A thermal release pin puller for satellite

Abstract

The utility model relates to the field of satellite technology, and discloses a thermal release pin puller for satellites, the thermal release pin puller for satellites comprises a buffer rubber pad, the buffer rubber pad is fixedly connected to the right end of the pulling handle, the connecting rod one is fixedly connected to the right end of the pulling handle, the fixed cylinder is fixedly connected to the right end of the connecting rod one, the connecting rod two is fixedly connected to the right end of the fixed cylinder, the fixed column is fixedly connected to the right end of the connecting rod two, the pin pulling device is fixedly connected to the right end of the fixed column, and the mounting plate is movably connected to the lower side of the pulling handle. The thermal release pin puller for satellites improves the movable release and pull-out capability of the thermal release pin puller through the improvement of the thermal release pin puller. In the actual use of the thermal release pin puller, the thermal release pin puller can be quickly and effectively released and pulled out as needed, which is convenient for the use of the satellite antenna base and improves the user experience of the thermal release pin puller for satellites.

Description

Technical Field

[0001] The utility model relates to the technical field of satellites, in particular to a thermal release pin puller for satellites. Background Art

[0002] A satellite refers to a natural celestial body that orbits a planet and moves periodically in a closed orbit. Artificial satellites are also generally called satellites. Artificial satellites are built by humans and launched into space by space flight vehicles such as rockets and space shuttles. They are devices that orbit the earth or other planets like natural satellites. Gas planets often have many satellites. A satellite thermal release pin puller is a satellite thermal release pin puller.

[0003] The prior art patent document with publication number CN208706833U discloses a satellite antenna base, wherein the legs are connected to the arms correspondingly, and the legs are pivotally connected to the arms correspondingly; and

[0009] a rotating assembly, wherein the rotating assembly connects the corresponding arms and legs, and the legs are connected and fixed to the arms through the rotating assembly; the rotating assembly is used to control the legs to fold around the outside of the antenna chassis body to be in a folded state, or to control the legs to tilt outward from the arms away from the antenna chassis body. The extended setting is in a working state, and a rotating assembly is arranged between the support arm and the support leg, so that the support leg is pivotally connected to one end of the support arm and fixed by the rotating assembly, so that the support leg can be folded outside the antenna case body during transportation, which greatly reduces the transportation volume. When the equipment is working, each support leg can be stretched out to ensure the stability of the antenna case body, thereby effectively avoiding the problem of poor timeliness caused by disassembly and assembly. The rotating assembly includes a rotating shaft, an elastic element sleeved on the rotating shaft, a limit seat abutting against one end of the elastic element, and a limit seat abutting against the limit seat The connecting block, the rotating shaft respectively passes through the support arm and the support leg, the rotating shaft is connected and fixed to the support arm, the support leg is pivoted on the rotating shaft, and the two latches are arranged on the limit seat relatively; the four adjustment holes are arranged correspondingly; the four adjustment holes are arranged opposite to each other in pairs, and the rotating assembly also includes a sleeve; the sleeve is sleeved on the rotating shaft and connected and fixed to the rotating shaft, the elastic element is arranged in the sleeve, the elastic element is clamped between the sleeve and the limit seat, and the sleeve is provided with a guide The cam is provided with a guide block on the limit seat; the guide block is correspondingly arranged in the guide slot so that the limit seat abuts against the sleeve, and the rotating assembly also includes a fixing bolt; the fixing bolt is arranged at the end of the rotating shaft facing away from the pressing block, and a leveling element is arranged on the leg; the leveling element is correspondingly installed at the end of the leg facing away from the arm, and the leg includes a stop portion, a pivot portion connected to the stop portion, an extension portion connected to the pivot portion, and an adjustment portion connected to the extension portion; the stop portion is arranged at one end of the leg close to the arm.

[0004] However, in the prior art patent CN208706833U, due to the poor ability of the satellite antenna base to be released and pulled out, it is impossible to quickly and effectively release and pull out the heat release pin puller as needed during the actual use of the satellite antenna base, which is inconvenient to use the satellite antenna base and affects the user experience of the satellite antenna base. Utility Model Content

[0005] 1. Technical issues to be solved

[0006] The utility model aims to provide a thermal release pin puller for satellites to solve the problem of poor movable release and pull-out capability of the satellite antenna base in the above-mentioned background technology.

