Portable satellite station

Abstract

The utility model provides a portable satellite station, and relates to the technical field of communication equipment, an upper cover module is detachably installed on a satellite alignment module through a buckle member, the satellite alignment module can rotate relative to an information processing module in use so as to adjust the orientation of an antenna assembly, and after use, the satellite alignment module can rotate relative to the information processing module so as to adjust the orientation of the antenna assembly. The satellite alignment module is clamped on the information processing module through the clamping component, rotation of the satellite alignment module relative to the information processing module is limited, the first antenna part and the second antenna part are detachably installed on the antenna main supporting part, antenna disassembly and assembly are convenient, the whole device is easy to unfold and fold, disassembly and assembly are convenient, and the antenna assembly and disassembly are convenient. The technical problems that in the prior art, a traditional portable satellite antenna is inconvenient to unfold, fold and store, and an integrated antenna is difficult to fold and store are solved.

Description

Technical Field

[0001] The utility model relates to the technical field of communication equipment, in particular to a portable satellite station. Background Art

[0002] The existing technical solutions are based on the current status of existing communication equipment, while ensuring reliable communication at any time, any place and any environment to cope with major emergencies, sudden natural disasters and other emergency tasks.

[0003] The system can realize three major functions including image transmission, voice transmission and data communication through a portable satellite antenna and a remote command center, meeting the needs of video conferencing, images, sound, data and telephone between the command center station and the portable satellite station.

[0004] However, conventional portable satellite antennas are inconvenient to unfold and fold, and integrated antennas are also difficult to fold and store. Utility Model Content

[0005] The utility model aims to provide a portable satellite station to alleviate the technical problems in the prior art that the conventional portable satellite antenna is inconvenient to unfold and fold, and the integrated antenna is also difficult to fold and store.

[0006] The portable satellite station provided by the utility model comprises: an upper cover module, a satellite alignment module, an information processing module, a power supply module and an antenna assembly;

[0007] The upper cover module, the satellite alignment module, the information processing module and the power module are stacked from top to bottom;

[0008] The upper cover module is detachably connected to the star alignment module via a snap member;

[0009] The star alignment module is configured to be able to rotate relative to the information processing module with a direction perpendicular to the information processing module as an axis;

[0010] The information processing module is provided with a clamping member, and the clamping member is used to connect with the star alignment module to limit the star alignment module from rotating relative to the information processing module;

[0011] The antenna assembly includes an antenna main support portion, a first antenna portion, and a second antenna portion;

[0012] The antenna main support part is rotatably connected to the satellite alignment module, and the first antenna part and the second antenna part are respectively detachably mounted on the antenna main support part.

[0013] In an alternative embodiment,

[0014] The clamping member comprises a fixed base and a rotating hook;

[0015] The fixed base is arranged on the information processing module, and the rotating hook is rotatably connected to the fixed base;

[0016] The star alignment module is provided with a protrusion, and the rotating hook is provided with a slot. When the rotating hook rotates until the protrusion extends into the slot, the star alignment module is restricted from rotating relative to the information processing module.

[0017] In an alternative embodiment,

[0018] A plurality of locking components are arranged along the edge of the antenna main support portion, and the first antenna portion and the second antenna portion are detachably connected to the antenna main support portion through the plurality of locking components.

[0019] In an alternative embodiment,

[0020] The portable satellite station also includes an angle adjustment component;

[0021] The angle adjustment component is disposed on the satellite alignment module, and the angle adjustment component is configured to be able to drive the antenna main support portion to rotate relative to the satellite alignment module to adjust the opening and closing angle of the antenna main support portion.

[0022] In an alternative embodiment,

[0023] The angle adjustment component includes a knob, a transmission component and a connecting component;

[0024] The transmission component comprises a transmission part and a driving part which are transmission-connected to each other;

[0025] The knob is in transmission connection with the transmission part, and the driving part is connected with the antenna main support part through the connecting member;

[0026] When the knob is turned, the transmission part and the driving part drive the connecting member and the antenna main supporting part to rotate relative to the satellite alignment module.

