Satellite corner reflector protection device

Abstract

The utility model discloses a protection device for a satellite corner reflector, which belongs to the technical field of satellite corner reflectors and is characterized in that a stabilizing part is mounted on an adjusting disc, four corners of a satellite corner reflector main body are wrapped with corner protectors, revolute pairs are symmetrically mounted on one side of the adjusting disc, and driving parts are mounted on the outer sides of the revolute pairs; the stabilizing piece and the satellite corner reflector main body are of a cross structure, the inner side of the stabilizing piece is of an elastic structure, the corner protector is of an inward-sunken structure, and the stabilizing piece and the satellite corner reflector main body are of a four-side cross structure, so that the use range is widened, and the stability of the satellite corner reflector main body is improved by placing the satellite corner reflector main body into the stabilizing piece for synchronous fixing; the four corners outside the satellite corner reflector main body are provided with the corner protectors which can wrap and connect the four corners of the satellite corner reflector main body so that disassembly and protection can be facilitated, and the front-back angle or the left-right angle of the adjusting disc, the satellite corner reflector main body and the corner protectors can be adjusted through the driving pieces on the chassis. And the swinging direction and angle are solved by adjusting the placement position of the revolute pair.

Description

Technical Field

[0001] This utility model relates to a satellite corner reflector protection device, belonging to the field of satellite corner reflector technology. Background Technology

[0002] After searching, the closest prior art is the prior art with application number 201821345579.5. The prior art disclosed in the prior art document is a support column with a circular panel at the top. The upper surface of the circular panel is provided with a first panel, a second panel, a third panel and a fourth panel respectively. The first panel, the second panel, the third panel and the fourth panel are all perpendicular to the circular panel. The first panel and the second panel are perpendicular to each other, and the third panel and the fourth panel are perpendicular to each other. A base is provided at the bottom of the support column.

[0003] Existing satellite corner reflector protection devices suffer from instability during installation and lack of protective structures at the four corners. Therefore, a satellite corner reflector protection device is needed to optimize the aforementioned existing technology. Utility Model Content

[0004] The main purpose of this invention is to provide a satellite corner reflector protection device.

[0005] The objective of this utility model can be achieved by adopting the following technical solution:

[0006] A satellite corner reflector protection device includes an adjustment disc for limiting position, a base plate installed at the bottom of the adjustment disc, and a satellite corner reflector body installed on the corner guard.

[0007] A stabilizing component is installed on the adjustment plate. The stabilizing component has positioning holes. The main body of the satellite corner reflector is placed inside the stabilizing component. The four corners of the main body of the satellite corner reflector are covered with corner protectors.

[0008] An angle adjustment assembly is installed between the adjustment plate and the chassis.

[0009] Preferably, the angle adjustment assembly includes a rotary joint and a driving component. The rotary joint is symmetrically installed on one side of the adjustment disk, and the driving component is installed on the outer side of the rotary joint. The output end of the driving component is oscillatingly connected to the adjustment disk.

[0010] Preferably, the stabilizing element and the main body of the satellite corner reflector have a cross-shaped structure.

[0011] Preferably, the inner side of the stabilizing member has an elastic structure, and the corner guards have an indented structure.

[0012] Preferably, the main body of the satellite corner reflector is fixedly connected inside the stabilizing component.

[0013] Preferably, the adjusting plate is connected to the chassis by swinging motion, and the chassis is equipped with fixing holes.

[0014] The beneficial technical effects of this utility model are as follows:

[0015] This utility model provides a satellite corner reflector protection device.

[0016] 1. Connect the adjustment plate to the chassis in a swinging manner. After the adjustment plate is installed, place the main body of the satellite corner reflector into the stabilizing component and fix it to the main body of the satellite corner reflector by screws through the stabilizing component. The four corners of the main body of the satellite corner reflector are covered with corner protectors.

[0017] The stabilizer and the main body of the satellite corner reflector have a four-sided cross structure, which increases the range of use. The stability of the satellite corner reflector is improved by inserting it into the stabilizer for synchronous fixation. The four outer corners of the satellite corner reflector are equipped with corner protectors, which can wrap around the four corners of the satellite corner reflector for easy disassembly and protection.

[0018] 2. A rotating pair is symmetrically installed on the outer side of the adjusting plate, and a driving component is installed on the outer side of the rotating pair. The output end of the driving component is connected to the chassis for swinging.

[0019] The adjustment disc, satellite corner reflector body, and corner protectors on this device are adjusted by the drive components on the chassis to change their front-to-back or left-to-right angles. The direction and angle of the swing are determined by adjusting the placement of the rotating joints. Attached Figure Description

[0020] Figure 1 This is an exploded three-dimensional structural diagram of a preferred embodiment of a satellite corner reflector protection device according to the present invention;

[0021] Figure 2 This is a schematic diagram of the adjusting disc structure according to a preferred embodiment of a satellite corner reflector protection device of the present invention;

[0022] Figure 3 This is a schematic diagram of the adjusting base structure according to a preferred embodiment of a satellite corner reflector protection device of the present invention.

[0023] In the diagram: 1. Adjustment disc; 101. Stabilizer; 102. Positioning hole; 103. Satellite corner reflector body;

[0024] Corner protectors;

[0025] Chassis; 301; mounting holes;

[0026] 4. Rotating joint; 401. Driving component. Detailed Implementation

[0027] To make the objectives, technical solutions, and advantages of the embodiments of this utility model clearer, the technical solutions of the embodiments of this utility model will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only some, not all, of the embodiments of this utility model.

[0028] Therefore, the following detailed description of the embodiments of this utility model is not intended to limit the scope of the claimed utility model, but merely to illustrate some embodiments of the utility model. All other embodiments obtained by those skilled in the art based on the embodiments of this utility model without inventive effort are within the scope of protection of this utility model.

