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JETELA, V.; KLEMENT, J.; AUGUSTIN, P.
Originální název
Possibility for improving damage tolerance of integral structure by high strength bonded straps
Anglický název
Druh
Stať ve sborníku v databázi WoS či Scopus
Originální abstrakt
Integral stringer panels can attain weight reduction in a primary aircraft structures, but does not contain physical barriers for fatigue crack growth. One of the promising technique for prolonging fatigue life are bonded crack retarders made of materials with high stiffness. Experimental study was done on two specimens with different geometries. The straps consisted of high strength corrosion resistant steel AISI 301 was adhesively bonded to an aluminium alloy 2024-T351 Center-Cracked Tension (CCT) specimens fabricated by a high-speed machining process to promote fatigue crack growth retardation. Specimens were tested at constant amplitude load. The study concludes that the fatigue crack growth life can be significantly improved.
Anglický abstrakt
Klíčová slova
Bonded crack retarder, Damage tolerance, Fatigue crack growth, Integral structure, Strap
Klíčová slova v angličtině
Autoři
Rok RIV
2018
Vydáno
01.06.2017
Nakladatel
University of Defence
Místo
Brno
ISBN
978-80-7231-420-1
Kniha
14th Seminar "Materials and technologies in Special Technics Production 2017"
Strany od
29
Strany do
33
Strany počet
5
BibTex
@inproceedings{BUT136641, author="Václav {Jetela} and Josef {Klement} and Petr {Augustin}", title="Possibility for improving damage tolerance of integral structure by high strength bonded straps", booktitle="14th Seminar {"}Materials and technologies in Special Technics Production 2017{"}", year="2017", pages="29--33", publisher="University of Defence", address="Brno", isbn="978-80-7231-420-1" }