The synthesic description of the results, scientific achievements and practical applications the EUREKA initiative, the project IMPERJA, E3496!, improving the fatigue performance of revieted joints in air frames

• Autorzy: Kaniowski J.
• Języki publikacji: EN

Abstrakty

EN

Consortium Members: Institute of Aviation Poland, Coordinator; Polish Aviation Factory - PZL Mielec; AGH - University of Science and Technology, Faculty of mechanical Engineering & Robotics; UTP - University of technology and Sciences in Bydgoszcz - Faculty of Mechanical Eng., Dept. of machine Design; WAT - Military University of Technology, Inst. of Materials Science and Applied Mechanics, Dept. of General Mechanics; Stresstech Oy in Finland, Evektor Spol. S.R.O. Czech Republic.

Słowa kluczowe

EN

synthesic description; results; scientific achievements; practical applications; IMERJA Project

PL

syntetyczny opis wyników, osiągnięć naukowych i zastosowań praktycznych inicjatywy EUREKA projekt IMPERIA

• Wydawca: Wydawnictwa Naukowe Instytutu Lotnictwa
• Czasopismo: Prace Instytutu Lotnictwa
• Rocznik: 2011
• Tom: Nr 1 (210)
• Strony: 35--41
• Opis fizyczny: Bibliogr. 3 poz.

Twórcy

autor

Kaniowski J.

• Institute of Aviation Poland

Bibliografia

• [1] Li, G., Shi, G., Bellinger N.C. (2006). Studies of Residual Stress in Single-Row Countersunk Riveted Lap Joints, Journal of Aircraft, Vol. 43, No 3.
• [2] Muller R. G. P. (1995). An experimental and numerical investigation on the fatigue behaviour of fuselage riveted lap joints, PhD thesis, Delft University of Technology.
• [3] Müller R. P.G., Hart-Smith L.J. (1997). Making fuselage riveting lap splices with 200-year crackfree fatigue life. ICAF 97` „Fatigue in new and ageing aircraft”. Proceedings of the I9-th Symposium of the International Committee of Aeronautical Fatigue, Edinburgh, EMAS Publishing, 499-522.