| 摘要 |
A damping device (10) and aircraft (100) using the damping device (10); the damping device (10) comprises a base (1) and a mounting base (2) being spaced a certain distance from the base (1). The damping device (10) also comprises at least one damper (3) sandwiched between the base (1) and the mounting base (2), and a securing piece (4) connecting the base (1) and the mounting base (2); one end of the damper (3) is connected to the base (1), the other end of the damper (3) is connected to the mounting base (2), and the securing piece (4) at least in part runs through the damper (3). The damper (3) is added between the base (1) and the mounting base (2) of the damping device (10), providing damping function. |
