Satellite cabin plate horizontal moving clamp

Abstract

The utility model provides a satellite cabin board horizontal movement clamp relates to clamp technical field, including traction equipment and fixed plate, the fixed plate sets up at the bottom of traction equipment, the left and right sides of fixed plate all have the first clamping plate that moves and inserts, the front and back sides of fixed plate all have the second clamping plate that moves and inserts, and the stable mechanism is hinged between two second clamping plates, the utility model discloses through drive piece operation control two first clamping plate shrink, and through drive piece to the winding of steel cable, immediately through the steel cable traction second clamping plate shrink, and make the stable mechanism downshift and cabin board resist contact, thereby through first clamping plate, second clamping plate and stable mechanism cooperation increase the stability that cabin board clamped, when steel cable draws second clamping plate and inserts second slot inside drive piston plate synchronous movement, and push the airflow in second slot to the inside of nozzle, immediately through nozzle jet airflow, thereby to the surface of cabin board carries out the blowing.

Description

Technical Field

[0001] This utility model relates to the field of clamping technology, specifically to a horizontal moving clamp for a satellite cabin panel. Background Technology

[0002] In recent years, with the gradual improvement of the national satellite navigation system, my country's satellite application industry has experienced explosive growth. The constellation network with a weight of around 200kg is very large. The manufacturing capacity of traditional satellite module-level products can no longer meet the current equipment requirements. The current technical equipment involves multiple physical operations in the processes of lifting, transferring, transporting, hovering, grabbing, releasing and assembling, resulting in waste of facilities, environment and manpower.

[0003] In the prior art, clamps generally use clamping plates to hold and fix the cabin plate. However, the clamping plates can only reinforce the side walls of the cabin plate. The top and bottom of the cabin plate lack limiting mechanisms, resulting in poor stability when the clamps hold and fix the cabin plate.

[0004] This utility model proposes a horizontal moving fixture for satellite cabin panels to solve the problem that fixtures generally use clamping plates to hold and fix the cabin panels. However, the clamping plates can only reinforce the side walls of the cabin panels, and the top and bottom of the cabin panels lack limiting mechanisms. Therefore, the stability of the fixture is not good when it holds and fixes the cabin panels. Utility Model Content

[0005] The purpose of this invention is to overcome the problem that in the above-mentioned background technology, clamps generally use clamping plates to hold and fix the cabin plate. However, the clamping plates can only reinforce the side walls of the cabin plate, and the top and bottom of the cabin plate lack limiting mechanisms. Therefore, the clamps are not stable when holding and fixing the cabin plate.

[0006] Based on the above technical concept, the technical solution adopted by this utility model is as follows:

[0007] A horizontal moving clamp for a satellite module includes a traction device and a fixed plate. The fixed plate is disposed at the bottom of the traction device. First clamping plates are movably inserted into the left and right sides of the fixed plate, and second clamping plates are movably inserted into the front and rear sides of the fixed plate. A stabilizing mechanism is hinged between the two second clamping plates. A driving component is disposed inside the fixed plate. The two ends of the driving component are respectively threaded into the two first clamping plates. The second clamping plates are connected to the driving component by steel cables.

[0008] The driving component is used to control the movement of the first clamping plate and the second clamping plate, and the stabilizing mechanism is used to assist the first clamping plate and the second clamping plate in fixing the cabin plate.

[0009] Further defining the above technical solution, the traction device includes a horizontal adjusting guide rail and a traction machine, the traction machine being movably disposed inside the horizontal adjusting guide rail, and a sling being provided at the bottom of the traction machine, the lower end of which is fixedly connected to a fixed plate.

[0010] Further defining the above technical solution, both the first clamping plate and the second clamping plate are U-shaped, and the fixing plate has first slots on both the left and right sides, with the first clamping plate movably inserted into the first slots. The fixing plate has second slots on both the front and rear sides, with the second clamping plate movably inserted into the second clamping plate.

[0011] To further define the above technical solution, two piston plates are symmetrically arranged at one end of the second clamping plate that is inserted into the inner wall of the second slot, and the piston plates are connected to the inner wall of the second slot by means of springs.

[0012] To further define the above technical solution, the bottom of the fixing plate is provided with a plurality of nozzles, and the air inlet end of the nozzles is connected to the inner wall of the second slot.

