CN220935176U - Signal receiving and transmitting device for satellite communication - Google Patents
Signal receiving and transmitting device for satellite communication Download PDFInfo
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- CN220935176U CN220935176U CN202322727762.9U CN202322727762U CN220935176U CN 220935176 U CN220935176 U CN 220935176U CN 202322727762 U CN202322727762 U CN 202322727762U CN 220935176 U CN220935176 U CN 220935176U
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- signal transceiver
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- 230000004224 protection Effects 0.000 claims abstract description 22
- 230000001681 protective effect Effects 0.000 abstract description 11
- 230000005484 gravity Effects 0.000 abstract description 6
- 238000010586 diagram Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000001632 homeopathic effect Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000009979 protective mechanism Effects 0.000 description 1
- 239000007858 starting material Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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Abstract
The utility model discloses a signal receiving and transmitting device for satellite communication, comprising: a satellite signal transceiver and a guard mechanism; the protection mechanism comprises a base and a movable plate fixedly connected to the base of the satellite signal transceiver, wherein the bottom of the movable plate is movably connected with the base, the top of the base is fixedly connected with a protection cover, one side of the protection cover is fixedly connected with a supporting plate, and the bottom of the supporting plate is fixedly provided with a motor; according to the signal transceiver for satellite communication, the protection mechanism is arranged on the satellite signal transceiver, so that the movable plate can drive the satellite signal transceiver to move into the protective cover in the mode of starting the motor in the extreme weather in the future, and after the threaded rod is screwed out of the movable block, the baffle can seal the opening of the protective cover under the action of gravity; through the arrangement, the problem that the satellite signal receiving and transmitting device is easy to damage due to collision when extreme weather comes is avoided.
Description
Technical Field
The utility model relates to the technical field of satellite communication, in particular to a signal transceiver for satellite communication.
Background
As is well known, satellite communication is communication between radio communication stations on earth by using satellites as relays, and a satellite communication system is composed of two parts, a satellite and an earth station; in addition, satellite communication is characterized in that: communication can be performed from any two points as long as the communication is within the range covered by the electric wave emitted by the satellite; is not easily affected by land disasters; the earth station circuit can be opened only by setting; meanwhile, the system can be received at a plurality of places, and can economically realize broadcast and multiple access communication; the circuit is very flexible to set, and can disperse the telephone traffic which is too concentrated at any time; the same channel may be used for different directions or for different intervals.
When the existing satellite signal transceiver is used, due to the lack of measures for protecting equipment in extreme weather conditions, hail, typhoon and other extreme weather conditions are caused to be temporary, the satellite signal transceiver positioned at the top of a building is easy to damage due to collision, and therefore, the satellite signal transceiver for satellite communication is provided.
The above information disclosed in the background section is only for enhancement of understanding of the background of the disclosure and therefore it may include information that does not form the prior art that is already known to a person of ordinary skill in the art.
Disclosure of utility model
The present utility model is directed to a signal transceiver for satellite communication, which solves the above-mentioned problems.
In order to achieve the above purpose, the present utility model provides the following technical solutions: a signal transmitting and receiving device for satellite communication, comprising: a satellite signal transceiver and a guard mechanism;
The protection machanism includes base and fixed connection fly leaf on satellite signal transceiver base, the bottom and the base swing joint of fly leaf, the top fixedly connected with protection casing of base, one side fixedly connected with backup pad of protection casing, the bottom fixed mounting of backup pad has the motor, the output shaft fixedly connected with lead screw of motor, the outer wall and the fly leaf threaded connection of lead screw, the top fixedly connected with riser of protection casing, the inside swing joint of riser has the movable block, one side fixedly connected with baffle of movable block, one side fixedly connected with connecting block of riser, the inside threaded connection of connecting block has the threaded rod, outer wall one side and the movable block threaded connection of threaded rod.
Through adopting above-mentioned technical scheme, when extreme weather come temporarily can make the motor drive the lead screw homeopathic rotation through the mode of starter motor and rotate to make the fly leaf drive satellite signal transceiver under the lead screw effect and remove to inside the protection casing, and can make the baffle down move under the action of gravity through the mode of unscrewing the threaded rod from the movable block, and then make the baffle protect the opening part of protection casing, make satellite signal transceiver can obtain effective protection when extreme weather.
Preferably, an empty slot is formed in the vertical plate, and the inner side wall of the empty slot is in sliding connection with the movable block.
By adopting the technical scheme, the movable block can be more stable when moving on the vertical plate.
Preferably, the top end of the threaded rod is fixedly connected with a lug.
Through adopting above-mentioned technical scheme, can be convenient for twist the threaded rod.
