CN218632417U - Satellite antenna equipment support frame - Google Patents
Satellite antenna equipment support frame Download PDFInfo
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- CN218632417U CN218632417U CN202222566564.4U CN202222566564U CN218632417U CN 218632417 U CN218632417 U CN 218632417U CN 202222566564 U CN202222566564 U CN 202222566564U CN 218632417 U CN218632417 U CN 218632417U
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- support
- supporting
- satellite antenna
- support frame
- transverse edge
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02D—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN INFORMATION AND COMMUNICATION TECHNOLOGIES [ICT], I.E. INFORMATION AND COMMUNICATION TECHNOLOGIES AIMING AT THE REDUCTION OF THEIR OWN ENERGY USE
- Y02D30/00—Reducing energy consumption in communication networks
- Y02D30/70—Reducing energy consumption in communication networks in wireless communication networks
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Abstract
The utility model discloses a satellite antenna equipment support frame, including a plurality of backup pads and a plurality of supporting beam, a plurality of supporting beam enclose in proper order and close the connection, and every supporting beam's lateral wall corresponds the upper portion of connecting a backup pad, and the lower part leanin of backup pad sets up, and each backup pad is used for corresponding the laminating and supports first antenna element. This satellite antenna equipment support frame can carry out the adaptation to the many oscillator antennas and support, and structural reliability is strong.
Description
Technical Field
The utility model belongs to the antenna field especially relates to a satellite antenna equipment support frame.
Background
In the prior art, a satellite antenna has a plurality of antenna elements combined, each element is arranged in a different manner, and has specific requirements on the shape, the arrangement angle, the direction and the like of each element, and the antenna elements need to be fixedly arranged by corresponding to adaptive supporting structures and can be adapted to the shape structure and the arrangement manner of the antenna elements.
Therefore, how to realize adaptive support of the multi-element antenna is a technical problem to be solved by those skilled in the art.
SUMMERY OF THE UTILITY MODEL
The utility model discloses the main technical problem who solves provides a satellite antenna equipment support frame, and it is convenient inadequately to solve among the prior art antenna support frame assembly and disassembly, and is bulky, and weight is heavy, can't carry out the problem of stabilizing the support to the antenna element.
For solving above-mentioned technical problem, the utility model provides a satellite antenna equipment support frame is provided, including a plurality of backup pads and a plurality of supporting beam, a plurality of supporting beam enclose in proper order and close the connection, and every supporting beam's lateral wall corresponds the upper portion of connecting a backup pad, and the lower part leanin of backup pad sets up, and each backup pad is used for corresponding the laminating and supports a first antenna element.
Preferably, the number of the supporting plates and the number of the supporting beams are four, and the four supporting beams are enclosed to form a square.
Preferably, the whole supporting plate is of a linear hexagonal structure and comprises a first transverse edge and a second transverse edge which are horizontally arranged in parallel, the first transverse edge is positioned at the upper part, the second transverse edge is positioned at the lower part, and the length of the first transverse edge is greater than that of the second transverse edge; the first vertical edge is positioned at the upper part, the upper end of the first vertical edge is combined with the left end of the first transverse edge, the second vertical edge is positioned at the lower part, and the lower end of the second vertical edge is combined with the right end of the second transverse edge; the lower extreme on first perpendicular limit is connected to the upper end on first slope limit, and the left end on the horizontal limit of second is connected to the lower extreme on first slope limit, and the right-hand member on first horizontal limit is connected to the upper end on second slope limit, and the upper end on second perpendicular limit is connected to the lower extreme on second slope limit.
Preferably, the lower portion of the support plate is inclined inwardly by an angle in the range of 20 to 70.
Preferably, the support plate is combined with the support beam surface, the surface of the support beam combined with the support plate is an inclined surface, and the angle of the inclined surface is the same as the inward inclined angle of the lower part of the support plate.
Preferably, the support device further comprises a support foot, wherein the support foot is provided with an inclined support surface, and the support surface is used for being attached to the lower part of the support plate.
Preferably, still include the supporting disk, the supporting disk level sets up, and the border of the lateral wall connection supporting disk of a plurality of supporting beams closes the supporting disk, and the supporting disk is used for the laminating to support second antenna oscillator.
Preferably, four connecting portions extend out of the edge of the supporting plate, and the four connecting portions are respectively connected with the middle positions of the four supporting beams in a one-to-one correspondence manner.
Preferably, a first via hole is formed in the center of the supporting disc, a plurality of second via holes are annularly formed around the first via hole, and each second via hole corresponds to one second antenna oscillator up and down.
