CN210235913U - Satellite portable station containing box - Google Patents
Satellite portable station containing box Download PDFInfo
- Publication number
- CN210235913U CN210235913U CN201920774722.0U CN201920774722U CN210235913U CN 210235913 U CN210235913 U CN 210235913U CN 201920774722 U CN201920774722 U CN 201920774722U CN 210235913 U CN210235913 U CN 210235913U
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- Prior art keywords
- satellite
- containing box
- portable station
- storage box
- box
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Abstract
The utility model belongs to the technical field of radio transmission, a portable station containing box of satellite is disclosed, including the containing box, the satellite radar subassembly is equipped with in the containing box, and containing box circumference lateral wall rotates and is connected with a plurality of landing legs, and containing box outer wall terminal surface is opened there is the circular slot, and the circular slot internal rotation is connected with the disc, and the disc top surface can be dismantled and be connected with the radar subassembly. An object of the utility model is to provide a portable station containing box of satellite to solve the portable station base of satellite and be not convenient for place the technical problem in the containing box.
Description
Technical Field
The utility model belongs to the technical field of radio transmission.
Background
The satellite communication has an irreplaceable effect in the aspect of emergency communication, but the traditional satellite communication is heavy by several tons, is difficult to carry and complex to operate, and a general vehicle-mounted satellite communication system is relatively large in size, weighs more than 50 kilograms, cannot be carried by a person and greatly limits the application occasions. Accordingly, portable satellite communication stations have been produced, and the main trend of future development of portable satellite communication stations is toward miniaturization and portability with light weight.
To ensure the stability of the use of the satellite portable station, the satellite portable station usually needs to be additionally provided with a base with larger volume and heavier weight to ensure balance. However, such a base is bulky, and therefore, it is difficult to put the satellite radar module in the storage box together with the base.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a portable station containing box of satellite to solve the portable station base of satellite and be not convenient for place the technical problem in the containing box.
In order to achieve the purpose, the utility model discloses a basic scheme provides a portable station containing box of satellite, including the containing box, the satellite radar subassembly is equipped with in the containing box, and containing box circumference lateral wall rotates and is connected with a plurality of landing legs, and containing box outer wall terminal surface is opened there is the circular slot, and the circular slot internal rotation is connected with the disc, and the disc top surface can be dismantled and be connected with the radar subassembly.
The principle of the basic scheme is as follows: according to the technical scheme, the containing box is directly used as a base of the satellite portable station, and the whole satellite radar assembly is spliced and fixed on the end face of the disc. The disk is rotatably connected to the groove of the storage box, so that the satellite radar can adjust the circumferential angle orientation on the storage box. When the storage box is in a use state, the supporting legs of the side walls of the storage box rotate to the designated positions, and finally the whole storage box is supported.
The beneficial effect of this basic scheme lies in: this technical scheme is direct to play the effect that supports as the base with the containing box to the satellite radar, directly regards the containing box as the base of satellite radar, has effectively saved the occupation space of base, has the convenient beneficial effect of easy operation.
Furthermore, the inner wall of the containing box is provided with a cavity, and negative weight blocks are uniformly distributed in the cavity.
This technical scheme is through adding the burden heavy piece in the containing box, and then reaches the stiction between containing box and the ground, improves the stability under the state of placing, avoids containing box horizontal displacement to appear under the fixed state.
Furthermore, the storage box top surface is articulated to have branch, branch is kept away from storage box one end and is equipped with hook portion, hook portion hook disc top surface.
According to the technical scheme, the supporting rod is rotated, so that the hook part on the supporting rod is hooked on the disc, and the technical effect of fixing the disc at any angle is achieved.
Furthermore, the landing leg includes first rotation portion and second rotation portion, first rotation portion and second rotation portion are articulated each other, and articulated department is equipped with locking device.
This technical scheme is articulated through two rotation portions that utilize the landing leg, and then makes the bottom of each landing leg can both be in different heights. When the accommodating box meets the fluctuant protruding objects, the height of the supporting leg far away from one end of the seat body can be raised, so that the top end of the accommodating box is always kept in a horizontal state.
Furthermore, the landing leg includes a plurality of telescopic joints, and is adjacent telescopic joint sliding connection, adjacent the telescopic joint is equipped with fixed knot.
This technical scheme is through the scalability that utilizes the landing leg, and then makes the landing leg can be the regulation length of adaptability relatively when meetting the barrier to reach the technological effect that final containing box steadily placed.
Furthermore, the supporting seat can be detachably connected to one end, far away from the containing box, of the supporting leg.
This technical scheme is through the adsorption of utilizing the supporting seat to reach the fixed effect of reinforcing containing box.
Furthermore, the bottom surface of the supporting seat is provided with a blind hole, and a pull ring is connected in the blind hole in a telescopic sliding manner.
The base of this technical scheme can play the effect of fixed stay containing box on the one hand, and under non-user state, operating personnel also can prolong the landing leg to tensile grabs the pull ring, in order to reach the technological effect who draws or hook containing box.
Further, pulleys are arranged on two opposite sides of the bottom surface of the storage box.
