Resin infusion process applies a vacuum to draw resin into the mold cavity for mold filling. In this study, a low cost mold of a helicopter landing gear with a bow shape was constructed. A vacuum-assisted resin infusion process was used to fabricate the landing gear. A preheater is constructed and integrated in the process to heat the resin to a specified temperature before flowing into the mold while the mold is kept at a room temperature. Numerical simulation of the resin infusion process was used to study the effect of the heated resin on the filling result. An adiabatic boundary condition was used to simulate the heat transfer condition at the foam core side of the part during the filling process. During the resin infusion process, the filling pressure is lower than the atmosphere pressure and the resulting filling flow is very slow in this case. Temperature of the resin will decrease quickly as entering the mold to meet the cool preplaced fiber reinforcements. However, increase of the resin temperature can reduce the viscosity and reduce the filling time. A critical temperature is identified in the simulation below which the heated resin can fill the mold without any gellation.


    Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Process analysis of a helicopter landing gear prototype using resin infusion molding


    Contributors:


    Publication date :

    2007


    Size :

    6 Seiten, 9 Bilder, 1 Tabelle, 15 Quellen



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English





    Helicopter landing gear

    Allward, M.F. | Engineering Index Backfile | 1953


    HELICOPTER SKID LANDING GEAR

    BERNIER SIMON / FEWS ROBERT CLIVE / GUILLOT MICHEL et al. | European Patent Office | 2017

    Free access

    HELICOPTER SKID LANDING GEAR

    LARKIN III JOHN C / WARD EMERY N / SUMNER WILLIAM P et al. | European Patent Office | 2019

    Free access

    Helicopter skid landing gear

    LARKIN III JOHN C / WARD EMERY N / SUMNER WILLIAM P et al. | European Patent Office | 2020

    Free access