Vacuum bag only co-bonding prepreg skins to aramid honeycomb core. Part I. Model and material properties for core pressure during processing

Abstract A process model was developed for the honeycomb core pressure during sandwich panel manufacturing. The model predicted the inflow of moisture from the cell walls into the cell void space using by Fick’s law, and the outflow of moist air through the bag-side skin was governed by Darcy’s law. The model required the core moisture content and honeycomb skin through-thickness air permeability to be experimentally measured. A partially saturated out-of-autoclave woven prepreg was used as the skin material in this study. In-order to accurately apply Darcy’s law during elevated temperature processing, an incremental temperature measurement technique was proposed to maintain constant skin thickness during air permeability characterization. Micro-CT imaging was performed on cure quenched samples to confirm that the proposed characterization technique maintained the impregnation dynamics of the target cure cycle. Model predictions using the characterized material properties are compared to in-situ core pressure measurements in Part II.

[1]  J. Månson,et al.  Influence of Process Pressure on Local Facesheet Instability for Ultra-light Sandwich Structures , 2009 .

[2]  F. Dullien Porous Media: Fluid Transport and Pore Structure , 1979 .

[3]  J. Seferis,et al.  Prepreg gas permeation as a function of fiber orientation and aging time , 1995 .

[4]  S. Advani,et al.  Resin film impregnation in fabric prepregs with dual length scale permeability , 2013 .

[5]  J. Bear Dynamics of Fluids in Porous Media , 1975 .

[6]  S. Drapier,et al.  Gas transport in fibrous media: Application to in-plane permeability measurement using transient flow , 2013 .

[7]  P. Hubert,et al.  Anisotropic air permeability in out-of-autoclave prepregs: Effect on honeycomb panel evacuation prior to cure , 2013 .

[8]  Y. Çengel Heat and Mass Transfer: A Practical Approach , 2006 .

[9]  Response of Graphite/Epoxy Sandwich Panels to Moisture and Temperature Transients , 1980 .

[10]  V. Michaud,et al.  Vacuum-bag processing of sandwich structures: role of honeycomb pressure level on skin-core adhesion and skin quality , 2010 .

[11]  Jan-Anders E. Månson,et al.  Hybrid processing of thick skins for honeycomb sandwich structures , 2011 .

[12]  P. Hubert,et al.  Modelling the effect of material properties and process parameters on tow impregnation in out-of-autoclave prepregs , 2012 .

[13]  Jan-Anders E. Månson,et al.  Assessment of semi-impregnated fabrics in honeycomb sandwich structures , 2010 .

[14]  Karsten Pruess,et al.  Gas Flow in Porous Media With Klinkenberg Effects , 1996 .

[15]  Timotei Centea,et al.  Measuring the impregnation of an out-of-autoclave prepreg by micro-CT , 2011 .

[16]  Suresh G. Advani,et al.  Desirable features in mold filling simulations for Liquid Composite Molding processes , 2004 .

[17]  G. Springer,et al.  Moisture Absorption and Desorption of Composite Materials , 1976 .

[18]  Jan-Anders E. Månson,et al.  Non-autoclave processing of honeycomb sandwich structures: Skin through thickness air permeability during cure , 2010 .

[19]  J. Jiao,et al.  A falling-pressure method for measuring air permeability of asphalt in laboratory , 2004 .

[20]  A. Fick V. On liquid diffusion , 1855 .

[21]  Yu Wang,et al.  Measurement of permeability of continuous filament mat glass–fibre reinforcements by saturated radial airflow , 2007 .

[22]  F. C. Campbell Manufacturing technology for aerospace structural materials , 2006 .

[23]  P. Hubert,et al.  Thermal models for MTM45-1 and Cycom 5320 out-of-autoclave prepreg resins , 2013 .

[24]  Shawn M. Walsh,et al.  Permeability characterization of dual scale fibrous porous media , 2006 .

[25]  Jan-Anders E. Månson,et al.  Through thickness air permeability of prepregs during cure , 2009 .

[26]  Z. Zhang,et al.  Measurement and analysis on in-plane and through-thickness air permeation of fiber/resin prepreg , 2011 .

[27]  J. Nam,et al.  Gas permeation and viscoelastic deformation of prepregs in composite manufacturing processes , 1995 .

[28]  S. Grove,et al.  An investigation of the skin/core bond in honeycomb sandwich structures using statistical experimentation techniques , 2006 .

[29]  J. Seferis,et al.  Thermal and air permeation properties of a carbon fiber/toughened epoxy based prepreg system , 1997 .

[30]  C. Wilke A Viscosity Equation for Gas Mixtures , 1950 .

[31]  P. Hubert,et al.  Air evacuation during vacuum bag only prepreg processing of honeycomb sandwich structures: in-plane air extraction prior to cure , 2015 .