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[73950] Artykuł:

Composite Materials Having a Layer Structure of "Sandwich" Construction as Above Used in Car Safety Bumpers

Czasopismo: Automotive Safety, 2018 XI International Science-Technical Conference   Strony: 1-8
ISBN:  978-1-5386-4578-9
Wydawca:  IEEE, 345 E 47TH ST, NEW YORK, NY 10017 USA
Opublikowano: 2018
 
  Autorzy / Redaktorzy / Twórcy
Imię i nazwisko Wydział Katedra Do oświadczenia
nr 3
Grupa
przynależności
Dyscyplina
naukowa
Procent
udziału
Liczba
punktów
do oceny pracownika
Liczba
punktów wg
kryteriów ewaluacji
Rafał Chatys orcid logo WMiBMKatedra Technik Komputerowych i Uzbrojenia**Takzaliczony do "N"Inżynieria mechaniczna2515.003.75  
A. Panich Niespoza "N" jednostki25.00.00  
Rafał Stanisław Jurecki orcid logo WMiBMKatedra Pojazdów Samochodowych i Transportu*Takzaliczony do "N"Inżynieria lądowa, geodezja i transport2515.003.75  
Martinsh Kleinhofs Niespoza "N" jednostki25.00.00  

Grupa MNiSW:  Materiały z konferencji międzynarodowej (zarejestrowane w Web of Science)
Punkty MNiSW: 15
Klasyfikacja Web of Science: Proceedings Paper


Web of Science Logo Web of Science    
Keywords:

honeycomb  passive safety  safety  safety systems  sandwich composites  



Abstract:

This paper is devoted to modern problems of reinforcement materials used in car bumpers manufacturing and as well as safety issues. Paper discusses methods and provisions for car bumper reinforcement material., As result the fail-safe energy absorbing construction is presented and tested, made from laminates A, B and C with sandwich filling of the method vacuum bagging, which confirmed the possibility of absorbing energy (i.e. work) in the entire range from 3.858 -6.680J (for a stationary barrier with an impact velocity of V = 10-15 km/h-formula 1). It was found that the destruction of sandwich laminates with sandwich fillers took place by cutting the interface and the resin layer between the carbon cloth layer and the glass matting layer. The highest impact value was determined for laminate A at the level of 133.75 J (with Soric XF (TM) filling), which was characterized by inter-layer cracking with plastic deformation of the core. Lower by about 65 and about 36% of the average impact strength for laminate C and B respectively compared to the average impact strength of laminate A, the of observed as a result of defects in the structure (i.e. plastic core deformation and one-sided delamination of aluminum and polypropylene respectively - PP from the components of the composites). In future using sandwich structured composites materials is very important from cost profitability from point through, testing and manufacturing, as well as composites repairs.