[0027] In an alternative embodiment,

[0028] The information processing module is rotatably connected with a rotating part, and the angle adjustment member is connected to the rotating part, so that the angle adjustment member, the star alignment module and the antenna main support part rotate around the rotating part to adjust the direction of the antenna main support part.

[0029] In an alternative embodiment,

[0030] The information processing module is provided with angle scale lines;

[0031] An angle indicating line is arranged on the rotating part.

[0032] In an alternative embodiment,

[0033] The information processing module is rotatably connected to a support leg.

[0034] In an alternative embodiment,

[0035] The power module is provided with a locking and fixing module, and the locking and fixing module is used to clamp the supporting leg onto the power module.

[0036] In an alternative embodiment,

[0037] The locking and fixing module includes a locking base and a locking rotating block;

[0038] The locking base is fixed on the power module, and the locking rotating block is rotatably connected to the locking base;

[0039] The supporting leg is provided with a locking hole, and the locking rotating block passes through the locking hole and then rotates to clamp the supporting leg.

[0040] The portable satellite station provided by the utility model has an upper cover module detachably mounted on the star-pointing module by means of a snap-fit ​​component. When in use, the star-pointing module can rotate relative to the information processing module to adjust the orientation of the antenna assembly. After use, the star-pointing module is snap-fitted to the information processing module by means of the snap-fit ​​component to limit the rotation of the star-pointing module relative to the information processing module. In addition, the first antenna part and the second antenna part are detachably mounted on the antenna main support part, which is convenient for disassembly and assembly of the antenna. The overall device has simple deployment and folding and storage operations and is convenient for disassembly and assembly, which alleviates the technical problem in the prior art that the traditional portable satellite antenna is inconvenient to deploy and fold, and the integrated antenna is also difficult to fold and store. BRIEF DESCRIPTION OF THE DRAWINGS

[0041] In order to more clearly illustrate the specific implementation methods of the utility model or the technical solutions in the prior art, the drawings required for use in the specific implementation methods or the description of the prior art will be briefly introduced below. Obviously, the drawings described below are some implementation methods of the utility model. For ordinary technicians in this field, other drawings can be obtained based on these drawings without paying creative work.

[0042] Figure 1 An exploded view of the overall structure of a portable satellite station provided by an embodiment of the utility model;

[0043] Figure 2 An exploded view of the overall structure of the portable satellite station provided by the embodiment of the utility model from another perspective;

[0044] Figure 3 A schematic diagram of the installation structure of the clamping member in the portable satellite station provided by the embodiment of the utility model;

[0045] Figure 4 A schematic diagram of the structure of a portable satellite station provided by an embodiment of the utility model in a folded and stored state;

[0046] Figure 5 This is a schematic diagram of the enlarged structure of the angle adjustment component in the portable satellite station provided by the embodiment of the utility model;

[0047] Figure 6 This is a schematic diagram of the enlarged structure of the rotating part of the portable satellite station provided in the embodiment of the utility model;

[0048] Figure 7 A schematic diagram of the installation structure of a locking and fixing module in a portable satellite station provided in an embodiment of the utility model.

[0049] Icons: 10- snap-fit ​​component; 20- snap-fit ​​component; 21-fixed base; 22-rotating hook; 30-locking component; 40-locking and fixing module; 41-locking base; 42-locking rotating block; 100-upper cover module; 200-satellite module; 210-bump; 300-information processing module; 310-rotating part; 311-angle indicator line; 320-angle scale line; 400-power module; 500-antenna assembly; 510-antenna main support part; 520-first antenna part; 530-second antenna part; 600-angle adjustment component; 610-knob; 620-transmission component; 630-connecting component; 700-leg; 710-locking hole; 800-feed system. DETAILED DESCRIPTION

[0050] The technical solution of the utility model will be described clearly and completely below in conjunction with the accompanying drawings. Obviously, the described embodiments are part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments of 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.

[0051] In the description of the present invention, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", etc., indicating the orientation or positional relationship, are based on the orientation or positional relationship shown in the drawings, and are only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore cannot be understood as limiting the present invention. In addition, the terms "first", "second", and "third" are used for descriptive purposes only, and cannot be understood as indicating or implying relative importance.

