CN210778932U - VSAT satellite antenna supporting seat - Google Patents
VSAT satellite antenna supporting seat Download PDFInfo
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- CN210778932U CN210778932U CN201922415226.9U CN201922415226U CN210778932U CN 210778932 U CN210778932 U CN 210778932U CN 201922415226 U CN201922415226 U CN 201922415226U CN 210778932 U CN210778932 U CN 210778932U
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Abstract
The utility model discloses a VSAT satellite antenna supporting seat, including the every single move board, the every single move extension board, extended base, the rotatable setting of every single move board is in extended base top, every single move board and every single move extension board pass through locking Assembly and connect, the every single move extension board can be followed the every single move board and carried out rectilinear movement, the every single move extension board is connected by the supporter, locking Assembly includes the locking knob and can with locking knob swivelling joint's stripper plate, the locking knob sets up the lateral surface at the every single move extension board, the stripper plate sets up the medial surface at the every single move board, make the interval between locking knob and the stripper plate shorten when forward or reverse rotation locking knob, every single move board and every single move extension board are extruded the fastening and are realized locking, it is corresponding, make the interval increase between locking knob and the stripper plate when reverse or forward rotation locking knob, locking. The supporting seat can adjust the supporting height and the pitching angle, can also rotate, and is stable in supporting and convenient to store.
Description
Technical Field
The utility model belongs to the technical field of the satellite antenna, especially, relate to a VSAT satellite antenna supporting seat.
Background
Among the prior art, the design as an organic whole is mostly followed to the VSAT satellite antenna supporting seat, can't carry out the altitude mixture control transform, and orientation angle also is difficult to control, still has the condition of supporting insecure, even the support area of VSAT satellite antenna supporting seat has been increased, also still exists easily to accomodate and deposits inconvenient problem.
Therefore, how to make the adjustment of VSAT satellite antenna supporting seat realization support height, every single move angle and self rotation angle, guarantee simultaneously that the support of VSAT satellite antenna supporting seat is firm and accomodate conveniently the technical problem that technical personnel in this technical field need solve.
SUMMERY OF THE UTILITY MODEL
The utility model discloses the main technical problem who solves provides a VSAT satellite antenna supporting seat, solves among the prior art height, every single move and the unable regulation of orientation of VSAT satellite antenna supporting seat, supports simultaneously not jail and accomodates inconvenient problem.
For solving the technical problem, the utility model provides a VSAT satellite antenna supporting seat, including every single move board, every single move extension board, extension base, the rotatable setting of every single move board is in extension base top, the every single move board with the every single move extension board passes through locking Assembly and connects, the every single move extension board can be followed the every single move board carries out rectilinear movement, every single move extension board is connected by the supporter, locking Assembly including the locking knob and can with locking knob swivelling joint's stripper plate, the locking knob sets up the lateral surface of every single move extension board, the stripper plate sets up the medial surface of every single move board.
When the locking knob is rotated forwards or reversely, the distance between the locking knob and the extrusion plate is shortened, and the pitching plate and the pitching support plate are extruded and fastened to realize locking; correspondingly, when the locking knob is rotated reversely or positively, the distance between the locking knob and the extrusion plate is increased, and the pitching plate and the pitching support plate are unlocked.
The utility model discloses in another embodiment of VSAT satellite antenna supporting seat, vertical first recess has been seted up to the medial surface of every single move board, the lateral surface of every single move board be provided with the vertical boss that first recess position corresponds, the setting that the stripper plate can be slided from top to bottom is in the first recess vertical rectangular shape through-hole has been seted up in the first recess, vertical second recess has been seted up to the medial surface of every single move extension board, the boss can slide from top to bottom in the second recess, first through-hole has been seted up to the stripper plate, the second through-hole has been seted up in the second recess, first through-hole, second through-hole and rectangular shape through-hole position correspond, the locking knob has the double-screw bolt, the double-screw bolt can pass second through-hole, rectangular shape through-hole, first through-hole will locking knob and stripper plate threaded connection.
The utility model discloses in another embodiment of VSAT satellite antenna supporting seat, be provided with the supporting seat between every single move board and the expansion base, the supporting seat top is provided with and is used for rotating the connection the platform of connecting of every single move board, the supporting seat below is rotated and is connected the expansion base.
