Retrofitting scheme and experimental research of severally damaged carbon fiber reinforced lattice-core sandwich cylinder

Abstract To improve the reutilization of advanced carbon fiber reinforced composite (CFRC) lattice-core sandwich cylinder (LSC), a severely damaged LSC was retrofitted by CFRC laminate through wrapping and riveting schemes. Free vibration and uniaxial compression experiments were carried out to reveal its mechanical performances. Natural frequencies and vibration modes of the repaired cylinder are close to the intact cylinder. Compared with the stiffness of the intact cylinder, 98.7 kN/mm, stiffness of the repaired cylinder is 138.83 kN/mm, even a little stiffer. Failure of the repaired cylinder locates at the lower end. Initially, the inner skin delaminated from the core and finally fracture of the outer skin made the cylinder out of work. The repaired segment is not damaged. Ultimate load of the repaired cylinder is 377.38 kN, only a little smaller than of the intact cylinder. The retrofitting scheme is effective to re-utilize the severally damaged CFRC LSC.

[1]  Z. Gürdal,et al.  Optimal design of composite lattice shell structures for aerospace applications , 2009 .

[2]  Daining Fang,et al.  Improved manufacturing method and mechanical performances of carbon fiber reinforced lattice-core sandwich cylinder , 2013 .

[3]  Changliang Lai,et al.  Failure analysis of 1D lattice truss composite structure in uniaxial compression , 2015 .

[4]  O. Anwar Bég,et al.  Bending analysis of FGM plates under hygro-thermo-mechanical loading using a four variable refined plate theory , 2014 .

[5]  Chunfang Huang,et al.  Analysis of failure loads and optimal design of composite lattice cylinder under axial compression , 2015 .

[6]  S. Panda,et al.  Nonlinear finite element analysis of thermal post-buckling vibration of laminated composite shell panel embedded with SMA fibre , 2013 .

[7]  Daining Fang,et al.  Free vibration behaviors of carbon fiber reinforced lattice-core sandwich cylinder , 2014 .

[8]  D. Fang,et al.  Free vibration of CFRC lattice-core sandwich cylinder with attached mass , 2015 .

[9]  D. Fang,et al.  Characterization of edge effects of composite lattice structures , 2009 .

[10]  Daining Fang,et al.  Manufacturing and testing of a CFRC sandwich cylinder with Kagome cores , 2009 .

[11]  Chang Fo-van Analysis of adhesive lap joint , 1986 .

[12]  G. Totaro,et al.  Recent advance on design and manufacturing of composite anisogrid structures for space launchers , 2012 .

[13]  G. Rahimi,et al.  Analysis of the effect of stiffener profile on buckling strength in composite isogrid stiffened shell under axial loading , 2013 .

[14]  Changliang Lai,et al.  A flexible tooling and local consolidation process to manufacture 1D lattice truss composite structure , 2015 .

[15]  M. Uyaner,et al.  Repairing impact damaged fiber reinforced composite pipes by external wrapping with composite patches , 2015 .

[16]  Su-Seng Pang,et al.  Buckling load analysis of grid stiffened composite cylinders , 2003 .

[17]  Abdelouahed Tounsi,et al.  A refined trigonometric shear deformation theory for thermoelastic bending of functionally graded sandwich plates , 2013 .

[18]  V. V. Vasiliev,et al.  Anisogrid composite lattice structures – Development and aerospace applications ☆ , 2012 .

[19]  Daining Fang,et al.  Equivalent analysis and failure prediction of quasi-isotropic composite sandwich cylinder with lattice core under uniaxial compression , 2013 .