Skip to main content
Log in

Experimental Investigation on Performance Evaluation of Composite T-Stiffened Skins Fabricated by Integral Molding Technologies Under Tensile Loading

  • Published:
Applied Composite Materials Aims and scope Submit manuscript

Abstract

Composite T-stiffened skins widely used in aircraft industry nowadays were fabricated by using the co-curing, co-bonding and secondary bonding processes. The stiffener thickness and the tensile property of T-stiffened skins under tensile loading were performed as evaluation indexes to evaluate the manufacturing quality and mechanical property of T-stiffened skins, respectively. The results show that the better manufacturing quality and higher tensile property of T-stiffened skins are found in the co-bonding process, and the tensile property increases with the increase of the adhesive film thickness in the co-bonding process. The co-curing process provides a similar tensile property of the co-bonding process with 0.15 mm thickness adhesive film, but different failure modes in the stiffener/skin interface are found in co-curing and co-bonding processes. Moreover, the filler content and the filler type in the triangle filling area of T-stiffened skins also have significant influence on the tensile property of T-stiffened skins, and rolling adhesive films as fillers into the triangle filling area exhibits the highest tensile property in five kinds of fillers during the co-bonding process.

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.

Fig.1
Fig.2
Fig.3
Fig.4
Fig.5
Fig.6
Fig.7
Fig.8
Fig.9
Fig.10
Fig.11
Fig.12
Fig.13
Fig.14
Fig.15
Fig.16
Fig.17
Fig.18

Similar content being viewed by others

References

  1. Stickler, P.B., Ramulu, M., Johnson, P.S.: Experimental and numerical analysis of transverse stitched T-joints in bending. Compos. Struct. 50(1), 17–27 (2000)

    Article  Google Scholar 

  2. Stickler, P.B., Ramulu, M.: Investigation of mechanical behavior of transverse stitched T-joints with PR520 resin in flexure and tension. Compos. Struct. 52(3–4), 307–314 (2001)

    Article  Google Scholar 

  3. Ayensa, A., Oller, E., Beltarn, B., et al.: Influence of the flanges width and thickness on the shear strength of reinforced concrete beams with T-shaped cross section. Eng. Struct. 188, 506–518 (2019)

    Article  Google Scholar 

  4. Tan, R.M., Guan, Z.D., Sun, W., et al.: Experiment investigation on impact damage and influences on compression behaviors of single T-stiffened composite panels. Compos. Struct. 203, 486–497 (2018)

    Article  Google Scholar 

  5. Justo, J., Reinoso, J., Blazquez, A.: Experimental failure investigation of pull-off tests of single T-stiffened composite specimens. Compos. Struct. 177, 13–27 (2017)

    Article  Google Scholar 

  6. Denis, D.R., Cartie, G.A., Emilie, P., et al.: 3D reinforcement of stiffener-to-skin T-joints by Z-pinning and tufting. Eng. Fract. Mech. 73(16), 2532–2540 (2006)

    Article  Google Scholar 

  7. Vijayaraju, K., Mangalgiri, P.D., Dattaguru, B.: Experimental study of failure and failure progression in T-stiffened skins. Compos. Struct. 64(2), 227–234 (2004)

    Article  Google Scholar 

  8. Huang C. K.: Study on co-cured composite panels with blade-shaped stiffeners. Composites, Part A Appl. Sci. Manuf. 34 (5), 403–410(2003).

  9. Soden J. A., Weissenbach G., Hill B. J.: The desing and fabrication of 3D multi-layer woven T-section reinforcements. Composites, Part A Appl. Sci. Manuf. 30, 213–220(1999).

  10. Li J, Sen J.: Analysis of frame to skin joint pull-off test and prediction of the delamination failure. In: 42nd AIAA/ASME/ASCE/AHS/ASC structures, structural dynamics and materials conference, Seattle, Washington, April 16–19, AIAA-2001–1484(2001).

  11. Wang, X.M., Xie, F.Y., Lin, M., Zhang, Z.G.: Influence of tool assembly schemes and integral molding technologies on compaction of T-stiffened skins in autoclave process. J. Reinf. Plast. Compos. 29(9), 1311–1322 (2010a)

    Article  CAS  Google Scholar 

  12. Lin, M., Wang, X.M., Xie, F.Y., Zhang, Z.G.: Influence of fillers in stiffener core and structural parameters on compaction of T-stiffened skins in autoclave process. Polym. Polym. Compos. 17(5), 273–280 (2009)

    Google Scholar 

  13. Wang, X.M., Xie, F.Y., Lin, M., Zhang, Z.G.: Influence of core fillers on resin flow and fiber compaction of cocured skin-to-stiffener structures. Polym. Compos. 31(8), 1360–1368 (2010b)

    Article  CAS  Google Scholar 

  14. Wang, X.M., Xie, F.Y., Lin, M., Zhang, Z.G.: Correlated rules between complex structure of composite components and manufacturing defects in autoclave molding technology. J. Reinf. Plast. Compos. 28(22), 2791–2803 (2009)

    Article  CAS  Google Scholar 

  15. Shi Q. H., Dai D., Cao Z. H.: Effect of adhesive on interlaminar stress of composite stiffened structure. Aernaut. Manuf. Technol. 52(6), 80–84(2009) (in Chinese).

  16. Jiao G. Q., Yang B. N., Xu J. Y.: On better understanding of interlaminer toughness of interleaved CFRP composites. J. Nothwest Polytechnical Univ. 20(1), 6–9(2002) (in Chinese).

  17. Sela, N., Ishai, O., Banks-Sills, L.: The effect of adhesive thickness interlaminar toughness of interleaved CFRP specimens. Compos. 20(3), 257–263 (1989)

    Article  CAS  Google Scholar 

  18. Wang, X.M., Xie, F.Y., Lin, M., Zhang, Z.G.: Experimental investigation of the compaction and tensile strength of co-cured skin-to-stiffener structures. Appl. Compos. Mater. 18(5), 371–383 (2011)

    Article  Google Scholar 

Download references

Acknowledgments

The authors acknowledge the support of the funding from AVIC Composite Corporation LTD (Grant No. GC731920301).

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to Xueming Wang.

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

Wang, X., Xie, F., Li, M. et al. Experimental Investigation on Performance Evaluation of Composite T-Stiffened Skins Fabricated by Integral Molding Technologies Under Tensile Loading. Appl Compos Mater 27, 795–809 (2020). https://doi.org/10.1007/s10443-020-09843-1

Download citation

  • Received:

  • Accepted:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1007/s10443-020-09843-1

Keywords

Navigation