CN220492180U - Airborne antenna - Google Patents
Airborne antenna Download PDFInfo
- Publication number
- CN220492180U CN220492180U CN202321522794.9U CN202321522794U CN220492180U CN 220492180 U CN220492180 U CN 220492180U CN 202321522794 U CN202321522794 U CN 202321522794U CN 220492180 U CN220492180 U CN 220492180U
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- mounting
- mounting seat
- unmanned aerial
- aerial vehicle
- antenna
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- 238000009434 installation Methods 0.000 claims description 36
- 230000008878 coupling Effects 0.000 claims 1
- 238000010168 coupling process Methods 0.000 claims 1
- 238000005859 coupling reaction Methods 0.000 claims 1
- 230000000694 effects Effects 0.000 abstract description 4
- 230000005540 biological transmission Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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Abstract
The utility model discloses an airborne antenna, which relates to the technical field of unmanned aerial vehicle antennas and comprises a first mounting seat, two second mounting seats and an antenna body, wherein the two second mounting seats are respectively arranged on two sides of the first mounting seat, and a connecting mechanism is arranged between the first mounting seat and the second mounting seat; the connecting mechanism comprises a connecting plate, a limiting plate and a spring, a mounting cavity is formed in the first mounting seat, the connecting plate is fixedly arranged on one side of the second mounting seat, and the spring is arranged on one side of the limiting plate; according to the technical scheme provided by the utility model, the mounting seat and the connecting mechanism are adopted, when the antenna body is required to be mounted on the surface of the unmanned aerial vehicle, firstly, idle mounting holes for mounting the antenna are determined, and the first threaded holes in the first mounting seat, the second threaded holes in the second mounting seat and the mounting holes are fixed by threads after the idle mounting holes are formed, so that the antenna body is stably fixed on the surface of the unmanned aerial vehicle, the mounting of the antenna of the unmanned aerial vehicle is more convenient, and the mounting effect is better.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicle antennas, in particular to an airborne antenna.
Background
Unmanned aerial vehicles ("unmanned aerial vehicles"), abbreviated as "UAVs" in english, are unmanned aerial vehicles that are operated by means of radio remote control devices and self-contained program control means, or are operated autonomously, either entirely or intermittently, by a vehicle-mounted computer, and unmanned aerial vehicle antennas are mainly used for the transmission and reception of signals.
Along with unmanned aerial vehicle size's change and functional equipment's increase, just need install unmanned aerial vehicle antenna in certain space, current unmanned aerial vehicle antenna mounting structure is inconvenient to adjust mounting structure according to the installation vacancy in the installation space, leads to the installation inconvenient.
Disclosure of Invention
The utility model aims to solve the technical problem that the unmanned aerial vehicle antenna mounting structure overcomes the defects of the prior art and is used for solving the problem that the unmanned aerial vehicle antenna mounting structure in the prior art is inconvenient to adjust the mounting structure according to the mounting vacancy in the mounting space.
In view of the above, the utility model provides an unmanned aerial vehicle antenna mounting structure, which comprises a first mounting seat, two second mounting seats and an antenna body, wherein the two second mounting seats are respectively mounted on two sides of the first mounting seat, and a connecting mechanism is arranged between the first mounting seat and the second mounting seat;
the connecting mechanism comprises a connecting plate, a limiting plate and a spring, wherein an installation cavity is formed in the first installation seat, the connecting plate is fixedly installed on one side of the second installation seat, the connecting plate is slidably connected in the first installation seat, the limiting plate is fixedly installed on one end of the connecting plate, and the spring is installed on one side of the limiting plate.
Optionally, the spring is fixedly installed between the inner wall of the installation cavity and one side of the limiting plate, and the spring is located on the side wall of the connecting plate.
Optionally, the antenna body is fixedly mounted on the top of the first mounting seat.
Optionally, a plurality of first threaded holes are formed in the first mounting seat, and a plurality of second threaded holes are formed in the second mounting seat.
Optionally, the first mount pad and the second mount pad bottom are all fixed mounting has the supporting pad.
