Skip to main content
Log in

Study on Thermal Response of Adhesively Bonded Honeycomb Sandwich Structure in High Temperature

  • Published:
Fire Technology Aims and scope Submit manuscript

A Correction to this article was published on 31 May 2021

This article has been updated

Abstract

Thermal response of the honeycomb sandwich structure was evaluated using the steady-state method at different temperatures ranging from 100°C to 400°C. The results showed that effective thermal conductivity decreases when the temperature set is over 300°C, and the critical temperature is about 310°C. As a result, a set of experiments was conducted to observe the inner structure of the sandwich in a quest to understand why the thermal conductivity decreases. A black substance was found, and it adhered to the interfaces between the faces and the core where the adhesive is located. A series of experiments were carried out to study the thermal response of the adhesive. The TG curves showed that the total mass loss of adhesive can reach 90% due to the thermal decomposition, which can absorb a portion of energy. Meanwhile, the black substance was also produced during the TG measurements and its carbon content reached 64.38%.

This is a preview of subscription content, log in via an institution to check access.

Access this article

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

Figure 1
Figure 2
Figure 3
Figure 4
Figure 5
Figure 6
Figure 7
Figure 8
Figure 9

Similar content being viewed by others

Change history

References

  1. Blosser ML et al (1998) Reusable metallic thermal protection systems development. https://ntrs.nasa.gov/citations/20040095922

  2. Amraei M et al (2014) Application of aluminium honeycomb sandwich panel as an energy absorber of high-speed train nose. J Compos Mater 48(9):1027–1037

    Article  Google Scholar 

  3. Pan B et al (2015) Thermo-mechanical response of superalloy honeycomb sandwich panels subjected to non-steady thermal loading. Mater Des 88:528–536

    Article  Google Scholar 

  4. Zheng L et al (2013) Experimental investigation and numerical simulation of heat-transfer properties of metallic honeycomb core structure up to 900°C. Appl Therm Eng 60(1–2):379–386

    Article  Google Scholar 

  5. Li DH, Xia XL (2009) A study on numerical simulation method for transient heat transfer in metallic thermal protection systems. Yuhang Xuebao/J Astronaut 30(3):1195–1200. https://doi.org/10.1109/MILCOM.2009.5379889

    Article  Google Scholar 

  6. Dharmasena KP et al (2008) Mechanical response of metallic honeycomb sandwich panel structures to high-intensity dynamic loading. Int J Impact Eng 35(9):1063–1074

    Article  Google Scholar 

  7. Foo CC et al (2007) Mechanical properties of Nomex material and Nomex honeycomb structure. Compos Struct 80(4):588–594

    Article  Google Scholar 

  8. Tan C, Akil HM (2012) Impact response of fiber metal laminate sandwich composite structure with polypropylene honeycomb core. Compos Part B Eng 43(3):1433–1438

    Article  Google Scholar 

  9. Keerthan P, Mahendran M (2012) Thermal performance of composite panels under fire conditions using numerical studies: plasterboards, rockwool, glass fibre and cellulose insulations. Fire Technol 49(2):329–356

    Article  Google Scholar 

  10. Lattimer BY et al (2009) Thermal response of composite materials to elevated temperatures. Fire Technol 47(4):823–850

    Article  Google Scholar 

  11. Anjang A et al (2014) Tension modelling and testing of sandwich composites in fire. Compos Struct 113:437–445

    Article  Google Scholar 

  12. Hörold A et al (2013) Structural integrity of sandwich structures in fire: an intermediate-scale approach. Compos Interfaces 20(9):741–759

    Article  Google Scholar 

  13. Goodrich TW, Lattimer BY (2012) Fire decomposition effects on sandwich composite materials. Compos Part A Appl Sci Manuf 43(5):803–813

    Article  Google Scholar 

  14. Swann RT, Pittman CM (1961) Analysis of effective thermal conductivities of honeycomb-core and corrugated-core sandwich panels. National Aeronautics and Space Administration, Washington

    Google Scholar 

  15. Caogen Y et al (2008) A study on metallic thermal protection system panel for Reusable Launch Vehicle. Acta Astronaut 63(1–4):280–284

    Article  Google Scholar 

  16. Fatemi J, Lemmen M (2009) Effective thermal/mechanical properties of honeycomb core panels for hot structure applications. J Spacecr Rockets 46(3):514–525

    Article  Google Scholar 

  17. Daryabeigi K (2002) Heat transfer in adhesively bonded honeycomb core panels. J Thermophys Heat Transf 16(2):217–221

    Article  Google Scholar 

  18. Sánchez-Carballido S et al (2016) A quantitative infrared imaging system for in situ characterization of composite materials in fire tests. Fire Technol 53(3):1309–1331

    Article  Google Scholar 

  19. Garrido M et al (2015) Adhesively bonded connections between composite sandwich floor panels for building rehabilitation. Compos Struct 134:255–268

    Article  Google Scholar 

  20. Adams R, Drinkwater B (1997) Nondestructive testing of adhesively-bonded joints. NDT E Int 30(2):93–98

    Article  Google Scholar 

  21. Pascual C et al (2017) Adhesively-bonded GFRP-glass sandwich components for structurally efficient glazing applications. Compos Struct 160:560–573

    Article  Google Scholar 

  22. Henderson JB et al (1985) A model for the thermal response of polymer composite materials with experimental verification. J Compos Mater 19(6):579–595

    Article  Google Scholar 

  23. Bhat T et al (2015) Fire structural resistance of basalt fibre composite. Compos Part A Appl Sci Manuf 71:107–115

    Article  Google Scholar 

  24. Looyeh M et al (2001) Thermochemical responses of sandwich panels to fire. Finite Elem Anal Des 37(11):913–927

    Article  Google Scholar 

Download references

Acknowledgements

This work was supported by the National Key Research and Development Program of China (2016YFB1200505 and 2016YFB1200403).

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to Shouxiang Lu.

Ethics declarations

Conflict of interest

The authors declare that there are no conflicts of interest.

Additional information

Publisher's Note

Springer Nature remains neutral with regard to jurisdictional claims in published maps and institutional affiliations.

Rights and permissions

Reprints and permissions

About this article

Check for updates. Verify currency and authenticity via CrossMark

Cite this article

Yuan, R., Zhang, Y., Qin, Y. et al. Study on Thermal Response of Adhesively Bonded Honeycomb Sandwich Structure in High Temperature. Fire Technol 57, 1135–1147 (2021). https://doi.org/10.1007/s10694-020-01033-6

Download citation

  • Received:

  • Accepted:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1007/s10694-020-01033-6

Keywords

Navigation