Preferably, the top of base has seted up the spout, the inside wall and the fly leaf sliding connection of spout, logical groove has been seted up to one side of base, the inside intercommunication of one side and spout of logical groove.
Through adopting above-mentioned technical scheme, can make the fly leaf remove on the base more steadily to can be convenient for the rainwater discharge from the spout.
Preferably, the top of base fixedly connected with dog, one side of dog is connected with the lead screw rotation through the bearing.
By adopting the technical scheme, the rotating load of the screw rod can be reduced.
Preferably, the bottom of the baffle is provided with a groove, and one side of the baffle is fixedly connected with a handle.
By adopting the technical scheme, the baffle can be conveniently put down or lifted.
Preferably, the bottom of the supporting plate is fixedly connected with a box body, and the box body is arranged outside the motor.
Through adopting above-mentioned technical scheme, can be convenient for protect the motor.
In summary, the present application includes at least one of the following beneficial technical effects:
According to the signal transceiver for satellite communication, the protection mechanism is arranged on the satellite signal transceiver, so that the movable plate can drive the satellite signal transceiver to move into the protective cover in the mode of starting the motor in the extreme weather in the future, and after the threaded rod is screwed out of the movable block, the baffle can seal the opening of the protective cover under the action of gravity; through the arrangement, the problem that the satellite signal receiving and transmitting device is easy to damage due to collision when extreme weather comes is avoided.
Drawings
Fig. 1 is a schematic structural diagram of a signal transceiver for satellite communication according to the present utility model;
Fig. 2 is an enlarged schematic diagram of a region a of a schematic diagram of a signal transceiver for satellite communication according to the present utility model;
Fig. 3 is a schematic structural view of a baffle and a groove in the signal transceiver for satellite communication according to the present utility model;
fig. 4 is a schematic structural view of a motor and a screw in the signal transceiver for satellite communication according to the present utility model.
In the figure: 1. a satellite signal transceiver; 10. a movable plate; 2. a protective mechanism; 20. a base; 21. a support plate; 22. a motor; 23. a screw rod; 24. a protective cover; 25. a chute; 26. a vertical plate; 27. a baffle; 28. a movable block; 29. a connecting block; 201. a threaded rod; 202. a hollow groove; 203. a bump; 204. a case; 205. a stop block; 206. a groove; 207. a handle; 208. and (5) through grooves.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
Referring to fig. 1-4, the present utility model provides a technical solution: a signal transmitting and receiving device for satellite communication, comprising: a satellite signal transceiver 1 and a guard mechanism 2;
Firstly, in order to temporarily enable the motor 22 to drive the screw rod 23 to rotate clockwise by starting the motor 22 in extreme weather, so that the movable plate 10 drives the satellite signal transceiver 1 to move into the protective cover 24 under the action of the screw rod 23, and the baffle 27 can move downwards under the action of gravity by screwing the threaded rod 201 out of the movable block 28, so that the baffle 27 can protect the opening of the protective cover 24, and the satellite signal transceiver 1 can be effectively protected in extreme weather; the protection mechanism 2 comprises a base 20 and a movable plate 10 fixedly connected to a base of the satellite signal transceiver 1, wherein the bottom of the movable plate 10 is movably connected with the base 20, the top of the base 20 is fixedly connected with a protection cover 24, one side of the protection cover 24 is fixedly connected with a support plate 21, the bottom of the support plate 21 is fixedly provided with a motor 22, an output shaft of the motor 22 is fixedly connected with a screw rod 23, the outer wall of the screw rod 23 is in threaded connection with the movable plate 10, the top of the protection cover 24 is fixedly connected with a vertical plate 26, the inside of the vertical plate 26 is movably connected with a movable block 28, one side of the movable block 28 is fixedly connected with a baffle 27, one side of the vertical plate 26 is fixedly connected with a connecting block 29, the inside of the connecting block 29 is in threaded connection with a threaded rod 201, and one side of the outer wall of the threaded rod 201 is in threaded connection with the movable block 28;
Secondly, in order to make the movable block 28 move on the vertical plate 26 more stable, a hollow groove 202 is formed in the vertical plate 26, and the inner side wall of the hollow groove 202 is in sliding connection with the movable block 28; in order to facilitate screwing of the threaded rod 201, a bump 203 is fixedly connected to the top end of the threaded rod 201; in order to enable the movable plate 10 to move on the base 20 more stably and to facilitate the discharge of rainwater from the chute 25, the top of the base 20 is provided with the chute 25, the inner side wall of the chute 25 is in sliding connection with the movable plate 10, one side of the base 20 is provided with a through groove 208, and one side of the through groove 208 is communicated with the inside of the chute 25; in order to reduce the rotation load of the screw rod 23, a stop block 205 is fixedly connected to the top of the base 20, and one side of the stop block 205 is in rotation connection with the screw rod 23 through a bearing; in order to facilitate the lowering or lifting of the baffle 27, a groove 206 is formed in the bottom of the baffle 27, and a handle 207 is fixedly connected to one side of the baffle 27; in order to be able to facilitate the protection of the motor 22, the bottom of the support plate 21 is fixedly connected with a box 204, and the box 204 is disposed outside the motor 22.
