CN220996817U - Unmanned aerial vehicle equipped with meteorological sensor - Google Patents
Unmanned aerial vehicle equipped with meteorological sensor Download PDFInfo
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- CN220996817U CN220996817U CN202323212399.3U CN202323212399U CN220996817U CN 220996817 U CN220996817 U CN 220996817U CN 202323212399 U CN202323212399 U CN 202323212399U CN 220996817 U CN220996817 U CN 220996817U
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- 230000003139 buffering effect Effects 0.000 abstract description 8
- 230000000694 effects Effects 0.000 abstract description 2
- 230000006872 improvement Effects 0.000 description 6
- 238000012544 monitoring process Methods 0.000 description 5
- 238000010521 absorption reaction Methods 0.000 description 3
- 230000035939 shock Effects 0.000 description 3
- 208000035473 Communicable disease Diseases 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
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- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
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Abstract
The utility model discloses an unmanned aerial vehicle with a meteorological sensor, which comprises the following components: the unmanned aerial vehicle comprises an unmanned aerial vehicle core part, wherein a connecting arm is arranged on the side part of the unmanned aerial vehicle core part, a meteorological sensor mechanism is arranged on the upper part of the unmanned aerial vehicle core part, and a core supporting frame is arranged on the lower part of the unmanned aerial vehicle core part; the lower part of the connecting arm is provided with an adjustable supporting mechanism; the device has the function of expanding the supporting area, is convenient for outwards moving the sliding rod body on the adjustable supporting mechanism, has the function of expanding the supporting area, and ensures that the device is more stable and can not fall down when falling down; the buffer effect is good; the adjustable supporting mechanism has good buffering effect; the whole supportable height of the adjustable supporting mechanism is convenient to adjust according to the actual use condition, and the actual use is convenient; has high practicability and is worth popularizing.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle, in particular to an unmanned aerial vehicle with a meteorological sensor.
Background
At present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer shooting, express delivery transportation, disaster relief, wild animal observation, infectious disease monitoring, mapping, news reporting, electric power inspection, disaster relief, video shooting, romantic manufacturing and the like, and the application of the unmanned aerial vehicle is greatly expanded.
Compared with ground meteorological monitoring, the unmanned aerial vehicle is used for meteorological monitoring, has the advantages of being flexible, efficient and convenient, and is an effective and accurate scheme for meteorological monitoring. The unmanned aerial vehicle of prior art is used for meteorological monitoring, needs to install meteorological sensor, consequently can increase unmanned aerial vehicle's weight to influence unmanned aerial vehicle's safe and stable take off and land. Especially in the landing process, unmanned aerial vehicle does not have safety and stability to reduce, not only can influence unmanned aerial vehicle's safety, also can influence the safety of the meteorological sensor on the unmanned aerial vehicle.
Therefore, there is a need for a better unmanned aerial vehicle equipped with a weather sensor.
Disclosure of utility model
The technical problem to be solved by the utility model is to overcome the defects of the technology and provide the unmanned aerial vehicle with the meteorological sensor.
