A way to secure operational safety for an aircraft structure according to a strength criterion

Autor:	G. I. Nesterenko, B. G. Nesterenko
Rok vydání:	2013
Předmět:	Structure (mathematical logic) Engineering Advisory circular Aviation business.industry Mechanical Engineering Survivability Mechanical engineering Civil engineering Industrial and Manufacturing Engineering Operational safety Safety Risk Reliability and Quality business Federal Aviation Regulations
Zdroj:	Journal of Machinery Manufacture and Reliability. 42:62-75
ISSN:	1934-9394 1052-6188
DOI:	10.3103/s1052618813010093
Popis:	Fatigue and survivability requirements for transport aircraft structures formulated in the US Federal Aviation Regulations FAR 25.571, Advisory Circular AC 20-107B and in the Russian Aviation Regulations AR 25.571 are analyzed. Information on the lifetime of foreign and Russian aircraft, those new and those operating for a long time, is presented. Strength, fatigue and crack growth resistances of foreign and Russian improved aluminum alloys are compared. Ways for applying composite materials in the structure of foreign and Russian aircraft are illustrated. It is shown that aluminum and composite materials fail in different ways.
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_________::852157dacc9d86950f39848beeec496a https://doi.org/10.3103/s1052618813010093 Zobrazit plný text záznamu Full text from SpringerLink