CN212710022U - Many rotor unmanned aerial vehicle of volcanic vent with thermal imaging function - Google Patents

Many rotor unmanned aerial vehicle of volcanic vent with thermal imaging function Download PDF

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Publication number
CN212710022U
CN212710022U CN202021536654.3U CN202021536654U CN212710022U CN 212710022 U CN212710022 U CN 212710022U CN 202021536654 U CN202021536654 U CN 202021536654U CN 212710022 U CN212710022 U CN 212710022U
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China
Prior art keywords
aerial vehicle
unmanned aerial
motor
thermal imaging
frame
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CN202021536654.3U
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Chinese (zh)
Inventor
吴献文
孙照辉
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Guangzhou Quancheng Multidimensional Information Technology Co ltd
Guangdong College of Industry and Commerce
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Guangzhou Quancheng Multidimensional Information Technology Co ltd
Guangdong College of Industry and Commerce
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Priority to CN202021536654.3U priority Critical patent/CN212710022U/en
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Abstract

The utility model discloses a volcanic vent multi-rotor unmanned aerial vehicle with a thermal imaging function, which comprises an unmanned aerial vehicle, a thermal imager and a mounting rack, wherein the mounting rack is fixed at the bottom of the unmanned aerial vehicle, and the thermal imager is arranged on the mounting rack through an adjusting structure; the regulating structure comprises: mounting bracket, motor, moving part, connecting piece, bear frame and adjusting part, the utility model relates to an unmanned air vehicle technique field. This technical scheme provides an unmanned aerial vehicle that can adjust thermal imager angle, and this kind of unmanned aerial vehicle carries on the thermal imager, carries out thermal imaging to the crater to the person of being convenient for detects the state of crater, the effectual problem of mentioning among the background art of having solved.

Description

Many rotor unmanned aerial vehicle of volcanic vent with thermal imaging function
Technical Field
The utility model relates to an unmanned air vehicle technique field specifically is a many rotor unmanned aerial vehicle of volcanic entrance with thermal imaging function.
Background
The volcanic vent needs to be regularly detected for the temperature of the volcanic vent to prevent volcanic eruption, but an interested fan wants to see the wind of the volcanic vent at a glance, but due to high danger, the images of the volcanic vent are relatively few, and the shooting strength of the state of the volcanic vent is high.
SUMMERY OF THE UTILITY MODEL
The utility model provides a not enough to prior art, the utility model provides a many rotor unmanned aerial vehicle of volcanic vent with thermal imaging function has solved the volcanic vent owing to need regularly to detect its volcanic vent temperature, prevents the volcanic eruption, and more thinks one to see the wind sampling of volcanic vent to the interest fan, but because high danger, therefore the image of volcanic vent is less relatively, the reason lies in to shoot the higher technical problem of intensity to the state of volcanic vent.
In order to achieve the above purpose, the utility model discloses a following technical scheme realizes: a volcanic vent multi-rotor unmanned aerial vehicle with a thermal imaging function comprises an unmanned aerial vehicle, a thermal imager and a mounting rack, and is characterized in that the mounting rack is fixed at the bottom of the unmanned aerial vehicle, and the thermal imager is mounted on the mounting rack through an adjusting structure;
the regulating structure comprises: the device comprises a mounting frame, a motor, a movable piece, a connecting piece, a bearing frame and an adjusting component;
the mounting bracket is located the unmanned aerial vehicle bottom, and the motor is settled on the mounting bracket, and the moving part inlays and installs on the mounting bracket, and the drive end and the connecting piece of motor are connected, the other end and the moving part of connecting piece are connected, bear the frame and be connected with the moving part bottom, the adjusting part is located and bears the frame.
Preferably, the adjustment assembly comprises: the motor, a pair of connecting shafts and a pair of embedded frames;
the motor is located on the outer wall of the bearing frame, the pair of connecting shafts are inserted in the bearing frame, the driving of the motor is connected with one of the connecting shafts, the pair of embedded frames is connected with the pair of connecting shafts, and the thermal imager is embedded in the embedded frames.
Preferably, the mounting frame is connected with the bottom of the unmanned aerial vehicle through a plurality of bolts.
Preferably, a fixing frame is arranged between the motor and the mounting frame.
Preferably, a motor frame is arranged between the motor and the bearing frame.
Advantageous effects
The utility model provides a many rotor unmanned aerial vehicle of volcanic vent with thermal imaging function. Possess following beneficial effect, this technical scheme provides an unmanned aerial vehicle that can adjust thermal imager angle, and this kind of unmanned aerial vehicle carries on the thermal imager, carries out thermal imaging to the crater to convenient to use person detects the state of crater, the effectual problem of mentioning among the background art of having solved.
Drawings
Fig. 1 is a many rotor unmanned aerial vehicle's of volcanic vent structure with thermal imaging function schematic diagram.
Fig. 2 is a volcanic entrance multi-rotor unmanned aerial vehicle's local structure schematic diagram with thermal imaging function.
In the figure: 1-unmanned aerial vehicle; 2-a thermal imager; 3-mounting a frame; 4-a motor; 5-a movable part; 6-connecting piece; 7-a carrier; 8-a motor; 9-a connecting shaft; 10-a motor frame; 11-embedding a frame; 12-a fixing frame.
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. 1-2, the present invention provides a technical solution: a many rotor unmanned aerial vehicle of volcanic vent with thermal imaging function.
Example (b): a volcanic multi-rotor unmanned aerial vehicle with a thermal imaging function comprises an unmanned aerial vehicle 1, a thermal imager 2 and a mounting rack 3, wherein the mounting rack 3 is fixed at the bottom of the unmanned aerial vehicle 1, and the thermal imager 2 is mounted on the mounting rack 3 through an adjusting structure;
it should be noted that the adjusting structure may be used to adjust the thermal imager 2, so as to facilitate shooting and imaging at different positions of the crater;
specifically, the adjusting structure comprises: the device comprises a mounting frame 3, a motor 4, a movable piece 5, a connecting piece 6, a bearing frame 7 and an adjusting component;
mounting bracket 3 is located 1 bottom of unmanned aerial vehicle, and motor 4 settles on mounting bracket 3, and moving part 5 inlays and adorns on mounting bracket 3, and motor 4's drive end is connected with connecting piece 6, and connecting piece 6's the other end is connected with moving part 5, bears 7 and is connected with moving part 5 bottom, and adjusting part is located and bears 7.
It should be noted that, in the above, after the motor 4 drives the connecting member 6, the connecting member 6 is connected to the moving member 5, and the moving member 5 can drive the bearing frame 7 to rotate, so as to drive the adjusting assembly on the bearing frame 7 to adjust the plane angle, and further adjust the angle of the thermal imager 2.
Specifically, the adjusting assembly comprises: a motor 8, a pair of connecting shafts 9, and a pair of embedded frames 11;
the motor 8 is located on the outer wall of the bearing frame 7, the pair of connecting shafts 9 are inserted in the bearing frame 7, the motor 8 is driven to be connected with one of the connecting shafts 9, the pair of embedded frames 11 is connected with the pair of connecting shafts 9, and the thermal imager 2 is embedded in the embedded frames 11.
In the above, the thermal imager 2 is embedded on the embedded frame 11, the motor 8 drives the connecting shaft 9, and the connecting shaft 9 drives the embedded frame 11 to rotate, so that the thermal imager 2 is rotated, and the shooting angle of the thermal imager 2 is adjusted.
As a preferred solution, further, the mounting frame 3 is connected with the bottom of the unmanned aerial vehicle 1 through a plurality of bolts.
Preferably, a fixing frame 12 is disposed between the motor 4 and the mounting frame 3.
Preferably, a motor frame 10 is further provided between the motor 8 and the carriage 7.
It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. Without further limitation. The phrase "comprising an element defined by … … does not exclude the presence of additional identical elements in the process, method, article, or apparatus that comprises the element.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims (5)