In order to solve the technical problems, the technical scheme provided by the utility model is that the unmanned aerial vehicle is provided with a meteorological sensor: the unmanned aerial vehicle comprises an unmanned aerial vehicle core part, wherein connecting arms are arranged on the side parts of the unmanned aerial vehicle core part, the connecting arms are a plurality of and are uniformly arranged on the side parts of the unmanned aerial vehicle core part, and a spiral blade mechanism is arranged on the upper part of the tail end of each connecting arm; the upper part of the unmanned aerial vehicle core part is provided with a meteorological sensor mechanism, and the lower part of the unmanned aerial vehicle core part is provided with a core supporting frame; an adjustable supporting mechanism is arranged at the lower part of the connecting arm;
The connecting arm comprises a hollow sliding tube and a sliding rod body; the section of the hollow sliding tube is square, part of the sliding rod body is positioned in the hollow sliding tube and is in sliding fit in the hollow sliding tube, a vertical auxiliary rod is arranged at the front end of the sliding rod body, a damping rod body is arranged at the lower part of the vertical auxiliary rod, a supporting leg is arranged at the tail end of the damping rod body, a hydraulic buffer rod is rotatably arranged at the tail end of the upper part of the vertical auxiliary rod, a U-shaped support is arranged at the tail end of the hydraulic buffer rod, the tail ends of two side wings of the U-shaped support are fixedly connected with the lower part of the hydraulic buffer rod, the extending direction of the U-shaped support and the extending direction of the hydraulic buffer rod are in the same straight line, a nut is fixedly arranged at the back of the U-shaped support, a screw rod is rotatably arranged at the upper side of the tail end of the damping rod body, the screw rod penetrates through the back of the U-shaped support, the screw rod is in threaded fit with the damping rod body, and a rotating disc is arranged at the lower part of the screw rod; the extending direction of the screw rod and the extending direction of the hydraulic buffer rod are on the same straight line;
The upper part of the hollow sliding tube is fixedly connected with the connecting arm.
As a modification, the number of the connecting arms is four.
As an improvement, the bottom of the supporting leg is in a semicircular sphere shape.
As an improvement, friction lines are arranged at the edge of the rotating disc.
As an improvement, the hollow sliding tube and the connecting arm are fixedly connected in a threaded connection mode.
As an improvement, the unmanned aerial vehicle core part and the meteorological sensor mechanism are fixedly connected in a threaded connection mode.
As an improvement, the front part of the hollow sliding tube is provided with a butterfly bolt, the butterfly bolt penetrates through the outer wall of the hollow sliding tube and extends to the inner side of the hollow sliding tube, and the butterfly bolt plays a role in propping against the outer wall of the sliding rod body.
As an improvement, the extending direction of the sliding rod body and the extending direction of the vertical auxiliary rod are mutually perpendicular.
Compared with the prior art, the utility model has the advantages that: the hollow sliding tube on the adjustable supporting mechanism is fixedly connected with the connecting arm in a threaded connection mode, so that the adjustable supporting mechanism is convenient to install and detach; the adjustable supporting mechanism has the function of expanding the supporting area, is convenient for outwards moving the sliding rod body on the adjustable supporting mechanism, has the function of expanding the supporting area, and ensures that the device is more stable and can not fall down when falling down; the adjustable supporting mechanism has good buffering effect; because the hydraulic buffer rod is arranged, the device has good shock absorption and buffering functions, so that the unmanned aerial vehicle is more stable and safer when landing; the whole supportable height of the adjustable supporting mechanism is convenient to adjust according to the actual use condition, and the actual use is convenient; has high practicability and is worth popularizing.
Drawings
FIG. 1 is a schematic view of a structure of a unmanned aerial vehicle equipped with a weather sensor according to the present utility model.
FIG. 2 is a schematic diagram of a second embodiment of a weather sensor-equipped unmanned aerial vehicle according to the present utility model.
FIG. 3 is a side view of a weather sensor equipped drone of the present utility model.
Fig. 4 is a partial enlarged view at a in fig. 1.
Detailed Description
For the purpose of making the objects, technical solutions and advantages of the embodiments of the present utility model more apparent, the technical solutions of the embodiments of the present utility model will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present utility model, and it is apparent that the described embodiments are some embodiments of the present utility model, but not all embodiments of the present utility model. The components of the embodiments of the present utility model generally described and illustrated in the figures herein may be arranged and designed in a wide variety of different configurations.
In the description of the embodiments of the present utility model, it should be noted that, if the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", etc. indicate an azimuth or a positional relationship based on that shown in the drawings, or an azimuth or a positional relationship in which the product of the present utility model is conventionally put when used, it is merely for convenience of describing the present utility model and simplifying the description, and it does not indicate or imply that the apparatus or element to be referred to must have a specific azimuth, be configured and operated in a specific azimuth, and thus should not be construed as limiting the present utility model. Furthermore, the terms "first," "second," "third," and the like are used merely to distinguish between descriptions and should not be construed as indicating or implying relative importance.