[0029] It should be noted that, unless otherwise specified, the embodiments and features and technical solutions in the present invention can be combined with each other.

[0030] It should be noted that similar labels and letters in the following figures indicate similar items. Therefore, once an item is defined in one figure, it does not need to be further defined and explained in subsequent figures.

[0031] In the description of this utility model, it should be noted that the terms "upper" and "lower," etc., indicate the orientation or positional relationship based on the orientation or positional relationship shown in the accompanying drawings, or the orientation or positional relationship commonly used when the product is in use, or the orientation or positional relationship commonly understood by those skilled in the art. These terms are only for the convenience of describing this utility model and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, or be constructed and operated in a specific orientation, and therefore should not be construed as a limitation on this utility model. In addition, the terms "first" and "second," etc., are only used to distinguish descriptions and should not be construed as indicating or implying relative importance.

[0032] Example 1: As Figure 1 , Figure 2 and Figure 3 As shown, this embodiment proposes a satellite corner reflector protection device. The adjusting plate 1 is oscillatingly connected to the chassis 3. After the adjusting plate 1 is installed, the satellite corner reflector body 103 is placed into the stabilizing member 101 and fixedly connected to the satellite corner reflector body 103 by screws passing through the stabilizing member 101. The oscillating connection structure between the adjusting plate 1 and the chassis 3 realizes multi-angle protection and stable installation of the satellite corner reflector body 103. The four corners of the satellite corner reflector body 103 are wrapped with corner protectors 2. The corner protectors 2 wrapped at the four corners of the satellite corner reflector body 103 adopt a split structure. The inner side of the corner protectors 2 is pasted with an EVA buffer layer with a thickness of 3mm.

[0033] The stabilizer 101 and the satellite corner reflector body 103 have a four-sided cross structure, which improves the range of use. The satellite corner reflector body 103 is inserted into the stabilizer 101 for synchronous fixation, which improves the stability of the satellite corner reflector body 103. The positioning hole 102 is designed as a four-sided cross through structure, which is composed of an elongated hole (diameter 8mm × length 15mm) along the X-axis and a standard circular hole (diameter 6mm) along the Y-axis. It can be adapted to the bolt spacing adjustment in different installation scenarios. The positioning boss set on the back of the stabilizer 101 is interference-fitted with the positioning groove 105 of the adjustment plate 1 to achieve precise positioning of the satellite corner reflector body 103 and the adjustment plate 1. The four outer corners of the satellite corner reflector body 103 are equipped with corner protectors 2, which can wrap the four corners of the satellite corner reflector body 103 for easy disassembly and protection.

[0034] Example 2: As Figure 1 , Figure 2 and Figure 3 As shown, this embodiment proposes a satellite corner reflector protection device. A rotating pair 4 is symmetrically installed on the outer side of the adjustment disk 1. A driving component 401 is installed on the outer side of the rotating pair 4. The output end of the driving component 401 is oscillatingly connected to the chassis 3. The rotating pair 4 is symmetrically installed on the outer side of the adjustment disk 1. The rotating pair 4 adopts a double-pivot self-aligning bearing structure.

[0035] The adjustment disc 1, satellite corner reflector body 103, and corner protector 2 on this device are adjusted by the drive component 401 on the chassis 3 to change their front-to-back or left-to-right angles. The installation position of the rotating joint 4 has been mechanically optimized, with its axis distance from the geometric center of the adjustment disc 1 being L=80mm, ensuring that the driving torque does not exceed 80% of the motor's rated torque within a ±30° adjustment range. The bottom of the chassis 3 is provided with a triangular reinforcing rib 305, and its thickness in the area where it is installed with the drive component is increased to 10mm to improve the overall structural rigidity. The swing direction and angle are resolved by adjusting the placement of the rotating joint 4.

[0036] The above description is only a further embodiment of the present utility model, but the protection scope of the present utility model is not limited thereto. Any equivalent substitutions or changes made by those skilled in the art within the scope disclosed by the present utility model, based on the technical solution and concept of the present utility model, shall fall within the protection scope of the present utility model.

Claims

1. A satellite corner reflector protection device, comprising an adjustment disc (1) for limiting position, a base plate (3) mounted on the bottom of the adjustment disc (1), and a satellite corner reflector body (103) mounted on the corner guard (2). Its features are: A stabilizing component (101) is installed on the adjusting plate (1). A positioning hole (102) is provided on the stabilizing component (101). A satellite corner reflector body (103) is placed inside the stabilizing component (101). Corner guards (2) are wrapped around the four corners of the satellite corner reflector body (103). An angle adjustment assembly is installed between the adjustment plate (1) and the chassis (3).

2. The satellite corner reflector protection device according to claim 1, characterized in that: The angle adjustment assembly includes a rotating joint (4) and a drive member (401). The rotating joint (4) is symmetrically installed on one side of the adjustment disk (1), and the drive member (401) is installed on the outside of the rotating joint (4). The output end of the drive member (401) is oscillatingly connected to the adjustment disk (1).

3. The satellite corner reflector protection device according to claim 1, characterized in that: The stabilizing component (101) and the satellite corner reflector body (103) are cross-shaped.

4. A satellite corner reflector protection device according to claim 2, characterized in that: The inner side of the stabilizing member (101) is an elastic structure, and the corner guard (2) is an indented structure.

5. A satellite corner reflector protection device according to claim 2, characterized in that: The satellite corner reflector body (103) is fixedly connected inside the stabilizing member (101).

6. A satellite corner reflector protection device according to claim 4, characterized in that: The adjustment plate (1) is connected to the base (3) by swinging. The base (3) has a fixing hole (301).

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