrew R. ;
Sottos, Nancy R. ;
White, Scott R. .
ADVANCED MATERIALS, 2010, 22 (45) :5159-+
[9]   Modes I and II interlaminar fracture toughness and fatigue delamination of CF/epoxy laminates with self-same epoxy interleaf [J].
Hojo, Masaki ;
Ando, Tadashi ;
Tanaka, Mototsugu ;
Adachi, Taiji ;
Ochiai, Shojiro ;
Endo, Yoshihiro .
INTERNATIONAL JOURNAL OF FATIGUE, 2006, 28 (10) :1154-1165
[10]   Characterization and analysis of carbon fibre-reinforced polymer composite laminates with embedded circular vasculature [J].
Huang, C. -Y. ;
Trask, R. S. ;
Bond, I. P. .
JOURNAL OF THE ROYAL SOCIETY INTERFACE, 2010, 7 (49) :1229-1241