Furthermore, the terms "horizontal," "vertical," "overhang" and the like, if any, do not denote a requirement that the component be absolutely horizontal or overhang, but rather may be slightly inclined. As "horizontal" merely means that its direction is more horizontal than "vertical", and does not mean that the structure must be perfectly horizontal, but may be slightly inclined.
In the description of the embodiments of the present utility model, "plurality" means at least 2.
In the description of the embodiments of the present utility model, it should also be noted that, unless explicitly specified and limited otherwise, the terms "disposed," "mounted," "connected," and "connected" should be construed broadly, and may be, for example, fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; can be directly connected or indirectly connected through an intermediate medium, and can be communication between two elements. The specific meaning of the above terms in the present utility model can be understood by those of ordinary skill in the art according to the specific circumstances.
Referring to the accompanying drawings, the unmanned aerial vehicle with the weather sensor comprises an unmanned aerial vehicle core part 1, wherein connecting arms 2 are arranged on the side part of the unmanned aerial vehicle core part 1, the connecting arms 2 are uniformly arranged on the side part of the unmanned aerial vehicle core part 1, and a helical blade mechanism 3 is arranged on the upper part of the tail end of each connecting arm 2; the upper part of the unmanned aerial vehicle core part 1 is provided with a meteorological sensor mechanism 4, and the lower part of the unmanned aerial vehicle core part 1 is provided with a core supporting frame 17; the lower part of the connecting arm 2 is provided with an adjustable supporting mechanism 5;
The connecting arm 2 comprises a hollow sliding tube 6 and a sliding rod body 7; the section of the hollow sliding tube 6 is square, the section of the sliding rod body 7 is square, part of the sliding rod body 7 is positioned in the hollow sliding tube 6 and is in sliding fit in the hollow sliding tube 6, a vertical auxiliary rod 8 is arranged at the front end of the sliding rod body 7, a damping rod body 9 is arranged at the lower part of the vertical auxiliary rod 8, a supporting foot 10 is arranged at the tail end of the damping rod body 9, a hydraulic buffer rod 11 is rotatably arranged at the upper tail end of the vertical auxiliary rod 8, a U-shaped support 12 is arranged at the tail end of the hydraulic buffer rod 11, the tail ends of two side wings of the U-shaped support 12 are fixedly connected with the lower part of the hydraulic buffer rod 11, the extending direction of the U-shaped support 12 and the extending direction of the hydraulic buffer rod 11 are in the same straight line, a nut 13 is fixedly arranged at the back of the U-shaped support 12, a screw 14 is rotatably arranged at the upper side of the tail end of the damping rod body 9, the screw 14 passes through the back of the U-shaped support 12, a threaded fit between the screw 14 and the damping rod body 9 is provided with a disc 15; the extending direction of the screw 14 and the extending direction of the hydraulic buffer rod 11 are on the same straight line;
the upper part of the hollow sliding tube 6 is fixedly connected with the connecting arm 2.
The number of the connecting arms 2 is four.
The bottom of the supporting leg 10 has a semicircular sphere shape.
Friction lines are arranged at the edge of the rotating disc 15.
The hollow sliding tube 6 is fixedly connected with the connecting arm 2 in a threaded connection mode.
The unmanned aerial vehicle core part 1 and the meteorological sensor mechanism 4 are fixedly connected in a threaded connection mode.
The front part of the hollow sliding tube 6 is provided with a butterfly bolt 16, the butterfly bolt 16 penetrates through the outer wall of the hollow sliding tube 6 to extend to the inner side of the hollow sliding tube 6, and the butterfly bolt 16 plays a role in propping against the outer wall of the sliding rod body 7.
