Fatigue Degradation of the Ram-Air Parachute Canopy Structure

Q4 Engineering Fatigue of Aircraft Structures Pub Date : 2019-12-01 DOI:10.2478/fas-2019-0010
K. Szafran, Ireneusz Kramarski
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引用次数: 2

Abstract

Abstract In this work, the authors continue researching issues related to fatigue of aircraft structures made of fabrics. Parachute systems are widely used in military, sport and recreational aviation. Braking parachutes as well as skydiving and troop parachutes are characterized by the repeated use of parachute canopies, which are exposed to wear and fatigue. Until now, parachutes were difficult to design aviation systems due to their complex and unsteady opening characteristics, large changes in the geometry of canopies, suspension lines and tape risers as well as exposure to stochastic atmospheric turbulence. The fatigue of the canopy fabric, suspension lines and tape risers is a problem that must be addressed by textile designers and designers of reusable parachute systems. The authors of this work demonstrate the complexity of operating a parachute in hard multiple use conditions and propose ways to extend the parachute’s service life without compromising safety.
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冲压空气伞篷结构的疲劳退化
在这项工作中,作者继续研究与织物制成的飞机结构疲劳有关的问题。降落伞系统广泛应用于军事、体育和娱乐航空。制动伞以及跳伞和部队伞的特点是反复使用伞篷,暴露在磨损和疲劳中。到目前为止,降落伞的打开特性复杂且不稳定,伞盖、悬挂绳和胶带立管的几何形状变化很大,并且暴露于随机的大气湍流中,这给航空系统的设计带来了困难。伞篷织物、悬挂绳和胶带立管的疲劳是纺织品设计师和可重复使用降落伞系统设计师必须解决的问题。这项工作的作者展示了在多种使用条件下操作降落伞的复杂性,并提出了在不影响安全的情况下延长降落伞使用寿命的方法。
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来源期刊
Fatigue of Aircraft Structures
Fatigue of Aircraft Structures Engineering-Safety, Risk, Reliability and Quality
CiteScore
0.40
自引率
0.00%
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0
期刊介绍: The publication focuses on problems of aeronautical fatigue and structural integrity. The preferred topics include: full-scale fatigue testing of aircraft and aircraft structural components, fatigue of materials and structures, advanced materials and innovative structural concepts, damage tolerant design of aircraft structure, life extension and management of ageing fleets, structural health monitoring and loads, fatigue crack growth and life prediction methods, NDT inspections, airworthiness considerations.
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