Single-rod double-end locking locking device and locking method for swing mirror satellite laser communication terminal
A technology of laser communication and locking device, applied in supporting machines, mechanical equipment, pivot connections, etc., can solve the problems of large volume and mass, complex locking device structure, etc., and meet the requirements of small volume and mass, installation and operation Not high, the effect of mass production
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specific Embodiment approach 1
[0028] Specific implementation mode one: refer to Figure 1 to Figure 3 Describe this embodiment in detail, the single-rod double-end locking locking device for the swing mirror satellite laser communication terminal described in this embodiment, the swing mirror satellite laser communication terminal includes a swing mirror mounting base 1, a swing mirror 2, The pitch shaft 3, the U-shaped frame 4, the azimuth shaft 5 and the optical body, the azimuth shaft 5 and the optical body are cylindrical structures, one end of the azimuth shaft 5 is fixedly connected to one end of the optical body, and the two ends of the U-shaped frame 4 It is a U-shaped structure, and two U-shaped structures are arranged opposite to each other. A circular through hole is respectively arranged on the side wall of the top of the two U-shaped structures, and the pitch rotating shaft 3 is connected with the swing mirror mounting base 1 through the circular through hole. One side of the swing mirror moun...
specific Embodiment approach 2
[0034] Specific embodiment 2: This embodiment is to further explain the single-rod double-end locking locking device for the pendulum-mirror satellite laser communication terminal described in the specific embodiment 1. In this embodiment, the model of the cancellation device 8 For 6TL01-9C, there are four screw holes on the horizontal plate of the swing mirror single-rod pressing plate 6 .
specific Embodiment approach 3
[0035] Specific embodiment 3: This embodiment is a further description of the single-rod double-end locking locking device for the pendulum-mirror satellite laser communication terminal described in the specific embodiment 1. In this embodiment, the lock of the cancellation device 8 Tight pin 8-1 is coated with 5 μm molybdenum dichloride lubricant.
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