Research article Topical Sections

Development and evaluation of aerogel-filled BMI sandwich panels for thermal barrier applications

  • Received: 09 May 2016 Accepted: 13 July 2016 Published: 19 July 2016
  • This study details a fabrication methodology envisaged to manufacture Glass/BMI honeycomb core aerogel-filled sandwich panels. Silica aerogel granules are used as core fillers to provide thermal insulation properties with little weight increase. Experimental heat transfer studies are conducted on these panels to study the temperature distribution between their two surfaces. Numerical studies are also carried out to validate the results. Despite exhibiting good thermal shielding capabilities, the Glass/BMI sandwich panels are found to oxidise at 180 ºC if exposed directly to heat. In order to increase the temperature bearing capacity and the operating temperature range for these panels, a way of coating them from outside with high temperature spray paint was tried. With a silicone-based coating, the temperature sustainability of these sandwich panels is found to increase to 350 ºC. This proved the effectiveness of the formed manufacturing process, selected high temperature coating, the coating method as well as the envisaged sandwich panel concept.

    Citation: Sunil C. Joshi, Abdullah A. Sheikh, A. Dineshkumar, Zhao Yong. Development and evaluation of aerogel-filled BMI sandwich panels for thermal barrier applications[J]. AIMS Materials Science, 2016, 3(3): 938-953. doi: 10.3934/matersci.2016.3.938

    Related Papers:

  • This study details a fabrication methodology envisaged to manufacture Glass/BMI honeycomb core aerogel-filled sandwich panels. Silica aerogel granules are used as core fillers to provide thermal insulation properties with little weight increase. Experimental heat transfer studies are conducted on these panels to study the temperature distribution between their two surfaces. Numerical studies are also carried out to validate the results. Despite exhibiting good thermal shielding capabilities, the Glass/BMI sandwich panels are found to oxidise at 180 ºC if exposed directly to heat. In order to increase the temperature bearing capacity and the operating temperature range for these panels, a way of coating them from outside with high temperature spray paint was tried. With a silicone-based coating, the temperature sustainability of these sandwich panels is found to increase to 350 ºC. This proved the effectiveness of the formed manufacturing process, selected high temperature coating, the coating method as well as the envisaged sandwich panel concept.


