CN211869695U - Meteorological unmanned aerial vehicle with shock-absorbing structure - Google Patents
Meteorological unmanned aerial vehicle with shock-absorbing structure Download PDFInfo
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- CN211869695U CN211869695U CN202020312708.1U CN202020312708U CN211869695U CN 211869695 U CN211869695 U CN 211869695U CN 202020312708 U CN202020312708 U CN 202020312708U CN 211869695 U CN211869695 U CN 211869695U
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- aerial vehicle
- unmanned aerial
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- 238000013016 damping Methods 0.000 claims abstract description 11
- 239000000523 sample Substances 0.000 claims abstract description 8
- 230000001681 protective effect Effects 0.000 claims description 15
- 230000009471 action Effects 0.000 abstract description 9
- 238000013461 design Methods 0.000 abstract description 5
- 238000012544 monitoring process Methods 0.000 abstract description 4
- 230000007246 mechanism Effects 0.000 abstract description 2
- 238000011161 development Methods 0.000 description 4
- 230000000694 effects Effects 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- 238000010586 diagram Methods 0.000 description 3
- 230000035939 shock Effects 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 2
- 230000006872 improvement Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000004880 explosion Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
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Abstract
The utility model discloses a meteorological unmanned aerial vehicle with shock-absorbing structure, including the unmanned aerial vehicle body, it is a plurality of actuating motor, it is a plurality of all to install at the top of fixing base helical blade is all installed at actuating motor's top, and is a plurality of the safety cover corresponding with helical blade is all installed in actuating motor's the outside, the top of supporting seat is provided with wind speed monitor, two support columns of the equal fixedly connected with in both sides at unmanned aerial vehicle body bottom center, it is two sets of flexible leg, two damping spring corresponding with flexible leg are all installed at the center of spout, the center of unmanned aerial vehicle body bottom is provided with camera probe. The utility model discloses in, this meteorological unmanned aerial vehicle with shock-absorbing structure not only can carry out normal meteorological monitoring and the control of making a video recording, also the design has multiple protection and damper simultaneously, can play fine guard action to unmanned aerial vehicle's fuselage and flight mechanism, is worth wideling popularize.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field especially relates to a meteorological unmanned aerial vehicle with shock-absorbing structure.
Background
Unmanned aerial vehicle, as the name suggests unmanned aircraft, since the birth of the aircraft in the beginning of the 20 th century, people at that time have already proposed the idea of unmanned aircraft due to the safety of piloting aircraft, as the unmanned aerial vehicle technology is gradually mature, the manufacturing cost and the entrance threshold are reduced, the market of consumer-grade unmanned aerial vehicle has exploded, the market of civil unmanned aerial vehicle is in the early night before the explosion, the market of domestic unmanned aerial vehicle is a happy piece, the industry experts show that although the development of the domestic unmanned aerial vehicle industry is still in the starting stage, the domestic unmanned aerial vehicle enterprise is thick and thin in the years, grows rapidly and becomes the outstanding people in the whole industry, the future development of civil unmanned aerial vehicle focuses on the use mode and the use safety of subjective unmanned aerial vehicle, firstly, after the unmanned aerial vehicle has a trend of greatly reduced price, the common small civil unmanned aerial vehicle is more easily used as a monitoring tool, the security can not be guaranteed, and due to the consideration of the security and the privacy, the supervision policy of the civil unmanned aerial vehicle is not completely opened by all countries in the world so far.
Along with the continuous progress of society, the continuous development of science and technology, unmanned aerial vehicle technique has also obtained big development, and unmanned aerial vehicle has all obtained using in many fields in recent years, and meteorological unmanned aerial vehicle is exactly used for carrying out high altitude meteorological monitoring, but there is certain defect in present unmanned aerial vehicle device structural design, and stability and shock resistance all remain to be improved for this reason, we have provided a new meteorological unmanned aerial vehicle who has shock-absorbing structure.