Optionally, the bottom surface of the supporting pad is an arc surface.
From the above technical solutions, the embodiment of the present utility model has the following advantages:
1. according to the unmanned aerial vehicle antenna installation structure, the installation seat and the connecting mechanism are adopted, when the antenna body is required to be installed on the surface of the unmanned aerial vehicle, firstly, idle installation holes for antenna installation are determined, and after the first threaded holes in the first installation seat, the second threaded holes in the second installation seat and the installation holes are fixed through threads, the antenna body is stably fixed on the surface of the unmanned aerial vehicle, so that the unmanned aerial vehicle antenna is more convenient to install, and the installation effect is better.
2. According to the unmanned aerial vehicle antenna mounting structure, the design of the supporting pad is adopted, so that the filling effect can be achieved between the bottom surface of the mounting seat and the surface of the unmanned aerial vehicle after the first mounting seat and the second mounting seat are mounted, the bottom surface of the mounting seat is attached to the surface of the unmanned aerial vehicle, and the mounting is stable.
These features and advantages of the present utility model will be disclosed in detail in the following detailed description and the accompanying drawings.
Drawings
The utility model is further described with reference to the accompanying drawings:
FIG. 1 is a schematic diagram of the structure of the present utility model;
FIG. 2 is a schematic cross-sectional view of the present utility model;
FIG. 3 is a schematic view of a partial structure of one side of the present utility model.
Reference numerals illustrate: 1. a first mount; 2. a second mounting base; 3. an antenna body; 4. a first threaded hole; 5. a second threaded hole; 6. a mounting cavity; 7. a connecting plate; 8. a limiting plate; 9. a spring; 10. and a support pad.
Detailed Description
The technical solutions of the embodiments of the present utility model will be explained and illustrated below with reference to the drawings of the embodiments of the present utility model, but the following embodiments are only preferred embodiments of the present utility model, and not all embodiments. Based on the examples in the implementation manner, other examples obtained by a person skilled in the art without making creative efforts fall within the protection scope of the present utility model.
An unmanned aerial vehicle antenna mounting structure according to an embodiment of the present utility model is specifically described below with reference to the accompanying drawings.
Example 1
For easy understanding, referring to fig. 1 to 3, an embodiment of an antenna mounting structure for an unmanned aerial vehicle provided by the utility model includes a first mounting seat 1, two second mounting seats 2 and an antenna body 3, wherein the two second mounting seats 2 are respectively mounted at two sides of the first mounting seat 1, and a connecting mechanism is arranged between the first mounting seat 1 and the second mounting seat 2;
the connecting mechanism comprises a connecting plate 7, a limiting plate 8 and a spring 9, wherein an installation cavity 6 is formed in the first installation seat 1, the connecting plate 7 is fixedly installed on one side of the second installation seat 2, the connecting plate 7 is slidably connected inside the first installation seat 1, the limiting plate 8 is fixedly installed on one end of the connecting plate 7, the spring 9 is installed on one side of the limiting plate 8, a plurality of first threaded holes 4 are formed in the first installation seat 1, a plurality of second threaded holes 5 are formed in the second installation seat 2, and the first installation seat 1 and the second installation seat 2 can be installed on the unmanned aerial vehicle through the anti-falling bolts by the aid of the first threaded holes 4 and the second threaded holes 5.
When the antenna body 3 is required to be mounted on the surface of the unmanned aerial vehicle, the idle mounting hole of the antenna is firstly determined, the first threaded hole 4 and the surface mounting hole of the unmanned aerial vehicle are firstly fixed through threads after the first threaded hole is moved by the first mounting seat 1, the second threaded hole 5 and other mounting holes in the second mounting seat 2 are fixed through threads after the second mounting seat 2 is pulled and adjusted, and therefore the antenna body 3 is stably fixed on the surface of the unmanned aerial vehicle.
In some embodiments, as shown in fig. 2, the spring 9 is fixedly installed between the inner wall of the installation cavity 6 and one side of the limiting plate 8, and the spring 9 is located on the side wall of the connecting plate 7.
