CN218662359U - Following type unmanned aerial vehicle for emergency rescue - Google Patents

Following type unmanned aerial vehicle for emergency rescue Download PDF

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Publication number
CN218662359U
CN218662359U CN202222912307.1U CN202222912307U CN218662359U CN 218662359 U CN218662359 U CN 218662359U CN 202222912307 U CN202222912307 U CN 202222912307U CN 218662359 U CN218662359 U CN 218662359U
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unmanned aerial
aerial vehicle
connecting hole
fuselage
follow
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邓萍
赖航
赵华慧
龙露鸿
邬忠萍
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Chengdu Technological University CDTU
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Chengdu Technological University CDTU
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Abstract

The utility model relates to the technical field of unmanned aerial vehicles, specifically disclose a follow-up unmanned aerial vehicle for emergency rescue, including the unmanned aerial vehicle fuselage, can dismantle on the integration switching box and be fixed with lighting system, propaganda directed to the public system and collection system, collection system includes 360 revolving stages and the camera based on yolo algorithm, the camera is installed on 360 revolving stages; the utility model discloses an installation lighting system in the below of unmanned aerial vehicle fuselage, propaganda directed to system and collection system, the processing of data collection is managed to the yolo algorithm that makes this unmanned aerial vehicle accessible camera gather and camera from taking, realize that unmanned aerial vehicle is automatic to follow, through lighting system, provide the illumination for the place ahead personnel, through the propaganda directed to system of one-to-one, ensure that should be suffered from a disaster personnel and carry out the fastest safety evacuation according to appointed unmanned aerial vehicle, thereby make unmanned aerial vehicle possess and follow, the function of illumination and propaganda directed to say, the search and rescue efficiency is improved, personnel's safety is ensured to furthest.

