Satellite common-view instrument with supporting and stabilizing structure

Abstract

The utility model discloses a satellite common-view instrument with a supporting and stabilizing structure, which comprises a satellite common-view instrument main body, and further comprises a damping assembly arranged right below the satellite common-view instrument main body. The bottoms of the four supporting rod bodies can be embedded in the limiting circular grooves, the limiting circular grooves can limit the supporting rod bodies so that the supporting rod bodies can be more stable in the placing process, at the moment, the arranged shock pads can reduce the influence of external vibration on the satellite common-view instrument body, the four supporting rod bodies can be rotationally stored in the storage groove body, and therefore the supporting rod bodies can be stored more stably. The supporting rod body is clamped in the clamping groove body, multiple installation modes can be selected according to the external environment, meanwhile, the influence of external vibration on the satellite common-view instrument body can be reduced, the service life of the satellite common-view instrument body is prolonged, and the equipment is higher in applicability and more convenient to use.

Description

Technical Field

[0001] The utility model relates to the technical field of satellite common-view instruments, in particular to a satellite common-view instrument with a supporting and stable structure. Background Art

[0002] Satellite common view meter is a high-precision time comparison test instrument, which is mainly used to measure the deviation between the time at the user's location and the national standard time, so as to realize the performance calibration of satellite timing equipment. Satellite common view meter has a wide range of application scenarios, covering many important fields such as finance, scientific research, national defense, Internet and public security. It provides reliable time synchronization services for these fields, ensuring the efficient operation and security of the system.

[0003] Satellite common-view instruments are relatively expensive, but most of them lack a stable supporting structure at the bottom, which will be affected by external vibrations and cause damage to internal components. At the same time, it is difficult to select the supporting structure according to the external placement environment. Therefore, we propose a satellite common-view instrument with a stable supporting structure to solve this problem. Utility Model Content

[0004] The purpose of the utility model is to provide a satellite common-view instrument with a supporting stable structure to solve the problem that the satellite common-view instrument proposed in the above background technology may be affected by external vibrations, causing damage to internal components, and it is difficult to select a supporting structure according to the external placement environment.

[0005] To achieve the above-mentioned purpose, the utility model provides the following technical solutions: a satellite common-view instrument with a supporting and stabilizing structure, including a satellite common-view instrument body, and also including:

[0006] A shock absorbing component is arranged directly below the satellite common-view instrument body and is used to absorb shock to the satellite common-view instrument body;

[0007] The support components are evenly distributed at the bottom of the satellite common-view instrument body and are used to support the satellite common-view instrument body.

[0008] Preferably, the support assembly includes a storage slot body and a support rod body. The storage slot bodies are evenly distributed and opened at the bottom of the satellite common-view instrument body, and the support rod body is rotatably connected to one side of the interior of the storage slot body.

[0009] Preferably, an anti-skid pad is fixed to the outer side of the support rod body, and the anti-skid pad can contact the upper end surface of the placement table.

[0010] Preferably, the shock absorbing assembly includes a carrying tray and a shock absorbing pad. The carrying tray is arranged directly below the satellite common view meter body. The shock absorbing pad is fixed to the bottom of the satellite common view meter body, and the bottom of the shock absorbing pad is in contact with the placement table.

[0011] Preferably, a clamping groove is evenly distributed at the central position of the upper end surface of the carrying tray, and the supporting rod can be clamped inside the clamping groove. A limiting circular groove is provided on one side of the lower end surface inside the clamping groove, and the bottom end of the supporting rod can be embedded in the limiting circular groove.

[0012] Preferably, a display screen and a control button are respectively provided at the front left end and the front right end of the satellite common view instrument body, and the display screen and the control button are electrically connected to a circuit board fixed inside the satellite common view instrument body.

[0013] Compared with the prior art, the beneficial effects of the utility model are:

[0014] 1. When the four groups of support rods of the utility model can be rotated and opened from the inside of the storage slot, the bottom of the four groups of support rods can be embedded in the inside of the limiting circular groove. The limiting circular groove can limit the support rods to make them more stable during placement. At this time, the provided shock-absorbing pads can reduce the impact of external vibrations on the satellite common-view instrument body. The four groups of support rods can also be rotated and stored in the inside of the storage slot, and the support rods can be clamped in the inside of the clamping slot. A variety of installation methods can be selected according to the external environment. At the same time, the impact of external vibrations on the satellite common-view instrument body can be reduced, and its service life can be extended, making the equipment more applicable and more convenient to use.