[0013] Further defining the above technical solution, the number of the second clamping plates is four, the four second clamping plates are divided into two groups, the stabilizing mechanism includes two folding rods and a rubber plate, the two folding rods are respectively arranged between the two groups of second clamping plates, and the two ends of the rubber plate are respectively rotatably inserted into the hinge shafts of the two folding rods.

[0014] Further defining the above technical solution, the second clamping plate has a groove at one end inserted into the second slot, the folding rod includes two inclined rods, the upper ends of the two inclined rods are inserted into the groove and hinged to the inner wall of the groove, and the lower ends of the two inclined rods are hinged together by a hinge shaft.

[0015] Further defining the above technical solution, the driving component includes a dual-head motor and two rotating rods. The dual-head motor is fixedly installed inside the fixed plate, and the two rotating rods are respectively fixedly installed at both ends of the dual-head motor. The outer wall of the end of the rotating rod inserted into the first clamping plate has an external thread. One end of the steel cable is wound around the rotating rod, and one end of the steel cable is fixedly connected to the inner wall of the groove.

[0016] Compared with the prior art, the beneficial effects of this utility model are:

[0017] The two first clamping plates are controlled to retract by the operation of the drive component, and the steel cable is wound up by the drive component. Then, the second clamping plate is retracted by the steel cable, and the stabilizing mechanism is moved down to contact the cabin plate. Thus, the stability of the cabin plate clamping is increased by the cooperation of the first clamping plate, the second clamping plate and the stabilizing mechanism.

[0018] When the steel cable pulls the second clamping plate into the second slot, it drives the piston plate to move synchronously and pushes the airflow in the second slot into the nozzle. Then, the airflow is sprayed through the nozzle to blow the surface of the cabin plate. Attached Figure Description

[0019] To more clearly illustrate the technical solutions in the embodiments of this utility model or the prior art, the drawings used in the description of the embodiments or the prior art will be briefly introduced below. Obviously, the drawings described below are only some embodiments of this utility model. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort.

[0020] Figure 1 This is a three-dimensional structural diagram of a satellite cabin horizontal moving clamp according to the present invention;

[0021] Figure 2 This is a partial three-dimensional cross-sectional view of a satellite cabin horizontal moving clamp according to the present invention;

[0022] Figure 3 This is a partial three-dimensional unfolded cross-sectional view of a satellite cabin horizontal moving clamp according to the present invention.

[0023] Among them, 1. Traction device; 11. Horizontal adjustment guide rail; 12. Traction machine; 13. Hoisting cable; 2. Fixing plate; 21. First slot; 22. Second slot; 23. Nozzle; 3. First clamping plate; 4. Second clamping plate; 41. Piston plate; 42. Spring; 43. Groove; 5. Stabilizing mechanism; 51. Folding rod; 52. Rubber plate; 6. Driving component; 61. Double-headed motor; 62. Rotating rod; 7. Steel cable. Detailed Implementation

[0024] The following is in conjunction with the appendix Figures 1-3 The present invention will be described in further detail below.

[0025] Example 1: This example provides a horizontal movement fixture for a satellite module, such as... Figure 1 As shown, this invention solves the problem that clamps typically use clamping plates to hold and fix the cabin panels. However, the clamping plates can only reinforce the side walls of the cabin panels, and the top and bottom of the cabin panels lack limiting mechanisms, resulting in poor stability when clamping and fixing the cabin panels. The invention includes a traction device 1 and a fixing plate 2. The fixing plate 2 is located at the bottom of the traction device 1. First clamping plates 3 are movably inserted into the left and right sides of the fixing plate 2, and second clamping plates 4 are movably inserted into the front and rear sides of the fixing plate 2. A stabilizing mechanism 5 is hinged between the two second clamping plates 4. A driving component 6 is provided inside the fixing plate 2. The two ends of the driving component 6 are threaded into the two first clamping plates 3 respectively. The second clamping plates 4 are connected to the driving component 6 by steel cables 7.

[0026] Among them, the driving component 6 is used to control the movement of the first clamping plate 3 and the second clamping plate 4, and the stabilizing mechanism 5 is used to assist the first clamping plate 3 and the second clamping plate 4 in fixing the cabin plate.