According to the technical scheme, the working steps of the scheme are summarized and carded: when the satellite signal transceiver is used, the motor 22 can drive the screw rod 23 to rotate clockwise by starting the motor 22 when the extreme weather comes, so that the movable plate 10 drives the satellite signal transceiver 1 to move into the protective cover 24 under the action of the screw rod 23, the baffle 27 can move downwards under the action of gravity by screwing the threaded rod 201 out of the movable block 28, and then the baffle 27 can protect the opening of the protective cover 24, and the satellite signal transceiver 1 can be effectively protected in the extreme weather.
To sum up: according to the signal transceiver for satellite communication, the protection mechanism 2 is arranged on the satellite signal transceiver 1, so that the movable plate 10 can drive the satellite signal transceiver 1 to move into the protective cover 24 by starting the motor 22 in the extreme weather in the future, and after the threaded rod 201 is screwed out of the movable block 28, the baffle 27 can seal the opening of the protective cover 24 under the action of gravity; through the arrangement, the problem that the satellite signal receiving and transmitting device is easy to damage due to collision when extreme weather comes is avoided.
None of the utility models are related to the same or are capable of being practiced in the prior art. Although embodiments of the present utility model have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made therein without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.
Claims (7)
1. A signal transmitting/receiving device for satellite communication, comprising: a satellite signal transceiver (1) and a guard mechanism (2);
Protection machanism (2) are including base (20) and fly leaf (10) of fixed connection on satellite signal transceiver (1) base, the bottom and the base (20) swing joint of fly leaf (10), the top fixedly connected with protection casing (24) of base (20), one side fixedly connected with backup pad (21) of protection casing (24), the bottom fixed mounting of backup pad (21) has motor (22), the output shaft fixedly connected with lead screw (23) of motor (22), the outer wall and the fly leaf (10) threaded connection of lead screw (23), the top fixedly connected with riser (26) of protection casing (24), the inside swing joint of riser (26) has movable block (28), one side fixedly connected with baffle (27) of movable block (28), one side fixedly connected with connecting block (29) of riser (26), the inside threaded connection of connecting block (29) has threaded rod (201), outer wall one side and movable block (28) threaded connection.
2. The signal transmitting-receiving device for satellite communication according to claim 1, wherein: an empty groove (202) is formed in the vertical plate (26), and the inner side wall of the empty groove (202) is in sliding connection with the movable block (28).
3. The signal transmitting-receiving device for satellite communication according to claim 1, wherein: the top end of the threaded rod (201) is fixedly connected with a lug (203).
4. The signal transmitting-receiving device for satellite communication according to claim 1, wherein: the top of base (20) has seted up spout (25), the inside wall and the fly leaf (10) sliding connection of spout (25), logical groove (208) have been seted up to one side of base (20), the inside intercommunication of one side and spout (25) of logical groove (208).
5. The signal transmitting-receiving device for satellite communication according to claim 4, wherein: the top of base (20) fixedly connected with dog (205), one side of dog (205) is connected with lead screw (23) rotation through the bearing.
6. The signal transmitting-receiving device for satellite communication according to claim 1, wherein: the bottom of baffle (27) is seted up recess (206), one side fixedly connected with handle (207) of baffle (27).
7. The signal transmitting-receiving device for satellite communication according to claim 1, wherein: the bottom of backup pad (21) fixedly connected with box (204), box (204) set up the outside of motor (22).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202322727762.9U CN220935176U (en) | 2023-10-11 | 2023-10-11 | Signal receiving and transmitting device for satellite communication |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202322727762.9U CN220935176U (en) | 2023-10-11 | 2023-10-11 | Signal receiving and transmitting device for satellite communication |
Publications (1)
Publication Number | Publication Date |
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CN220935176U true CN220935176U (en) | 2024-05-10 |
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Family Applications (1)
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CN202322727762.9U Active CN220935176U (en) | 2023-10-11 | 2023-10-11 | Signal receiving and transmitting device for satellite communication |
Country Status (1)
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CN (1) | CN220935176U (en) |
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2023
- 2023-10-11 CN CN202322727762.9U patent/CN220935176U/en active Active
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