[0015] 2. The set support rod body can be rotated and opened from the inside of the storage slot. After the four groups of support rod bodies are tilted outward, the bottom of the four groups of support rod bodies are in contact with the placement table, which can support the satellite common view instrument body. When the four groups of support rod bodies are rotated and stored inside the storage slot, the set anti-slip pad can contact with the placement table, which can increase the friction between the satellite common view instrument body and the placement table, making it more stable to place. BRIEF DESCRIPTION OF THE DRAWINGS

[0016] Figure 1 The overall structure of the utility model is shown in a top view Figure 1 ;

[0017] Figure 2 This is a schematic diagram of the support assembly of the utility model when viewed from above Figure 1 ;

[0018] Figure 3 This is a top view schematic diagram of the shock absorbing assembly of the utility model;

[0019] Figure 4 This is a schematic diagram of the support assembly of the utility model when viewed from above Figure 2 ;

[0020] Figure 5 The overall structure of the utility model is shown in a top view Figure 2 .

[0021] In the figure: 1. Satellite common-view instrument body; 2. Display screen; 3. Control button; 4. Carrying tray; 5. Shock-absorbing pad; 6. Card-connecting slot; 7. Limiting circular groove; 8. Storage slot; 9. Anti-slip pad; 10. Support rod. DETAILED DESCRIPTION

[0022] The technical solutions in the embodiments of the present invention will be described clearly and completely below in conjunction with the accompanying drawings in the embodiments of the present invention.

[0023] See also Figure 1-5 The utility model provides a satellite common-view instrument with a supporting and stabilizing structure, including a satellite common-view instrument body 1, and also includes:

[0024] A circuit board is arranged inside the satellite common-view instrument body 1, and a communication port is also arranged on the front side of the satellite common-view instrument body 1, and the communication port is electrically connected to the circuit board inside the satellite common-view instrument body 1. A display screen 2 and a control button 3 are arranged on the left and right ends of the front side of the satellite common-view instrument body 1, respectively, and the display screen 2 and the control button 3 are electrically connected to the circuit board fixed inside the satellite common-view instrument body 1. The display screen 2 can display calibrated time data, and the control button 3 is used to adjust the display content of the display screen 2, so as to facilitate use;

[0025] The support components are evenly distributed at the bottom of the satellite common-view instrument body 1 and are used to support the satellite common-view instrument body 1. The support components include a storage slot 8 and a support rod 10. The storage slot 8 is evenly distributed at the bottom of the satellite common-view instrument body 1. The support rod 10 is rotatably connected to one side of the interior of the storage slot 8. An anti-skid pad 9 is fixed to the outside of the support rod 10, and the anti-skid pad 9 can contact the upper end surface of the placement table. The set support rod 10 can be rotated and opened from the inside of the storage slot 8. After the four groups of support rods 10 are tilted outward, the bottoms of the four groups of support rods 10 are in contact with the placement table, so as to support the satellite common-view instrument body 1. When the four groups of support rods 10 are rotated and stored in the storage slot 8, the set anti-skid pad 9 can contact with the placement table, which can increase the friction between the satellite common-view instrument body 1 and the placement table, making it more stable to place.

[0026] A shock absorbing component is arranged directly below the satellite common-view instrument body 1 and is used to absorb shock to the satellite common-view instrument body 1. The shock absorbing component includes a carrying tray 4 and a shock absorbing pad 5. The carrying tray 4 is arranged directly below the satellite common-view instrument body 1. The shock absorbing pad 5 is fixed to the bottom of the satellite common-view instrument body 1, and the bottom of the shock absorbing pad 5 is in contact with the placement table. A card slot 6 is evenly distributed at the central position of the upper end surface of the carrying tray 4, and a support rod body 10 can be carded inside the card slot 6. A limited circular groove 7 is arranged on one side of the lower end surface of the card slot 6, and the bottom end of the support rod body 10 can be embedded in the limited circular groove 7. Four groups of support rod bodies 10 When the storage slot 8 can be rotated and opened, the bottom of the four groups of support rods 10 can be embedded in the limiting circular groove 7, and the limiting circular groove 7 can limit the support rods 10, so that it is more stable during placement. At this time, the provided shock-absorbing pads 5 can reduce the impact of external vibration on the satellite common-view instrument body 1, and the four groups of support rods 10 can also be rotated and stored in the storage slot 8, and the support rods 10 can be clamped in the clamping slot 6. A variety of installation methods can be selected according to the external environment. At the same time, the impact of external vibration on the satellite common-view instrument body 1 can be reduced, and its service life can be extended, so that the device is more applicable and more convenient to use;

