CN217282917U - Portable satellite station - Google Patents
Portable satellite station Download PDFInfo
- Publication number
- CN217282917U CN217282917U CN202221343641.3U CN202221343641U CN217282917U CN 217282917 U CN217282917 U CN 217282917U CN 202221343641 U CN202221343641 U CN 202221343641U CN 217282917 U CN217282917 U CN 217282917U
- Authority
- CN
- China
- Prior art keywords
- satellite station
- fixedly connected
- sliding
- portable satellite
- plates
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Images
Classifications
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02D—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN INFORMATION AND COMMUNICATION TECHNOLOGIES [ICT], I.E. INFORMATION AND COMMUNICATION TECHNOLOGIES AIMING AT THE REDUCTION OF THEIR OWN ENERGY USE
- Y02D30/00—Reducing energy consumption in communication networks
- Y02D30/70—Reducing energy consumption in communication networks in wireless communication networks
Landscapes
- Purses, Travelling Bags, Baskets, Or Suitcases (AREA)
Abstract
The utility model relates to a satellite station technical field especially relates to portable satellite station, has solved among the prior art because be hemispherical structure, and the receiver in the tradition all is monolithic structure simultaneously, and this will cause to occupy very big space in the transportation in later stage, and is not convenient for carry, and then has caused the problem that satellite station transported the difficulty, need adopt large-scale transport vechicle just can load the problem. Portable satellite station, including the main part, bolt fixedly connected with carrier block is passed through to the bottom of main part, and bolt fixedly connected with bracing piece is passed through to the bottom of main part, the bottom fixedly connected with underframe of bracing piece, and the equal sliding connection in inboard both sides of underframe has the bottom plate. The utility model discloses in the mode of proposing, through carrying out the aggregate erection with all loading boards and compoboards, be convenient for dismantle simultaneously, and then can make the receiver when transporting, can dismantle, be convenient for transport, occupation space is little.
Description
Technical Field
The utility model relates to a satellite station technical field especially relates to portable satellite station.
Background
The small satellite station consists of a plurality of small equipment boxes and detachable antennas, can be carried by common vehicles (airplanes, trains, automobiles, ships and the like) or manpower, is quickly and flexibly arranged, and realizes the mobile communication station with the functions of remote transmission, short-range coverage and wireless access (without wireless cluster phones) of emergency communication services, wherein the mobile communication station comprises a receiving device which is of a hemispherical structure.
Receiver on the small satellite station among the prior art, owing to be hemispherical structure, receiver in the tradition all is monolithic structure simultaneously, and this will cause and occupy very big space in the transportation in later stage, is not convenient for carry, and then has caused the problem of satellite station transportation difficulty, needs to adopt large-scale transport vechicle just can load, seems very inconvenient, so need portable satellite station urgently.
SUMMERY OF THE UTILITY MODEL
The utility model aims at providing a portable satellite station has solved among the prior art because be hemispherical structure, and the receiver in the tradition all is monolithic structure simultaneously, and this will cause to occupy very big space in the transportation in later stage, and is not convenient for carry, and then has caused the problem that satellite station transportation difficulty, need adopt large-scale transport vechicle just can load the problem.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
the portable satellite station comprises a main body, the bottom of the main body is fixedly connected with a bearing block through a bolt, the bottom of the main body is fixedly connected with a supporting rod through a bolt, the bottom end of the supporting rod is fixedly connected with a bottom frame, and the two sides of the inner side of the bottom frame are both connected with bottom plates in a sliding way, one end of each of the two bottom plates penetrates through the side wall of the bottom frame, and the bottoms of the extending parts of the two bottom plates can be detachably connected with supporting legs, a plurality of bearing grooves are arranged on the outer sides of the bearing blocks along the circumferential direction, the inner sides of all the bearing grooves are rotatably connected with rotating rods, and one side of all the rotating rods is fixedly connected with a connecting block, the top of all the connecting blocks is fixedly connected with a bearing plate, and both sides of all the bearing plates are provided with sliding grooves, and all be equipped with the compoboard between adjacent two in all loading boards, sliding connection between the both sides of compoboard all pass through sliding tray and two adjacent loading boards.
