In the current trend toward thicker aluminium plates, a major concern is the generation of high internal stresses during quenching, which can cause distortions during machining and pose serious safety concerns. Although the material is stretched after quench, substantially reducing residual stresses, they are not fully suppressed. In addition, the cooling rate is not large enough at the core of such thick plates to prevent any precipitation. This has a great impact on the efficiency of ageing. In this work, residual stress distributions in a heat-treatable aluminium alloy AA7449 thick plate in the as-quenched state measured by neutron diffraction are presented. A comparison between single (311) diffraction peak and multiple peaks analysis using Pawley algorithm is shown. The variation of the stress free reference value through the plate thickness is discussed and measured stresses are compared with residual stresses predicted by a thermomechanical finite element model of quenching.
IntroductionIn the processing route of heat-treatable aluminium alloys (AA), a critical step is quenching from the solutionising temperature. High cooling rates are desired to avoid the formation of coarse precipitates that would reduce mechanical properties. Fast quenching, however, cannot be achieved in the center of thick components, where the quenching rate can be more than one order of magnitude lower than that at the surface. The existence of a thermal gradient between core and surface leads to differential thermal deformation which is accommodated by elastic and plastic deformation to satisfy the compatibility of deformation. Whenever the material yields, residual stress (RS) remains after quenching due to the irreversibility of plastic deformation. The final stress pattern of biaxial compression at the skin balanced by triaxial tension at the core is referred to as the "skin-core" effect [1]. After quenching, the RS state may cause both unacceptable distortions during machining and a dramatically reduced service life time. Since RS relaxation is low during ageing treatments, thick components are usually stress relieved prior to ageing. This is achieved by applying plastic deformation: stretching from 1.5 to 3 % in the rolling direction (L) can reduce RS by a factor of approximately 10 [2]. However, complex geometries or thicker components like thick sheets require other approaches. Reducing the quenching rate by using boiling water for instance leads to lower RS [3]. For high quench