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This paper presents methods of cushioning package design. The analysis of existing shortcoming is made when the maximum accelerationstatic stress curve (what is called curve) is applied to the cushion package design, at the same time ,the principle and method steps to get curve are briefly introduced when the stressenergy method is used .the function between the key parameters of cushioning package design is acquired by the stressenergy method .By comparing the data produced with matlab software with the real experimental ones in some paper, the possibilities to get curve of casual drop height and cushion thickness by one-time experiment to get curve with stress-energy method is demonstrated. Based on the function of key parameters of cushioning package acquired, the reversed cushioning package design method is carried out.

Based on the analysis of the loads, constraints and its mechanisms applying to the duct system, a finite element model of the anti-ice system is developed and the Lanczos algorithm is used for modal analysis. Then, the first eight natural frequencies and vibration modes are obtained. The thermodynamic parameters of the gas and the kinetic parameters of the ball joint which have influence on the modal analysis are considered. The results show that the first eight order natural frequencies of the anti-ice Part1 are low and concentrated, and decrease with temperature of the gas while increase with pressure of the gas. Meanwhile, the natural frequencies increase with the stiffness and starting torque of the ball joint. This work could be helpful for reliability design of civil-aircraft ducting system.