Because the containing box has increased heavy burden for guaranteeing stability, consequently set up the pulley at the terminal surface of containing box, and then be convenient for operating personnel pulls the pull ring under non-user state in order to drag the removal of containing box.
Furthermore, the containing box lateral wall fixed connection has the spirit level.
This technical scheme is through setting up the spirit level on the lateral wall, and then makes technical staff observe the levelness that the containing box was placed directly perceivedly.
Drawings
Fig. 1 is a schematic structural view of a satellite portable station storage box according to a first embodiment of the present invention;
fig. 2 is a schematic side view of a satellite portable station storage box according to a second embodiment of the present invention;
fig. 3 is a front sectional view of a satellite portable station storage box according to a second embodiment of the present invention;
fig. 4 is a partial cross-sectional view of a support base according to a second embodiment of the present invention.
Detailed Description
The following is further detailed by way of specific embodiments:
reference numerals in the drawings of the specification include: the radar hanging device comprises a storage box 1, an upper box 101, a lower box 102, a disc 2, a radar assembly 3, a strip-shaped groove 4, a support leg 5, a first rotating part 501, a second rotating part 502, a first telescopic joint 5021, a second telescopic joint 5022, a support seat 6, a pull ring 601, a level gauge 7, a load block 8, a pulley 9 and a hook rod 10.
Example one
As shown in fig. 1, the storage box for the satellite portable station comprises a storage box 1, wherein the storage box 1 comprises an upper box 101 and a lower box 102, and the side walls of the upper box 101 and the lower box 102 are hinged to each other through a hinge. The upper box body 101 and the lower box body 102 cover to form a cavity, and parts of the satellite radar are placed in the cavity of the containing box 1.
The top surface of the upper box body 101 is provided with a circular groove, a disc 2 is rotationally connected in the circular groove, the outer diameter of the disc 2 is smaller than the inner diameter of the circular groove, and the height of the disc 2 is larger than the depth of the circular groove. The side wall of the lower box body 102 is respectively provided with a strip-shaped groove 4 along the circumferential direction, the inner wall of the strip-shaped groove 4 extends outwards to form a rotating shaft, one end of the supporting leg 5 is provided with a shaft hole, and the rotating shaft is inserted into the shaft hole of the supporting leg 5, so that the supporting leg 5 is rotatably connected with the side wall of the lower box body 102. The axial length of the leg 5 is greater than the height of the container 1. The top of the disc 2 is provided with a threaded hole, and the parts of the satellite radar are spliced into the radar component 3 and then are fixedly connected to the threaded hole of the disc 2 through a bolt.
The specific implementation process is as follows: when the folding type storage box is used, the supporting legs 5 on the rotary storage box 1 are firstly opened, and the supporting legs 5 support the storage box 1 to ensure that the top surface of the storage box 1 is in a horizontal state. Then the containing box 1 is opened to take out the parts of the satellite radar, the parts of the satellite radar are spliced and assembled into a satellite radar component 3, and the satellite radar component 3 after being spliced is fixedly connected to the top surface of the disc 2 through bolts.
Example two
As shown in fig. 2 and fig. 3, the present embodiment is different from the first embodiment in that the inner walls of the upper case 101 and the lower case 102 are both provided with a separation chamber, and an iron disc-shaped negative weight 8 is uniformly fixed in the separation chamber. Go up box 101 outer wall and open and have rectangular recess, the recess is embedded to have spirit level 7. The bottom end of the lower box body 102 is rotatably connected with two pulleys 9 with the same axial direction, and one surface of the lower box body 102 opposite to the pulleys 9 is provided with a telescopic pull rod. The top surface of the disc 2 is provided with 12 grooves in a circumferential array. Go up box 101 top surface along circular slot circumference array and have four couple poles 10, couple pole 10 one end articulates at last box 101 top surface, and the one end that last box 101 was kept away from to couple pole 10 is equipped with the couple, and formula as an organic whole shaping between couple and the couple pole. The length of the hook rod 10 can be just enough to enable the hook rod 10 to hook in the groove on the top surface of the disc 2.
