CN212556825U - Unmanned aerial vehicle with prevent falling structure - Google Patents
Unmanned aerial vehicle with prevent falling structure Download PDFInfo
- Publication number
- CN212556825U CN212556825U CN202020991551.XU CN202020991551U CN212556825U CN 212556825 U CN212556825 U CN 212556825U CN 202020991551 U CN202020991551 U CN 202020991551U CN 212556825 U CN212556825 U CN 212556825U
- Authority
- CN
- China
- Prior art keywords
- frame
- screw
- aerial vehicle
- unmanned aerial
- protection
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Images
Landscapes
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The utility model discloses an unmanned aerial vehicle with prevent falling structure, include frame, screw, prevent falling the frame and shoot the subassembly, the top of screw is installed through the helicitic texture and is prevented falling the frame, the undercarriage is installed through the screw thread end in the bottom of installation end. The utility model discloses an install at the top of screw and prevent falling the frame, when the preventing device striking damaged, insert the screw thread post of mounting disc bottom earlier in, and rotatory screw thread post to form the interlock with the screw thread post fixed, and can form the protection casing at a top through the cooperation of mounting disc outside welded multiunit connecting rod and protection hoop, prevent that there is birds or high altitude whereabouts thing to destroy the screw, it has the protection frame to weld in the outside of protection hoop simultaneously, utilize the protection frame to carry out the side wall protection to the screw, prevent the device from descending, or the striking building causes the screw to damage, the security of screw has been guaranteed, the anti-falling performance of device has been improved, the life of device has been prolonged.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field specifically is an unmanned aerial vehicle with prevent falling structure.
Background
Modern society's flying speed development makes people to the cognition of society broader, and people are eager for exploring the sky, want to soaring with the sky like the bird, then we have had unmanned aerial vehicle, and unmanned aerial vehicle is people and flies the sky, explores the equipment in sky, flies to sky unmanned aerial vehicle and also needs safeguard measure equally, but current unmanned aerial vehicle that has the structure of preventing falling has many problems or defects:
traditional unmanned aerial vehicle is in the in-service use, and the device does not have protective structure, and the thing that appears striking damage very easily takes place, prevents falling the performance poor, has shortened the life of device.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an unmanned aerial vehicle with prevent falling structure to the problem of preventing falling the performance difference that proposes in solving above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides an unmanned aerial vehicle with prevent falling structure, includes frame, screw, prevents falling frame and shooting subassembly, the both sides of frame are equipped with two sets of wings, the installation end is installed to the one end of wing, the screw is installed at the top of installation end, the top of screw is installed through the helicitic texture and is prevented falling the frame, the undercarriage is installed through the whorl end in the bottom of installation end, the bottom of frame is installed through the bolt and is protected the chassis, the shooting subassembly is installed through the bolt in the inside of protection chassis, the battery case is installed through the bolt in the front of frame.
Preferably, the anti-falling frame is internally provided with a mounting disc, the bottom of the mounting disc is welded with a threaded column, the outer side of the mounting disc is provided with a protective hoop through a connecting rod, and the outer side of the protective hoop is welded with a protective frame.
Preferably, a support frame is installed in the undercarriage, a threaded sleeve is welded at the top of the support frame, and an anti-skid rubber pad is welded at the bottom of the support frame.
Preferably, install the mounting bracket in the shooting component, the pedestal is installed through the pintle in the inside of mounting bracket, and the camera is installed through the pintle in the inside of pedestal.
Preferably, a motor support is installed in the propeller, a spiral blade is installed at the output end of the motor support, and a threaded seat is arranged at the top of the spiral blade.
Preferably, the front of the battery box is provided with a switch, and three groups of display lamps are arranged above the switch.