Description

Following type unmanned aerial vehicle for emergency rescue
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicle, concretely relates to following type unmanned aerial vehicle is used in emergency rescue.
Background
The disasters often occur in mountainous areas, and the geographic environment of the mountainous areas is more complicated than that of plain areas. Therefore, compare with ordinary unmanned aerial vehicle, emergency rescue unmanned aerial vehicle needs stronger adaptive capacity to environment, requires that unmanned aerial vehicle has stronger wind resistance, and still can carry out the relevant task of emergency rescue in rainy day.
Through retrieval, the Chinese patent document with the application number of 202210631868.6 discloses an auxiliary unmanned aerial vehicle, an emergency rescue system and a first aid rescue method, wherein the auxiliary unmanned aerial vehicle comprises a vehicle body, four rotor wings and a duct competition body, wherein the four rotor wings are respectively connected with the vehicle body and are arranged in the duct shell; be equipped with image transmission device, charging device and function extension device on the fuselage, image transmission device is used for gathering image information and transmits image information to emergent vehicle, and charging device is used for filling electric pile with on the emergent vehicle and is connected, and function extension device includes at least one in alarm, megaphone and the communications facilities. This supplementary unmanned aerial vehicle security is high, can in time know the road conditions in emergent vehicle the place ahead, for emergent vehicle planning optimum path, in time takes corresponding rescue measures, improves rescue efficiency.
However, the unmanned aerial vehicle still has the following defects:
at present, shout unmanned aerial vehicle, aerial illumination unmanned aerial vehicle or possess the unmanned aerial vehicle that shout the illumination in the air simultaneously all stop in the crowd top, shout to the below, to some panic places, like conflagration etc. because personnel are panic and chaotic and are difficult to full play efficiency, therefore we need propose a following unmanned aerial vehicle for emergency rescue and solve the problem that above-mentioned exists.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an emergency rescue is with following formula unmanned aerial vehicle, through installing lighting system, propaganda directed to the public system and collecting system in the below of unmanned aerial vehicle fuselage, make possess the function of following, illumination and propaganda directed to the public, improved search and rescue efficiency, furthest ensures personnel's safety to solve the problem of proposing in the above-mentioned background art.
In order to achieve the above purpose, the utility model adopts the following technical proposal:
the utility model provides an emergency rescue is with following unmanned aerial vehicle, includes the unmanned aerial vehicle fuselage, six horn are installed to the angles such as lateral wall of unmanned aerial vehicle fuselage, the vane is installed to the one end of horn, the integration switching box is installed to the below of unmanned aerial vehicle fuselage, can dismantle on the integration switching box and be fixed with lighting system, propaganda directed to speech system and collection system, collection system includes 360 revolving stages and the camera based on yolo algorithm, the camera is installed on 360 revolving stages, lighting system is located the middle part of integration switching box, propaganda directed to speech system and camera are located lighting system's both sides respectively.
Preferably, lighting system includes the light, the light is the setting of the down-four pyramid shape, wherein three personally submits 45 of light and installs the LED lamp.
Preferably, a connecting rod is fixed to one end of the illuminating lamp, clamping blocks are symmetrically arranged on the side wall of one end of the connecting rod, and a lighting quick-release connecting hole is formed in the lower surface of the integrated switching box and used for clamping and connecting the clamping blocks.
Preferably, the integrated adapter box is a rectangle, a fuselage duplex hole is formed in the upper surface of the integrated adapter box, and the unmanned aerial vehicle fuselage is fixedly connected with the fuselage duplex hole through a bolt.
Preferably, 360 revolving stages is including making the camera around the 360 rotatory mounts seats of X axle, the upper end lateral wall integrated into one piece of mount seat has two first joint pieces that are the symmetry and set up, the cloud platform quick detach connecting hole that supplies first joint piece joint is seted up to the lower surface of integration switching box.
Preferably, the system of shouting includes speaker and fixing base, the upper end at the fixing base is installed in the speaker slope, the upper end lateral wall symmetry of fixing base is fixed with the second joint piece, the lower surface of integration switching box is seted up the quick detach connecting hole that shouts that supplies the joint of second joint piece.