[0007] (II) Technical solution

[0008] To achieve the above-mentioned purpose, the utility model provides the following technical solutions: a thermal release pin puller for satellite, which comprises a lifting handle, a buffer rubber pad, a connecting rod 1, a fixing tube, a connecting rod 2, a fixing column, a pin pulling device, a mounting plate, a satellite receiver, a movable tube, a supporting base, a counterweight, a connecting plate, a fixing block, a mounting disk, a rotating disk, a connecting disk, an electric push rod 1, a pushing rod 1 and a movable universal wheel, wherein the buffer rubber pad is fixedly connected to the right end of the lifting handle, the connecting rod 1 is fixedly connected to the right end of the lifting handle, the fixing tube is fixedly connected to the right end of the connecting rod 1, the connecting rod 2 is fixedly connected to the right end of the fixing tube, the fixing column is fixedly connected to the right end of the connecting rod 2, the pin pulling device is fixedly connected to the right end of the fixing column, and the mounting plate is movably connected to the lower side of the lifting handle.

[0009] Preferably, the satellite receiver is fixedly connected to the upper end of the mounting plate, and the movable cylinder is movably connected to the left end of the satellite receiver. By improving the thermal release pin puller, the movable releasing and pulling ability of the thermal release pin puller is improved. During the actual use of the thermal release pin puller, the thermal release pin puller can be quickly and effectively released and pulled as needed, which facilitates the use of the satellite antenna base and improves the user experience of the thermal release pin puller for the satellite.

[0010] Preferably, the support base is movably connected to the lower side of the mounting plate, and the counterweight block is fixedly connected to the upper end of the support base. By controlling the rotation of the mounting plate, the rotating plate and the connecting plate, the mounting plate and the satellite receiver are moved to a suitable angle, and then the connection of the mounting plate is facilitated through the connecting plate. Then, through the installation of the satellite receiver and the movable cylinder, the movable use of the pulling handle, the buffer rubber pad, the connecting rod one, the fixed cylinder, the connecting rod two, the fixed column, and the pin pulling device are facilitated, thereby improving the user experience of the thermal release pin puller for the satellite.

[0011] Preferably, the connecting plate is fixedly connected to the upper end of the counterweight block, and the fixing block is fixedly connected to the upper end of the connecting plate.

[0012] Preferably, the mounting disk is fixedly connected to the upper end of the fixed block, and the rotating disk is movably connected to the upper end of the mounting disk. By controlling the movement of the movable universal wheel, the satellite heat release pin puller is moved to a suitable position, and then by controlling the extension and retraction of the electric push rod 1 and the push rod 1, the supporting base and the counterweight block are moved to a suitable height. Then, the installation and connection of the mounting disk, the rotating disk and the connecting disk are facilitated by the installed connecting plate and the fixed block.

[0013] Preferably, the connecting disk is fixedly connected to the upper end of the rotating disk, and the electric push rod is fixedly connected to the lower end of the supporting base.

[0014] Preferably, the push rod 1 is movably connected to the lower end of the electric push rod 1, and the movable universal wheel is fixedly connected to the lower end of the push rod 1.

[0015] Compared with the prior art, the beneficial effects of the utility model are:

[0016] 1. The thermal release pin puller for satellites improves the ability of the thermal release pin puller to release and pull out. During the actual use of the thermal release pin puller, the thermal release pin puller can be quickly and effectively released and pulled out as needed, which is convenient for the use of the satellite antenna base and improves the user experience of the thermal release pin puller for satellites.

[0017] 2. The satellite heat release pin puller controls the rotation of the mounting plate, the rotating plate and the connecting plate to move the mounting plate and the satellite receiver to a suitable angle, and then facilitates the connection of the mounting plate through the connecting plate. Then, through the installation of the satellite receiver and the movable cylinder, it facilitates the use of the lifting handle, the buffer rubber pad, the connecting rod 1, the fixing cylinder, the connecting rod 2, the fixing column and the pin puller, thereby improving the user experience of the satellite heat release pin puller;

[0018] 3. The satellite heat release pin puller moves the satellite heat release pin puller to a suitable position by controlling the movement of the mobile universal wheel, and then moves the support base and the counterweight block to a suitable height by controlling the extension and retraction of the electric push rod 1 and the push rod 1, and then facilitates the installation and connection of the mounting plate, the rotating plate and the connecting plate through the installed connecting plate and the fixed block. BRIEF DESCRIPTION OF THE DRAWINGS

[0019] Figure 1 It is a schematic diagram of the three-dimensional structure of the utility model;

[0020] Figure 2 This is a schematic diagram of the structure of the pin pulling device of the utility model;

[0021] Figure 3 This is a schematic diagram of the structure of a satellite receiver of the utility model;

[0022] Figure 4 This is a schematic diagram of the support base structure of the utility model.

[0023] In the figure: 1. lifting handle; 2. cushioning rubber pad; 3. connecting rod 1; 4. fixing cylinder; 5. connecting rod 2; 6. fixing column; 7. pin pulling device; 8. mounting plate; 9. satellite receiver; 10. movable cylinder; 11. supporting base; 12. counterweight block; 13. connecting plate; 14. fixing block; 15. mounting plate; 16. rotating plate; 17. connecting plate; 18. electric push rod 1; 19. pushing rod 1; 20. movable universal wheel. DETAILED DESCRIPTION

[0024] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.

[0025] See also Figure 1-Figure 4 The utility model provides a technical solution: a heat release pin puller for satellite, which includes a lifting handle 1, a buffer rubber pad 2, a connecting rod 1 3, a fixing cylinder 4, a connecting rod 2 5, a fixing column 6, a pin pulling device 7, a mounting plate 8, a satellite receiver 9, a movable cylinder 10, a supporting base 11, a counterweight block 12, a connecting plate 13, a fixing block 14, a mounting disk 15, a rotating disk 16, a connecting disk 17, an electric push rod 18, a pushing rod 19 and a movable universal wheel 20. The buffer rubber pad 2 is fixedly connected to the right end of the lifting handle 1, the connecting rod 1 3 is fixedly connected to the right end of the lifting handle 1, the fixing cylinder 4 is fixedly connected to the right end of the connecting rod 1 3, the connecting rod 2 5 is fixedly connected to the right end of the fixing cylinder 4, the fixing column 6 is fixedly connected to the right end of the connecting rod 2 5, the pin pulling device 7 is fixedly connected to the right end of the fixing column 6, and the mounting plate 8 is movably connected to the lower side of the lifting handle 1.

[0026] The satellite receiver 9 is fixedly connected to the upper end of the mounting plate 8, the movable cylinder 10 is movably connected to the left end of the satellite receiver 9, the supporting base 11 is movably connected to the lower side of the mounting plate 8, the counterweight 12 is fixedly connected to the upper end of the supporting base 11, the connecting plate 13 is fixedly connected to the upper end of the counterweight 12, and the fixed block 14 is fixedly connected to the upper end of the connecting plate 13. By controlling the rotation of the mounting disk 15, the rotating disk 16, and the connecting disk 17, the mounting plate 8 and the satellite receiver 9 are moved to a suitable angle, and then the connecting disk 17 is used to facilitate the connection of the mounting plate 8. Then, through the installation of the satellite receiver 9 and the movable cylinder 10, the movable use of the pulling handle 1, the buffer rubber pad 2, the connecting rod 1 3, the fixed cylinder 4, the connecting rod 2 5, the fixed column 6, and the pin pulling device 7 are facilitated, thereby improving the use experience of the satellite heat release pin puller.

[0027] The mounting disk 15 is fixedly connected to the upper end of the fixed block 14, the rotating disk 16 is movably connected to the upper end of the mounting disk 15, the connecting disk 17 is fixedly connected to the upper end of the rotating disk 16, the electric push rod mounting disk 15, the rotating disk 16, and the connecting disks 17-18 are fixedly connected to the lower end of the support base 11, the pushing rod 19 is movably connected to the lower end of the electric push rod 18, and the movable universal wheel 20 is fixedly connected to the lower end of the pushing rod 19. By controlling the movement of the movable universal wheel 20, the satellite heat release pin puller is moved to a suitable position, and then by controlling the extension and retraction of the electric push rod 18 and the pushing rod 19, the support base 11 and the counterweight block 12 are moved to a suitable height, and then the installation and connection of the mounting disk 15, the rotating disk 16, and the connecting disk 17 are facilitated by the installed connecting plate 13 and the fixed block 14.

[0028] Working principle: by controlling the movement of the mobile universal wheel 20, the satellite heat release pin puller is moved to a suitable position, and then by controlling the extension and retraction of the electric push rod 18 and the push rod 19, the support base 11 and the counterweight block 12 are moved to a suitable height, and then through the installed connecting plate 13 and the fixed block 14, the installation and connection of the mounting plate 15, the rotating plate 16 and the connecting plate 17 are facilitated, and then by controlling the rotation of the mounting plate 15, the rotating plate 16 and the connecting plate 17, the mounting plate 8 and the satellite receiver 9 are moved to a suitable angle, and then through the connecting plate 17, the connection of the mounting plate 8 is facilitated, and then through the installation of the satellite receiver 9 and the movable cylinder 10, the activity of the pulling handle 1, the buffer rubber pad 2, the connecting rod 1 3, the fixed cylinder 4, the connecting rod 2 5, the fixed column 6 and the pin pulling device 7 are facilitated, thereby improving the use experience of the satellite heat release pin puller.

[0029] Finally, it should be noted that the above content is only used to illustrate the technical solution of the utility model, rather than to limit the protection scope of the utility model. Simple modifications or equivalent substitutions of the technical solution of the utility model by ordinary technicians in this field do not deviate from the essence and scope of the technical solution of the utility model.

Claims

1. A satellite heat release pin puller, comprising a lifting handle (1), a buffer rubber pad (2), a connecting rod (3), a fixing cylinder (4), a connecting rod (5), a fixing column (6), a pin puller (7), a mounting plate (8), a satellite receiver (9), a movable cylinder (10), a supporting base (11), a counterweight (12), a connecting plate (13), a fixing block (14), a mounting plate (15), a rotating plate (16), a connecting plate (17), an electric push rod (18), a push rod (19), and a movable universal wheel (20), characterized in that: The buffer rubber pad (2) is fixedly connected to the right end of the lifting handle (1), the connecting rod 1 (3) is fixedly connected to the right end of the lifting handle (1), the fixing tube (4) is fixedly connected to the right end of the connecting rod 1 (3), the connecting rod 2 (5) is fixedly connected to the right end of the fixing tube (4), the fixing column (6) is fixedly connected to the right end of the connecting rod 2 (5), the pin pulling device (7) is fixedly connected to the right end of the fixing column (6), and the mounting plate (8) is movably connected to the lower side of the lifting handle (1).

2. A satellite thermal release pin puller according to claim 1, characterized in that: The satellite receiver (9) is fixedly connected to the upper end of the mounting plate (8), and the movable cylinder (10) is movably connected to the left end of the satellite receiver (9).

3. A satellite thermal release pin puller according to claim 2, characterized in that: The support base (11) is movably connected to the lower side of the mounting plate (8), and the counterweight (12) is fixedly connected to the upper end of the support base (11).

4. A satellite thermal release pin puller according to claim 3, characterized in that: The connecting plate (13) is fixedly connected to the upper end of the counterweight block (12), and the fixing block (14) is fixedly connected to the upper end of the connecting plate (13).

5. A satellite thermal release pin puller according to claim 4, characterized in that: The mounting plate (15) is fixedly connected to the upper end of the fixed block (14), and the rotating plate (16) is movably connected to the upper end of the mounting plate (15).

6. A satellite thermal release pin puller according to claim 5, characterized in that: The connecting disk (17) is fixedly connected to the upper end of the rotating disk (16), and the electric push rod 1 (18) is fixedly connected to the lower end of the supporting base (11).

7. A satellite thermal release pin puller according to claim 6, characterized in that: The push rod 1 (19) is movably connected to the lower end of the electric push rod 1 (18), and the movable universal wheel (20) is fixedly connected to the lower end of the push rod 1 (19).

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