[0052] In the description of the present invention, it should be noted that, unless otherwise clearly specified and limited, the terms "installation", "connection" and "connection" should be understood in a broad sense, for example, it can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be a direct connection, or it can be indirectly connected through an intermediate medium, or it can be the internal communication of two components. For ordinary technicians in this field, the specific meanings of the above terms in the present invention can be understood according to specific circumstances.

[0053] The specific implementation of the present invention is described in detail below in conjunction with the accompanying drawings. It should be understood that the specific implementation described here is only used to illustrate and explain the present invention, and is not used to limit the present invention.

[0054] like Figure 1 As shown, the portable satellite station provided in this embodiment includes: an upper cover module 100, a satellite alignment module 200, an information processing module 300, a power module 400 and an antenna assembly 500; the upper cover module 100, the satellite alignment module 200, the information processing module 300 and the power module 400 are stacked from top to bottom.

[0055] like Figure 4 As shown, the upper cover module 100 and the star alignment module 200 are detachably connected via a snap component 10. The snap component 10 can be specifically configured as a luggage lock. Any existing snap component 10 that can detachably connect the upper cover module 100 and the star alignment module 200 is acceptable. Therefore, the specific structure of the snap component 10 will not be repeated.

[0056] In addition, the feed system 800 is detachably mounted on the star alignment module 200 , and a bracket is provided on the star alignment module 200 . When in use, the feed system 800 is fixed to the bracket by bolts.

[0057] like Figure 2As shown, the antenna assembly 500 includes an antenna main support portion 510, a first antenna portion 520 and a second antenna portion 530; the antenna main support portion 510 can be rotatably connected to the satellite module 200 so that the antenna main support portion 510 can adjust the opening and closing angle, and the first antenna portion 520 and the second antenna portion 530 are respectively detachably installed on the antenna main support portion 510. When in use, the first antenna portion 520 and the second antenna portion 530 are installed on the antenna main support portion 510. When use is completed and storage is required, the first antenna portion 520 and the second antenna portion 530 can be removed from the antenna main support portion 510.

[0058] In an optional embodiment, a plurality of locking components 30 are provided along the edge of the antenna main support portion 510. The locking components 30 may be specifically configured into a variety of types, such as luggage locks, butterfly locks, military locks, aluminum box locks, and aviation box locks. By configuring the locking components 30, quick release of the first antenna portion 520 and the second antenna portion 530 from the antenna main support portion 510 is achieved.

[0059] The alignment module 200 is configured to be rotatable relative to the information processing module 300 about a direction perpendicular to the information processing module 300 , and because the antenna main support portion 510 can be mounted on the alignment module 200 , the orientation of the entire antenna assembly 500 can be adjusted.

[0060] The information processing module 300 is provided with a snap-fitting component 20. When the entire device needs to be folded and stored, the snap-fitting component 20 is connected to the star alignment module 200 to limit the star alignment module 200 from rotating relative to the information processing module 300, and snap-fits the star alignment module 200 to the information processing module 300.

[0061] Specifically, if Figure 3 As shown, the clamping component 20 includes a fixed base 21 and a rotating hook 22; the fixed base 21 is arranged on the information processing module 300, and the fixed base 21 is fixed to the outer shell of the information processing module 300 by screws, and the rotating hook 22 is rotatably connected to the fixed base 21, that is, the rotating hook 22 is connected to the fixed base 21 through a rotating shaft; a protrusion 210 is arranged on the star alignment module 200, and a slot is arranged on the rotating hook 22. When the rotating hook 22 rotates until the protrusion 210 extends into the slot, the star alignment module 200 can be limited from rotating relative to the information processing module 300, thereby realizing the clamping connection between the star alignment module 200 and the information processing module 300.

[0062] In an optional embodiment, if Figure 5As shown, the portable satellite station also includes an angle adjustment component 600; the angle adjustment component 600 is arranged on the satellite alignment module 200, and the angle adjustment component 600 is configured to be able to drive the antenna main support part 510 to rotate relative to the satellite alignment module 200 to adjust the opening and closing angle of the antenna main support part 510. When in use, the antenna main support part 510 is first installed on the angle adjustment component 600, and then the angle of the antenna main support part 510 is adjusted using the angle adjustment component 600 to perform the satellite alignment operation.

