CN214397221U - Unmanned aerial vehicle capable of effectively avoiding obstacles - Google Patents
Unmanned aerial vehicle capable of effectively avoiding obstacles Download PDFInfo
- Publication number
- CN214397221U CN214397221U CN202120427043.3U CN202120427043U CN214397221U CN 214397221 U CN214397221 U CN 214397221U CN 202120427043 U CN202120427043 U CN 202120427043U CN 214397221 U CN214397221 U CN 214397221U
- Authority
- CN
- China
- Prior art keywords
- mounting
- aerial vehicle
- fixed mounting
- unmanned aerial
- organism
- 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
- Traffic Control Systems (AREA)
Abstract
The utility model provides an unmanned aerial vehicle that can effectively keep away barrier relates to unmanned air vehicle technical field. The novel airplane comprises an airplane body, the both sides surface of the airplane body all is equipped with the horn, every the equal fixed mounting in horn side surface has a mounting bracket, every the equal fixed mounting in mounting bracket upper end has a plurality of screws, the equal fixed mounting in both sides surface has infrared perception system around the organism, infrared perception system includes signal receiving terminal, signal transmission end, organism side surface lower extreme fixed mounting has the camera, the mounting groove has been seted up to organism lower extreme surface middle part position, the inside fixed mounting in mounting groove has remote control device. The utility model discloses a through setting up infrared perception system, can accurately detect the distance between barrier and the aircraft when the side flies, it is big not only to survey the area, can effectively accurately discern the nearest object distance apart from the aircraft.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle field particularly, relates to an unmanned aerial vehicle that can effectively keep away barrier.
Background
The unmanned plane is called as an unmanned plane for short, and is an unmanned plane operated by utilizing a radio remote control device and a self-contained program control device; the airplane is not provided with a cockpit, but is provided with an automatic pilot, a program control device and other equipment; tracking, positioning, remote control, remote measurement and digital transmission are carried out on the personnel at the ground, the naval vessel or the mother aircraft remote control station through equipment such as a radar; the related technology of the unmanned aerial vehicle at home and abroad is rapidly developed, the unmanned aerial vehicle system has various types, and the unmanned aerial vehicle has great difference in various aspects such as size, quality, range, time of flight, flying height, flying speed and the like, and can meet the use requirements of military, shooting, monitoring and other fields.
Traditional unmanned aerial vehicle that can keep away barrier all adopts the ultrasonic wave to keep away the barrier, and the mode that the barrier was kept away to the ultrasonic wave, detects the precision ratio and than lower, and thereby because its structural feature produces unstable phenomenon and takes place by the influence of aircraft oar frequent vibration easily, not only influences work efficiency, and leads to people's availability factor to descend, for this reason, we provide an unmanned aerial vehicle that can effectively keep away the barrier.
SUMMERY OF THE UTILITY MODEL
The utility model provides an unmanned aerial vehicle that can effectively keep away barrier aims at improving and can effectively accurately discern the nearest object distance apart from the aircraft, can effectively strengthen the interference killing feature, effectively improves the perception performance and the reliability problem of device.
In order to achieve the purpose, the utility model provides a can effectively keep away unmanned aerial vehicle of barrier, which comprises a bod, organism both sides surface all is equipped with the horn, every equal fixed mounting in horn one side surface has a mounting bracket, every equal fixed mounting in mounting bracket upper end has a plurality of screws, the equal fixed mounting in both sides surface has infrared perception system around the organism, infrared perception system includes signal receiving terminal, signal transmission end, organism one side surface lower extreme fixed mounting has the camera, the mounting groove has been seted up to organism lower extreme surface middle part position, the inside fixed mounting of mounting groove has remote control device.
Preferably, every equal fixed mounting in mounting bracket lower extreme surface middle part position has the supporting leg, every the equal fixed mounting in supporting leg surface has damping spring, every the equal fixed mounting in supporting leg lower extreme surface has fixed stabilizer blade.
Preferably, each of the arms is fixedly installed on two side surfaces of the machine body, and each of the arms is inclined outwards by 45 degrees along the edge of the machine body.
Preferably, each the structure of mounting bracket is the cylinder type structure, the mounting groove comprises two semicircle and rectangles.
