CN211592901U

CN211592901U - Low-altitude remote sensing emergency monitoring equipment

Info

Publication number: CN211592901U
Application number: CN201921804843.1U
Authority: CN
Inventors: 伍宜丹; 肖逸; 梁媛; 段鉴书
Original assignee: Sichuan Agricultural University
Current assignee: Sichuan Agricultural University
Priority date: 2019-10-25
Filing date: 2019-10-25
Publication date: 2020-09-29
Anticipated expiration: 2029-10-25

Abstract

The utility model discloses a low latitude remote sensing emergency monitoring equipment, including hydrogen spheroid, lifting rope, monitoring devices, hawser, the hydrogen spheroid is connected with monitoring devices through the lifting rope, the hydrogen spheroid passes through the hawser with draw gear and is connected, monitoring devices includes spherical gasbag, metal casing, first servo motor, a supporting bench, camera, machine carries controlling means and battery, be equipped with the pore that is used for placing the pipeline of charging head on the gasbag, the pipeline open end is equipped with the jam piston, draw gear includes controller casing, support column, reel, second servo motor, be equipped with ground controlling means in the controller casing; this device simple structure for traditional unmanned aerial vehicle check out test set, has practiced thrift the cost, and this device can effectively protect monitoring facilities through the gasbag.

Description

Low-altitude remote sensing emergency monitoring equipment

Technical Field

The utility model belongs to the technical field of the remote sensing equipment and specifically relates to an emergent monitoring of low latitude remote sensing is equipped.

Background

The aerial remote sensing equipment is with the remote sensing equipment who carries out photographic (or scanning) formation of image on the basis of well low latitude remote sensing platform, remote sensing equipment divide into flight equipment and ground controlgear, and what the flight equipment that adopts now mostly used is unmanned aerial vehicle equipment, however, unmanned aerial vehicle cost is higher, carry out unmanned aerial vehicle monitoring to some low latitude and some high pollution areas, harm to unmanned aerial vehicle is great, detect the cost and rise, and unmanned in case the emergence is dropped, very easily break, the serious person can cause the loss of data collection, cause unnecessary loss, therefore, the cost is with low costs to the design, prevent falling waterproof low latitude monitoring facilities.

SUMMERY OF THE UTILITY MODEL

The utility model discloses an it is not enough to overcome above-mentioned condition, aims at providing the technical scheme that can solve above-mentioned problem.

A low-altitude remote sensing emergency monitoring device comprises a hydrogen ball body, a lifting rope, a monitoring device and a cable rope, wherein the lower end of the hydrogen ball body is fixedly connected with the lifting rope, the lifting rope is connected with the monitoring device, the hydrogen ball body is connected with a traction device through the cable rope, the monitoring device comprises a spherical air bag, a cavity is arranged at the center of the interior of the air bag, a metal shell with a fan-shaped section is fixedly glued in the cavity, a first servo motor is fixedly glued in the metal shell, a support table is fixedly sleeved on an output shaft of the first servo motor, a camera is fixedly bolted on the support table and drives the first servo motor to drive the support table and the camera to rotate, so that the camera can be observed in all directions, an onboard control device and a storage battery are installed in the metal shell, and a charging port of the storage battery is positioned on the metal shell, be equipped with the pore that is used for placing the pipeline of the head that charges on the gasbag, the pipeline open end is equipped with the jam piston, the gasbag can effectively protect power components such as camera, draw gear includes the controller casing, controller casing front end welded fastening has two support columns, install the reel between two support columns, insert to fix in the bearing frame at the pivot both ends of wire winding theory, bearing frame welded fastening is in the inboard of two support columns, the outside bolt fastening of a support column has second servo motor, be equipped with ground controlling means in the controller casing.

As a further aspect of the present invention: the lower end of the lifting rope is fixedly connected with a lock catch, the top of the air bag is provided with a buckle, and the lock catch is buckled on the buckle, so that the air bag and the hydrogen balloon body can be conveniently separated.

As a further aspect of the present invention: the airborne control device comprises a WiFi communication receiving module, a central processing module and a storage module.

As a further aspect of the present invention: the ground control device comprises a WiFi communication transmitting module, a processing module and a storage battery module.

As a further aspect of the present invention: and the ground control device is electrically connected with the second servo motor.

As a further aspect of the present invention: the air bag is provided with a heat dissipation pore passage, so that heat dissipation is facilitated.

The utility model has the advantages that: this device simple structure for traditional unmanned aerial vehicle check out test set, has practiced thrift the cost, and this device can effectively protect monitoring facilities through the gasbag.

Additional aspects and advantages of the invention will be set forth in part in the description which follows and, in part, will be obvious from the description, or may be learned by practice of the invention.

Drawings

In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings needed to be used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without inventive exercise.

FIG. 1 is a schematic structural view of the present invention;

fig. 2 is a schematic structural view of the monitoring device of the present invention;

fig. 3 is a schematic structural view of the traction device of the present invention.

In the figure: the system comprises a hydrogen balloon 1, a hydrogen balloon 2, a lifting rope 21, a lock catch 3, a monitoring device 31, an air bag 311, a retaining ring 32, a cavity 33, a metal shell 34, a first servo motor 35, a support platform 36, a camera 37, an onboard control device 38, a storage battery 39, a pipeline 391, a blocking piston 4, a cable 5, a traction device 51, a controller shell 52, a support column 52, a winding wheel 53, a bearing seat 54, a second servo motor 55, a ground control device 56 and a heat dissipation channel 6.