Preferably, one side of all loading boards all is equipped with the gag lever post, and the lateral wall of loading board is run through to the one end of gag lever post to the extension of gag lever post is located the inboard of sliding tray, wherein on the compoboard with all set up the spacing groove that the cooperation gag lever post used on the inner wall of sliding tray, the part that the gag lever post is located the sliding tray outside is overlapped and is equipped with extension spring, and elastic connection between the lateral wall of extension spring and loading board is passed through to the one end of gag lever post.
Preferably, the both sides of all compoboards all fixedly connected with sliding block, and sliding connection between the outer wall of sliding tray and loading board is passed through to the sliding block.
Preferably, the top and the bottom of two bottom plates are fixedly connected with sliding blocks, and the sliding blocks are connected with the inner wall of the bottom frame through sliding rails in a sliding mode.
Preferably, the bottom that two bottom plates are located the underframe outside portion has all seted up the notch, and the inboard all detachable of two notches is connected with the supporting leg.
Preferably, one side of two bottom plates all is equipped with the inserted bar, and the slot that the cooperation inserted bar was used is all seted up to one side that the bottom plate is close to the notch and upper portion one side of supporting leg.
The utility model discloses possess following beneficial effect at least:
when the portable satellite station is used, the support rod and the main body are firstly installed through the bolt, then the receiver is assembled, namely all the bearing plates and all the combination plates are assembled, the combination plates slide in along between the two bearing plates, and then the combination plates are limited, the rest combination plates and the bearing plates are sequentially assembled and installed according to the principle, finally the bearing block and the main body are installed, when the satellite station is carried, only all the combination plates and the bearing plates are needed to be disassembled, then the support rod is disassembled, compared with the prior art, the receiver in the prior art which is in a hemispherical structure is in an integral structure, the receiver in the prior art occupies a large space in later transportation, is inconvenient to carry, and further causes the problem of difficult transportation of the satellite station, need adopt large-scale transport vechicle just can load the problem, the utility model discloses in the mode of proposing, through carrying out the aggregate erection with all loading boards and compoboard, be convenient for dismantle simultaneously, and then can make the receiver when transporting, can dismantle, be convenient for transport, occupation space is little.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings required to be used in the description of the embodiments are briefly introduced below, and it is obvious that the drawings in the following description are some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without any creative effort.
FIG. 1 is a schematic view of the overall structure of the present invention;
FIG. 2 is a schematic top view of the combination board and the loading board of the present invention;
FIG. 3 is a schematic view of the enlarged structure of the area B of the present invention;
fig. 4 is a schematic view of the a region enlarged structure of the present invention.
In the figure: 1. a main body; 2. a support bar; 3. a bottom frame; 4. a slider; 5. a slide rail; 6. a bearing groove; 7. rotating the rod; 8. connecting blocks; 9. a carrier plate; 10. a sliding groove; 11. a composition board; 12. a slider; 13. a limiting rod; 14. an extension spring; 15. a limiting groove; 16. a base plate; 17. supporting legs; 18. inserting a rod; 19. a slot; 20. a bearing block; 21. a notch.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more clearly understood, the present invention is further described in detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the invention and are not intended to limit the invention.
Referring to fig. 1 to 3, the portable satellite station includes a main body 1, a bearing block 20 fixedly connected to the bottom of the main body 1 through bolts, a support rod 2 fixedly connected to the bottom of the main body 1 through bolts, a bottom frame 3 fixedly connected to the bottom end of the support rod 2, bottom plates 16 slidably connected to both sides of the inner side of the bottom frame 3, one ends of the two bottom plates 16 penetrating the side wall of the bottom frame 3, support legs 17 detachably connected to the bottom of the extending portion of the two bottom plates 16, a plurality of bearing grooves 6 formed in the outer side of the bearing block 20 along the circumferential direction, rotating rods 7 rotatably connected to the inner sides of all the bearing grooves 6, connecting blocks 8 fixedly connected to one sides of all the rotating rods 7, bearing plates 9 fixedly connected to the tops of all the connecting blocks 8, sliding grooves 10 formed in both sides of all the bearing plates 9, and a combination plate 11 provided between adjacent two of all the bearing plates 9, sliding connection between sliding tray 10 and two adjacent loading boards 9 is all passed through to the both sides of compoboard 11, and is concrete, through carrying out built-up mounting with all loading boards 9 and compoboard 11, is convenient for dismantle simultaneously, and then can make the receiver when transporting, can dismantle, is convenient for transport, and occupation space is little.