[0027] Working principle: First, a circuit board is arranged inside the satellite common-view instrument body 1, and a communication port is also arranged on the front side of the satellite common-view instrument body 1, and the communication port is electrically connected to the circuit board inside the satellite common-view instrument body 1. A display screen 2 and a control button 3 are arranged on the left and right ends of the front side of the satellite common-view instrument body 1, respectively, and the display screen 2 and the control button 3 are electrically connected to the circuit board fixed inside the satellite common-view instrument body 1. The display screen 2 can display the calibrated time data, and the control button 3 is used to adjust the display content of the display screen 2, so as to facilitate the use;

[0028] When in use, the support rod body 10 can be rotated and opened from the inside of the storage slot body 8. After the four groups of support rod bodies 10 are tilted outward, the bottoms of the four groups of support rod bodies 10 are in contact with the placement table, so as to support the satellite common-view instrument body 1. When the four groups of support rod bodies 10 are rotated and stored in the storage slot body 8, the anti-slip pads 9 can be in contact with the placement table, thereby increasing the friction between the satellite common-view instrument body 1 and the placement table, making it more stable to place.

[0029] In addition, when the four groups of support rod bodies 10 can be rotated and opened from the inside of the storage slot body 8, the bottom of the four groups of support rod bodies 10 can be embedded in the inside of the limiting circular groove 7. The limiting circular groove 7 can limit the support rod bodies 10 to make them more stable during the placement process. At this time, the set shock-absorbing pads 5 can reduce the impact of external vibrations on the satellite common-view instrument body 1. The four groups of support rod bodies 10 can also be rotated and stored in the inside of the storage slot body 8, and the support rod bodies 10 can be clamped in the inside of the clamping slot body 6. A variety of installation methods can be selected according to the external environment. At the same time, the impact of external vibrations on the satellite common-view instrument body 1 can be reduced, its service life can be extended, and the equipment can be more applicable and more convenient to use.

[0030] Although the present invention has been described in detail with reference to the aforementioned embodiments, those skilled in the art may still modify the technical solutions described in the aforementioned embodiments, or make equivalent substitutions for some of the technical features therein. Any modifications, equivalent substitutions, improvements, etc. made within the spirit and principles of the present invention shall be included in the protection scope of the present invention.

Claims

1. A satellite common-view instrument with a supporting and stabilizing structure, comprising a satellite common-view instrument body (1), characterized in that: Said A shock absorbing component is arranged directly below the satellite common-view instrument body (1) and is used to absorb shock to the satellite common-view instrument body (1); The support components are evenly distributed on the bottom of the satellite common-view instrument body (1) and are used to support the satellite common-view instrument body (1).

2. The satellite common-view instrument with a supporting and stabilizing structure according to claim 1, characterized in that: The support assembly comprises a storage slot body (8) and a support rod body (10); the storage slot body (8) is evenly distributed and opened at the bottom of the satellite common view instrument body (1); and the support rod body (10) is rotatably connected to one side of the interior of the storage slot body (8).

3. The satellite common-view instrument with a supporting and stabilizing structure according to claim 2, characterized in that: An anti-skid pad (9) is fixed on the outer side of the support rod body (10), and the anti-skid pad (9) can be in contact with the upper end surface of the placement table.

4. The satellite common-view instrument with a supporting and stabilizing structure according to claim 3, characterized in that: The shock absorbing assembly comprises a carrying tray (4) and a shock absorbing pad (5); the carrying tray (4) is arranged directly below the satellite common view instrument body (1); the shock absorbing pad (5) is fixed to the bottom of the satellite common view instrument body (1), and the bottom of the shock absorbing pad (5) is in contact with a placement table.

5. The satellite common-view instrument with a supporting and stabilizing structure according to claim 4, characterized in that: The central position of the upper end surface of the carrying tray (4) is evenly distributed with a snap-fit ​​groove body (6), and the support rod body (10) can be snap-fitted inside the snap-fit ​​groove body (6). A limiting circular groove (7) is provided on one side of the lower end surface inside the snap-fit ​​groove body (6), and the bottom end of the support rod body (10) can be embedded in the limiting circular groove (7).

6. The satellite common-view instrument with a supporting and stabilizing structure according to claim 1, characterized in that: A display screen (2) and an operating button (3) are respectively arranged at the front left end and the front right end of the satellite common-view instrument body (1), and the display screen (2) and the operating button (3) are electrically connected to a circuit board fixed inside the satellite common-view instrument body (1).

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