The extending direction of the sliding rod body 7 and the extending direction of the vertical auxiliary rod 8 are mutually perpendicular.
In the implementation of the utility model, when a worker using the device uses the device, the weather sensor mechanism 4 is arranged on the unmanned plane core part 1, and the unmanned plane core part 1 and the weather sensor mechanism 4 are fixedly connected through the threaded connection mode, so that the device is convenient to install and detach, and the connection and fixing effects are better through the threaded connection mode. Then the user installs the adjustable supporting mechanisms 5 under the connecting arms 2, and the number of the adjustable supporting mechanisms 5 is the same as the number of the connecting arms 2; the hollow sliding tube 6 on the adjustable supporting mechanism 5 is fixedly connected with the connecting arm 2 in a threaded connection mode, so that the adjustable supporting mechanism is convenient to install and detach.
After the adjustable supporting mechanism 5 is installed, the adjustable supporting mechanism 5 has the function of expanding the supporting area, and because the sliding rod body 7 is positioned in the hollow sliding tube 6 and is in sliding fit in the hollow sliding tube 6, the butterfly bolt 16 is arranged on the front part of the hollow sliding tube 6, the butterfly bolt 16 penetrates through the outer wall of the hollow sliding tube 6 to extend to the inner side of the hollow sliding tube 6, and the butterfly bolt 16 plays a role of propping against the outer wall of the sliding rod body 7, the sliding rod body 7 on the adjustable supporting mechanism 5 can be conveniently moved outwards, the function of expanding the supporting area is realized, and the device is more stable and can not topple when falling.
The adjustable supporting mechanism 5 has good buffering effect; because the hydraulic buffer rod 11 is arranged, the device has good shock absorption and buffering functions, so that the unmanned aerial vehicle is more stable and safer when falling, and the unmanned aerial vehicle and the meteorological sensor mechanism 4 positioned on the core part 1 of the unmanned aerial vehicle are not damaged; the user realizes the rotation of the screw 14 by rotating the rotating disc 15 on the screw 14, thereby realizing the position of the tail end of the damping rod body 9 on the adjustable supporting mechanism 5, being convenient for adjusting the whole supportable height of the adjustable supporting mechanism 5 according to the actual use condition and being convenient for the actual use.
The structure is novel, the design is unique, and the hollow sliding tube 6 on the adjustable supporting mechanism 5 is fixedly connected with the connecting arm 2 in a threaded connection mode, so that the adjustable supporting mechanism is convenient to install and detach; the adjustable supporting mechanism 5 has the function of expanding the supporting area, so that the sliding rod body 7 on the adjustable supporting mechanism 5 can be conveniently moved outwards, and the adjustable supporting mechanism has the function of expanding the supporting area, so that the adjustable supporting mechanism is more stable and does not fall down when falling down; the adjustable supporting mechanism 5 has good buffering effect; the adjustable supporting mechanism 5 has good buffering effect; because the hydraulic buffer rod 11 is arranged, the device has good shock absorption and buffering functions, so that the unmanned aerial vehicle is more stable and safer when landing; the whole supportable height of the adjustable supporting mechanism 5 is convenient to adjust according to the actual use condition, and the actual use is convenient; has high practicability and is worth popularizing.
The utility model and its embodiments have been described above with no limitation, and the actual construction is not limited to the embodiments of the utility model as shown in the drawings. In summary, if one of ordinary skill in the art is informed by this disclosure, a structural manner and an embodiment similar to the technical solution should not be creatively devised without departing from the gist of the present utility model.
