Discrete point type satellite adapter improved structure

Abstract

The utility model relates to the technical field of satellite adapters, in particular to an improved structure of a discrete point type satellite adapter, which comprises four upright posts, two side walls of the upright posts are respectively provided with a first connecting sleeve and a second connecting sleeve, and the first connecting sleeve is inclined; an inclined first surrounding plate is arranged between every two adjacent first connecting sleeves; a vertical second surrounding plate is arranged between every two adjacent second connecting sleeves. Through the arrangement of the stand column, the first connecting sleeve, the second connecting sleeve, the first surrounding plate and the second surrounding plate, the two ends of the first surrounding plate and the two ends of the second surrounding plate are in inserted fit with the first connecting sleeve and the second connecting sleeve correspondingly, and under the action of the first bolt and the second bolt, the first surrounding plate and the second surrounding plate can be stably connected with the first connecting sleeve and the second connecting sleeve; by means of the design, the assembling convenience of the coaming is improved, meanwhile, the installation firmness and stability of the coaming are guaranteed, and the stability of satellite-rocket butt joint is guaranteed.

Description

TECHNICAL FIELD

[0001] The utility model relates to satellite adapter technical field, concretely is discrete point formula satellite adapter improvement structure. BACKGROUND

[0002] The satellite adapter is a non-standard equipment, and its core function is to adapt various terminal protocols to a satellite protocol platform. Common satellite adapters include discrete point formula satellite adapters and enhanced satellite adapters. The discrete point formula satellite adapter is a structure designed to meet the non-central symmetric point interface requirements of specific small and medium-sized satellites. This adapter has the characteristics of simple structure, reasonable layout, and convenient installation and operation. It is particularly suitable for the non-symmetric point interface requirements of specific small and medium-sized satellites, and has higher flexibility and adaptability compared with traditional skin stringer satellite adapters.

[0003] The utility model discloses a discrete point formula satellite adapter, and the technical scheme of the discrete point formula satellite adapter is: the number of the baffle of the discrete point formula satellite adapter is 4, and the four baffles form a rectangle, and the baffles are fixedly connected through the stand column. The stand column is composed of a top plate, a bottom plate and a cross stand plate, and the cross stand plate is axially supported in the middle of the bottom plate and the top plate. The cross stand plate axially divides the stand column into four areas, two diagonal areas of which are fixedly connected with the baffles respectively, and the inner angle area of the stand column between the two baffles is used for installing a separation spring. The outer angle area of the stand column between the two baffles is horizontally divided into upper and lower two areas by a partition plate, and is used for installing a low-impact separation device and a separation stroke switch respectively. Every two baffles are installed as a group, one group of baffles is a vertical straight baffle, and the other group is an inclined baffle. The inclined baffle is inclined from bottom to top to the inside of the rectangle. The angle between the inclined baffle and the vertical line is 12-18°. The utility model has the advantages of simple structure, reasonable layout, compact structure, convenient installation and operation, and can adjust the size of each area of the stand column and the inclination angle of the stand plate according to the size of the satellite, thereby providing a good strength and rigidity environment for the use of each component.

[0004] Although the discrete point formula satellite adapter provides a good strength and rigidity environment, the device still has the following problems in actual use: in the device, the baffles are fixedly connected through the stand column, and the structure and shape of the stand column are relatively complex, thereby affecting the assembly convenience between the baffles and the stand column. In view of this, the discrete point formula satellite adapter improvement structure is proposed. UTILITY MODEL CONTENTS

[0005] The utility model aims to provide a discrete point formula satellite adapter improvement structure to solve the problems raised in the background technology.

[0006] To achieve the above-mentioned purpose, the utility model provides the following technical scheme:

[0007] The improved structure of the discrete point satellite adapter comprises four columns, the two side walls of the columns are respectively provided with a first connecting sleeve and a second connecting sleeve, the first connecting sleeve is inclined, two first bolts are arranged on the outer wall of the first connecting sleeve, the first bolts are threadedly connected with first nuts, two second bolts are arranged on the outer wall of the second connecting sleeve, and the second bolts are threadedly connected with second nuts.

[0008] A first mounting plate is fixed to the top of the column, and a second mounting plate is fixed to the outer wall of the column near the bottom end.

[0009] An inclined first baffle is arranged between the two adjacent first connecting sleeves, the two ends of the first baffle are inserted into the opening of the first connecting sleeve, and the first bolts pass through the two ends of the first baffle.

[0010] A vertical second baffle is arranged between the two adjacent second connecting sleeves, the two ends of the second baffle are inserted into the opening of the second connecting sleeve, and the second bolts pass through the two ends of the second baffle.

[0011] As a preferred technical scheme of the utility model, the cross section shape of the first connecting sleeve and the second connecting sleeve is all mouth-shaped, and the first connecting sleeve and the second connecting sleeve are integrally formed with the column.

[0012] As a preferred technical scheme of the utility model, the overall shape of the first baffle and the second baffle is all rectangular, and the first baffle and the second baffle are galvanized steel products.