The scheme has the following working processes:
the utility model discloses when well portable satellite station carries out the use, at first install bracing piece 2 and main part 1 through the bolt, assemble the receiver after that, be about to all loading boards 9 and all compoboards 11 and assemble, slide into compoboard 11 between two loading boards 9, carry out compoboard 11 spacing again can, all the other compoboards 11 and loading board 9 carry out the composite mounting work in proper order with this principle, install carrier block 20 and main part 1 at last can, when carrying out the carrying of satellite station, only need with all compoboards 11 with loading board 9 dismantle can, dismantle bracing piece 2 again.
According to the working process, the following steps are known:
through carrying out aggregate erection with all loading boards 9 and compoboard 11, be convenient for dismantle simultaneously, and then can make the receiver when transporting, can dismantle, be convenient for transport, occupation space is little.
Further, one side of all loading boards 9 all is equipped with gag lever post 13, and the lateral wall of loading board 9 is run through to the one end of gag lever post 13, and the extending part of gag lever post 13 is located the inboard of sliding tray 10, wherein all offer the spacing groove 15 that cooperation gag lever post 13 used on the compoboard 11 with the inner wall of sliding tray 10, the cover is equipped with extension spring 14 on the part that gag lever post 13 is located the sliding tray 10 outside, and elastic connection between the lateral wall of extension spring 14 and loading board 9 is passed through to the one end of gag lever post 13, and is concrete, utilize gag lever post 13 and spacing groove 15 to peg graft, and then can carry on spacingly to compoboard 11.
Further, the equal fixedly connected with sliding block 12 in both sides of all compoboards 11, and sliding connection between sliding block 12 and the outer wall of loading board 9 through sliding tray 10, it is concrete, utilize sliding block 12 to slide in sliding tray 10, can be convenient for dock the installation to compoboards 11 and loading board 9.
Further, the top and the bottom of two bottom plates 16 are fixedly connected with sliders 4, and the sliders 4 are slidably connected with the inner wall of the bottom frame 3 through slide rails 5, specifically, the sliders 4 are utilized to slide in the slide rails 5, and then the bottom plates 16 can be moved conveniently.
Further, two bottom plates 16 are located the bottom of the outer portion of underframe 3 and have all seted up notch 21, and the inboard all detachable connection of two notch 21 has supporting leg 17.
Further, one side of two bottom plates 16 all is equipped with inserted bar 18, and bottom plate 16 is close to slot 21 one side and the upper portion one side of supporting leg 17 and all has seted up the slot 19 that cooperation inserted bar 18 used, and is concrete, utilizes inserted bar 18 and slot 19 to peg graft, can be convenient for fix supporting leg 17.
In conclusion: utilize gag lever post 13 and spacing groove 15 to peg graft, and then can carry on spacingly to combination board 11, utilize sliding block 12 to slide in sliding tray 10, can be convenient for dock the installation to combination board 11 and loading board 9, utilize slider 4 to slide in slide rail 5, and then can be convenient for remove bottom plate 16, utilize inserted bar 18 and slot 19 to peg graft, can be convenient for fix supporting leg 17.
The foregoing shows and describes the general principles, essential features, and advantages of the invention. It will be understood by those skilled in the art that the present invention is not limited to the above embodiments, and that the principles of the present invention may be applied to any other embodiment without departing from the spirit and scope of the present invention. The scope of the invention is defined by the appended claims and equivalents thereof.
Claims (8)
1. Portable satellite station, including main part (1), the bottom of main part (1) is through bolt fixedly connected with carrier block (20), its characterized in that, the bottom of main part (1) is through bolt fixedly connected with bracing piece (2), the bottom fixedly connected with underframe (3) of bracing piece (2), and the inboard both sides of underframe (3) all sliding connection have bottom plate (16), two the one end of bottom plate (16) all runs through the lateral wall of underframe (3), and the bottom of the extension of two bottom plates (16) all can be dismantled and be connected with supporting leg (17), a plurality of bearing groove (6) have been seted up along the circumferencial direction in the outside of carrier block (20), and the inboard of all bearing groove (6) all rotates and is connected with dwang (7), and one side of all dwang (7) all fixedly connected with connecting block (8), all the top of connecting block (8) all fixedly connected with carrier board (9), and sliding grooves (10) have all been seted up to the both sides of all loading boards (9) to all loading boards (9) all are equipped with compoboard (11) between adjacent two, sliding connection between sliding grooves (10) and two adjacent loading boards (9) is all passed through to the both sides of compoboard (11).