Claims (8)
1. An unmanned aerial vehicle equipped with meteorological sensor, its characterized in that:
the unmanned aerial vehicle comprises an unmanned aerial vehicle core part (1), wherein connecting arms (2) are arranged on the side parts of the unmanned aerial vehicle core part (1), the connecting arms (2) are arranged on the side parts of the unmanned aerial vehicle core part (1) in a plurality and uniformly arranged manner, and a helical blade mechanism (3) is arranged on the upper part of the tail end of each connecting arm (2); the upper part of the unmanned aerial vehicle core part (1) is provided with a meteorological sensor mechanism (4), and the lower part of the unmanned aerial vehicle core part (1) is provided with a core supporting frame (17); an adjustable supporting mechanism (5) is arranged at the lower part of the connecting arm (2);
The connecting arm (2) comprises a hollow sliding tube (6) and a sliding rod body (7); the cross section of the hollow sliding tube (6) is square, the cross section of the sliding rod body (7) is square, part of the sliding rod body (7) is positioned in the hollow sliding tube (6) and is in sliding fit with the hollow sliding tube (6), a vertical auxiliary rod (8) is arranged at the front end of the sliding rod body (7), a damping rod body (9) is arranged at the lower part of the vertical auxiliary rod (8), a supporting leg (10) is arranged at the tail end of the damping rod body (9), a hydraulic buffer rod (11) is rotatably arranged at the tail end of the upper part of the vertical auxiliary rod (8), U-shaped brackets (12) are arranged at the tail ends of two side wings of the U-shaped brackets (12) and the lower part of the hydraulic buffer rod (11) are fixedly connected, the extending direction of the U-shaped brackets (12) and the extending direction of the hydraulic buffer rod (11) are on the same straight line, a nut (13) is fixedly arranged at the back of the U-shaped brackets (12), a screw rod (14) is rotatably arranged at the upper side of the tail end of the damping rod body (9), and a screw rod (14) penetrates through the screw rod (14) and is screwed between the screw rod (14) and the lower part of the screw rod (14) in a rotary joint mode; the extending direction of the screw (14) and the extending direction of the hydraulic buffer rod (11) are on the same straight line;
The upper part of the hollow sliding tube (6) is fixedly connected with the connecting arm (2).
2. A weather sensor-equipped drone as claimed in claim 1, wherein:
The number of the connecting arms (2) is four.
3. A weather sensor-equipped drone as claimed in claim 1, wherein:
The bottom of the supporting leg (10) is in a semicircle shape.
4. A weather sensor-equipped drone as claimed in claim 1, wherein:
Friction lines are arranged at the edge of the rotating disc (15).
5. A weather sensor-equipped drone as claimed in claim 1, wherein:
The hollow sliding tube (6) is fixedly connected with the connecting arm (2) in a threaded connection mode.
6. A weather sensor-equipped drone as claimed in claim 1, wherein:
the unmanned aerial vehicle core part (1) and the air-condition sensor mechanism (4) are fixedly connected in a threaded connection mode.
7. A weather sensor-equipped drone as claimed in claim 1, wherein:
The front part of the hollow sliding tube (6) is provided with a butterfly bolt (16), the butterfly bolt (16) penetrates through the outer wall of the hollow sliding tube (6) to extend to the inner side of the hollow sliding tube (6), and the butterfly bolt (16) plays a role in propping against the outer wall of the sliding rod body (7).
8. A weather sensor-equipped drone as claimed in claim 1, wherein:
The extending direction of the sliding rod body (7) and the extending direction of the vertical auxiliary rod (8) are mutually perpendicular.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202323212399.3U CN220996817U (en) | 2023-11-28 | 2023-11-28 | Unmanned aerial vehicle equipped with meteorological sensor |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202323212399.3U CN220996817U (en) | 2023-11-28 | 2023-11-28 | Unmanned aerial vehicle equipped with meteorological sensor |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220996817U true CN220996817U (en) | 2024-05-24 |
Family
ID=91113949
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202323212399.3U Active CN220996817U (en) | 2023-11-28 | 2023-11-28 | Unmanned aerial vehicle equipped with meteorological sensor |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220996817U (en) |
-
2023
- 2023-11-28 CN CN202323212399.3U patent/CN220996817U/en active Active
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