Preferably, cloud platform quick detach connecting hole, the quick detach connecting hole of propaganda directed to communicate and illumination quick detach connecting hole are the same setting, just cloud platform quick detach connecting hole is the same with the joint direction of the quick detach connecting hole of propaganda directed to communicate, the joint direction of illumination quick detach connecting hole is perpendicular with the joint direction of the quick detach connecting hole of propaganda directed to communicate.
Preferably, adopt between unmanned aerial vehicle fuselage and the horn to make the unmanned aerial vehicle fuselage be the dihedral installation of six rotor overall arrangements.
Preferably, the unmanned aerial vehicle upper cover is installed to the upper end of unmanned aerial vehicle fuselage, the upper end of unmanned aerial vehicle upper cover is the arc setting.
Preferably, two supporting legs are installed to the lower extreme of unmanned aerial vehicle fuselage, two the supporting legs are the symmetry and set up, just integration switching box is located between two supporting legs.
The utility model provides a following formula unmanned aerial vehicle for emergency rescue compares with prior art, has following advantage:
1. the utility model discloses a below installation lighting system at the unmanned aerial vehicle fuselage, propaganda directed to speech system and collection system, make this unmanned aerial vehicle can gather below data through the camera, when unmanned aerial vehicle locks a certain concrete person in a disaster, fly to when this person in a disaster rear, the data and the camera taken from yolo algorithm to the processing of data collection through the camera collection, realize that unmanned aerial vehicle is automatic to follow, through lighting system, provide the illumination for the personnel in the place ahead, through the propaganda directed to speech system of one-to-one, ensure that this person in a disaster carries out the fastest safety evacuation according to appointed unmanned aerial vehicle, thereby make unmanned aerial vehicle possess and follow, illumination and function of propaganda directed to speech, search and rescue efficiency is improved, furthest ensures personnel's safety.
Drawings
FIG. 1 is a schematic view of the present invention;
FIG. 2 is a schematic view of the dual-connection hole structure of the fuselage of the present invention;
fig. 3 is a schematic structural view of the integrated adapter box of the present invention;
fig. 4 is a schematic structural view of the lighting system of the present invention;
in the figure: 11. an unmanned aerial vehicle body; 12. a horn; 13. an unmanned aerial vehicle upper cover; 14. an integrated adapter box; 15. a 360-degree rotary table; 16. a camera; 17. an illumination system; 1701. a lighting lamp; 1702. an LED lamp; 1703. a connecting rod; 1704. a clamping block; 18. a shouting system; 19. supporting legs; 20. rotating the leaves; 21. a fuselage double-link hole; 22. the holder is quickly disassembled from the connecting hole; 23. a lighting quick-release connecting hole; 24. the quick-release connecting hole is shout.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the 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. The specific embodiments described herein are merely illustrative of the invention and are not intended to be limiting of the invention. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative efforts all belong to the protection scope of the present invention.
The utility model provides a follow-up unmanned aerial vehicle for emergency rescue as shown in fig. 1-4, including unmanned aerial vehicle fuselage 11, six horn 12 are installed to the lateral wall of unmanned aerial vehicle fuselage 11 equiangularly, vane 20 is installed to the one end of horn 12, integrated switching box 14 is installed to the below of unmanned aerial vehicle fuselage 11, can dismantle on the integrated switching box 14 and be fixed with lighting system 17, propaganda directed to communicate system 18 and acquisition system, acquisition system includes 360 revolving stages 15 and camera 16 based on yolo algorithm, camera 16 installs on 360 revolving stages 15, lighting system 17 is located the middle part of integrated switching box 14, propaganda directed to communicate system 18 and camera 16 are located the both sides of lighting system 17 respectively;
the yolo algorithm is a typical object detection one stage method, and in the yolo algorithm, the core idea is to process an object detection (object detection) problem into a regression problem, and a bounding box and a class probability can be directly predicted from an input image by using a convolutional neural network Q structure. The target detection is carried out by a regression method, the execution speed is high, and the very high-efficiency detection is achieved.
During the use, gather below data through camera 16, when unmanned aerial vehicle locks a certain specific victim, fly to this victim rear, data and camera 16 taken from the yolo algorithm of taking through camera 16 are to the processing of data collection, realize that unmanned aerial vehicle follows automatically, through lighting system 17, provide the illumination for the place ahead personnel, through one-to-one system 18 of shouting, ensure that this victim carries out the fastest safety evacuation according to appointed unmanned aerial vehicle, thereby make unmanned aerial vehicle possess and follow, the function of illumination and shouting, the search and rescue efficiency has been improved, furthest ensures personnel's safety.
