Abstract

In this paper, we present an original experimental investigation on a pull-out test of a blind rivet from the external facing of sandwich panels with various core layer materials (polyisocyanurate foam, mineral wool, and expanded polystyrene). The blind rivets were subjected to an axial and eccentric tensile force introduced as static and quasi-cyclic loading. The statistical sample size was 5. The laboratory results depicted that the core layer of a sandwich panel influenced the load-displacement path of the investigated blind rivet connections, regardless of the nature of the load (static, quasi-cyclic) and the point of the load application (axial, eccentric). It was observed that the blind connection with the polyisocyanurate foam core sandwich panel was characterized by a reduction of both the capacity and the secant stiffness when compared with the blind connection with the mineral wool or the expanded polystyrene core sandwich panels. Moreover, the tested connections demonstrated that the eccentric load gave a higher flexural stiffness than the axial load and that the quasi-cyclic load did not reduce their stiffness and capacity.

Highlights

  • The research refers to the use of blind rivets with sandwich panels

  • The sandwich panels considered in this paper consist of two thin and stiff external facings and a thick and soft core

  • We present an experimental investigation on a pull-out test of blind rivets subjected to an axial and an eccentric tensile force introduced as a static and a quasi-cyclic loading

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Summary

Introduction

The sandwich panels considered in this paper consist of two thin and stiff external facings and a thick and soft core. The facings are made of high strength material such as steel, aluminum, or laminate. The core is made of thermal insulation materials, namely polyisocyanurate foam ( referred to as PIR foam), mineral wool, or expanded polystyrene. These types of composite structures are used in structural engineering applications, such as roofs and wall cladding elements. When using the typical materials for sandwich panel layers, the core/facing thickness ratios vary from 60 to 500, the facing/core density ratios vary from 10 to 600, while the facing/core Young modulus ratios vary from 600 to 95,000 (see Tables 1 and 2)

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