Preferably, the detection distance of the infrared sensing system is 7 meters, and the sensing range of the infrared sensing system is a cone shape with 70 degrees in the horizontal direction and 20 degrees in the vertical direction.
Preferably, the fixed support leg is cylindrical, a cushion pad is fixedly mounted on the surface of the lower end of each fixed support leg, and the cushion pad is made of rubber.
Compared with the prior art, the beneficial effects of the utility model are that:
(1) the distance between the obstacle and the aircraft can be accurately detected when the aircraft flies sideways by arranging the infrared sensing system, the infrared sensing system can be used for sensing side obstacles in a novice mode and a tripod mode, the effective detection distance reaches 7 meters, the sensing range is a cone shape with 70 degrees in the horizontal direction and 20 degrees in the vertical direction, the detection area is large, the distance of an object closest to the aircraft can be effectively and accurately identified, the anti-interference capability can be effectively enhanced, and the sensing performance and the reliability of the device can be effectively improved;
(2) the supporting legs and the fixed support legs are arranged at the lower end of the mounting frame, so that the supporting function can be achieved when the machine body falls to the ground, the vibration of the machine body when the machine body falls to the ground can be effectively reduced by installing the damping spring on the surface of each supporting leg, the impact force can be relieved by arranging the buffer cushion, the machine body is effectively protected, the service life of the device is prolonged, and the practicability of the device is enhanced;
drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings that are required to be used in the embodiments will be briefly described below, it should be understood that the following drawings only illustrate some embodiments of the present invention, and therefore should not be considered as limiting the scope, and for those skilled in the art, other related drawings can be obtained according to the drawings without inventive efforts.
Fig. 1 is a schematic structural view of the whole of the present invention;
fig. 2 is a schematic structural diagram of the infrared sensing system of the present invention;
FIG. 3 is a schematic structural view of the support leg of the present invention;
fig. 4 is a schematic structural diagram of the cushion pad of the present invention.
Description of the main elements
1. A body; 2. a horn; 3. a mounting frame; 4. a propeller; 5. a camera; 6. mounting grooves; 7. A remote control device; 8. an infrared sensing system; 9. supporting legs; 10. a damping spring; 11. a fixed leg; 12. a cushion pad.
Detailed Description
To make the objects, technical solutions and advantages of the embodiments of the present invention clearer, the drawings of the embodiments of the present invention are combined to clearly and completely describe the technical solutions of the embodiments of the present invention, and obviously, the described embodiments are 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. Thus, the following detailed description of the embodiments of the present invention, presented in the accompanying drawings, is not intended to limit the scope of the invention, as claimed, but is merely representative of selected embodiments of the invention. 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 present invention, unless otherwise expressly stated or limited, the terms "mounted," "connected," and "fixed" are to be construed broadly and may, for example, be fixedly connected, detachably connected, or integrally formed; can be mechanically or electrically connected; either directly or indirectly through intervening media, either internally or in any other relationship. The specific meaning of the above terms in the present invention can be understood according to specific situations by those skilled in the art.
In the present disclosure, unless expressly stated or limited otherwise, the first feature "on" or "under" the second feature may comprise direct contact between the first and second features, or may comprise contact between the first and second features not directly. Also, the first feature being "on," "above" and "over" the second feature includes the first feature being directly on and obliquely above the second feature, or merely indicating that the first feature is at a higher level than the second feature. A first feature being "under," "below," and "beneath" a second feature includes the first feature being directly under and obliquely below the second feature, or simply meaning that the first feature is at a lesser elevation than the second feature.