The utility model discloses another embodiment of VSAT satellite antenna supporting seat, the extension base includes first stabilizer blade and second stabilizer blade, be provided with first revolving stage on the first stabilizer blade, be provided with the second revolving stage on the second stabilizer blade, the adaptation is seted up to the supporting seat lower extreme and is held the first chamber that holds of first revolving stage, first stabilizer blade lower extreme has been seted up the adaptation and has been held the second of second revolving stage holds the chamber, first stabilizer blade can rotate on the second revolving stage, the supporting seat can rotate on the first revolving stage.
In another embodiment of the VSAT satellite antenna supporting base of the present invention, the first supporting plate is provided with a first supporting plate, the second supporting plate is provided with a second supporting plate, when the first supporting leg is rotated on the second rotating plate, the first supporting plate and the second supporting plate can be gathered together or extended, when the first supporting plate and the second supporting plate are gathered together, the first supporting plate and the second supporting plate are close to and parallel to each other, and when the first supporting plate and the second supporting plate are extended, a included angle can be formed between the first supporting plate and the second supporting plate.
The utility model discloses in another embodiment of VSAT satellite antenna supporting seat, the blind hole has all been seted up to two sides of connecting the platform two damping through-holes of coaxial line are seted up to the lower extreme of every single move board, two leave the confession between the damping through-hole connect the space of platform embedding, work as connect the platform embedding the space, the blind hole with damping through-hole coaxial line one-to-one be provided with damping piece in blind hole and the damping through-hole, damping piece includes fixed part and rotation portion, the fixed part sets up in the blind hole, rotation portion sets up in the damping through-hole, work as when every single move board rotates, drive rotation portion rotates and makes rotation portion with the fixed part produces damping friction.
In another embodiment of the VSAT satellite antenna supporting seat of the present invention, the rotating portion and the surface of the fixed portion contacting each other are provided with wavy concave-convex wheels, and when the rotating portion and the fixed portion rotate relatively, the concave-convex wheels are alternately extruded to generate friction.
The utility model discloses another embodiment of VSAT satellite antenna supporting seat, the mounting hole has been seted up on the every single move extension board be provided with on the mounting hole with the handhole door of mounting hole looks adaptation the medial surface of handhole door is provided with the connection pad, the inboard of mounting hole is provided with the retainer plate, the retainer plate set up with the bearing hole of mounting hole looks adaptation, be provided with nylon packing ring and rotor in the bearing hole set up the screw hole on connection pad and the rotor, connection pad, rotor and by the supporter accessible fix with screw.
The utility model discloses in another embodiment of VSAT satellite antenna supporting seat, the first intracavity that holds is provided with friction gasket and friction packing ring, the second holds the intracavity and is provided with friction gasket, second stabilizer blade lower extreme has been seted up the third and has been held the chamber, the third holds the intracavity and is provided with the connection piece, the connection piece below is provided with the lid and closes the third bottom that holds the chamber, the screw has been seted up on the connection piece, can with through the screw the connection piece with the supporting seat is fixed.
In another embodiment of the VSAT satellite antenna support base of the present invention, the first support plate and the second support plate have support plate through holes formed therein.
The utility model has the advantages that: the utility model discloses a VSAT satellite antenna supporting seat, including the every single move board, the every single move extension board, extended base, the rotatable setting of every single move board is in extended base top, every single move board and every single move extension board pass through locking Assembly and connect, the every single move extension board can be followed the every single move board and carried out rectilinear movement, the every single move extension board is connected by the supporter, locking Assembly includes the locking knob and can with locking knob swivelling joint's stripper plate, the locking knob sets up the lateral surface at the every single move extension board, the stripper plate sets up the medial surface at the every single move board, make the interval between locking knob and the stripper plate shorten when forward or reverse rotation locking knob, every single move board and every single move extension board are extruded the fastening and are realized locking, it is corresponding, make the interval increase between locking knob and the stripper plate when reverse or forward rotation locking knob, locking. This VSAT satellite antenna supporting seat adjustable support height, every single move angle, can also rotate, support simultaneously and stabilize, be convenient for accomodate.
Drawings
Fig. 1 is a schematic view of an embodiment of a VSAT satellite antenna support base according to the present invention;
fig. 2 is an exploded view of a pitch plate, a pitch support plate, and a locking assembly in another embodiment of the VSAT satellite antenna support of the present invention;
fig. 3 is an exploded view of a connection platform and an expansion base in another embodiment of the VSAT satellite antenna support base of the present invention;
fig. 4 is an exploded view of a connection platform and a pitching plate in another embodiment of the VSAT satellite antenna support base of the present invention;
FIG. 5 is a schematic view of the contact surface of the rotating part and the fixed part of the damping member in another embodiment of the VSAT satellite antenna supporting base of the present invention;
fig. 6 is an exploded view of an upper portion of a pitching support plate in another embodiment of the VSAT satellite antenna support of the present invention;
fig. 7 is a schematic view illustrating a bracket storage state in another embodiment of the VSAT satellite antenna support base according to the present invention.
