Research on Common Market Competitiveness of Civil Aircraft

Ai-ping, Yin; Zhuang, Duoduo

doi:10.1088/1755-1315/242/5/052034

Cited by 1 publication

(1 citation statement)

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“…[1][2][3][4][5] Nowadays, in order to meet the requirements of long life and high maneuverability of the new generation of aircraft, the aviation industry has more and more strict requirements on the perpendicularity of holes. [6][7][8] However, the formulation of the current hole quality evaluation standards often relies on experience and lacks theoretical and experimental basis. Whether the standard is reasonable will directly affect the cost of aircraft manufacturing and its safety in service.…”

Section: Introductionmentioning

confidence: 99%

Effects of hole perpendicularity error on fatigue behaviors of CFRP single-lap single-bolt joints

Sun

Qiu

et al. 2022

Proceedings of the Institution of Mechanical Engineers, Part L:

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The perpendicularity error of the holes is prone to occur in the process of manual hole making or robot hole making, which leaves a safety hazard for the composite structure. In this study, the fatigue tests are carried out on the Carbon Fibre-reinforced Polymer (CFRP) single-lap single-bolt joints and effects of the perpendicularity error on the fatigue behaviors are studied. By combining the permanent displacement and stiffness of the joints, the evolution of fatigue damage is analyzed. The results show that the perpendicularity error causes stress concentration and hole fastener clearance near the hole entrance under the preload. The perpendicularity error in the 0° direction will greatly reduce the high-cycle fatigue and the impact on the low-cycle fatigue is relatively small, while the error in the 180° direction is just the opposite. The fatigue life is negatively correlated with the angle of the perpendicularity error. The effect of perpendicularity error in 0° direction on the fatigue damage evolution is to speed up the accumulation of damage, while the effect of error in 180° direction is mainly to cause more damage in the early stage of cyclic loading. The effect of perpendicularity error on the stiffness during fatigue loading is relatively insignificant.

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