Embodiment 1, as shown in fig. 1-4, an unmanned aerial vehicle capable of effectively avoiding obstacles comprises a body 1, wherein arms 2 are respectively arranged on two side surfaces of the body 1, a mounting frame 3 is fixedly arranged on one side surface of each arm 2, a plurality of propellers 4 are fixedly arranged at the upper end of each mounting frame 3, infrared sensing systems 8 are respectively fixedly arranged on the front and back side surfaces of the body 1, each infrared sensing system 8 comprises a signal receiving end and a signal transmitting end, a camera 5 is fixedly arranged at the lower end of one side surface of the body 1, a mounting groove 6 is arranged in the middle of the lower end surface of the body 1, a remote control device 7 is fixedly arranged in the mounting groove 6, a supporting leg 9 is fixedly arranged in the middle of the lower end surface of each mounting frame 3, a damping spring 10 is fixedly arranged on the surface of each supporting leg 9, a fixed supporting leg 11 is fixedly arranged on the lower end surface of each supporting leg 9, every horn 2 equal fixed mounting is on 1 both sides surface of organism, every horn 2 prolongs 1 edge of organism and all leans out 45 degrees, the structure of every mounting bracket 3 is the cylinder type structure, mounting groove 6 comprises two semi-circles and rectangle, infrared perception system 8's detection distance is 7 meters, infrared perception system 8's perception scope is 70 degrees of horizontal direction, and the vertical direction is the toper shape of 20 degrees, fixed stabilizer blade 11's shape is cylindrical, 11 equal fixed mounting in lower extreme surface of every fixed stabilizer blade has blotter 12, every blotter 12's material is the rubber material, through setting up infrared perception system 8, can accurately detect the distance between barrier and the aircraft when the side flies, and infrared perception system 8 can be used to new hand mode, the side obstacle perception under the tripod mode, effective detection distance reaches 7 meters, the perception scope is 70 degrees of horizontal direction, The cone shape of 20 degrees in the vertical direction has large detection area, and can effectively and accurately identify the object distance closest to the aircraft.
The working principle is as follows: when using, through setting up infrared perception system 8, can accurate detection barrier and the aircraft between the distance when the side flies, and infrared perception system 8 can be used to the side barrier perception under novice mode, the tripod mode, and effective detection distance reaches 7 meters, and the perception scope is 70 for the horizontal direction, the 20 pyramis shapes of vertical direction, and not only the detection area is big, can effectively accurately discern the nearest object distance of distance aircraft.
The utility model discloses a working process and beneficial effect as follows: through setting up infrared perception system, but the distance between accurate detection barrier and the aircraft just when the side flies, infrared perception system can be used to the new hand mode, the side obstacle perception under the tripod mode, effective detection distance reaches 7 meters, the perception scope is the pyramid shape of horizontal direction 70 °, vertical direction 20 °, it is big not only to survey the area, can effectively accurately discern the nearest object distance from the aircraft, can effectively strengthen the interference killing feature, effectively improve the perception performance and the reliability of device.
The above description is only a preferred embodiment of the present invention and is not intended to limit the present invention, and various modifications and changes may be made by those skilled in the art. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
Claims (6)
1. The utility model provides an unmanned aerial vehicle that can effectively keep away barrier, includes organism (1), its characterized in that, organism (1) both sides surface all is equipped with horn (2), every the equal fixed mounting of horn (2) side surface has mounting bracket (3), every the equal fixed mounting in mounting bracket (3) upper end has a plurality of screws (4), the equal fixed mounting in both sides surface has infrared perception system (8) around organism (1), infrared perception system (8) are including signal receiving terminal, signal transmission end, organism (1) one side surface lower extreme fixed mounting has camera (5), mounting groove (6) have been seted up to organism (1) lower extreme surface middle part position, mounting groove (6) inside fixed mounting has remote control device (7).
2. The unmanned aerial vehicle capable of effectively avoiding obstacles according to claim 1, wherein each of the mounting frames (3) is fixedly provided with a support leg (9) at a middle position of the lower end surface thereof, each of the support legs (9) is fixedly provided with a damping spring (10) at a surface thereof, and each of the support legs (9) is fixedly provided with a fixed support leg (11) at a lower end surface thereof.
3. An unmanned aerial vehicle capable of avoiding obstacles effectively according to claim 1, wherein each of the arms (2) is fixedly installed on two side surfaces of the body (1), and each of the arms (2) is inclined outwards by 45 degrees along the edge of the body (1).
4. The unmanned aerial vehicle capable of avoiding obstacles effectively as claimed in claim 1, wherein each mounting frame (3) is of a cylindrical structure, and the mounting groove (6) is formed by two semi-circles and a rectangle.
5. The unmanned aerial vehicle capable of avoiding obstacles effectively as claimed in claim 1, wherein the detection distance of the infrared sensing system (8) is 7 meters, the sensing range of the infrared sensing system (8) is 70 degrees in the horizontal direction, and the sensing range is 20 degrees in the vertical direction.
