CN113325441A

CN113325441A - Satellite navigation receiver for space-time big data acquisition

Info

Publication number: CN113325441A
Application number: CN202110408483.9A
Authority: CN
Inventors: 吴献文; 孙照辉; 胡海宽
Original assignee: Guangzhou Quancheng Multidimensional Information Technology Co ltd; Guangdong College of Industry and Commerce
Current assignee: Guangzhou Quancheng Multidimensional Information Technology Co ltd; Guangdong College of Industry and Commerce
Priority date: 2021-04-16
Filing date: 2021-04-16
Publication date: 2021-08-31
Anticipated expiration: 2041-04-16
Also published as: CN113325441B

Abstract

The invention relates to the technical field of satellite positioning, and discloses a satellite navigation receiver for acquiring space-time big data. This a satellite navigation receiver for big data acquisition of space-time, possess the buffering support, the antenna turns to automatically and magnetism inhales advantages such as formula installation, it installs through a threaded rod to have solved current satellite navigation receiver most, only a stress point, it is great to meet the time vibration range of colliding with, because the wind current that the removal produced causes pressure to the antenna body easily when the antenna exposes in the air, thereby can lead to the antenna to be blown down by wind and lead to damaging, and when current satellite navigation receiver need maintain, can only open through the mode that destroys the casing, the problem of the follow-up use after the maintenance is accomplished has seriously been influenced.

Description

Satellite navigation receiver for space-time big data acquisition

Technical Field

The invention relates to the technical field of satellite positioning, in particular to a satellite navigation receiver for space-time big data acquisition.

Background

The satellite positioning system is a technology for accurately positioning a certain object by using satellites, and develops the current high-precision GPS from the initial low positioning precision, the incapability of positioning in real time and the difficulty of providing a timely navigation service to realize that 4 satellites can be observed at any time and any point on the earth so as to realize the functions of navigation, positioning, time service and the like;

the present satellite navigation receiver is mostly installed on the object of removal, and the object of removal can produce vibrations at the in-process of marcing inevitable, and present satellite navigation receiver is mostly installed through a threaded rod, only one stress point, the vibration amplitude is great when meetting to collide with, the top of the satellite navigation receiver of subtotal is provided with the antenna, because the windy current that the removal produced causes pressure to the antenna body easily when the antenna exposes in the air, thereby can lead to the antenna to be blown down by wind and lead to the damage, and when present satellite navigation receiver need maintain, can only open through the mode of destroying the casing, the follow-up use after the maintenance completion has been seriously influenced.

Disclosure of Invention

Technical problem to be solved

Aiming at the defects of the prior art, the invention provides a satellite navigation receiver for space-time big data acquisition, which has the advantages of a buffer support, automatic antenna steering, magnetic type installation and the like, and solves the problems that most of the conventional satellite navigation receivers are installed through a threaded rod, only one stress point exists, the vibration amplitude is large when collision occurs, the antenna is arranged at the top of a small part of the satellite navigation receivers, when the antenna is exposed in the air, the antenna is easy to cause pressure to the antenna body due to wind flow generated by movement, the antenna is likely to be blown down by wind, the antenna is damaged, and when the conventional satellite navigation receiver needs to be maintained, the conventional satellite navigation receiver can be opened only in a mode of damaging a shell, and the follow-up use after the maintenance is seriously influenced.

(II) technical scheme

In order to achieve the purpose, the invention provides the following technical scheme: a satellite navigation receiver for space-time big data acquisition comprises a device body, wherein a first bearing is fixedly connected to the top of the device body, a cover plate is fixedly connected to the inner surface of the first bearing, a base is fixedly mounted at the bottom of the device body, a rotary drum is fixedly mounted at the top of the cover plate, an antenna is rotatably connected to the inner surface of the rotary drum, a wind deflector is fixedly sleeved on the outer surface of the antenna, a bottom plate is fixedly mounted at the bottom of the base, a second bearing is fixedly connected to the bottom of the bottom plate, a support plate is fixedly connected to the bottom of the second bearing, a rotary column is rotatably connected to one side, away from the second bearing, of the support plate, a push rod is fixedly welded to the outer surface of the rotary column, a pressure boosting pipe is movably sleeved on the outer surface of the push rod, a support plate is fixedly welded to the bottom of the base, and an air bag is fixedly mounted on the outer surface of the support plate, the utility model discloses a device, including device body, fixed surface, the fixed end of device body is equipped with the runner, the fixed cover of one end that the device body was kept away from to the runner is equipped with the knob, the bottom fixed mounting of apron has first magnet, the fixed surface cover of runner is equipped with second magnet, the fixed surface cover of runner is equipped with the carousel, the fixed surface welding of carousel has a plurality of roller tooth, the fixed surface of carousel installs two stoppers, one side fixedly connected with fifth bearing of device body inner wall, the outer fixed surface of fifth bearing is connected with well post, the internal surface sliding connection of well post has the gag lever post.

Preferably, the top fixed mounting of apron has two go-between, two the surface of go-between is all fixed around being equipped with the haulage rope, two the haulage rope is kept away from the equal fixedly connected with connecting rod of one end of go-between, two the one end that the haulage rope was kept away from to the connecting rod respectively with the external surface fixed connection of wind vane.

Preferably, the bottom of the support plate is fixedly provided with a bearing plate, the bottom of the base is fixedly connected with a connecting cylinder, and the bottom of the connecting cylinder and the bottom of the bearing plate are positioned on the same plane.

Preferably, one end of the pressure increasing pipe, which is far away from the push rod, is fixedly connected with the bottom of the base through a third bearing.

Preferably, the inner surface of the pressure increasing pipe is fixedly communicated with a conduit, and one end of the conduit, far away from the pressure increasing pipe, penetrates through the bearing plate and is fixedly communicated with the inner surface of the air bag.

Preferably, the first magnet and the second magnet have opposite magnetic poles, and the outer surfaces of the two limiting blocks are matched with the outer surface of the limiting rod.

Preferably, the outer fixed surface of gag lever post is connected with the spring, the one end that the gag lever post was kept away from to the spring is connected with the internal fixed surface of cavity post, fixedly connected with arc elastic plate between the surface of extension board and the surface of base.

Compared with the prior art, the invention provides a satellite navigation receiver for acquiring space-time big data, which has the following beneficial effects:

1. this a satellite navigation receiver for big data acquisition of space-time, at first bear the impact force through the bearing board, the extension board atress rotates along the second bearing afterwards, thereby the arc elastic plate is pressed the dynamic stress by the extension board and takes place deformation and carry out the secondary buffering, remaining impact force drives the push rod and slides along the internal surface of pressure boost pipe afterwards, thereby the inside air of pressure boost pipe is extruded and is carried out the buffering for the third time along the inside of pipe entering gasbag this moment, multiple buffer structure has been increased, it installs through a threaded rod to have solved current satellite navigation receiver majority, only a stress point, meet the great problem of vibration amplitude when colliding with.

2. The satellite navigation receiver for space-time big data acquisition rotates along the center of the rotary drum through the antenna, so that the wind direction plate is gradually adjusted to a windward state, when multi-angle wind blows, the wind direction plate tends to continuously rotate, at the moment, the wind direction plate is limited by the connecting ring matched with the traction rope through the connecting rod, so that the wind direction plate is prevented from rotating, when a cover plate needs to be opened, the knob is firstly rotated, the rotating rod is driven to rotate along the center of the fourth bearing through the knob, the rotating rod drives the second magnet to rotate when rotating, at the moment, the limiting rod is jacked by the roller teeth to shrink towards the inner surface of the hollow column, the limiting rod is jacked outwards through the spring to do reciprocating motion along the inner wall of the hollow column, the limiting rod stops after being clamped with the outer surface of the limiting block, at the moment, the first magnet is opposite to the second magnet in magnetic pole, the repulsion that produces drives the apron and upwards turns to open along the center department of first bearing, increased antenna automatic steering structure and magnetism and inhaled mounting structure, thereby solved the antenna and exposed when the air because the wind current that removes the production causes pressure to the antenna body easily, thereby can lead to the antenna to be blown down by wind and lead to damaging, and when current satellite navigation receiver need maintain, can only open through the mode that destroys the casing, seriously influenced the problem of the follow-up use after the maintenance is accomplished.