2. The portable satellite station as claimed in claim 1, characterized in that all the carrying plates (9) are provided with a stopper rod (13) on one side, and one end of the stopper rod (13) penetrates the side wall of the carrying plate (9), and the extension of the stopper rod (13) is located inside the sliding groove (10).
3. The portable satellite station as claimed in claim 1, wherein sliding blocks (12) are fixedly connected to both sides of all the combination boards (11), and the sliding blocks (12) are slidably connected to the outer wall of the bearing board (9) through sliding grooves (10).
4. The portable satellite station according to claim 1, characterized in that the two bottom plates (16) are fixedly connected with sliding blocks (4) at the top and the bottom, and the sliding blocks (4) are slidably connected with the inner wall of the bottom frame (3) through sliding rails (5).
5. A portable satellite station according to claim 1, wherein the two bottom plates (16) are provided with notches (21) at the bottom of the outer side of the bottom frame (3), and the inner sides of the two notches (21) are detachably connected with the supporting legs (17).
6. A portable satellite station as claimed in claim 5, wherein the two base plates (16) are provided with an insert rod (18) on one side, and the base plates (16) are provided with a slot (19) on one side close to the slot (21) and one side of the upper part of the support leg (17) for cooperating with the insert rod (18).
7. The portable satellite station as claimed in claim 2, wherein a portion of the stopper rod (13) located outside the sliding groove (10) is sleeved with a tension spring (14), and one end of the stopper rod (13) is elastically connected to the side wall of the bearing plate (9) through the tension spring (14).
8. The portable satellite station of claim 2, wherein the combination plate (11) and the inner wall of the sliding groove (10) are provided with limiting grooves (15) used for matching with the limiting rods (13).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202221343641.3U CN217282917U (en) | 2022-05-31 | 2022-05-31 | Portable satellite station |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202221343641.3U CN217282917U (en) | 2022-05-31 | 2022-05-31 | Portable satellite station |
Publications (1)
Publication Number | Publication Date |
---|---|
CN217282917U true CN217282917U (en) | 2022-08-23 |
Family
ID=82887821
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202221343641.3U Active CN217282917U (en) | 2022-05-31 | 2022-05-31 | Portable satellite station |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN217282917U (en) |
-
2022
- 2022-05-31 CN CN202221343641.3U patent/CN217282917U/en active Active
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN103026060B (en) | For the system and method for handling wind turbine tower sections | |
CN210952524U (en) | Movable rocket launching cradle and rocket launching vehicle | |
CN201206342Y (en) | Rapid integration communication device | |
CN217282917U (en) | Portable satellite station | |
CN103640862B (en) | The transportation system of electrical equipment spare part | |
CN107554704B (en) | Offshore comprehensive supply system | |
CN111572814A (en) | Configuration and assembly method of ultra-large type assembled satellite platform of static orbit | |
CN102409877B (en) | Fast communication base station | |
CN207944728U (en) | The circle haul of platen installation is seen for venue | |
CN103600681B (en) | A kind of full automaticity dormitory car | |
CN211709846U (en) | Secondary foaming production system for refrigerated container | |
CN216888281U (en) | Fixing device of container energy storage module and container | |
CN110154859A (en) | A kind of logistics bedding storage formula transport vehicle | |
CN212605763U (en) | Cargo carrying device for passenger cabin cargo carrying system | |
CN201873912U (en) | Support for transporting four-layer steel rail | |
CN116202383B (en) | Ammunition frame | |
CN110861249B (en) | Secondary foaming production system and production method for frozen container | |
CN202299519U (en) | Quick communication base station | |
CN219728013U (en) | Slat handling equipment | |
CN108100503B (en) | Vehicle container loading method | |
CN212705375U (en) | Assembly line | |
CN215187404U (en) | Device for testing wireless network performance of LTE-M system | |
CN205355231U (en) | Portable satellite communications antenna | |
CN213898177U (en) | Construction is with platform of unloading | |
CN221074328U (en) | Prefabricated rail top air duct |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
GR01 | Patent grant | ||
GR01 | Patent grant |