## 1 Introduction  
As the aerospace field develops towards large-scale, intelligent, and high-performance aspects, various types of equipment are faced with increasingly severe vibration damping and buffering problems in special environments [1]. In engineering reality, plate structures have the characteristics of a simple structure, high space utilization, and strong adaptability, so they are widely used in aerospace structures and weapon equipment. Many scholars have performed considerable research to suppress the vibration and noise levels of plate structures, including composite structure design [2], application of damping materials [3], damping mass [4], boundary constraints [5], and active vibration control [6]. An effective method of improving the damping performance of the overall structure in a wide frequency range is to incorporate damping materials into the plate structure [7; 8; 9]. By attaching damping materials to the plate structure, the vibration energy dissipation is increased, the vibration frequency response is improved, the durability and stability of the structure are enhanced, and the structural design space is expanded so as to compensate for the shortcomings of simplification of the plate structure. Therefore, a great deal of research has been invested in plate structures. [PERSON] et al. [10] studied the high-temperature performance of high-temperature epoxy resin material and found that the tensile strength was improved by adding 5% organic nano montmorillonite to ensure the damping performance, but the damping temperature range of this material was not higher than 256 \({}^{\circ}\)C. [PERSON] et al. [11] tested the free vibration behavior of embedded co-cured porous damped sandwich composites filled with resin, and the results indicated that the loss factor modal frequency showed a more obvious upward trend as the damping area ratio became larger. However, the modal frequency showed the opposite trend. [PERSON] et al. (2018) revealed that reducing the deformation produced by forced vibration of the blade--increasing the damping performance of the blade and extending its service life--can be achieved by the technique of rotating the blade and coating it with an aluminum oxide coating. [PERSON] et al. (2018) used a combination of linear and nonlinear elastic metamaterials based on the collision enhancement energy dissipation mechanism. By embedding the damping layer into the collision unit, it can be made to play the role of absorbing and dispersing energy in the vibration process. [PERSON] et al. (2018) conducted structural vibration damping tests on a cantilever beam structure in the form of additional particles and showed that by varying the fill rate and particle diameter, the vibration amplitude was attenuated by up to about 40%. [PERSON] et al. (2018) investigated the behavior of corrugated core composite sandwich panels (CCCS) consisting of composite panels reinforced with elastic NiTi shape memory alloy (SMA) wires and aluminum patterned cores under high-velocity impacts. Increasing the number of SMAs and applying a pre-strain to the SMAs were effective in increasing the amount of energy dissipated by the sandwich panels. [PERSON] et al. (2018) prepared a bilayer polyurethane composite material by forming or bonding individual films layer by layer. This preparation method resulted in the formation of good connection between the materials, and the mechanical properties of this composite material were easily controllable in the region of effective damping temperature. [PERSON] et al. (2018) investigated the mechanical properties composite foams filled with hollow glass spheres with epoxy resin as the core material and composite sandwich materials of kenaf/glass fiber hybrid sheets. Through various tests, the mechanical properties of tensile, compressive, and flexural strength under different interlayers were shown. [PERSON] et al. (2018) focused on the impact resistance of sandwich structures and prepared different combinations of woven carbon/Kevlar integral panels and sandwich panels.