The lighting system 17 comprises a lighting lamp 1701, the lighting lamp 1701 is arranged in an inverted quadrangular pyramid shape, three surfaces of the lighting lamp 1701 are 45 degrees, LED lamps 1702 are installed on the three surfaces, the inverted quadrangular pyramid shape of the lighting lamp 1701 is formed, the installation directions of the side walls of the LED lamps 1702 and the lighting lamp 1701 are 45 degrees, the front lighting requirement is ensured, and meanwhile the lighting area is increased.
The lighting lamp 1701 is fixed with connecting rod 1703 in one end, the one end lateral wall symmetry of connecting rod 1703 is provided with fixture block 1704, the lower surface of integration switching box 14 is seted up and is supplied fixture block 1704 joint to be fixed with illumination quick detach connecting hole 23, when the lighting lamp 1701 is installed, insert fixture block 1704 the interior joint of illumination quick detach connecting hole 23 and can be connected the lighting lamp 1701 fast with integration switching box 14 and fix, when the lighting lamp 1701 is dismantled, take out fixture block 1704 from illumination quick detach connecting hole 23, realized the quick installation and the dismantlement of lighting lamp 1701, improved the convenience of bright lamp installation.
Integration switching box 14 is the rectangle setting, fuselage doubly-linked hole 21 has been seted up to the upper surface of integration switching box 14, unmanned aerial vehicle fuselage 11 passes through the bolt and is connected fixedly with fuselage doubly-linked hole 21, makes integration switching box 14 can be connected with unmanned aerial vehicle fuselage 11 fast, improves the agility of unmanned aerial vehicle equipment.
360 revolving stage 15 can drive the camera automatically and carry out 360 rotations including making camera 16 around 360 rotatory mounts seats of X axle through the mount seat, makes unmanned aerial vehicle have bigger field of vision scope at the search and rescue in-process, realizes the purpose that unmanned aerial vehicle followed, the upper end lateral wall integrated into one piece of mount seat has two first joint pieces that are the symmetry and set up, the cloud platform quick detach connecting hole 22 that supplies first joint piece joint is seted up to the lower surface of integration switching box 14, through the cooperation of first joint piece and cloud platform quick detach connecting hole 22, makes and sets up for dismantling between mount seat and the integration switching box 14, is convenient for install the mount seat on integration switching box 14 or take off from integration switching box 14 fast according to the in-service use demand.
The system of shouting 18 includes speaker and fixing base, the speaker slope is installed in the upper end of fixing base, is convenient for fix the speaker and support through the fixing base, the upper end lateral wall symmetry of fixing base is fixed with the second joint piece, the quick detach connecting hole 24 of shouting that supplies second joint piece joint is seted up to the lower surface of integration switching box 14, through the second joint piece with shout the cooperation of quick detach connecting hole 24, for can dismantling the setting between messenger's fixing base and the integration switching box 14, be convenient for according to the in-service use demand with the fixing base quick-mounting on integration switching box 14 or take off from integration switching box 14 fast.
Cloud platform quick detach connecting hole 22, call quick detach connecting hole 24 and illumination quick detach connecting hole 23 and be the same setting, just cloud platform quick detach connecting hole 22 is the same with the joint direction of calling quick detach connecting hole 24, the joint direction of illumination quick detach connecting hole 23 is perpendicular with the joint direction of calling quick detach connecting hole 24, makes the installation direction of 360 revolving stage, fixing base and mount pad be the dislocation set, improves the installation convenience of 360 revolving stage, fixing base and mount pad, just.
Adopt between unmanned aerial vehicle fuselage 11 and the horn 12 to make unmanned aerial vehicle fuselage 11 be the dihedral installation of six rotor overall arrangements, make unmanned aerial vehicle fuselage 11 can steadily fly, improve the adaptability of unmanned aerial vehicle emergency rescue in the field.
Unmanned aerial vehicle upper cover 13 is installed to unmanned aerial vehicle fuselage 11's upper end, unmanned aerial vehicle upper cover 13's upper end is the arc setting, protects unmanned aerial vehicle fuselage 11 through unmanned aerial vehicle upper cover 13, reduces the inside of rainwater infiltration unmanned aerial vehicle fuselage 11, improves the anti-rainwater performance of unmanned aerial vehicle.
Two supporting legs 19 are installed to unmanned aerial vehicle fuselage 11's lower extreme, two supporting legs 19 are the symmetry and set up, just integration switching box 14 is located between two supporting legs 19, and every supporting legs 19 of group includes horizontal pole and two montants, and two montants vertical fixation are on the horizontal pole, and the both ends of horizontal pole are provided with anti-skidding line, when unmanned aerial vehicle fuselage 11 stops, support unmanned aerial vehicle fuselage 11 through supporting legs 19, are convenient for make unmanned aerial vehicle fuselage 11 can land steadily.
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 (10)