[0027] First, the traction device 1 controls the fixed plate 2 to move downward, and the drive component 6 controls the first clamping plate 3 and the second clamping plate 4 to unfold. As the fixed plate 2 moves downward, the cabin plate is below the fixed plate 2. At this time, the drive component 6 controls the two first clamping plates 3 to retract, and the drive component 6 also winds up the steel cable 7. Then, the steel cable 7 pulls the second clamping plate 4 to retract, and causes the stabilizing mechanism 5 to move downward and come into contact with the cabin plate. Thus, the stability of the cabin plate clamping is increased by the cooperation of the first clamping plate 3, the second clamping plate 4 and the stabilizing mechanism 5.

[0028] Combination Figure 1 In an embodiment of this utility model, the traction device 1 includes a horizontal adjustment guide rail 11 and a traction machine 12. The traction machine 12 is movably disposed inside the horizontal adjustment guide rail 11. A sling 13 is provided at the bottom of the traction machine 12. The lower end of the sling 13 is fixedly connected to the fixed plate 2. The horizontal adjustment guide rail 11 facilitates the horizontal movement of the traction machine 12. Then, the traction machine 12 and the sling 13 work together to drive the fixed plate 2 and the cabin plate to move horizontally synchronously.

[0029] It should be noted that the horizontal adjusting guide rail 11 and the traction machine 12 are existing equipment. The traction machine 12 is installed inside the horizontal adjusting guide rail 11, and the movement of the traction machine 12 can be controlled by a lead screw inside the horizontal adjusting guide rail 11.

[0030] Combination Figure 2 In the embodiments of this utility model, the first clamping plate 3 and the second clamping plate 4 are both U-shaped. The left and right sides of the fixing plate 2 are provided with first slots 21, and the first clamping plate 3 is movably inserted into the first slots 21. The front and rear sides of the fixing plate 2 are provided with second slots 22, and the second clamping plate 4 is movably inserted into the second clamping plate 4. The cooperation between the U-shaped first clamping plate 3 and the second clamping plate 4 facilitates the increase of the stability of the device when clamping the cabin plate.

[0031] Combination Figure 2 In this embodiment of the utility model, the driving component 6 includes a dual-head motor 61 and two rotating rods 62. The dual-head motor 61 is fixedly installed inside the fixed plate 2, and the two rotating rods 62 are respectively fixedly installed at both ends of the dual-head motor 61. The outer wall of one end of the rotating rod 62 inserted into the first clamping plate 3 has an external thread. One end of the steel cable 7 is wound around the rotating rod 62, and one end of the steel cable 7 is fixedly connected to the inner wall of the groove 43. The dual-head motor 61 facilitates the control of the rotation of the rotating rod 62. As the rotating rod 62 rotates, it facilitates the control of the movement of the first clamping plate 3, so as to control the unfolding and retraction of the first clamping plate 3. The rotating rod 62 facilitates the winding or releasing of the steel cable 7, and then the steel cable 7 facilitates the control of the unfolding and retraction of the second clamping plate 4.

[0032] Example 2: Reference Figure 2 , Figure 3 Two piston plates 41 are symmetrically arranged at one end of the second clamping plate 4 that is inserted into the inner wall of the second slot 22. The piston plates 41 are connected to the inner wall of the second slot 22 by springs 42. When the steel cable 7 pulls the second clamping plate 4 into the second slot 22, it drives the piston plates 41 to move synchronously and causes the springs 42 to compress and deform. When the steel cable 7 loses tension, the springs 42 push the piston plates 41 and the second clamping plate 4 to reset, thereby controlling the second clamping plate 4 to unfold.

[0033] The bottom of the fixed plate 2 is provided with several nozzles 23. The air inlet end of the nozzle 23 is connected to the inner wall of the second slot 22. When the piston plate 41 moves, it is convenient to push the airflow in the second slot 22 into the nozzle 23, and then spray the airflow through the nozzle 23 to blow the surface of the compartment plate.

[0034] Example 3: Reference Figure 2 , Figure 3 There are four second clamping plates 4, which are divided into two groups. The stabilizing mechanism 5 includes two folding rods 51 and a rubber plate 52. The two folding rods 51 are respectively set between the two groups of second clamping plates 4. The two ends of the rubber plate 52 are respectively rotatably inserted into the hinge shafts of the two folding rods 51. When the two groups of second clamping plates 4 retract, the two folding rods 51 are folded synchronously. As the folding rods 51 fold, the rubber plate 52 is controlled to move down and abut against the cabin plate, thereby increasing the stability of the cabin plate when it is clamped.