Compared with the prior art, the beneficial effects of the utility model are that: this unmanned aerial vehicle with prevent falling structure is rational in infrastructure, has following advantage:
(1) the anti-falling frame is arranged at the top of the propeller, when the device is prevented from being damaged by impact, the threaded base is inserted into the threaded column at the bottom of the mounting disc, the threaded column is rotated to be meshed with the threaded base for fixing, the mounting disc is convenient to mount, a top protective cover can be formed by matching a plurality of groups of connecting rods welded on the outer side of the mounting disc with the protective hoop, birds or high-altitude falling objects are prevented from damaging the propeller, the protective structure of the device is increased, meanwhile, the protective frame is welded on the outer side of the protective hoop, the propeller can be protected from being surrounded by the protective frame, the device is prevented from falling down, or the building is impacted to damage the propeller, the safety of the propeller is ensured, the anti-falling performance of the device is improved, and the service life of the device is prolonged;
(2) the two groups of landing gears are arranged on the outer side of the bottom of the rack, when the device lands, the support frame can be conveniently fixed at the bottom of the rack through the matching of the threaded sleeves and the threaded ends, the support frame is convenient to mount, the anti-skid rubber pads are mounted at the bottom of the support frame, the soft anti-skid rubber pads can effectively reduce the vibration of the device to the rack during landing, and the device is prevented from slipping on the ground during landing to cause a side-falling phenomenon, so that the device is more stable during landing, the damping structure of the device is increased, the damping performance of the device is improved, and the safe landing of the device is ensured;
(3) through the internally mounted at the protection chassis have the subassembly of shooing, when the device carries out the flight record, can fix the pedestal in the inside of protection chassis through the mounting bracket, and the inside of pedestal is through pintle movable mounting camera, can be convenient for adjust the shooting angle of camera in the cooperation through mounting bracket and pedestal, make it adjust according to the shooting needs, the camera of being convenient for carries out multi-angle shooting, make its camera can shoot the picture of different angles, the controllability of device has been increased, the picture sense of device flight record has been improved, the practicality of device has been improved.
Drawings
Fig. 1 is a schematic front view of the overall structure of the present invention;
fig. 2 is a schematic front view of the structure of the present invention;
fig. 3 is a schematic top view of the present invention;
fig. 4 is a schematic view of the anti-falling frame of the present invention;
FIG. 5 is a schematic view of the landing gear of the present invention;
fig. 6 is a schematic diagram of the shooting assembly structure of the present invention.
In the figure: 1. a frame; 101. an airfoil; 102. an installation end; 103. a threaded end; 104. a protective chassis; 2. a propeller; 201. a motor bracket; 202. helical leaves; 203. a threaded seat; 3. an anti-falling frame; 301. mounting a disc; 302. a threaded post; 303. a connecting rod; 304. a protective collar; 305. a protective frame; 4. a landing gear; 401. a support frame; 402. a threaded sleeve; 403. an anti-skid rubber pad; 5. a shooting component; 501. a mounting frame; 502. a pedestal; 503. a camera; 6. a battery case; 601. a switch; 602. and a display lamp.
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.
Referring to fig. 1-6, the present invention provides an embodiment: an unmanned aerial vehicle with an anti-falling structure comprises a frame 1, propellers 2, an anti-falling frame 3 and a shooting assembly 5, wherein two groups of wings 101 are arranged on two sides of the frame 1, a mounting end 102 is mounted at one end of each wing 101, the propellers 2 are mounted at the top of the mounting end 102, a motor support 201 is mounted in each propeller 2, a spiral blade 202 is mounted at the output end of each motor support 201, a screw seat 203 is arranged at the top of each spiral blade 202, the anti-falling frame 3 is mounted at the top of each propeller 2 through a threaded structure, a mounting disc 301 is mounted in each anti-falling frame 3, a threaded column 302 is welded at the bottom of each mounting disc 301, a protective hoop 304 is mounted on the outer side of each mounting disc 301 through a connecting rod 303, a protective frame 305 is welded on the outer side of each protective hoop 304, a protective bottom frame 104 is mounted at the bottom of the frame 1, three groups of display lamps 602 are arranged above the switch 601;
specifically, when the device is prevented from being damaged by impact, the threaded seat 203 is inserted into the threaded column 302 at the bottom of the mounting disc 301, the threaded column 302 is rotated to be meshed and fixed with the threaded seat 203, the mounting disc 301 is convenient to mount, a top protective cover can be formed by matching a plurality of groups of connecting rods 303 welded on the outer side of the mounting disc 301 with the protective hoop 304, birds or high-altitude falling objects are prevented from damaging the propeller 2, the protective structure of the device is increased, meanwhile, the protective frame 305 is welded on the outer side of the protective hoop 304, the propeller 2 can be protected by the protective frame 305 in a side surrounding mode, the device is prevented from falling down or impacting a building to damage the propeller 2, the safety of the propeller 2 is guaranteed, the anti-falling performance of the device is improved, and the service life of the device is prolonged;