    加载中
    [1] Pilato LA, Michno MJ (1994) Advanced composite materials. Berlin: New York: Springer-Verlag.
    [2] Seferis JC, Nicolais L (Eds.) (1983) The role of the polymeric matrix in the processing and structural properties of composite materials. New York: Plenum Press.
    [3] Vinson J (2001) Sandwich Structures. Appl Mech Rev 54: 201.
    [4] Smith S, Shivakumar K (2001) Modified mode-I cracked sandwich beam (CSB) fracture test. 19th AIAA Applied Aerodynamics Conference. Anaheim, CA, USA.
    [5] Smith S, Shivakumar K (2004) In situ fracture toughness testing of core materials in sandwich panels. J Compos Mater 38: 655–668.
    [6] Gibson L, Ashby M (1997) Cellular Solids: structure and properties. New York: Cambridge University Press.
    [7] Mujika F, Pujana J, Olave M (2011) Test Method: On the determination of out-of-plane elastic properties of honeycomb sandwich panels. Polym Test 30: 222–228.
    [8] Foo C, Chai G, Seah L (2007) Mechanical properties of Nomex material and Nomex honeycomb structure. Compos Struct 80: 588–594.
    [9] Foo C, Chai G, Seah L (2008) A model to predict low-velocity impact response and damage in sandwich composites. Compos Sci Technol 68: 1348–1356.
    [10] Herup E, Palazotto A (1998) Low-velocity impact damage initiation in graphite/epoxy/Nomex honeycomb-sandwich plates. Compos Sci Technol 57: 1581–1598.
    [11] Aktay L, Johnson A, Holzapfel M (2005) Prediction of impact damage on composite panels. Comput Mater Sci 32: 252–260.
    [12] Czabaj M, Zehnder A, Davidson B, et al. (2014) Compressive strength of honeycomb-stiffened graphite/epoxy sandwich panels with barely-visible indentation damage. J Compos Mater 48: 2455–2471.
    [13] Sadowski T, Bec J (2011) Effective properties for sandwich plates with aluminium foil honeycomb core and polymer foam filling – Static and dynamic response. Comput Mater Sci 50: 1269–1275.
    [14] Chen Z, Yan N, Sam-Brew S, et al. (2014) Investigation of mechanical properties of sandwich panels made of paper honeycomb core and wood composite skins by experimental testing and finite element (FE) modelling methods. Eur J Wood Wood Prod 72: 311–319.
    [15] Wang L, Liu W, Fang H, et al. (2015) Behavior of sandwich wall panels with GFRP face sheets and foam-GFRP web core loaded under four-point bending. J Compos Mater 49: 2765–2778.
    [16] Cahyono S, Widodo A, Anwar M, et al. (2016) Light-weight sandwich panel honeycomb core with hybrid carbon-glass fiber composite skin for electric vehicle application. AIP Conference Proceedings 040025-1-040025-5. doi:10.1063/1.4943468.
    [17] Feli S, Namdari Pour M (2012) An analytical model for composite sandwich panels with honeycomb core subjected to high-velocity impact. Compos Part B Eng 43: 2439–2447.
    [18] Xiong J, Zhang M, Stocchi A, et al. (2014) Mechanical behaviors of carbon fiber composite sandwich columns with three dimensional honeycomb cores under in-plane compression. Compos Part B Eng 60: 350–358.
    [19] Wang B, Zhang G, He Q, et al. (2014) Technical report: Mechanical behavior of carbon fiber reinforced polymer composite sandwich panels with 2-D lattice truss cores. Mater Des 55: 591–596.
    [20] Stocchi A, Colabella L, Cisilino A, et al. (2014) Manufacturing and testing of sandwich panel honeycomb core reinforced with natural-fibre fabrics. Mater Des 55: 394–403.
    [21] Bitzer TN (1998) Recent honeycomb core developments. Sandwich Constructions 4, Proceedings of 4th International Conference on Sandwich Constructions, K-A Olsson (ed.) 555–563.
    [22] Bitzer T (1997) Honeycomb technology: materials, design, manufacturing, applications and testing. New York: Chapman & Hall.
    [23] Lonno A, Hellbratt S (1996) Use of carbon fibre in a 63M high speed vessel, YS2000, for the Swedish Navy. Sandwich Constructions 3, Proceedings of 3rd International Conference on Sandwich Constructions, EMAS Publication, UK.
    [24] Gu S, Lu T, Evans A (2001) On the design of two-dimensional cellular metals for combined heat dissipation and structural load capacity. Int J Heat Mass Transfer 44: 2163–2175.
    [25] Joshi S, Xu K (2010) Fabrication and thermal performance of aerogel-filled carbon composite sandwich structures. Innovative Materials for Processes in Energy Systems – For Fuel Cells, Heat Pumps and Sorption System, 301–305.
    [26] HTM®556 High Temperature BMI Matrix System, Adv Compos Group, umeco composites.
    [27] Nanogel™ Translucent Aerogel (Datasheet), CABOT.
    [28] Material Safety Data Sheet (2013) R J London Chemical (S) PTE. LTD.
    [29] Wang M (2011) Micromechanical analysis of thermally-induced deformations and stresses in unidirectional continuous carbon fibre reinforced composites. Master of Science dissertation, Faculty of Engineering and Physical Science, University of Manchester.
  • Reader Comments
  • © 2016 the Author(s), licensee AIMS Press. This is an open access article distributed under the terms of the Creative Commons Attribution License (http://creativecommons.org/licenses/by/4.0)
通讯作者: 陈斌, bchen63@163.com
  • 1. 

    沈阳化工大学材料科学与工程学院 沈阳 110142

  1. 本站搜索
  2. 百度学术搜索
  3. 万方数据库搜索
  4. CNKI搜索

Metrics

Article views(8287) PDF downloads(1783) Cited by(3)

Article outline

Figures and Tables

Figures(13)  /  Tables(7)

/

DownLoad:  Full-Size Img  PowerPoint
Return
Return

Catalog