SUMMERY OF THE UTILITY MODEL
The utility model aims at solving the shortcoming that exists among the prior art, and the meteorological unmanned aerial vehicle with shock-absorbing structure who proposes.
In order to achieve the above purpose, the utility model adopts the following technical scheme: a meteorological unmanned aerial vehicle with a damping structure comprises an unmanned aerial vehicle body, wherein fixed seats are fixedly connected at the corners of the unmanned aerial vehicle body, driving motors are mounted at the tops of the fixed seats, helical blades are mounted at the tops of the driving motors, protective covers corresponding to the helical blades are mounted on the outer sides of the driving motors, a supporting seat is fixedly connected with the center of the top of the unmanned aerial vehicle body, a wind speed monitor is arranged at the top of the supporting seat, a protective top cover is arranged at the top of the wind speed monitor, two supporting columns are fixedly connected with two sides of the center of the bottom of the unmanned aerial vehicle body, telescopic legs are mounted at the bottoms of the two groups of supporting columns, sliding grooves are formed in the centers of the two supporting columns, damping springs corresponding to the telescopic legs are mounted at the centers of the two sliding grooves, and a camera probe is arranged at the center, and mounting frames are arranged on two sides of the camera probe.
As a further description of the above technical solution:
it is a plurality of the outside of safety cover all is installed the elasticity guard circle, and is a plurality of the inboard equal fixedly connected with of elasticity guard circle is a plurality of and the corresponding rubber connecting block of safety cover.
As a further description of the above technical solution:
the outer wall of two flexible legs has all cup jointed the sponge protective sheath.
As a further description of the above technical solution:
two the flexible leg all is the setting of U type structure.
As a further description of the above technical solution:
the through-hole corresponding with flexible leg is all seted up at the center of support column bottom two the both ends of flexible leg are all run through the through-hole and are extended to the center of spout, two the equal fixedly connected with stopper in both ends of flexible leg.
As a further description of the above technical solution:
equal fixedly connected with in edge of unmanned aerial vehicle body bottom and the corresponding rubber support pole of helical blade.
The utility model discloses following beneficial effect has: 1. the utility model provides a meteorological unmanned aerial vehicle with shock-absorbing structure compares with traditional device, the device simple structure, convenient and practical through the simple protection machanism of design, can play omnidirectional shock attenuation and guard action to the organism when unmanned aerial vehicle is out of control or drops suddenly to greatly reduced its loss.
2. The device compares with traditional device, and its structure and design all have great innovation and improvement, and this meteorological unmanned aerial vehicle with shock-absorbing structure not only can carry out normal meteorological monitoring and the control of making a video recording, also has multiple protection and damper of design simultaneously, can play fine guard action to unmanned aerial vehicle's fuselage and flight mechanism, and work efficiency improves greatly, is worth wideling popularize.
Drawings
Fig. 1 is a main view structure diagram of a meteorological unmanned aerial vehicle with a damping structure provided by the present invention;
fig. 2 is a top view structural diagram of a meteorological unmanned aerial vehicle with a damping structure provided by the present invention;
fig. 3 is the utility model provides a mounting structure schematic diagram of meteorological unmanned aerial vehicle supporting leg with shock-absorbing structure.
Illustration of the drawings:
1. an unmanned aerial vehicle body; 2. a fixed seat; 3. a drive motor; 4. a helical blade; 5. a protective cover; 6. an elastic protection ring; 7. a rubber connecting block; 8. a supporting seat; 9. a wind speed monitor; 10. a protective top cover; 11. a support pillar; 12. a telescopic leg; 13. a sponge protective sleeve; 14. a chute; 15. a damping spring; 16. a rubber support rod; 17. a camera probe; 18. and (7) mounting frames.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
In the description of the present invention, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplification of description, but do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus, should not be construed as limiting the present invention; the terms "first," "second," and "third" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance, and furthermore, unless otherwise explicitly stated or limited, the terms "mounted," "connected," and "connected" are to be construed broadly and may be, for example, fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.