1. The utility model provides an emergency rescue is with following formula unmanned aerial vehicle which characterized in that: including unmanned aerial vehicle fuselage (11), six horn (12) are installed to angles such as lateral wall of unmanned aerial vehicle fuselage (11), vane (20) are installed to the one end of horn (12), integration switching box (14) is installed to the below of unmanned aerial vehicle fuselage (11), can dismantle on integration switching box (14) and be fixed with lighting system (17), propaganda directed to communicate system (18) and collection system, collection system includes 360 revolving stage (15) and camera (16) based on yolo algorithm, install camera (16) on 360 revolving stage (15), lighting system (17) are located the middle part of integration switching box (14), propaganda directed to communicate system (18) and camera (16) are located the both sides of lighting system (17) respectively.
2. The follow-up unmanned aerial vehicle for emergency rescue according to claim 1, characterized in that: the lighting system (17) comprises lighting lamps (1701), wherein the lighting lamps (1701) are arranged in an inverted quadrangular pyramid shape, and LED lamps (1702) are arranged on three surfaces of the lighting lamps (1701) at 45 degrees.
3. The follow-up unmanned aerial vehicle for emergency rescue according to claim 2, characterized in that: one end of the illuminating lamp (1701) is fixed with a connecting rod (1703), the side wall of one end of the connecting rod (1703) is symmetrically provided with clamping blocks (1704), and the lower surface of the integrated adapter box (14) is provided with a clamping block (1704) which is clamped and fixed with an illuminating quick-release connecting hole (23).
4. The follow-up unmanned aerial vehicle for emergency rescue according to claim 3, characterized in that: integration adapter box (14) are the rectangle setting, fuselage pair hole (21) have been seted up to the upper surface of integration adapter box (14), unmanned aerial vehicle fuselage (11) are connected fixedly through bolt and fuselage pair hole (21).
5. The follow-up unmanned aerial vehicle for emergency rescue according to claim 4, characterized in that: 360 revolving stage (15) are including making camera (16) around the 360 rotatory mount pads of X axle, the upper end lateral wall integrated into one piece of mount pad has two first joint pieces that are the symmetry and set up, cloud platform quick detach connecting hole (22) that supply first joint piece joint are seted up to the lower surface of integration switching box (14).
6. The follow-up unmanned aerial vehicle for emergency rescue according to claim 5, characterized in that: the system of shouting (18) includes speaker and fixing base, the upper end at the fixing base is installed in the speaker slope, the upper end lateral wall symmetry of fixing base is fixed with the second joint piece, the lower surface of integration switching box (14) is seted up and is supplied shouting quick detach connecting hole (24) of second joint piece joint.
7. The follow-up unmanned aerial vehicle for emergency rescue according to claim 6, characterized in that: cloud platform quick detach connecting hole (22), shout quick detach connecting hole (24) and illumination quick detach connecting hole (23) are the same setting, just cloud platform quick detach connecting hole (22) are the same with the joint direction of shout quick detach connecting hole (24), the joint direction of illumination quick detach connecting hole (23) is perpendicular with the joint direction of shout quick detach connecting hole (24).
8. The follow-up unmanned aerial vehicle for emergency rescue according to claim 1, characterized in that: adopt between unmanned aerial vehicle fuselage (11) and horn (12) to make unmanned aerial vehicle fuselage (11) be the dihedral installation of six rotor layouts.
9. The follow-up unmanned aerial vehicle for emergency rescue according to claim 1, characterized in that: unmanned aerial vehicle upper cover (13) are installed to the upper end of unmanned aerial vehicle fuselage (11), the upper end of unmanned aerial vehicle upper cover (13) is the arc setting.
10. The follow-up unmanned aerial vehicle for emergency rescue according to claim 1, characterized in that: two supporting legs (19) are installed to the lower extreme of unmanned aerial vehicle fuselage (11), two supporting legs (19) are the symmetry and set up, just integration switching box (14) are located between two supporting legs (19).
CN202222912307.1U 2022-11-02 2022-11-02 Following type unmanned aerial vehicle for emergency rescue Active CN218662359U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202222912307.1U CN218662359U (en) 2022-11-02 2022-11-02 Following type unmanned aerial vehicle for emergency rescue

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202222912307.1U CN218662359U (en) 2022-11-02 2022-11-02 Following type unmanned aerial vehicle for emergency rescue

Publications (1)

Publication Number Publication Date
CN218662359U true CN218662359U (en) 2023-03-21

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ID=85567578

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202222912307.1U Active CN218662359U (en) 2022-11-02 2022-11-02 Following type unmanned aerial vehicle for emergency rescue

Country Status (1)

Country Link
CN (1) CN218662359U (en)

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