6. The unmanned aerial vehicle capable of avoiding obstacles effectively as claimed in claim 2, wherein the shape of the fixing legs (11) is cylindrical, a cushion pad (12) is fixedly mounted on the lower end surface of each fixing leg (11), and each cushion pad (12) is made of rubber.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202120427043.3U CN214397221U (en) | 2021-02-26 | 2021-02-26 | Unmanned aerial vehicle capable of effectively avoiding obstacles |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202120427043.3U CN214397221U (en) | 2021-02-26 | 2021-02-26 | Unmanned aerial vehicle capable of effectively avoiding obstacles |
Publications (1)
Publication Number | Publication Date |
---|---|
CN214397221U true CN214397221U (en) | 2021-10-15 |
Family
ID=78026552
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202120427043.3U Active CN214397221U (en) | 2021-02-26 | 2021-02-26 | Unmanned aerial vehicle capable of effectively avoiding obstacles |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN214397221U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113859541A (en) * | 2021-11-24 | 2021-12-31 | 徐州独角兽信息科技有限公司 | Unmanned aerial vehicle for environment detection |
-
2021
- 2021-02-26 CN CN202120427043.3U patent/CN214397221U/en active Active
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113859541A (en) * | 2021-11-24 | 2021-12-31 | 徐州独角兽信息科技有限公司 | Unmanned aerial vehicle for environment detection |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US10669024B2 (en) | Unmanned aerial vehicle, control system and method thereof, and unmanned aerial vehicle landing control method | |
CN214397221U (en) | Unmanned aerial vehicle capable of effectively avoiding obstacles | |
CN109725315B (en) | Obstacle avoidance detection device for electric power inspection unmanned aerial vehicle | |
CN204846371U (en) | Can keep away unmanned aerial vehicle system of barrier | |
CN113895622A (en) | Unmanned aerial vehicle's safety protection structure | |
CN212386694U (en) | Unmanned aerial vehicle with laser rangefinder automatic planning route function | |
CN211810287U (en) | Lightweight electric power corridor data acquisition equipment and unmanned aerial vehicle | |
CN211044017U (en) | Unmanned aerial vehicle and location and keep away barrier device based on laser radar | |
CN209905079U (en) | Unmanned aerial vehicle | |
CN209956241U (en) | Support structure suitable for flight device and helicopter | |
CN213200102U (en) | Unmanned aerial vehicle subassembly with three-dimensional laser scanner | |
CN209640730U (en) | A kind of anti-interference power-line patrolling flight control system of double antenna | |
CN113702988A (en) | Survey and drawing unmanned aerial vehicle range finding keeps away barrier device | |
CN217951081U (en) | Airborne mobile measurement system shock-absorbing structure | |
CN106672213B (en) | A kind of unmanned plane of adaptive touch down attitude emergency adjustment | |
CN215664027U (en) | Patrol unmanned aerial vehicle | |
CN207523953U (en) | Unmanned plane with buffer structure | |
KR102482749B1 (en) | Dual-sensor structure system and method for unmanned aerial vehicle | |
CN220786183U (en) | Taking-off and landing mechanism for professional unmanned aerial vehicle under multiple scenes | |
CN111169650A (en) | Lightweight electric power corridor data acquisition equipment and unmanned aerial vehicle | |
CN218949486U (en) | Aircraft flight error correcting device | |
CN206984321U (en) | A kind of light-duty rotor wing unmanned aerial vehicle damping undercarriage | |
CN214824196U (en) | Unmanned aerial vehicle laser radar nacelle | |
CN209747708U (en) | Unmanned aerial vehicle antenna fixed knot constructs | |
CN221273567U (en) | Anticollision unmanned aerial vehicle |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
GR01 | Patent grant | ||
GR01 | Patent grant | ||
TR01 | Transfer of patent right |
Effective date of registration: 20230323 Address after: Room 3672, Xuanye Building, No. 11, Huohuo East Road, Pioneer Park, Xiamen Torch Hi-tech Zone, Xiamen, Fujian Province, 361000 Patentee after: Xiamen HNA General Aviation Technology Co.,Ltd. Address before: 361000 No. 484-3, Hengtian Road, Jimei District, Xiamen City, Fujian Province Patentee before: Xiamen xiaofeike Education Technology Co.,Ltd. |
|
TR01 | Transfer of patent right |