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 to 3, in an embodiment of the present invention, a low altitude remote sensing emergency monitoring device includes a hydrogen balloon 1, a lifting rope 2, a monitoring device 3, and a cable 4, the lower end of the hydrogen balloon 1 is fixedly connected with the lifting rope 2, the lifting rope 2 is connected with the monitoring device 3, the hydrogen balloon 1 is connected with a traction device 5 through the cable 4, the monitoring device 3 includes a spherical air bag 31, a cavity 32 is disposed at a central position inside the air bag 31, a metal shell 33 with a fan-shaped cross section is adhesively fixed inside the cavity 32, a first servo motor 34 is adhesively fixed inside the metal shell 33, a support table 35 is fixedly connected to an output shaft of the first servo motor 34 in a sleeved manner, a camera 36 is bolted to the support table 35, and drives the first servo motor 34 to drive the support table 35 and the camera 36 to rotate, so that the camera 36 can perform omnidirectional observation, the traction device comprises a metal shell 33, a machine-mounted control device 37 and a storage battery 38 are installed in the metal shell 33, a charging port of the storage battery 38 is located on the metal shell 33, a pore channel for placing a pipeline 39 of a charging head is formed in the air bag 31, a blocking piston 391 is arranged at the opening end of the pipeline 39, the air bag 31 can effectively protect power supply parts such as a camera 36, the traction device 5 comprises a controller shell 51, two support columns 52 are welded and fixed to the front end of the controller shell 51, a winding wheel 53 is installed between the two support columns 52, two ends of a rotating shaft of the winding wheel 53 are inserted and fixed in a bearing seat 54, the bearing seat 54 is welded and fixed to the inner sides of the two support columns 52, a second servo motor 55 is fixed to the outer side of each support column 52 through bolts, and a ground.

The lower end of the lifting rope 2 is fixedly connected with a lock 21, the top of the air bag 31 is provided with a buckle 311, the lock 21 is buckled on the buckle 311, and the air bag 31 and the hydrogen balloon 1 can be conveniently separated.

The onboard control device 37 comprises a WiFi communication receiving module, a central processing module and a storage module.

The ground control device 56 comprises a WiFi communication transmitting module, a processing module and a storage battery module.

The ground control device 56 is electrically connected to the second servomotor 55.

The air bag 31 is provided with a heat dissipation pore passage 6, so that heat dissipation is facilitated.

The utility model discloses a theory of operation is: during the use, detain hasp 21 on buckle 311, later take whole monitoring devices 3 to the air through hydrogen spheroid 1, adjust the position height through receiving and releasing hawser 4, come control monitoring devices 3's roughly position through traction cable 4, later through ground controlling means 56 transmission signal, with signal transmission for airborne controlling means 37 control first servo motor 34 rotate realize that camera 36 is rotatory to be shot, and gasbag 31 can alleviate equipment weight and protect equipment that can be fine simultaneously, prevent falling waterproof.

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

1. A low-altitude remote sensing emergency monitoring device comprises a hydrogen ball body, a lifting rope, a monitoring device and a cable rope, and is characterized in that the lower end of the hydrogen ball body is fixedly connected with the lifting rope, the lifting rope is connected with the monitoring device, the hydrogen ball body is connected with a traction device through the cable rope, the monitoring device comprises a spherical air bag, a cavity is arranged at the center of the interior of the air bag, a metal shell with a fan-shaped section is fixedly glued in the cavity, a first servo motor is fixedly glued in the metal shell, a supporting table is fixedly sleeved on an output shaft of the first servo motor, a camera is fixedly bolted on the supporting table and drives the first servo motor to drive the supporting table and the camera to rotate, an onboard control device and a storage battery are installed in the metal shell, a charging port of the storage battery is positioned on the metal shell, and a pore channel for placing a pipeline of a charging head is arranged on the air bag, the pipeline open end is equipped with the jam piston, draw gear includes controller casing, support column, reel, controller casing front end welded fastening has two support columns, install the reel between two support columns, the pivot both ends of reel insert to be fixed in the bearing frame, bearing frame welded fastening is in the inboard of two support columns, the outside bolt fastening of a support column has second servo motor, be equipped with ground controlling means in the controller casing.

2. The low altitude remote sensing emergency monitoring equipment according to claim 1, wherein a lock catch is fixedly connected to the lower end of the lifting rope, and a retaining ring is arranged at the top of the air bag.

3. The low altitude remote sensing emergency monitoring equipment of claim 1, wherein the onboard control device comprises a WiFi communication receiving module, a central processing module and a storage module.

4. The low altitude remote sensing emergency monitoring equipment of claim 1, wherein the ground control device comprises a WiFi communication transmitting module, a processing module and a storage battery module.

5. The low altitude remote sensing emergency monitoring equipment of claim 1, wherein the ground control device is electrically connected to a second servo motor.

6. The low altitude remote sensing emergency monitoring equipment according to claim 1, wherein a heat dissipation pore passage is arranged on the air bag.