the bottom of the mounting end 102 is provided with an undercarriage 4 through a threaded end 103, a support frame 401 is mounted in the undercarriage 4, a threaded sleeve 402 is welded at the top of the support frame 401, and an anti-skid rubber pad 403 is welded at the bottom of the support frame 401;
specifically, when the device is landed, the support frame 401 can be conveniently fixed at the bottom of the rack 1 by matching the threaded sleeve 402 with the threaded end 103, the support frame 401 can be conveniently mounted, the anti-skid rubber pad 403 is mounted at the bottom of the support frame 401, the soft anti-skid rubber pad 403 can effectively reduce the vibration of the device to the rack 1 when the device is landed, and the phenomenon of side falling caused by skidding on the ground when the device is landed is prevented, so that the device is more stable when landed, the damping structure of the device is increased, the damping performance of the device is improved, and the safe landing of the device is ensured;
the inside of the protective underframe 104 is provided with a shooting assembly 5 through bolts, the shooting assembly 5 is internally provided with a mounting frame 501, the inside of the mounting frame 501 is provided with a shaft bracket 502 through a shaft bolt, and the inside of the shaft bracket 502 is provided with a camera 503 through a shaft bolt;
specifically, when the device carries out the flight record, can fix pedestal 502 in the inside of protection chassis 104 through mounting bracket 501, and pedestal 502's inside is through pintle movable mounting camera 503, can be convenient for adjust the shooting angle of camera 503 through the cooperation of mounting bracket 501 and pedestal 502, make it adjust according to the shooting needs, be convenient for camera 503 carries out multi-angle and shoots, make its camera 503 can shoot the picture of different angles, the adjustability of device has been increased, the picture sense of device flight record has been improved, the practicality of device has been improved.
The working principle is as follows: when the device is used, firstly, the threaded seat 203 is inserted into the threaded column 302 at the bottom of the mounting disc 301, the threaded column 302 is rotated to form occlusion fixation with the threaded seat 203, the mounting disc 301 is convenient to mount, a top protective cover can be formed by matching a plurality of groups of connecting rods 303 welded on the outer side of the mounting disc 301 with the protective hoop 304, birds or high-altitude falling objects are prevented from damaging the propeller 2, a protective structure of the device is added, meanwhile, the protective frame 305 is welded on the outer side of the protective hoop 304, the propeller 2 can be protected from side surrounding by the protective frame 305, the device is prevented from falling down or impacting buildings to damage the propeller 2, the safety of the propeller 2 is ensured, the anti-falling performance of the device is improved, and the service life of the device is prolonged;
secondly, the support frame 401 can be conveniently fixed at the bottom of the rack 1 by matching the threaded sleeve 402 with the threaded end 103, the support frame 401 is convenient to mount, the anti-skid rubber pad 403 is mounted at the bottom of the support frame 401, the soft anti-skid rubber pad 403 can effectively reduce the vibration of the device on the rack 1 when the device falls down, and the phenomenon of side falling caused by the slip of the device on the ground when the device falls down is prevented, so that the device is more stable when falling to the ground, the damping structure of the device is increased, the damping performance of the device is improved, and the safe falling of the device is ensured;
finally, the shaft bracket 502 can be fixed inside the protective underframe 104 through the mounting frame 501, the shaft bolt is movably mounted in the shaft bracket 502 through the camera 503, the shooting angle of the camera 503 can be conveniently adjusted through the matching of the mounting frame 501 and the shaft bracket 502, the camera 503 can be adjusted according to the shooting requirement, the camera 503 can conveniently shoot at multiple angles, the camera 503 can shoot pictures at different angles, the adjustability of the device is increased, the picture sense of the flight record of the device is improved, and the practicability of the device is improved.
It is obvious to a person skilled in the art that the invention is not restricted to details of the above-described exemplary embodiments, but that it can be implemented in other specific forms without departing from the spirit or essential characteristics of the invention. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
Claims (6)
1. The utility model provides an unmanned aerial vehicle with prevent falling structure, includes frame (1), screw (2), prevents falling frame (3) and shoots subassembly (5), its characterized in that: the both sides of frame (1) are equipped with two sets of wings (101), installation end (102) are installed to the one end of wing (101), screw (2) are installed at the top of installation end (102), the top of screw (2) is installed through the helicitic texture and is prevented falling frame (3), undercarriage (4) are installed through whorl end (103) in the bottom of installation end (102), protection chassis (104) are installed through the bolt in the bottom of frame (1), shooting subassembly (5) are installed through the bolt in the inside of protection chassis (104), battery case (6) are installed through the bolt in the front of frame (1).