Preferably, the edge of the supporting disk extends out of four connecting parts, and the four connecting parts are respectively connected with the middle positions of the four supporting beams in a one-to-one correspondence manner.
The utility model has the advantages that: the utility model discloses a satellite antenna equipment support frame, including a plurality of backup pads and a plurality of supporting beam, a plurality of supporting beam enclose in proper order and close the connection, and every supporting beam's lateral wall corresponds the upper portion of connecting a backup pad, and the lower part leanin of backup pad sets up, and each backup pad is used for corresponding laminating support first antenna element. This satellite antenna equipment support frame can carry out the adaptation to the many oscillator antennas and support, and structural reliability is strong.
Drawings
Fig. 1 is a schematic view of an embodiment of the satellite antenna assembly support frame of the present invention;
fig. 2 is a schematic view of another embodiment of the satellite antenna assembling support frame of the present invention;
fig. 3 is a schematic view of the connection relationship between the support plate and the first antenna element in another embodiment of the satellite antenna assembly support frame of the present invention;
fig. 4 is a schematic view of a support plate in another embodiment of the satellite antenna assembly support frame of the present invention;
fig. 5 is a schematic view of a supporting leg in another embodiment of the satellite antenna assembling support frame of the present invention;
fig. 6 is a schematic view of a supporting leg in another embodiment of the satellite antenna assembling support frame of the present invention;
fig. 7 is a cross-sectional view of another embodiment of the satellite antenna assembly support frame of 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.
In the drawings, an arrow X indicates a front-side direction, i.e., a front-rear direction, an arrow Y indicates a side direction, i.e., a left-right direction, and an arrow Z indicates a vertical direction, i.e., an up-down direction.
With reference to fig. 1, fig. 2, fig. 3 and fig. 4, this satellite antenna assembles support frame includes a plurality of backup pads 1 and a plurality of supporting beam 2, a plurality of supporting beam 2 enclose in proper order and close the connection, increase the convenience of equipment or dismantlement, the whole degree of stability of this satellite antenna assembles support frame has also been strengthened, and the upper portion of a backup pad 1 is connected to every supporting beam 2's lateral wall correspondence, the lower part of backup pad 1 inwards inclines to set up, each backup pad 1 is used for corresponding laminating and supports a first antenna element Z1, here first antenna element can be the antenna element of shape and size and backup pad 1 looks adaptation, backup pad 1 can carry out the stable support to antenna element or antenna, supporting beam 2's setting has strengthened the stability of backup pad 1 simultaneously.
Preferably, the lower portion of the support plate 1 is inclined inwardly by an angle ranging from 20 to 70.
Preferably, the support plate 1 is surface-coupled to the support beam 2, and the surface of the support beam 2 coupled to the support plate 1 is an inclined surface having the same angle as the inward inclination of the lower portion of the support plate 1.
Preferably, still include supporting disk 3, supporting disk 3 level sets up, the border of a plurality of supporting beams 2's lateral wall connection supporting disk 3 and enclose supporting disk 3, this kind of setting form makes supporting beam 2 and supporting disk 3 surround and is connected, strengthens the firm degree of supporting disk 3 self, supporting disk 3 is used for the laminating to support the second antenna oscillator, the second antenna oscillator here can be the antenna oscillator of shape and size and supporting disk 3 looks adaptations.
Preferably, the lower part of the supporting plate 1 inclines towards the central axis of the supporting plate 3, that is, the opening formed by the enclosing of the upper edges of the supporting plates 1 is larger than the opening formed by the enclosing of the lower edges of the supporting plates 1, so that on one hand, the lower edges of the supporting plates 1 can stably support the whole satellite antenna assembling and supporting frame, on the other hand, the occupied space area of the lower edge support of the supporting plates 1 can be reduced, and the whole volume of the satellite antenna assembling and supporting frame is reduced.
Preferably, the acute angle formed by the support plate 1 and the central axis of the support plate 3 is in the range of 20 ° to 70 °.
Preferably, the angle of the acute angle formed by the central axes of the supporting plate 1 and the supporting plate 3 is 30 degrees, a supporting included angle can be formed well, the supporting stability is enhanced, meanwhile, the included angle of 30 degrees can be balanced between the supporting stability and the supporting height of the supporting plate 1, the supporting height of the supporting plate 1 can be reduced when the angle of the acute angle is gradually increased, and the overall height of the satellite antenna assembling supporting frame can also be reduced.
Preferably, the supporting plate 1 and the supporting beam 2 are four, and the four supporting beams 2 are enclosed to form a square, so that the supporting beams 2 are uniformly arranged, and the supporting plate 3 is conveniently surrounded.