[0035] The second clamping plate 4 has a groove 43 at one end inserted into the second slot 22. The folding rod 51 includes two inclined rods. The upper ends of the two inclined rods are inserted into the groove 43 and hinged to the inner wall of the groove 43. The lower ends of the two inclined rods are hinged together by a hinge shaft. The groove 43 facilitates the installation of the inclined rods, and the hinge shaft facilitates the hinge of the two inclined rods together. When the second clamping plate 4 moves, it is easy to control the folding or unfolding of the two inclined rods so as to control the movement of the rubber plate 52.

[0036] The above description is a further detailed explanation of the present invention in conjunction with specific preferred embodiments, which is intended to enable those skilled in the art to understand and apply the present invention. However, it should not be assumed that the specific implementation of the present invention is limited to these descriptions.

Claims

1. A horizontal moving fixture for a satellite module, comprising a traction device (1) and a fixing plate (2), characterized in that, The fixing plate (2) is set at the bottom of the traction device (1). The left and right sides of the fixing plate (2) are movably inserted with first clamping plates (3). The front and rear sides of the fixing plate (2) are movably inserted with second clamping plates (4). A stabilizing mechanism (5) is hinged between the two second clamping plates (4). A driving component (6) is provided inside the fixing plate (2). The two ends of the driving component (6) are threaded into the two first clamping plates (3). The second clamping plates (4) are connected to the driving component (6) by setting steel cables (7). The driving component (6) is used to control the movement of the first clamping plate (3) and the second clamping plate (4), and the stabilizing mechanism (5) is used to assist the first clamping plate (3) and the second clamping plate (4) in fixing the cabin plate.

2. The satellite cabin horizontal moving clamp according to claim 1, characterized in that, The traction device (1) includes a horizontal adjustment guide rail (11) and a traction machine (12). The traction machine (12) is movably disposed inside the horizontal adjustment guide rail (11). A sling (13) is provided at the bottom of the traction machine (12). The lower end of the sling (13) is fixedly connected to the fixing plate (2).

3. The satellite cabin horizontal moving clamp according to claim 1, characterized in that, The first clamping plate (3) and the second clamping plate (4) are both U-shaped. The left and right sides of the fixing plate (2) are provided with first slots (21). The first clamping plate (3) is movably inserted into the first slots (21). The front and rear sides of the fixing plate (2) are provided with second slots (22). The second clamping plate (4) is movably inserted into the second clamping plate (4).

4. The satellite cabin horizontal moving clamp according to claim 3, characterized in that, Two piston plates (41) are symmetrically arranged at one end of the second clamping plate (4) inserted into the inner wall of the second slot (22). The piston plates (41) are connected to the inner wall of the second slot (22) by means of springs (42).

5. The satellite cabin horizontal moving clamp according to claim 4, characterized in that, The bottom of the fixing plate (2) is provided with a number of nozzles (23), and the air inlet end of the nozzles (23) is connected to the inner wall of the second slot (22).

6. The satellite cabin horizontal moving clamp according to claim 3, characterized in that, The number of the second clamping plates (4) is four, and the four second clamping plates (4) are divided into two groups. The stabilizing mechanism (5) includes two folding rods (51) and a rubber plate (52). The two folding rods (51) are respectively arranged between the two groups of second clamping plates (4). The two ends of the rubber plate (52) are respectively rotatably inserted into the hinge shafts of the two folding rods (51).

7. The satellite cabin horizontal moving clamp according to claim 6, characterized in that, The second clamp (4) has a groove (43) at one end inserted into the second slot (22). The folding rod (51) includes two inclined rods. The upper ends of the two inclined rods are inserted into the groove (43) and hinged to the inner wall of the groove (43). The lower ends of the two inclined rods are hinged to each other through a hinge shaft.

8. The satellite cabin horizontal moving clamp according to claim 7, characterized in that, The driving component (6) includes a dual-head motor (61) and two rotating rods (62). The dual-head motor (61) is fixedly installed in the fixed plate (2). The two rotating rods (62) are respectively fixedly installed at both ends of the dual-head motor (61). The outer wall of the end of the rotating rod (62) inserted into the first clamping plate (3) is provided with external threads. One end of the steel cable (7) is wound around the rotating rod (62). One end of the steel cable (7) is fixedly connected to the inner wall of the groove (43).

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