1. A volcanic-mouth multi-rotor unmanned aerial vehicle with a thermal imaging function comprises an unmanned aerial vehicle (1), a thermal imager (2) and a mounting rack (3), and is characterized in that the mounting rack (3) is fixed at the bottom of the unmanned aerial vehicle (1), and the thermal imager (2) is mounted on the mounting rack (3) through an adjusting structure;
the regulating structure comprises: the device comprises a mounting frame (3), a motor (4), a movable piece (5), a connecting piece (6), a bearing frame (7) and an adjusting component;
the unmanned aerial vehicle is characterized in that the mounting frame (3) is located at the bottom of the unmanned aerial vehicle (1), the motor (4) is arranged on the mounting frame (3), the moving part (5) is embedded on the mounting frame (3), the driving end of the motor (4) is connected with the connecting piece (6), the other end of the connecting piece (6) is connected with the moving part (5), the bearing frame (7) is connected with the bottom of the moving part (5), and the adjusting assembly is located on the bearing frame (7).
2. The multi-rotor drone with thermal imaging function according to claim 1, characterized in that said adjustment assembly comprises: a motor (8), a pair of connecting shafts (9), and a pair of embedded frames (11);
the thermal imager is characterized in that the motor (8) is located on the outer wall of the bearing frame (7), the pair of connecting shafts (9) are inserted into the bearing frame (7), the motor (8) is driven to be connected with one of the connecting shafts (9), the pair of embedded frames (11) are connected with the pair of connecting shafts (9), and the thermal imager (2) is embedded into the embedded frames (11).
3. The multi-rotor drone with thermal imaging function according to claim 1, characterized in that the mounting frame (3) is connected with the bottom of the drone (1) by means of a plurality of bolts.
4. The multi-rotor drone with thermal imaging function according to claim 1, characterized in that a fixing frame (12) is provided between the motor (4) and the mounting frame (3).
5. A volcanic-type multi-rotor drone with thermal imaging functionality according to claim 2, characterized in that a motor mount (10) is provided between the motor (8) and the carrier (7).
CN202021536654.3U 2020-07-29 2020-07-29 Many rotor unmanned aerial vehicle of volcanic vent with thermal imaging function Active CN212710022U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202021536654.3U CN212710022U (en) 2020-07-29 2020-07-29 Many rotor unmanned aerial vehicle of volcanic vent with thermal imaging function

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202021536654.3U CN212710022U (en) 2020-07-29 2020-07-29 Many rotor unmanned aerial vehicle of volcanic vent with thermal imaging function

Publications (1)

Publication Number Publication Date
CN212710022U true CN212710022U (en) 2021-03-16

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN202021536654.3U Active CN212710022U (en) 2020-07-29 2020-07-29 Many rotor unmanned aerial vehicle of volcanic vent with thermal imaging function

Country Status (1)

Country Link
CN (1) CN212710022U (en)

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