Detailed Description
In order to facilitate understanding of the present invention, the present invention will be described in more detail with reference to the accompanying drawings and specific embodiments. Preferred embodiments of the present invention are shown in the drawings. The invention may, however, be embodied in many different forms and should not be construed as limited to the embodiments set forth herein. Rather, these embodiments are provided so that this disclosure will be thorough and complete.
It is to be noted that, unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs. The terminology used in the description of the invention herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the invention.
FIG. 1 is a schematic view showing an embodiment of a VSAT satellite antenna support according to the present invention, FIG. 2 is a schematic view showing an exploded view of a pitch plate, a pitch plate and a locking assembly in another embodiment of a VSAT satellite antenna support according to the present invention, FIG. 3 is a schematic view showing an exploded view of a connection platform and a docking station in another embodiment of a VSAT satellite antenna support according to the present invention, FIG. 4 is a schematic view showing an exploded view of a connection platform and a pitch plate in another embodiment of a VSAT satellite antenna support according to the present invention, FIG. 5 is a schematic view showing a contact surface of a rotating portion and a fixed portion of a damping member in another embodiment of a VSAT satellite antenna support according to the present invention, FIG. 6 is a schematic view showing an exploded view showing an upper portion of a pitch plate in another embodiment of a VSAT satellite antenna support according to the present invention, FIG., with reference to fig. 1 to 7, the VSAT satellite antenna supporting seat includes a pitching plate 1, a pitching plate 2, and an expansion base 3, wherein the pitching plate 1 is rotatably disposed above the expansion base 3, the pitching plate 1 and the pitching plate 2 are connected by a locking assembly 4, the pitching plate 2 is linearly movable along the pitching plate 1, the pitching plate 2 is connected to a supported body T1, the locking assembly 4 includes a locking knob 41 and a pressing plate 42 rotatably connected to the locking knob 41, the locking knob 41 is disposed on an outer side surface of the pitching plate 2, and the pressing plate 42 is disposed on an inner side surface of the pitching plate 1.
When the locking knob 41 is rotated forwards or backwards to shorten the distance between the locking knob 41 and the extrusion plate 42, the pitch plate 1 and the pitch support plate 2 are extruded and fastened to realize locking; correspondingly, when the locking knob 41 is rotated reversely or forwardly, so that the distance between the locking knob 41 and the extrusion plate 42 is increased, the pitch plate 1 and the pitch brace 2 are unlocked.
Preferably, a vertical first groove 11 is formed on the inner side surface of the pitching plate 1, a vertical boss 12 corresponding to the first groove 11 is arranged on the outer side surface of the pitching plate 1, the extrusion plate 42 is slidably arranged in the first groove 11 up and down, a vertical strip-shaped through hole 13 is arranged in the first groove 11, a vertical second groove 21 is arranged on the inner side surface of the pitching support plate 2, the boss 12 can slide up and down in the second groove 21, the extrusion plate 42 is provided with a first through hole 421, a second through hole 211 is formed in the second groove 21, the first through hole 421, the second through hole 211 and the elongated through hole 13 correspond in position, the locking knob 41 is provided with a stud 411, and the stud 411 can pass through the second through hole 211, the elongated through hole 13 and the first through hole 421 to connect the locking knob 41 and the extrusion plate 42 in a threaded manner.
Through the arrangement, the pitching support plate can move up and down along the pitching plate to determine the supporting height, and then the pitching support plate and the pitching plate are tightly fixed by locking the locking knob and the extrusion plate, so that the supporting height is adjusted.
Further preferably, the width of the pressing plate 42 is adapted to the width of the first groove 11, and the boss 12 is adapted to the second groove 21.
Preferably, a supporting seat 5 is arranged between the pitching plate 1 and the expansion base 3, a connecting platform 51 for rotatably connecting the pitching plate 1 is arranged above the supporting seat 5, and the expansion base 3 is rotatably connected below the supporting seat 5.