The landing leg 5 includes first rotation portion 501 and second rotation portion 502, and first rotation portion 501 and second rotation portion 502 are articulated each other, and second rotation portion 502 rotates the one end of connecting in first rotation portion 501 and keeping away from containing box 1, and first rotation portion 501 and second rotation portion 502 articulated department are equipped with the pinhole, and the round pin axle inserts in the pinhole and then reaches the technological effect of passing simultaneously and fixing first rotation portion 501 and second rotation portion 502. The end part of the second rotating part 502, which is far away from the first rotating part 501, is in threaded connection with a supporting seat 6, the supporting seat 6 is in a conical shape, a threaded rod is arranged on the top surface of the supporting seat 6, and a rubber ring is sleeved at the bottom of the supporting seat 6. The second rotating portion 502 comprises a first telescopic joint 5021 and a second telescopic joint 5022, the first telescopic joint 5021 is in telescopic sliding connection with an inner cavity of the second telescopic joint 5022, through holes with equal intervals are formed in the first telescopic joint 5021 and the second telescopic joint 5022 in the axial direction, and screws penetrate through the through holes formed in the two telescopic joints in a coincident mode and fix the two telescopic joints together. Second landing leg 5 rotates to be connected in the one end that storage box 1 was kept away from to first landing leg 5, and the tip threaded connection that first landing leg 5 was kept away from to second landing leg 5 has supporting seat 6, and 6 bottom covers of supporting seat have the rubber circle. The second leg 5 comprises a first telescopic joint 5021 and a second telescopic joint 5022, the first telescopic joint 5021 is in telescopic sliding connection with an inner cavity of the second telescopic joint 5022, through holes with equal intervals are axially formed in the first telescopic joint 5021 and the second telescopic joint 5022, and screws penetrate through the through holes formed in the first telescopic joint 5021 and the second telescopic joint 5022 in a coincident mode, so that the two telescopic joints are fixed together. As shown in fig. 4, a cavity is formed in the bottom surface of the support seat 6, a support rod is connected to the cavity in a sliding manner along the axial direction of the support seat, and a pull ring 601 is welded at one end of the support rod close to the bottom surface. The pull ring 601 can be embedded in the cavity of the support seat 6, and can also be pulled out from the cavity of the support seat 6.
The specific implementation process is as follows: first, the second rotating part 502 is rotated relative to the first rotating part 501, the length of the second supporting leg 5 is controlled by controlling the first telescopic joint 5021 and the second telescopic joint 5022, the supporting leg 5 reaches the best position and the best angle by observing the level gauge 7 on the outer wall of the upper box body 101 through the through hole of the operator, and the supporting seat 6 is adsorbed on the bottom surface to stably fix the storage box 1. Finally, the hook rod 10 is rotated to be hooked in the groove on the top surface of the disc 2, and finally the technical effect of preventing the radar component 3 from rotating is achieved.
The above description is only an example of the present invention, and the common general knowledge of the known specific structures and characteristics of the embodiments is not described herein. It should be noted that, for those skilled in the art, without departing from the structure of the present invention, several modifications and improvements can be made, which should also be regarded as the protection scope of the present invention, and these will not affect the effect of the implementation of the present invention and the practicability of the patent. The scope of the claims of the present application shall be determined by the contents of the claims, and the description of the embodiments and the like in the specification shall be used to explain the contents of the claims.
Claims (9)
1. The utility model provides a portable station containing box of satellite, includes the containing box, be equipped with the satellite radar subassembly in the containing box, its characterized in that: the storage box circumference lateral wall rotates and is connected with a plurality of landing legs, storage box outer wall terminal surface is opened there is the circular slot, the circular slot internal rotation is connected with the disc, the disc top surface can be dismantled and be connected with the satellite radar subassembly.
2. A satellite portable station container as claimed in claim 1, wherein: the inner wall of the containing box is provided with a separation cavity, and negative weight blocks are uniformly distributed in the separation cavity.
3. A satellite portable station container as claimed in claim 1, wherein: the storage box top surface articulates there is branch, branch is kept away from storage box one end and is equipped with hook portion, hook portion hook disc top surface.
4. A satellite portable station container as claimed in claim 1, wherein: the landing leg includes first rotation portion and second rotation portion, first rotation portion and second rotation portion are articulated each other, and articulated department is equipped with locking device.
5. A satellite portable station container as claimed in claim 1, wherein: the landing leg includes a plurality of telescopic joints, and is adjacent telescopic joint sliding connection, adjacent the telescopic joint is equipped with fixed knot and constructs.
6. A satellite portable station container as claimed in claim 1, wherein: the supporting seat can be detachably connected to one end, far away from the containing box, of the supporting leg.
7. The satellite portable station container according to claim 6, wherein: the bottom surface of the supporting seat is provided with a blind hole, and a pull ring is connected in the blind hole in a telescopic sliding manner.
8. A satellite portable station container as claimed in claim 7, wherein: pulleys are arranged on two opposite sides of the bottom surface of the storage box.
9. A satellite portable station container as claimed in claim 1, wherein: the level gauge is embedded in the side wall of the containing box.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920774722.0U CN210235913U (en) | 2019-05-27 | 2019-05-27 | Satellite portable station containing box |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920774722.0U CN210235913U (en) | 2019-05-27 | 2019-05-27 | Satellite portable station containing box |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210235913U true CN210235913U (en) | 2020-04-03 |
Family
ID=69972615
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920774722.0U Expired - Fee Related CN210235913U (en) | 2019-05-27 | 2019-05-27 | Satellite portable station containing box |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210235913U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111812548A (en) * | 2020-06-05 | 2020-10-23 | 深圳供电局有限公司 | Transformer vibration noise collection device containing box and vibration noise collection equipment |
-
2019
- 2019-05-27 CN CN201920774722.0U patent/CN210235913U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111812548A (en) * | 2020-06-05 | 2020-10-23 | 深圳供电局有限公司 | Transformer vibration noise collection device containing box and vibration noise collection equipment |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20200403 Termination date: 20200527 |