Referring to fig. 1-3, the present invention provides an embodiment: a meteorological unmanned aerial vehicle with a damping structure comprises an unmanned aerial vehicle body 1, wherein fixed seats 2 are fixedly connected at the corners of the unmanned aerial vehicle body 1, driving motors 3 are mounted at the tops of the fixed seats 2, helical blades 4 are mounted at the tops of the driving motors 3, protective covers 5 corresponding to the helical blades 4 are mounted on the outer sides of the driving motors 3, a supporting seat 8 is fixedly connected at the center of the top of the unmanned aerial vehicle body 1, a wind speed monitor 9 is arranged at the top of the supporting seat 8, a protective top cover 10 is arranged at the top of the wind speed monitor 9, two supporting columns 11 are fixedly connected at two sides of the center of the bottom of the unmanned aerial vehicle body 1, telescopic legs 12 are mounted at the bottoms of the two groups of supporting columns 11, sliding grooves 14 are arranged at the centers of the two groups of supporting columns 11, and damping springs 15 corresponding to the telescopic, the center of unmanned aerial vehicle body 1 bottom is provided with camera probe 17, and camera probe 17's both sides are provided with mounting bracket 18.
Sponge protective sheath 13 has all been cup jointed to the outer wall of two flexible legs 12, and sponge protective sheath 13 can play protection and cushioning effect when unmanned aerial vehicle body 1 falls to the ground to produced vibrations when reducing to descend.
The two telescopic legs 12 are both arranged in a U-shaped structure.
The through-hole corresponding with flexible leg 12 has all been seted up at the center of two sets of support columns 11 bottoms, and the both ends of two flexible legs 12 all run through the through-hole and extend to the center of spout 14, the equal fixedly connected with stopper in both ends of two flexible legs 12.
Equal fixedly connected with in the edge of 1 bottom of unmanned aerial vehicle body and the corresponding rubber support pole 16 of helical blade 4, a plurality of rubber support poles 16 can play the auxiliary stay effect when falling the ground surface and not steady, even also can play fine support and guard action when dropping from the sky suddenly.
The working principle is as follows: the utility model provides a meteorological unmanned aerial vehicle with shock-absorbing structure has great improvement innovation with traditional device, when using this meteorological unmanned aerial vehicle with shock-absorbing structure, we can place this unmanned aerial vehicle on a steady ground, then we can control it to take off through remote control unit, the center at unmanned aerial vehicle body 1 top is provided with wind speed monitor 9, after unmanned aerial vehicle body 1 flies to a take-up height, wind speed monitor 9 can monitor wind speed and meteorological condition in the air automatically, the camera 17 of unmanned aerial vehicle body 1 bottom also can monitor the ground condition, in the process of flying, when the safety cover 5 collides the thing, the elastic protection circle 6 of outside can extrude a plurality of rubber connecting blocks 7 inwards, thereby realize playing the guard action to safety cover 5 and helical blade 4, thereby the stability of unmanned aerial vehicle body 1 flight has been improved, sponge protective sheath 13 has all been cup jointed to the outer wall of two flexible legs 12, sponge protective sheath 13 can play protection and cushioning effect when unmanned aerial vehicle body 1 falls to the ground, thereby reduce produced vibrations when descending, a plurality of rubber support pole 16 can play the auxiliary stay effect when falling to the ground surface and not steady, also can play fine support and guard action when falling aloft suddenly, when unmanned aerial vehicle body 1 drops from half sky suddenly, unmanned aerial vehicle body 1 can extrude two flexible legs 12 downwards, two damping spring 15 are all extruded to spout 14 in at the both ends of two flexible legs 12 this moment, under the elastic action of a plurality of damping spring 15 self, can play fine shock attenuation and guard action to flexible leg 12 and unmanned aerial vehicle body 1.
Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications and variations can be made in the embodiments or in part of the technical features of the embodiments without departing from the spirit and the scope of the invention.
Claims (6)
1. The utility model provides a meteorological unmanned aerial vehicle with shock-absorbing structure, includes unmanned aerial vehicle body (1), its characterized in that: the unmanned aerial vehicle comprises an unmanned aerial vehicle body (1), wherein all fixed seats (2) are fixedly connected at the corners of the unmanned aerial vehicle body (1), driving motors (3) are installed at the tops of a plurality of fixed seats (2), helical blades (4) are installed at the tops of a plurality of driving motors (3), protective covers (5) corresponding to the helical blades (4) are installed at the outer sides of a plurality of driving motors (3), a supporting seat (8) is fixedly connected at the center of the top of the unmanned aerial vehicle body (1), a wind speed monitor (9) is arranged at the top of the supporting seat (8), a protective top cover (10) is arranged at the top of the wind speed monitor (9), two supporting columns (11) are fixedly connected at the two sides of the bottom center of the unmanned aerial vehicle body (1), telescopic legs (12) are installed at the bottoms of the two groups of supporting columns (11), and sliding chutes (14), two damping spring (15) corresponding with flexible leg (12) are all installed at the center of spout (14), the center of unmanned aerial vehicle body (1) bottom is provided with camera probe (17), the both sides of camera probe (17) are provided with mounting bracket (18).
2. The meteorological unmanned aerial vehicle with shock-absorbing structure of claim 1, wherein: it is a plurality of elasticity guard circle (6) are all installed in the outside of safety cover (5), and are a plurality of the inboard equal fixedly connected with of elasticity guard circle (6) a plurality of rubber connecting blocks (7) corresponding with safety cover (5).
3. The meteorological unmanned aerial vehicle with shock-absorbing structure of claim 1, wherein: the outer walls of the two telescopic legs (12) are sleeved with sponge protective sleeves (13).
4. The meteorological unmanned aerial vehicle with shock-absorbing structure of claim 1, wherein: two flexible leg (12) all are the setting of U type structure.
5. The meteorological unmanned aerial vehicle with shock-absorbing structure of claim 1, wherein: two sets of the through-hole corresponding with flexible leg (12) is all seted up at the center of support column (11) bottom, two the both ends of flexible leg (12) all run through the through-hole and extend to the center of spout (14), two the equal fixedly connected with stopper in both ends of flexible leg (12).
6. The meteorological unmanned aerial vehicle with shock-absorbing structure of claim 1, wherein: equal fixedly connected with in edge department of unmanned aerial vehicle body (1) bottom and helical blade (4) corresponding rubber support pole (16).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020312708.1U CN211869695U (en) | 2020-03-13 | 2020-03-13 | Meteorological unmanned aerial vehicle with shock-absorbing structure |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020312708.1U CN211869695U (en) | 2020-03-13 | 2020-03-13 | Meteorological unmanned aerial vehicle with shock-absorbing structure |
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| Publication Number | Publication Date |
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| CN211869695U true CN211869695U (en) | 2020-11-06 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN202020312708.1U Expired - Fee Related CN211869695U (en) | 2020-03-13 | 2020-03-13 | Meteorological unmanned aerial vehicle with shock-absorbing structure |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114435610A (en) * | 2022-02-09 | 2022-05-06 | 国网河北省电力有限公司曲周县供电分公司 | External infrared temperature measuring device of unmanned aerial vehicle patrols and examines |
-
2020
- 2020-03-13 CN CN202020312708.1U patent/CN211869695U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114435610A (en) * | 2022-02-09 | 2022-05-06 | 国网河北省电力有限公司曲周县供电分公司 | External infrared temperature measuring device of unmanned aerial vehicle patrols and examines |
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Granted publication date: 20201106 |
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| CF01 | Termination of patent right due to non-payment of annual fee |