It should be noted that, through installing the spring 9 between limiting plate 8 and installation cavity 6, the holding power of spring 9 still can prevent that first mount pad 1 from sending out the condition of taking off when the bolt loosens in first screw hole 4, makes the antenna installation more stable.
Example 2
In some embodiments, as shown in fig. 3, a plurality of first threaded holes 4 are formed in the first mounting seat 1, a plurality of second threaded holes 5 are formed in the second mounting seat 2, the bottom surface of the support pad 10 is an arc surface, and the support pad 10 is made of rubber.
It should be noted that, through setting up supporting pad 10 can be installed the back at first mount pad 1 and second mount pad 2 and play the filling effect between mount pad bottom surface and unmanned aerial vehicle surface, make mount pad bottom surface and unmanned aerial vehicle surface more laminate, make the installation back more stable.
The bolts, springs 9 and support pads 10 are well known components and will not be described here.
Working principle: when the antenna body 3 is required to be installed on the surface of the unmanned aerial vehicle, firstly, idle installation holes for antenna installation are determined, the first threaded holes 4 and the surface installation holes of the unmanned aerial vehicle are firstly fixed through threads after the first installation seat 1 is moved, the second threaded holes 5 and other installation holes in the second installation seat 2 are fixed through threads after the second installation seat 2 is pulled and adjusted, and therefore the antenna body 3 is stably fixed on the surface of the unmanned aerial vehicle.
The above embodiments are merely for illustrating the technical solution of the present application, and not for limiting the same; although the present application has been described in detail with reference to the foregoing embodiments, it should be understood by those of ordinary skill in the art that: the technical scheme described in the foregoing embodiments can be modified or some technical features thereof can be replaced by equivalents; such modifications and substitutions do not depart from the spirit and scope of the corresponding technical solutions.
Claims (6)
1. An airborne antenna, characterized by: the antenna comprises a first mounting seat (1), two second mounting seats (2) and an antenna body (3), wherein the two second mounting seats (2) are respectively arranged on two sides of the first mounting seat (1), and a connecting mechanism is arranged between the first mounting seat (1) and the second mounting seat (2);
coupling mechanism includes connecting plate (7), limiting plate (8) and spring (9), installation cavity (6) have been seted up to inside first mount pad (1), connecting plate (7) fixed mounting is in second mount pad (2) one side, connecting plate (7) sliding connection is in inside first mount pad (1), limiting plate (8) fixed mounting is in connecting plate (7) one end, spring (9) are installed limiting plate (8) one side.
2. An airborne antenna according to claim 1, characterized in that: the spring (9) is fixedly arranged between the inner wall of the mounting cavity (6) and one side of the limiting plate (8), and the spring (9) is positioned on the side wall of the connecting plate (7).
3. An airborne antenna according to claim 1, characterized in that: the antenna body (3) is fixedly arranged at the top of the first mounting seat (1).
4. An airborne antenna according to claim 1, characterized in that: the first mounting seat (1) is internally provided with a plurality of first threaded holes (4), and the second mounting seat (2) is internally provided with a plurality of second threaded holes (5).
5. An airborne antenna according to claim 1, characterized in that: the bottoms of the first mounting seat (1) and the second mounting seat (2) are fixedly provided with supporting pads (10).
6. An airborne antenna according to claim 5, characterized in that: the bottom surface of the supporting pad (10) is an arc-shaped surface.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321522794.9U CN220492180U (en) | 2023-06-14 | 2023-06-14 | Airborne antenna |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321522794.9U CN220492180U (en) | 2023-06-14 | 2023-06-14 | Airborne antenna |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220492180U true CN220492180U (en) | 2024-02-13 |
Family
ID=89828180
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321522794.9U Active CN220492180U (en) | 2023-06-14 | 2023-06-14 | Airborne antenna |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220492180U (en) |
-
2023
- 2023-06-14 CN CN202321522794.9U patent/CN220492180U/en active Active
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| Date | Code | Title | Description |
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| GR01 | Patent grant | ||
| GR01 | Patent grant |