Preferably, the width of the supporting plate 1 is gradually widened from bottom to top, and the plate body of the supporting plate 1 is gradually inclined to the left from bottom to top.
Preferably, the whole supporting plate 1 is of a straight line hexagonal structure and comprises a first transverse edge 101 and a second transverse edge 102 which are horizontally arranged in parallel, the first transverse edge 101 is positioned at the upper part, the second transverse edge 102 is positioned at the lower part, and the length of the first transverse edge 101 is greater than that of the second transverse edge 102; the device also comprises a first vertical edge 103 and a second vertical edge 104 which are vertically arranged in parallel, wherein the first vertical edge 103 is positioned at the upper part, the upper end of the first vertical edge 103 is combined with the left end of the first transverse edge 101, the second vertical edge 104 is positioned at the lower part, and the lower end of the second vertical edge 104 is combined with the right end of the second transverse edge 102; the antenna support plate is characterized by further comprising a first inclined edge 105 and a second inclined edge 106 which are obliquely arranged, the upper end of the first inclined edge 105 is connected with the lower end of the first vertical edge 103, the lower end of the first inclined edge 105 is connected with the left end of the second transverse edge 102, the upper end of the second inclined edge 106 is connected with the right end of the first transverse edge 101, the lower end of the second inclined edge 106 is connected with the upper end of the second vertical edge 104, and the support plate 1 is matched with the first antenna oscillator in shape.
Further preferably, the first fixing hole 109 is formed in the peripheral edge of the supporting plate 1, and similarly, a fixing hole for screw connection with the first fixing hole 109 is also formed in the first antenna oscillator, so that the first antenna oscillator and the first antenna oscillator can be conveniently and fixedly connected through screws.
Preferably, the plate surface of the support plate 1 is provided with a plurality of mutually cross-connected reinforcing ribs 11, and the arrangement of the reinforcing ribs 11 enhances the structural firmness of the support plate 1 and enhances the support stability of the support plate 1.
Preferably, four connecting portions 31 extend out from the edge of the supporting disk 3, four connecting portions 31 respectively connect the middle positions of four supporting beams 2 in a one-to-one correspondence manner, the connecting portions 31 are arranged to enhance the connection stability of the supporting disk 3 and the supporting beams 2, the supporting of the supporting disk 3 is more stable, meanwhile, the connecting portions 31 are arranged to realize the rapid disassembly and assembly of the supporting disk 3 from the supporting beams 2, and the supporting disk 3 and the supporting beams 2 are connected through screws or bolts.
Further preferably, the connecting portion 31 is square, and the connecting portion 31 is provided with a screw hole for facilitating the fixation of a screw or a screw.
Preferably, the support disc 3 is circular disc-shaped.
Preferably, a first through hole 32 is formed in the center of the support plate 3, the first through hole 32 is used for exposing the navigation positioning antenna, a plurality of second through holes 33 are annularly formed around the first through hole 32, and each second through hole 33 corresponds to one second antenna oscillator up and down.
Further preferably, a plurality of second through holes 33 are uniformly arranged around the central point of the support plate 3 in an annular manner, the second through holes 33 are oblong holes, and each second through hole 33 vertically corresponds to an antenna element.
Preferably, with reference to fig. 5 and 6, the support device further includes a support leg 4, the support leg 4 has a support surface 41 disposed obliquely and a fixing groove 42 disposed on the back of the support surface 41 and opened vertically, a lower portion of the fixing groove 42 is a horizontally disposed fixing surface, and the support surface 41 is used for attaching to the lower portion of the support plate 1.
Preferably, the inclination angle of the supporting surface 41 is the same as the inclination angle of the supporting plate 1, the supporting surface 41 is used for attaching the supporting plate 1, and the supporting surface 41 is provided with a screw hole 411 for connecting with the supporting plate 1 by a screw, so as to enhance the connection stability between the supporting plate 1 and the supporting foot 4.
Preferably, the supporting leg fixed orifices has been seted up at the lower part border of backup pad 1, the supporting leg fixed orifices includes first supporting leg fixed orifices 107 and second supporting leg fixed orifices 108, first supporting leg fixed orifices 107 is located the lower part left side of backup pad 1, second supporting leg fixed orifices 108 is located the lower part right side of backup pad 1, and is same, set up the screw hole of position and supporting leg fixed orifices one-to-one respectively on the left side and the right side of the lower part of first antenna oscillator Z1, first antenna oscillator Z1's screw hole promptly, supporting leg fixed orifices and screw 411 three pass through screw fastening and link together, make supporting legs 4 laminating support first antenna oscillator Z1 and backup pad 1.