Preferably, the extension base 3 includes a first supporting leg 31 and a second supporting leg 32, a first rotating platform 311 is provided on the first supporting leg 31, a second rotating platform 321 is provided on the second supporting leg 32, the lower end of the supporting seat 5 is provided with an adaptation accommodating cavity for accommodating the first rotating platform 311, the lower end of the first supporting leg 31 is provided with an adaptation accommodating cavity for accommodating the second rotating platform 321, the first supporting leg 31 can rotate on the second rotating platform 321, and the supporting seat 5 can rotate on the first rotating platform 311.
Further preferably, a friction gasket D1 and a friction washer D2 are arranged in the first accommodating cavity, a friction gasket D1 is arranged in the second accommodating cavity, a third accommodating cavity is formed in the lower end of the second supporting leg 32, a connecting piece P1 is arranged in the third accommodating cavity, a bottom cover S1 of the third accommodating cavity is arranged below the connecting piece P1 in a covering mode, a screw hole P11 is formed in the connecting piece P1, and the connecting piece P1 and the supporting seat 5 can be fixed through screws. The friction washer and the friction washer are arranged to increase friction force during rotation, so that fixation is facilitated when the friction washer and the friction washer are rotated to a proper position.
Realize through this kind of setting that the dead axle of supporting seat on the expansion base rotates, realized the dead axle rotation of this VSAT satellite antenna supporting seat promptly.
Preferably, first revolving stage 311 side is provided with first backup pad 312, second revolving stage 321 side is provided with second backup pad 322, works as first foot 31 is in when rotating on second revolving stage 321, first backup pad 312 and second backup pad 322 can be gathered together or expand, works as when first backup pad 312 and second backup pad 322 are gathered together, first backup pad 312 and second backup pad 322 are close to and are parallel, works as when first backup pad 312 and second backup pad 322 expand, can form the contained angle between first backup pad 312 and the second backup pad 322.
Further preferably, gathering together and expanding of first backup pad 312 and second backup pad 322 has realized that this VSAT satellite antenna supporting seat supports the regulation of steadiness, can change the steadiness of support through adjusting the contained angle between first backup pad and the second backup pad, when first backup pad and second backup pad draw in and are close to, the two is parallel, area occupied has been reduced, be convenient for accomodate regularly, especially every single move extension board and every single move board rotate simultaneously with the extension base parallel and be close to this extension base, the extension base and every single move board and the every single move extension board that gather together this moment can form a platelike, conveniently get and put.
Preferably, the first support plate 312 and the second support plate 322 are provided with support plate through holes K1. Backup pad through-hole K1 has realized reducing the effect of this VSAT satellite antenna supporting seat weight on the one hand, and usable ground nail passes this backup pad through-hole K1 on the other hand and realizes further improving this VSAT satellite antenna supporting seat and support firm purpose.
Further preferably, another side of first revolving stage is provided with first afterbody W1, first afterbody structure with first backup pad structure is similar, and the length of first afterbody is less than the length of first backup pad, and is corresponding, and another side of second revolving stage is provided with the second afterbody, second afterbody structure with second backup pad structure is similar, and the length of second afterbody is less than the length of second backup pad, and when first backup pad and second backup pad were gathered together, first afterbody and second afterbody were close to together, and the support of first backup pad and second backup pad has been balanced in the setting up of first afterbody and second afterbody, has extended support length.
Further preferably, the first tail portion W1 and the second tail portion are provided with tail through holes, so that on one hand, the weight of the VSAT satellite antenna support seat is reduced, and on the other hand, the VSAT satellite antenna support seat can be firmly fixed at a supporting position by inserting ground nails into the tail through holes.
Preferably, connect two sides of platform 51 and all seted up blind hole 511 two damping through-holes 14 of coaxial line are seted up to the lower extreme of every single move board 1, two leave the confession between damping through-hole 14 connect the space 15 of platform 51 embedding, work as connect platform 51 embedding space 15, blind hole 511 with damping through-hole 14 coaxial line one-to-one be provided with damping piece 6 in blind hole 511 and the damping through-hole 14, damping piece 6 includes fixed part 61 and rotation portion 62, fixed part 61 sets up in the blind hole 511, rotation portion 62 sets up in the damping through-hole 14, work as when every single move board 1 rotates, drive rotation portion 62 rotates and makes rotation portion 62 with fixed part 61 produces damping friction.
The arrangement realizes the stable fixation of the pitching plate when the pitching plate is adjusted to a proper angle.
It is further preferred that a sealing cover 64 is provided to fit the damping through hole 14, and the sealing cover 64 prevents dust from entering the damping through hole 14 and affecting the rotation of the damping member.
It is further preferable that the surface of the rotating part 62 contacting the fixed part 61 is provided with a wavy concave-convex wheel 63, and when the rotating part 62 and the fixed part 61 rotate relatively, the concave-convex wheel 63 alternately presses to generate friction.
Preferably, the pitch brace 2 is provided with a mounting hole 22, the mounting hole 22 is provided with a hole cover 23 adapted to the mounting hole 22, the inner side surface of the hole cover 23 is provided with a connecting disc 24, the inner side of the mounting hole 22 is provided with a fixing ring 25, the fixing ring 25 is provided with a bearing hole 251 adapted to the mounting hole 22, the bearing hole 251 is provided with a nylon gasket 26 and a rotating body 27, the connecting disc 24 and the rotating body 27 are provided with screw holes L1, and the connecting disc 24, the rotating body 27 and a supported body T1 can be fixed by screws.
When the supported body T1 rotates, the connecting disc and the rotating body rotate, and the nylon washer 26 plays a friction role to facilitate the stable fixation when the supported body T1 rotates to a proper angle.
Based on the above embodiment, the utility model discloses a VSAT satellite antenna supporting seat, which comprises a pitching plate, a pitching supporting plate and an expanding base, wherein the pitching plate is rotatably arranged above the expanding base, the pitching plate and the pitching supporting plate are connected through a locking component, the pitching supporting plate can linearly move along the pitching plate, the pitching supporting plate is connected with a supported body, the locking component comprises a locking knob and a pressing plate which can be rotatably connected with the locking knob, the locking knob is arranged on the outer side surface of the pitching supporting plate, the pressing plate is arranged on the inner side surface of the pitching plate, when the locking knob is rotated forward or reversely to shorten the distance between the locking knob and the extrusion plate, the pitching plate and the pitching support plate are extruded and fastened to realize locking, correspondingly, when the locking knob is rotated reversely or positively, the distance between the locking knob and the extrusion plate is increased, and the pitching plate and the pitching support plate are unlocked. This VSAT satellite antenna supporting seat adjustable support height, every single move angle, can also rotate, support simultaneously and stabilize, be convenient for accomodate.
The above only is the embodiment of the present invention, not limiting the scope of the present invention, all the equivalent structure changes made in the specification and the attached drawings or directly or indirectly applied to other related technical fields are included in the protection scope of the present invention.
Claims (10)
1. A VSAT satellite antenna supporting seat is characterized by comprising a pitching plate, a pitching supporting plate and an expansion base, wherein the pitching plate is rotatably arranged above the expansion base, the pitching plate and the pitching supporting plate are connected through a locking assembly, the pitching supporting plate can linearly move along the pitching plate, the pitching supporting plate is connected with a supported body, the locking assembly comprises a locking knob and a squeezing plate which can be rotatably connected with the locking knob, the locking knob is arranged on the outer side surface of the pitching supporting plate, and the squeezing plate is arranged on the inner side surface of the pitching plate;
when the locking knob is rotated forwards or reversely, the distance between the locking knob and the extrusion plate is shortened, and the pitching plate and the pitching support plate are extruded and fastened to realize locking; correspondingly, when the locking knob is rotated reversely or positively, the distance between the locking knob and the extrusion plate is increased, and the pitching plate and the pitching support plate are unlocked.
2. The VSAT satellite antenna support base of claim 1, wherein the inner side surface of the pitching plate is provided with a first vertical groove, the outer side surface of the pitching plate is provided with a vertical boss corresponding to the first groove, the extrusion plate can be arranged in the first groove in a vertically sliding manner, a vertical strip-shaped through hole is arranged in the first groove, a vertical second groove is arranged on the inner side surface of the pitching support plate, the boss can slide up and down in the second groove, the extrusion plate is provided with a first through hole, a second through hole is arranged in the second groove, the first through hole, the second through hole and the strip-shaped through hole are corresponding in position, the locking knob is provided with a stud, and the stud can penetrate through the second through hole, the long strip-shaped through hole and the first through hole to connect the locking knob and the extrusion plate in a threaded mode.
3. The VSAT satellite antenna support base of claim 2, wherein a support base is disposed between the elevation plate and the docking station, a connection platform is disposed above the support base for rotatably connecting the elevation plate, and the docking station is rotatably connected below the support base.
