A High-Consolidation Electron Beam-Curing Process for Manufacturing Three-Dimensional Advanced Thermoset Composites

Author:

Rizzolo Robert H.1,Walczyk Daniel F.1,Montoney Daniel2,Simacek Pavel3,Mahbub Md Rashef1

Affiliation:

1. Rensselaer Polytechnic Institute Department of Mechanical, Aerospace & Nuclear Engineering, , 110 Eighth Street, Troy, NY 12180

2. Rapid Cure Technologies, Inc. , 7030 Fly Road, East Syracuse, NY 13057

3. Department of Mechanical Engineering, University of Delaware Center for Composite Materials, , 101 Academy Street, Newark, DE 19716

Abstract

Abstract This paper describes the application of a new manufacturing process for low-cost and rapid consolidation and curing of advanced thermoset composites that avoids the use of expensive prepreg, autoclaving, and thermally induced curing. The process, called VIPE, uses a novel tooling design that combines vacuum infusion (VI) of a dry preform with resin, a rigidly backed pressure focusing layer (P) made of an elastomer to consolidate the wet preform with uniform pressure, and high-energy electron beam curing (E). A VIPE tool is engineered and fabricated to manufacture 3D laminate bicycle seats composed of woven carbon fiber textile and an electron beam-curable epoxy acrylate. Details of the tooling design discussed include computational fluid dynamics (CFD) simulation of the vacuum infusion, iterative structural finite element analysis (FEA) to synthesize the pressure focusing layer (PFL), structural FEA to design the top mold made of a composite sandwich structure for electron beam transparency, and Monte Carlo electron absorption simulations to specify the e-beam energy level. Ten parts are fabricated using the matched tool (bottom aluminum mold covered with silicone layer and top mold with carbon/epoxy skins separated by foam core) after the dry textile preform contained within is infused with resin, the tool halves are clamped under load, and a 3.0 MeV e-beam machine bombards the tool for less than 1 min. Part thickness, part stiffness, surface roughness, and fiber and void volume fractions measurements show that aerospace quality parts with low cycle times are achievable, although there is high variability due to the small number of replicates and need for process optimization.

Funder

Division of Civil, Mechanical and Manufacturing Innovation

New York State Energy Research and Development Authority

Publisher

ASME International

Subject

Industrial and Manufacturing Engineering,Computer Science Applications,Mechanical Engineering,Control and Systems Engineering

Reference29 articles.

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2. Electron Beam Cure of Composites for Aerospace Structures;Crasto,1997

3. Electron-Beam-Curable Epoxy Resins for the Manufacture of High-Performance Composites;Lopata;Radiat. Phys. Chem.,1999

4. A Comparison of Radiation and Thermal Curing of Thick Composites;Glauser;Macromol. Mater. Eng.,2000

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