[0013] As a preferred technical scheme of the utility model, the two ends of the second mounting plate are provided with separate switch mounting hole positions, and the connecting position of the second mounting plate and the column is further provided with an inclined reinforcing plate.

[0014] As a preferred technical scheme of the utility model, the included angle between the first baffle and the vertical plane is 13-18°.

[0015] As a preferred technical scheme of the utility model, the top side of the first mounting plate is provided with a separate spring mounting hole position, and the side of the separate spring mounting hole position is provided with a separate spring mounting guide hole.

[0016] As a preferred technical scheme of the utility model, the outer wall of the first baffle and the second baffle is provided with a plurality of grooves, and the grooves are all fixed with reinforcing edges.

[0017] Compared with the prior art, the utility model has the advantages of:

[0018] Through the setting of the stand, the first connecting sleeve, the second connecting sleeve, the first baffle and the second baffle, the two ends of the first baffle and the second baffle are respectively inserted and matched with the first connecting sleeve and the second connecting sleeve, and under the action of the first bolt and the second bolt, the first baffle and the second baffle can be stably connected with the first connecting sleeve and the second connecting sleeve, the design improves the assembly convenience of the baffle, and also ensures the mounting firmness and stability of the baffle, and ensures the stability of the star-rocket docking. BRIEF DESCRIPTION OF DRAWINGS

[0019] Figure 1 It is an overall structure schematic view of the utility model;

[0020] Figure 2 It is an overall explosion structure schematic view of the utility model;

[0021] Figure 3 It is a structure schematic view of the stand in the utility model;

[0022] Figure 4 It is an explosion structure schematic view of the stand in the utility model;

[0023] Figure 5 It is a structure schematic view of the groove in the utility model;

[0024] In the drawing:

[0025] 1, stand; 10, first connecting sleeve; 100, first bolt; 101, first nut; 11, second connecting sleeve; 110, second bolt; 111, second nut;

[0026] 2, first mounting plate; 20, separation spring mounting hole; 21, separation spring installation guide hole;

[0027] 3, second mounting plate; 30, separation switch mounting hole; 31, reinforcing plate;

[0028] 4, first baffle;

[0029] 5, second baffle;

[0030] 6, groove; 60, reinforcing edge. DETAILED DESCRIPTION

[0031] The technical scheme in the embodiments of the utility model will be described clearly and completely below in conjunction with the drawings in the embodiments of the utility model, and obviously, the described embodiments are only part of the embodiments of the utility model, rather than all the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by those skilled in the art without creative labor fall within the protection scope of the utility model.

[0032] The embodiment provides a technical scheme:

[0033] Referring to Figures 1-5 As shown in the figure, the improved structure of the discrete point satellite adapter includes four columns 1, the two side walls of the column 1 are respectively provided with a first connecting sleeve 10 and a second connecting sleeve 11, the first connecting sleeve 10 is inclined; two first bolts 100 are arranged on the outer wall of the first connecting sleeve 10, and a first nut 101 is threadedly connected on the first bolt 100; two second bolts 110 are arranged on the outer wall of the second connecting sleeve 11, and a second nut 111 is threadedly connected on the second bolt 110; a first mounting plate 2 is fixed on the top of the column 1, and a second mounting plate 3 is fixed on the outer wall of the column 1 close to the bottom end; an inclined first baffle 4 is arranged between the two adjacent first connecting sleeves 10, the two ends of the first baffle 4 are inserted into the opening of the first connecting sleeve 10, and the first bolt 100 passes through the two ends of the first baffle 4; a vertical second baffle 5 is arranged between the two adjacent second connecting sleeves 11, the two ends of the second baffle 5 are inserted into the opening of the second connecting sleeve 11, and the second bolt 110 passes through the two ends of the second baffle 5.

[0034] In this embodiment, the cross-sectional shape of the first connecting sleeve 10 and the second connecting sleeve 11 is a mouth-shaped type, and the first connecting sleeve 10 and the second connecting sleeve 11 are an integral structure with the column 1. The design of the mouth-shaped type enhances the structural strength of the first connecting sleeve 10 and the second connecting sleeve 11, making them more stable and durable. The integral structure further improves the reliability and stability of the whole, reducing the risk of loosening at the connection.

[0035] In this embodiment, the overall shape of the first baffle 4 and the second baffle 5 is rectangular, and the first baffle 4 and the second baffle 5 are made of galvanized steel material. The design of the rectangle is conducive to the butt joint of the satellite by the first baffle 4 and the second baffle 5, meeting the bearing demand of the satellite, and the galvanized steel material has good corrosion resistance and strength, suitable for harsh environment, prolonging the service life of the product.

[0036] In this embodiment, the two ends of the second mounting plate 3 are provided with separate switch mounting holes 30, and the connection between the second mounting plate 3 and the column 1 is further provided with an inclined reinforcing plate 31. The separate switch mounting hole 30 facilitates the installation of the separate switch, improving the functionality and flexibility of the product, and the reinforcing plate 31 enhances the structural strength of the connection between the second mounting plate 3 and the column 1, improving the overall stability.