[0063] Specifically, the angle adjustment component 600 includes a knob 610, a transmission component 620 and a connecting component 630; the transmission component 620 includes a transmission part and a driving part that are transmission-connected to each other. The transmission part can be specifically set to a worm structure, and the driving part can be specifically set to a worm gear structure. The knob 610 is transmission-connected to the transmission part, that is, the knob 610 is installed on the worm, and the rotation of the knob 610 drives the worm to rotate along its own axis. The worm is meshed with the worm gear, and the rotation of the worm drives the worm gear to rotate. The worm gear is connected to the antenna main support part 510 through the connecting component 630. The connecting component 630 specifically includes a connecting shaft and a connecting plate. The connecting shaft is connected to the worm gear along the axis of the worm gear. The connecting plate and the connecting shaft are an integral structure. The end of the antenna main support part 510 is fixed to the connecting plate by bolts. The rotation of the worm gear drives the connecting shaft and the connecting plate to rotate together. Since the antenna main support part 510 is installed on the connecting plate, the antenna main support part 510 can be driven to rotate relative to the satellite module 200 to adjust the antenna angle.

[0064] In an optional embodiment, if Figure 6 As shown, the information processing module 300 is rotatably connected with a rotating part 310. Specifically, a through hole is opened on the outer shell of the information processing module 300, and the end of the rotating part 310 passes through the through hole and extends into the interior of the information processing module 300, and the rotating part 310 can rotate along its own axis through a bearing structure. The angle adjustment member 600 is connected to the rotating part 310, so that the angle adjustment member 600, the satellite module 200 and the antenna main support part 510 rotate around the rotating part 310 to adjust the direction of the antenna main support part 510.

[0065] In an optional embodiment, the information processing module 300 is provided with an angle scale line 320; the rotating part 310 is provided with an angle indication line 311, and the orientation of the antenna main support part 510 can be accurately adjusted by the cooperation of the angle scale line 320 and the angle indication line 311.

[0066] In an optional embodiment, the information processing module 300 is rotatably connected to a leg 700. When the portable satellite station is unfolded and used, the leg 700 rotates in a direction away from the information processing module 300. In addition, two legs 700 are provided, and the two legs 700 are respectively located on both sides of the power module 400, and both are rotatably connected to the information processing module 300.

[0067] In an optional implementation, a locking and fixing module 40 is provided on the power module 400 , and the locking and fixing module 40 is used to clamp the supporting leg 700 on the power module 400 .

[0068] Specifically, if Figure 7 As shown, the locking and fixing module 40 includes a locking base 41 and a locking rotating block 42; the locking base 41 is fixed on the power module 400, and the locking rotating block 42 is rotatably connected to the locking base 41, so that the locking rotating block 42 can rotate around its own axis; a locking hole 710 is provided on the leg 700, and the locking rotating block 42 rotates after passing through the locking hole 710, and the locking rotating block 42 is stuck, thereby locking the leg 700.

[0069] The portable satellite station provided in this embodiment uses a snap-fit ​​component 10 to detachably mount the upper cover module 100 on the satellite alignment module 200. When in use, the satellite alignment module 200 can rotate relative to the information processing module 300 to adjust the orientation of the antenna assembly 500. After use, the satellite alignment module 200 is snap-fitted to the information processing module 300 by the snap-fit ​​component 20 to limit the rotation of the satellite alignment module 200 relative to the information processing module 300, and the first antenna portion 520 and the second antenna portion 530 are detachably mounted on the antenna main support portion 510, so as to facilitate the disassembly and assembly of the antenna. The overall device is simple to deploy and fold for storage, and is easy to disassemble and assemble, thereby alleviating the technical problem in the prior art that the conventional portable satellite antenna is inconvenient to deploy and fold for storage, and the integrated antenna is also difficult to fold and store.

