Advanced design for lightweight structures: Review and prospects

作者：Braga Daniel F O^*; Tavares S M O; da Silva Lucas F M; Moreira P M G P; de Castro Paulo M S T

来源：Progress in Aerospace Sciences, 2014, 69: 29-39.

DOI：10.1016/j.paerosci.2014.03.003

• Structural design
• Safe-life
• Fail-safe
• Damage tolerance
• Structural health monitoring
• Self-healing structures

Current demand for fuel efficient aircraft has been pushing the aeronautical sector to develop ever more lightweight designs while keeping safe operation and required structural strength. Along with light-weighting, new structural design concepts have also been established in order to maintain the aircraft in service for longer periods of time, with high reliability levels. All these innovations and requirements have led to deeply optimized aeronautical structures contributing to more sustainable air transport. %26lt;br%26gt;This article reviews the major design philosophies which have been employed in aircraft structures, including safe-life, fail-safe and damage tolerance taking into account their impact on the structural design. A brief historical review is performed in order to analyse what led to the development of each philosophy. Material properties are related to each of the design philosophies. %26lt;br%26gt;Damage tolerant design has emerged as the main structural design philosophy in aeronautics, requiring deep knowledge on materials fatigue and corrosion strength, as well as potential failure modes and non-destructive inspection techniques, particularly minimum detectable defect and scan times. %26lt;br%26gt;A discussion on the implementation of structural health monitoring and self-healing structures within the current panorama of structures designed according to the damage tolerant philosophy is presented. This discussion is aided by a review of research on these two subjects. These two concepts show potential for further improving safety and durability of aircraft structures.

• 出版日期2014-8