A novel In-situ repair method of 7075 Al laminated interference-fit bolted joints under stress wave impact driven bushing cold expansion: numerical simulation and experimental validation
Mengyang Cui , Duquan Zuo , Haolin Ding , Rongmin Tu , Yuqin Chen , Zhongbo Zhang , Chong Gao
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引用次数: 0
Abstract
Interference-fit bolted joints are easily damaged due to alternating load and overload impact, and their repair quality is directly related to the re-service safety of aircraft thin-walled structures. Aiming at the actual repair requirements of the shaking head part of the thin-walled connection area between the wing and the fuselage, this paper innovatively proposes a bushing cold expansion interference composite strengthening repair method based on stress wave impact loading. It establishes a finite element simulation model of the whole process of repairing the damaged joint of an Al single-lap thin-walled laminated structure. The accuracy and reliability of the model are verified by comparative tests and simulations. Furthermore, the evolution rules of indentation load, plastic deformation around the hole, strengthening area and microstructure characteristics under different expansion amounts were analyzed, and the unique advantages of the composite strengthening method in improving the repair quality of thin-walled joints were proved from multiple perspectives. The results indicate that a friction retardation effect occurs at the interface of the bushing hole wall during the composite strengthening process. Under the appropriate expansion amount, this effect helps to increase the residual compressive stress amplitude and its radial action depth. Under the optimal expansion amount of 2.0% (E3), the distribution uniformity of residual compressive stress on the hole wall of the repaired part is the best, and the proportion of stress units is as high as 72.17%. The arc shape of the micro-grain boundary around the hole is moderate, the assembly gap is significantly reduced, and the exit tumor damage is slight. This fully confirms that the repair process of damaged joints can balance the strengthening effect and structural integrity by optimizing the expansion amount, to promote the transformation of residual tensile stress or zero stress unit on the hole wall to residual compressive stress, effectively inhibit the initiation and propagation of fatigue cracks, and realize the leap from geometric recovery to the structural integrity improvement of the repaired part.
期刊介绍:
Thin-walled structures comprises an important and growing proportion of engineering construction with areas of application becoming increasingly diverse, ranging from aircraft, bridges, ships and oil rigs to storage vessels, industrial buildings and warehouses.
Many factors, including cost and weight economy, new materials and processes and the growth of powerful methods of analysis have contributed to this growth, and led to the need for a journal which concentrates specifically on structures in which problems arise due to the thinness of the walls. This field includes cold– formed sections, plate and shell structures, reinforced plastics structures and aluminium structures, and is of importance in many branches of engineering.
The primary criterion for consideration of papers in Thin–Walled Structures is that they must be concerned with thin–walled structures or the basic problems inherent in thin–walled structures. Provided this criterion is satisfied no restriction is placed on the type of construction, material or field of application. Papers on theory, experiment, design, etc., are published and it is expected that many papers will contain aspects of all three.