[0070] Finally, it should be noted that the above embodiments are only used to illustrate the technical solution of the utility model, rather than to limit it. Although the utility model has been described in detail with reference to the aforementioned embodiments, ordinary technicians in this field should understand that they can still modify the technical solutions recorded in the aforementioned embodiments, or replace some or all of the technical features therein with equivalents. However, these modifications or replacements do not make the essence of the corresponding technical solution deviate from the scope of the technical solution of the embodiments of the utility model.

Claims

1. A portable satellite station, characterized in that: include: An upper cover module (100), a satellite alignment module (200), an information processing module (300), a power module (400) and an antenna assembly (500); The upper cover module (100), the satellite alignment module (200), the information processing module (300) and the power supply module (400) are stacked from top to bottom; The upper cover module (100) and the star alignment module (200) are detachably connected via a snap-fit ​​component (10); The star alignment module (200) is configured to be rotatable relative to the information processing module (300) with a direction perpendicular to the information processing module (300) as an axis; The information processing module (300) is provided with a clamping component (20), and the clamping component (20) is used to connect with the star alignment module (200) to limit the star alignment module (200) from rotating relative to the information processing module (300); The antenna assembly (500) comprises an antenna main support portion (510), a first antenna portion (520) and a second antenna portion (530); The antenna main support part (510) can be rotatably connected to the satellite alignment module (200), and the first antenna part (520) and the second antenna part (530) are respectively detachably mounted on the antenna main support part (510).

2. The portable satellite station according to claim 1, characterized in that: The clamping member (20) comprises a fixed base (21) and a rotating clamping hook (22); The fixed base (21) is arranged on the information processing module (300), and the rotating hook (22) is rotatably connected to the fixed base (21); The star alignment module (200) is provided with a protrusion (210), and the rotating hook (22) is provided with a slot. When the rotating hook (22) rotates until the protrusion (210) extends into the slot, the star alignment module (200) is restricted from rotating relative to the information processing module (300).

3. The portable satellite station according to claim 1, characterized in that: A plurality of locking components (30) are arranged along the edge of the antenna main support part (510), and the first antenna part (520) and the second antenna part (530) are detachably connected to the antenna main support part (510) via the plurality of locking components (30).

4. The portable satellite station according to any one of claims 1 to 3, characterized in that: The portable satellite station also includes an angle adjustment component (600); The angle adjustment component (600) is disposed on the satellite alignment module (200), and the angle adjustment component (600) is configured to be able to drive the antenna main support part (510) to rotate relative to the satellite alignment module (200) so as to adjust the opening and closing angle of the antenna main support part (510).

5. The portable satellite station according to claim 4, characterized in that: The angle adjustment component (600) comprises a knob (610), a transmission component (620) and a connecting component (630); The transmission component (620) comprises a transmission part and a driving part which are transmission-connected to each other; The knob (610) is in transmission connection with the transmission part, and the driving part is connected to the antenna main support part (510) via the connecting member (630); When the knob (610) is turned, the transmission part and the driving part drive the connecting member (630) and the antenna main support part (510) to rotate relative to the satellite alignment module (200).

6. The portable satellite station according to claim 4, characterized in that: The information processing module (300) is rotatably connected to a rotating part (310), and the angle adjustment member (600) is connected to the rotating part (310), so that the angle adjustment member (600), the satellite alignment module (200) and the antenna main support part (510) rotate around the rotating part (310) to adjust the orientation of the antenna main support part (510).

7. The portable satellite station according to claim 6, characterized in that: The information processing module (300) is provided with angle scale lines (320); The rotating part (310) is provided with an angle indicating line (311).

8. The portable satellite station according to claim 1, characterized in that: The information processing module (300) is rotatably connected to a support leg (700).

9. The portable satellite station according to claim 8, characterized in that: The power module (400) is provided with a locking and fixing module (40), and the locking and fixing module (40) is used to clamp the supporting leg (700) onto the power module (400).

10. The portable satellite station according to claim 9, characterized in that: The locking and fixing module (40) comprises a locking base (41) and a locking rotating block (42); The locking base (41) is fixed on the power module (400), and the locking rotating block (42) is rotatably connected to the locking base (41); The supporting leg (700) is provided with a locking hole (710), and the locking rotating block (42) passes through the locking hole (710) and then rotates to be clamped with the supporting leg (700).

Images