Further preferably, a screw hole 421 for fixing the support foot 4 is opened on the bottom surface of the fixing groove 42, for example, the support foot 4 is fixed on a base on which an antenna is mounted.
Referring to fig. 7 again, the supporting beam 2 and the supporting plate 1 are integrally formed, so that the structure is firmer, or the supporting beam 2 and the supporting plate 1 are in surface contact, that is, the edge of the supporting beam 2 in contact with the supporting plate 1 is an inclined plane, so that the supporting plate 1 can be attached to the surface of the supporting plate conveniently.
Based on above embodiment, the utility model discloses a satellite antenna equipment support frame, including a plurality of backup pads and a plurality of supporting beam, a plurality of supporting beam enclose in proper order and close the connection, and every supporting beam's lateral wall corresponds the upper portion of connecting a backup pad, and the lower part leanin of backup pad sets up, and each backup pad is used for corresponding the laminating and supports first antenna element. This satellite antenna equipment support frame can carry out the adaptation to the many oscillator antennas and support, and structural reliability is strong.
The above embodiments are only embodiments of the present invention, not limiting the scope of the present invention, all the equivalent structure changes made in the specification and drawings or directly or indirectly applied to other related technical fields are included in the protection scope of the present invention.
Claims (9)
1. The utility model provides a satellite antenna equipment support frame, its characterized in that includes a plurality of backup pads and a plurality of supporting beam, and is a plurality of supporting beam encloses in proper order and closes the connection, and every supporting beam's lateral wall corresponds connects one the upper portion of backup pad, the lower part leanin setting of backup pad, each the backup pad is used for corresponding the laminating and supports a first antenna element.
2. The satellite antenna assembly support frame of claim 1, wherein the number of the support plates and the support beams is four, and the four support beams enclose a square.
3. The satellite antenna assembly support frame of claim 2, wherein the support plate is generally of a rectilinear hexagonal configuration and includes a first transverse edge and a second transverse edge arranged horizontally in parallel, the first transverse edge being located at an upper portion and the second transverse edge being located at a lower portion, the first transverse edge being longer than the second transverse edge; the first vertical edge is positioned at the upper part, the upper end of the first vertical edge is combined with the left end of the first transverse edge, the second vertical edge is positioned at the lower part, and the lower end of the second vertical edge is combined with the right end of the second transverse edge; still including the first slope limit and the second slope limit that the slope set up, the upper end on first slope limit is connected the lower extreme on first perpendicular limit, the lower extreme on first slope limit is connected the left end on the horizontal limit of second, the upper end on second slope limit is connected the right-hand member on first horizontal limit, the lower extreme on second slope limit is connected the upper end on second perpendicular limit.
4. The satellite antenna assembly support bracket of claim 3, wherein the lower portion of the support plate is angled inwardly in the range of 20 ° -70 °.
5. The satellite antenna assembly support frame of claim 4, wherein the support plate and the support beam are combined, and the combination surface of the support beam and the support plate is an inclined surface having the same angle as the inward inclination angle of the lower portion of the support plate.
6. The satellite antenna assembly support frame of claim 5, further comprising a support foot having an inclined support surface for snugly supporting a lower portion of the support plate.
7. The satellite antenna assembles support frame of claim 1, further includes the supporting disk, the supporting disk sets up horizontally, the border of a plurality of the supporting beam's lateral wall connection the supporting disk and enclose the supporting disk, the supporting disk is used for laminating support second antenna element.
8. The satellite antenna assembly support bracket of claim 7, wherein a first via hole is formed in the center of the support plate, a plurality of second via holes are annularly formed around the first via hole, and each second via hole corresponds to one of the second antenna elements up and down.
9. The satellite antenna assembly support frame of claim 8, wherein four connecting portions extend from the edge of the support plate, and the four connecting portions are respectively connected with the middle positions of the four support beams in a one-to-one correspondence manner.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222566564.4U CN218632417U (en) | 2022-09-27 | 2022-09-27 | Satellite antenna equipment support frame |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222566564.4U CN218632417U (en) | 2022-09-27 | 2022-09-27 | Satellite antenna equipment support frame |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218632417U true CN218632417U (en) | 2023-03-14 |
Family
ID=85468568
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202222566564.4U Active CN218632417U (en) | 2022-09-27 | 2022-09-27 | Satellite antenna equipment support frame |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN218632417U (en) |
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2022
- 2022-09-27 CN CN202222566564.4U patent/CN218632417U/en active Active
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