4. The VSAT satellite antenna support base of claim 3, wherein the docking station comprises a first leg and a second leg, the first leg is provided with a first rotating platform, the second leg is provided with a second rotating platform, the lower end of the support base is provided with a first accommodating cavity adapted to accommodate the first rotating platform, the lower end of the first leg is provided with a second accommodating cavity adapted to accommodate the second rotating platform, the first leg is rotatable on the second rotating platform, and the support base is rotatable on the first rotating platform.
5. The VSAT satellite antenna support base of claim 4, wherein a first support plate is arranged on the side of the first rotating platform, a second support plate is arranged on the side of the second rotating platform, when the first support leg rotates on the second rotating platform, the first support plate and the second support plate can be gathered or expanded, when the first support plate and the second support plate are gathered, the first support plate and the second support plate are close to each other and parallel, and when the first support plate and the second support plate are expanded, an included angle can be formed between the first support plate and the second support plate.
6. The VSAT satellite antenna support base of claim 5, wherein blind holes are formed in both side surfaces of the connection platform, two damping through holes having a coaxial line are formed in the lower end of the pitching plate, a gap for the connection platform to be embedded is formed between the two damping through holes, when the connection platform is embedded in the gap, the blind holes and the damping through holes are in coaxial line one-to-one correspondence, damping members are arranged in the blind holes and the damping through holes, each damping member comprises a fixing portion and a rotating portion, the fixing portion is arranged in the blind hole, the rotating portion is arranged in the damping through hole, and when the pitching plate rotates, the rotating portion is driven to rotate and the rotating portion and the fixing portion generate damping friction.
7. The VSAT satellite antenna support base of claim 6, wherein the surface of the rotating portion in contact with the fixed portion is provided with wavy concave-convex wheels, and when the rotating portion rotates relative to the fixed portion, the concave-convex wheels are alternately squeezed to generate friction.
8. The VSAT satellite antenna support base of claim 7, wherein the elevation support plate is provided with a mounting hole, a hole cover is disposed on the mounting hole and is matched with the mounting hole, a connection disc is disposed on an inner side surface of the hole cover, a fixing ring is disposed on an inner side of the mounting hole, a bearing hole matched with the mounting hole is formed in the fixing ring, a nylon washer and a rotating body are disposed in the bearing hole, screw holes are formed in the connection disc and the rotating body, and the connection disc, the rotating body and a supported body can be fixed by screws.
9. The VSAT satellite antenna support base of any one of claims 4 to 8, wherein a friction gasket and a friction washer are disposed in the first accommodating cavity, a friction gasket is disposed in the second accommodating cavity, a third accommodating cavity is formed at a lower end of the second supporting leg, a connecting plate is disposed in the third accommodating cavity, a bottom cover for covering the third accommodating cavity is disposed below the connecting plate, a screw hole is formed in the connecting plate, and the connecting plate and the support base can be fixed by a screw.
10. The VSAT satellite antenna support stand of any one of claims 5-8, wherein the first and second support plates have support plate through holes formed therein.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922415226.9U CN210778932U (en) | 2019-12-29 | 2019-12-29 | VSAT satellite antenna supporting seat |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922415226.9U CN210778932U (en) | 2019-12-29 | 2019-12-29 | VSAT satellite antenna supporting seat |
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| Publication Number | Publication Date |
|---|---|
| CN210778932U true CN210778932U (en) | 2020-06-16 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201922415226.9U Active CN210778932U (en) | 2019-12-29 | 2019-12-29 | VSAT satellite antenna supporting seat |
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| CN (1) | CN210778932U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113419122A (en) * | 2021-05-14 | 2021-09-21 | 同济大学 | Test platform and test method for perception system of automatic driving automobile |
-
2019
- 2019-12-29 CN CN201922415226.9U patent/CN210778932U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113419122A (en) * | 2021-05-14 | 2021-09-21 | 同济大学 | Test platform and test method for perception system of automatic driving automobile |
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Address after: Room 704-717, building C, Huirong Business Plaza, No. 26 Hefeng Road, Xinwu District, Wuxi City, Jiangsu Province, 214000 Patentee after: Jiangsu Yixin Aerospace Technology Co.,Ltd. Address before: 211135 2nd floor, unit B, 300 Zhihui Road, Qilin science and Technology Innovation Park, Jiangning District, Nanjing City, Jiangsu Province Patentee before: NANJING YIXIN AEROSPACE TECHNOLOGY Co.,Ltd. |
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