СЕНСОР УСТАЛОСТИ АВИАЦИОННЫХ КОНСТРУКЦИЙ
Keywords:The application of finite element analysis to the optimization of sensor’s sensitivity has been shown
AbstractThe possibility of the application of the aircraft fatigue sensor is discussed. The parameters of the surface deformation relief are considered as diagnostic parameters of the sensor It has been substantiated the usage of the aluminum alloy D16AT as a material for sensor manufacturing. The application of finite element analysis to the optimization of sensor’s sensitivity has been shown. The results of the sensor state monitoring under cyclic loading are presented.