Drawings

FIG. 1 is a schematic front perspective view of the present invention;

FIG. 2 is a schematic side view of the structure of the present invention;

FIG. 3 is a perspective view of an antenna of the present invention;

FIG. 4 is a schematic side cross-sectional view of the device body of the present invention;

FIG. 5 is a schematic front sectional view of the magnetic attraction structure of the present invention.

Wherein: 1. a device body; 2. a cover plate; 3. a first bearing; 4. a base plate; 5. a second bearing; 6. a support plate; 7. a bearing plate; 8. turning the column; 9. a push rod; 10. a pressure increasing pipe; 11. a third bearing; 12. a conduit; 13. a carrier plate; 14. an air bag; 15. a rotating drum; 16. an antenna; 17. a connecting ring; 18. a hauling rope; 19. a connecting rod; 20. a knob; 21. a rotating rod; 22. a fourth bearing; 23. a first magnet; 24. a second magnet; 25. a turntable; 26. a roller tooth; 27. a limiting block; 28. a limiting rod; 29. a fifth bearing; 30. a hollow column; 31. a spring; 32. a wind vane; 33. a base.

Detailed Description

The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.

Referring to fig. 1-5, a satellite navigation receiver for space-time big data acquisition comprises a device body 1, a first bearing 3 is fixedly connected to the top of the device body 1, a cover plate 2 is fixedly connected to the inner surface of the first bearing 3, a base 33 is fixedly installed at the bottom of the device body 1, a rotary drum 15 is fixedly installed at the top of the cover plate 2, an antenna 16 is rotatably connected to the inner surface of the rotary drum 15, a wind deflector 32 is fixedly sleeved on the outer surface of the antenna 16, a bottom plate 4 is fixedly installed at the bottom of the base 33, a second bearing 5 is fixedly connected to the bottom of the bottom plate 4, a support plate 6 is fixedly connected to the bottom of the second bearing 5, a rotary column 8 is rotatably connected to one side of the support plate 6 away from the second bearing 5, a push rod 9 is fixedly welded to the outer surface of the rotary column 8, a pressurizing pipe 10 is movably sleeved on the outer surface of the push rod 9, a support plate 13 is fixedly welded to the bottom of the base 33, the fixed surface of carrier plate 13 installs gasbag 14, the surface swivelling joint of device body 1 has fourth bearing 22, the internal fixed surface of fourth bearing 22 inserts and is equipped with bull stick 21, the fixed cover of one end that device body 1 was kept away from to bull stick 21 is equipped with knob 20, the bottom fixed mounting of apron 2 has first magnet 23, the fixed surface cover of bull stick 21 is equipped with second magnet 24, the fixed surface cover of bull stick 21 is equipped with carousel 25, the fixed surface welding of carousel 25 has a plurality of roller tooth 26, the fixed surface of carousel 25 installs two stopper 27, one side fixedly connected with fifth bearing 29 of device body 1 inner wall, the outer fixed surface of fifth bearing 29 is connected with well post 30, the internal surface sliding connection of well post 30 has stopper 28.

Specifically, the top fixed mounting of apron 2 has two go-between 17, and the surface of two go-between 17 is all fixed around being equipped with haulage rope 18, and the equal fixedly connected with connecting rod 19 of the one end that go-between 17 was kept away from to two haulage ropes 18, and the one end that haulage rope 18 was kept away from to two connecting rods 19 is connected with the surface fixed of wind vane 32 respectively.

According to the technical scheme, the wind direction plate 32 can be limited by the traction rope 18 through the connecting rod 19 when rotating.

Specifically, the bottom of the support plate 6 is fixedly provided with a bearing plate 7, the bottom of the base 33 is fixedly connected with a connecting cylinder, and the bottom of the connecting cylinder and the bottom of the bearing plate 7 are positioned on the same plane.

