Active and passive integrated star vibration isolation device

[0046] Specific implementation mode one: as Figure 1 to Figure 5 , Figure 7 ~ Figure 11 , Figure 17 ~ Figure 19 , Figure 25 ~ Figure 29 As shown, the active and passive integrated star vibration isolation device of this embodiment includes a plurality of actuator support spring pieces 1, a plurality of actuators 2 and a plurality of actuator support brackets 3;

[0047] The upper end surfaces of the plurality of actuator support spring pieces 1 are all detachably connected to the lower end surface of the satellite 6, and the lower end surfaces of the plurality of actuator support spring pieces 1 are all detachably connected to the upper end surface of the adapter 4, so The plurality of actuators 2 described above are all arranged inside the adapter 4 perpendicular to the bottom surface of the adapter 4, and the upper end of each actuator 2 is detachably connected with the protruding end of a corresponding actuator supporting spring piece 1, each The lower end of the act...

[0049] Specific implementation mode two: as Figure 16 As shown, the active and passive integrated satellite vibration isolation device described in the first embodiment, the number of actuators 2 is eight, and the eight actuators 2 are located on the same circumference and are evenly distributed. In this way, different installation methods are obtained.

[0050] Specific implementation mode three: as Figure 23As shown, in the active and passive integrated star vibration isolation device described in Embodiment 1, the number of actuators 2 is six, and the six actuators 2 are located on the same circumference and are evenly distributed. In this way, different installation methods are obtained.