[0037] In this embodiment, the included angle between the first baffle 4 and the vertical plane is 13-18°. The preferred included angle between the first baffle 4 and the vertical plane is 15°, and the first baffle 4 with the inclined angle cooperates with the second baffle 5, meeting the requirement of the gradual change of the overall cross section of the satellite adapter.

[0038] In the embodiment, a separation spring mounting hole 20 is formed at the top end side of the first mounting plate 2, and a separation spring mounting guide hole 21 is formed at one side of the separation spring mounting hole 20. The separation spring mounting hole 20 and the separation spring mounting guide hole 21 simplify the installation process of the separation spring, improve the installation efficiency and accuracy, and further improve the installation efficiency of the satellite.

[0039] In the embodiment, a plurality of grooves 6 are formed in the outer walls of the first and second enclosing plates 4 and 5, and a reinforcing rib 60 is fixed in each groove 6. The grooves 6 and the reinforcing ribs 60 further enhance the structural strength of the first and second enclosing plates 4 and 5, and improve the impact resistance and compression resistance of the product.

[0040] It should be noted that the first and second mounting plates 2 and 3 in the embodiment are tightly welded with the column 1, which ensures the firm connection between the first and second mounting plates 2 and 3 and the column 1, and improves the stability and load-bearing capacity of the overall structure. This connection mode can effectively resist external forces and vibrations, ensuring the stable operation of the equipment, and further ensuring the load-bearing capacity of the satellite.

[0041] In specific use, the user first inserts the two ends of the first enclosing plate 4 into the first connecting sleeves 10 on both sides, then inserts the two ends of the second enclosing plate 5 into the second connecting sleeves 11 on both sides, and then the user inserts the first and second enclosing plates 4 and 5 into the first and second connecting sleeves 10 and 11, respectively, and then the user repeats the above steps to complete the installation of the other first and second enclosing plates 4 and 5.

[0042] The basic principles, main features and advantages of the present application are shown and described above. It should be understood by those skilled in the art that the present application is not limited by the above embodiments, and the above embodiments and descriptions in the specification are only preferred examples of the present application and do not limit the present application. Without departing from the spirit and scope of the present application, various changes and improvements can be made to the present application, and these changes and improvements all fall within the scope of the claimed present application. The scope of protection of the present application is defined by the appended claims and their equivalents.

Claims

1. An improved structure of a discrete spot satellite adapter, characterized in that: It includes four columns (1), and a first connecting sleeve (10) and a second connecting sleeve (11) are respectively installed on the two side walls of the columns (1). The first connecting sleeve (10) is inclined. Two first bolts (100) are inserted through the outer wall of the first connecting sleeve (10), and a first nut (101) is threaded on the first bolt (100). Two second bolts (110) are inserted through the outer wall of the second connecting sleeve (11), and a second nut (111) is threaded on the second bolt (110). The top of the column (1) is fixed with a first mounting plate (2), and the outer wall of the column (1) is fixed with a second mounting plate (3) near the bottom. An inclined first enclosure plate (4) is provided between two adjacent first connecting sleeves (10). The two ends of the first enclosure plate (4) are inserted into the opening of the first connecting sleeve (10), and the first bolt (100) passes through the two ends of the first enclosure plate (4). A vertical second enclosure plate (5) is provided between two adjacent second connecting sleeves (11). The two ends of the second enclosure plate (5) are inserted into the openings of the second connecting sleeves (11), and the second bolt (110) passes through the two ends of the second enclosure plate (5).

2. The discreet spot satellite adapter modification of claim 1, wherein: The first connecting sleeve (10) and the second connecting sleeve (11) are both in the shape of a square. The first connecting sleeve (10) and the second connecting sleeve (11) are integrally formed with the column (1).

3. The discreet spot satellite adapter modification of claim 1, wherein: The first enclosure (4) and the second enclosure (5) are both rectangular in shape, and both the first enclosure (4) and the second enclosure (5) are made of galvanized steel.

4. The discreet spot satellite adapter modification of claim 1, wherein: The second mounting plate (3) has a disconnect switch mounting hole (30) at both ends, and an inclined reinforcing plate (31) is fixed at the connection between the second mounting plate (3) and the column (1).

5. The discreet spot satellite adapter modification of claim 1, wherein: The angle between the first enclosure (4) and the vertical plane is 13-18°.

6. The discreet spot satellite adapter modification of claim 1, wherein: The first mounting plate (2) has a separation spring mounting hole (20) on one side of its top end, and a separation spring mounting guide hole (21) is provided on one side of the separation spring mounting hole (20).

7. The discreet spot satellite adapter modification of claim 1, wherein: The outer walls of the first enclosure (4) and the second enclosure (5) are provided with multiple grooves (6), and each groove (6) is fixed with a reinforcing rib (60).

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