2. The unmanned aerial vehicle with prevent falling structure of claim 1, characterized in that: install mounting disc (301) in anti-falling frame (3), the bottom welding of mounting disc (301) has screw thread post (302), and protection hoop (304) are installed through connecting rod (303) in the outside of mounting disc (301), and the outside welding of protection hoop (304) has protection frame (305).
3. The unmanned aerial vehicle with prevent falling structure of claim 1, characterized in that: a supporting frame (401) is installed in the undercarriage (4), a threaded sleeve (402) is welded at the top of the supporting frame (401), and an anti-skid rubber pad (403) is welded at the bottom of the supporting frame (401).
4. The unmanned aerial vehicle with prevent falling structure of claim 1, characterized in that: install mounting bracket (501) in shooting subassembly (5), pedestal (502) are installed through the pintle in the inside of mounting bracket (501), and camera (503) are installed through the pintle in the inside of pedestal (502).
5. The unmanned aerial vehicle with prevent falling structure of claim 1, characterized in that: install motor support (201) in screw (2), spiral leaf (202) are installed to the output of motor support (201), and the top of spiral leaf (202) is equipped with screw thread seat (203).
6. The unmanned aerial vehicle with prevent falling structure of claim 1, characterized in that: the front of the battery box (6) is provided with a switch (601), and three groups of display lamps (602) are arranged above the switch (601).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020991551.XU CN212556825U (en) | 2020-06-03 | 2020-06-03 | Unmanned aerial vehicle with prevent falling structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020991551.XU CN212556825U (en) | 2020-06-03 | 2020-06-03 | Unmanned aerial vehicle with prevent falling structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212556825U true CN212556825U (en) | 2021-02-19 |
Family
ID=74637702
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202020991551.XU Active CN212556825U (en) | 2020-06-03 | 2020-06-03 | Unmanned aerial vehicle with prevent falling structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN212556825U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113895622A (en) * | 2021-10-20 | 2022-01-07 | 新沂阿凡达智能科技有限公司 | Unmanned aerial vehicle's safety protection structure |
-
2020
- 2020-06-03 CN CN202020991551.XU patent/CN212556825U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113895622A (en) * | 2021-10-20 | 2022-01-07 | 新沂阿凡达智能科技有限公司 | Unmanned aerial vehicle's safety protection structure |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN203544368U (en) | Protection device for multi-rotor-wing unmanned plane | |
| CN212556825U (en) | Unmanned aerial vehicle with prevent falling structure | |
| CN108216588B (en) | Unmanned aerial vehicle | |
| CN108521731A (en) | Wireless sensor network node protective device | |
| CN110803280A (en) | Pure electric manned vehicle | |
| CN210027944U (en) | Unmanned aerial vehicle with fire control fire extinguishing bomb | |
| CN208070019U (en) | A kind of multi-rotor unmanned aerial vehicle | |
| CN107021217A (en) | A kind of medicine-chest rises and falls posture plant protection unmanned plane | |
| CN208360491U (en) | A kind of Combined unmanned machine based on Internet of Things | |
| CN107150796A (en) | A kind of multi-rotor unmanned aerial vehicle | |
| CN109050888A (en) | A kind of six rotor wing unmanned aerial vehicles | |
| CN115116699A (en) | Dry-type transformer for polycrystalline silicon reduction furnace | |
| CN112810795A (en) | Portable unmanned vehicles | |
| CN114227001A (en) | Airborne high-power laser obstacle clearing system and device | |
| CN210707883U (en) | Security protection control unmanned aerial vehicle that can protect camera | |
| CN210101984U (en) | Exploration unmanned aerial vehicle that forest fire prevention used | |
| CN106898187A (en) | A kind of rotor wing unmanned aerial vehicle landing training platform that takes off | |
| CN111478267A (en) | Cable dry-type terminal strutting arrangement with unmanned aerial vehicle platform that charges that rises and falls | |
| CN216375032U (en) | Integrated information processing apparatus | |
| CN110810390A (en) | Solar bird repeller | |
| CN219421392U (en) | Data acquisition device | |
| CN219989509U (en) | Unmanned aerial vehicle for line inspection of power system | |
| CN220315337U (en) | External anti-collision protection mechanism for unmanned aerial vehicle | |
| CN216332711U (en) | Unmanned aerial vehicle for highway road condition exploration | |
| CN211033007U (en) | Pure electric manned aircraft |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |