Pregled bibliografske jedinice broj: 141425
Fatique and Corrosion Issues for Safety Improvements in Aviation Industry
Fatique and Corrosion Issues for Safety Improvements in Aviation Industry // SAE Technical Papers - International Body Engineering Conference (IBEC 2003) Proceedings / Koibuchi, Koji (ur.).
Tokyo: Society of Automative Engineering, 2003. str. 367-370 doi:10.4271/2003-01-2800 (predavanje, međunarodna recenzija, cjeloviti rad (in extenso), znanstveni)
CROSBI ID: 141425 Za ispravke kontaktirajte CROSBI podršku putem web obrasca
Naslov
Fatique and Corrosion Issues for Safety Improvements in Aviation Industry
Autori
Galović, Borivoj ; Steiner, Sanja
Vrsta, podvrsta i kategorija rada
Radovi u zbornicima skupova, cjeloviti rad (in extenso), znanstveni
Izvornik
SAE Technical Papers - International Body Engineering Conference (IBEC 2003) Proceedings
/ Koibuchi, Koji - Tokyo : Society of Automative Engineering, 2003, 367-370
Skup
International Body Engineering Conference (IBEC 2003)
Mjesto i datum
Chiba, Japan, 27.10.2003. - 29.10.2003
Vrsta sudjelovanja
Predavanje
Vrsta recenzije
Međunarodna recenzija
Ključne riječi
Fatique ; Corrosion ; Structure Integrity ; Durability ; Reliability ; Crashworthiness
Sažetak
Analyzing structure elements in a design estimated lifetime, structure integrity and capability to withstand all loadings is highly reduced by the end of designed estimated lifetime. Durability and reliability of vehicle structures is a function of fatigue and corrosion issues, which respectively affects crashworthiness requirements and safety. In aviation industry, from the point of a structure design, three structure design generations could be differentiated: a) the generation where major structure design is based on static strength and build-in redundancy i.e. some fail-safe elements ; b) the generation introducing fail-tolerant structure design philosophy ; and c) the generation additionally introducing full scale fatigue testing to determine wide-spread fatigue damage and corrosion prevention and control program. Implementation of aircraft structure design and maintenance philosophy i.e. in aviation recommended and standardized programs such as Supplement Structure Inspection Program, Corrosion Prevention and Control Program, Wide-Spread Fatigue damage evaluation and Repair Assessment Evaluation, may result with significant contribution to safety level in automotive industry.
Izvorni jezik
Engleski
Znanstvena područja
Tehnologija prometa i transport
POVEZANOST RADA
Ustanove:
Fakultet prometnih znanosti, Zagreb,
Institut prometa i veza, Zagreb
Citiraj ovu publikaciju:
Časopis indeksira:
- Scopus