According to the technical scheme, the bearing plate 7 can be fixedly installed through the matching of the connecting cylinder and the bearing plate.

Specifically, one end of the pressure increasing pipe 10 far away from the push rod 9 is fixedly connected with the bottom of the base 33 through a third bearing 11.

According to the above-described technical solution, it is possible to pressurize while the push rod 9 slides along the inner wall of the pressurizing pipe 10, thereby injecting air into the inner surface of the balloon 14 through the guide tube 12.

Specifically, a conduit 12 is fixedly communicated with the inner surface of the pressure increasing pipe 10, and one end of the conduit 12 far away from the pressure increasing pipe 10 passes through a bearing plate 13 to be fixedly communicated with the inner surface of an air bag 14.

According to the technical scheme, the air bag 14 can be fixedly arranged on the inner wall of the base 33 through the carrier plate 13.

Specifically, the first magnet 23 and the second magnet 24 have opposite magnetic poles, and the outer surfaces of the two limit blocks 27 are matched with the outer surface of the limit rod 28.

According to the technical scheme, the first magnet 23 and the second magnet 24 can be attracted together so as to achieve the closing purpose.

Specifically, a spring 31 is fixedly connected to the outer surface of the limiting rod 28, one end of the spring 31, which is far away from the limiting rod 28, is fixedly connected to the inner surface of the hollow column 30, and an arc-shaped elastic plate is fixedly connected between the outer surface of the support plate 6 and the outer surface of the base 33.

According to the technical scheme, the spring 31 can be driven to be stressed and contracted when the limiting rod 28 slides along the inner surface of the hollow column 30.

When the device is used, when the bottom of the device is collided, the force bearing plate 7 firstly bears impact force, then the support plate 6 rotates along the second bearing 5 under stress, at the moment, the arc elastic plate is pressed by the support plate 6 to be deformed under stress so as to carry out secondary buffering, then the rest impact force drives the push rod 9 to slide along the inner surface of the pressure increasing pipe 10, at the moment, air in the pressure increasing pipe 10 is extruded to enter the air bag 14 along the guide pipe 12 so as to carry out third buffering, a multiple buffering structure is added, and the problem that most of the existing satellite navigation receiver is installed through a threaded rod, only one stress point exists, and the vibration amplitude is large under collision is solved;

when meeting high wind power, firstly the wind direction plate 32 is driven by the wind power to rotate, so as to drive the antenna 16 to rotate along the center of the rotary drum 15, so that the wind direction plate 32 is gradually adjusted to a windward state, when blowing wind from multiple angles, the wind direction plate 32 tends to continuously rotate, at this time, the wind direction plate 32 is limited by the connecting ring 17 matching with the traction rope 18 through the connecting rod 19, so as to prevent the wind direction plate from rotating, when the cover plate 2 needs to be opened, the knob 20 is firstly rotated, the rotating rod 21 is driven by the knob 20 to rotate along the center of the fourth bearing 22, the rotating rod 21 drives the second magnet 24 to rotate when rotating, at this time, the limiting rod 28 is jacked by the roller teeth 26 to contract towards the inner surface of the hollow column 30, and jacked outwards by the spring 31, the limiting rod 28 is driven to reciprocate along the inner wall of the hollow column 30, until the limiting rod 28 is clamped with the outer surface of the limiting block 27, and then stops, first magnet 23 is relative with the same magnetic pole of second magnet 24 this moment, the repulsion that produces drives apron 2 and upwards turns to open along the center department of first bearing 3, the antenna 16 automatic steering structure and magnetism mounting structure have been increased, thereby it causes pressure to the antenna 16 body easily because the wind current that the removal produced when having solved antenna 16 and exposing in the air, thereby probably lead to the antenna 16 to be blown down and lead to damaging, and when present satellite navigation receiver need maintain, can only open through the mode of destroying the casing, the problem of the follow-up use after the maintenance completion has seriously been influenced.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims

1. Satellite navigation receiver for spatio-temporal big data acquisition, comprising a device body (1), characterized in that: the wind power generation device is characterized in that a first bearing (3) is fixedly connected to the top of the device body (1), a cover plate (2) is fixedly connected to the inner surface of the first bearing (3), a base (33) is fixedly installed at the bottom of the device body (1), a rotary drum (15) is fixedly installed at the top of the cover plate (2), an antenna (16) is rotatably connected to the inner surface of the rotary drum (15), a wind deflector (32) is fixedly sleeved on the outer surface of the antenna (16), a bottom plate (4) is fixedly installed at the bottom of the base (33), a second bearing (5) is fixedly connected to the bottom of the bottom plate (4), a support plate (6) is fixedly connected to the bottom of the second bearing (5), a rotary column (8) is rotatably connected to one side, far away from the second bearing (5), of the support plate (6), and a push rod (9) is fixedly welded to the outer surface of the rotary column (8), the outer fixed surface cover of push rod (9) is equipped with pressure boost pipe (10), the fixed welding in bottom of base (33) has carrier plate (13), the outer fixed surface of carrier plate (13) installs gasbag (14), the outer surface swivelling joint of device body (1) has fourth bearing (22), the internal fixed surface of fourth bearing (22) is inserted and is equipped with bull stick (21), the fixed cover of one end that device body (1) was kept away from in bull stick (21) is equipped with knob (20), the bottom fixed surface of apron (2) installs first magnet (23), the outer fixed surface cover of bull stick (21) is equipped with second magnet (24), the outer fixed surface cover of bull stick (21) is equipped with carousel (25), the outer fixed surface welding of carousel (25) has a plurality of roller tooth (26), the outer fixed surface of carousel (25) installs two stopper (27), the device body (1) inner wall one side fixedly connected with fifth bearing (29), the surface fixedly connected with cavity post (30) of fifth bearing (29), the internal surface sliding connection of cavity post (30) has gag lever post (28).

2. The satellite navigation receiver for spatio-temporal big data acquisition according to claim 1, characterized in that: the top fixed mounting of apron (2) has two go-between (17), two the surface of go-between (17) is all fixed around being equipped with haulage rope (18), two the equal fixedly connected with connecting rod (19) of one end that go-between (17) were kept away from in haulage rope (18), two the one end that haulage rope (18) were kept away from in connecting rod (19) is connected with the surface fixed of wind vane (32) respectively.

3. The satellite navigation receiver for spatio-temporal big data acquisition according to claim 1, characterized in that: the bottom of the support plate (6) is fixedly provided with a bearing plate (7), the bottom of the base (33) is fixedly connected with a connecting cylinder, and the bottom of the connecting cylinder and the bottom of the bearing plate (7) are positioned on the same plane.

4. The satellite navigation receiver for spatio-temporal big data acquisition according to claim 1, characterized in that: one end of the pressure increasing pipe (10) far away from the push rod (9) is fixedly connected with the bottom of the base (33) through a third bearing (11).

5. The satellite navigation receiver for spatio-temporal big data acquisition according to claim 1, characterized in that: the inner surface of the pressure increasing pipe (10) is fixedly communicated with a guide pipe (12), and one end of the guide pipe (12) far away from the pressure increasing pipe (10) penetrates through the bearing plate (13) to be fixedly communicated with the inner surface of the air bag (14).

6. The satellite navigation receiver for spatio-temporal big data acquisition according to claim 1, characterized in that: the first magnet (23) is opposite to the second magnet (24) in different magnetic poles, and the outer surfaces of the two limiting blocks (27) are matched with the outer surface of the limiting rod (28).

7. The satellite navigation receiver for spatio-temporal big data acquisition according to claim 1, characterized in that: the outer fixed surface of gag lever post (28) is connected with spring (31), the one end that gag lever post (28) was kept away from in spring (31) is connected with the internal surface fixed connection of cavity post (30), fixedly connected with arc elastic plate between the surface of extension board (6) and the surface of base (33).