CN215098258U - Anticollision type unmanned aerial vehicle that takes photo by plane - Google Patents
Anticollision type unmanned aerial vehicle that takes photo by plane Download PDFInfo
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- CN215098258U CN215098258U CN202120740264.6U CN202120740264U CN215098258U CN 215098258 U CN215098258 U CN 215098258U CN 202120740264 U CN202120740264 U CN 202120740264U CN 215098258 U CN215098258 U CN 215098258U
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- 238000009434 installation Methods 0.000 claims description 15
- 238000013016 damping Methods 0.000 claims description 10
- 230000007306 turnover Effects 0.000 claims 4
- 238000012544 monitoring process Methods 0.000 abstract description 6
- 230000003313 weakening effect Effects 0.000 abstract description 5
- 230000002035 prolonged effect Effects 0.000 abstract description 2
- 238000004146 energy storage Methods 0.000 abstract 1
- 230000035939 shock Effects 0.000 description 4
- 230000003139 buffering effect Effects 0.000 description 3
- 238000006243 chemical reaction Methods 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 230000008569 process Effects 0.000 description 3
- 230000005611 electricity Effects 0.000 description 2
- 238000003825 pressing Methods 0.000 description 2
- 239000006096 absorbing agent Substances 0.000 description 1
- 230000004075 alteration Effects 0.000 description 1
- 230000004888 barrier function Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000004590 computer program Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000003287 optical effect Effects 0.000 description 1
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
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Abstract
The utility model relates to the technical field of aerial photography unmanned aerial vehicles, in particular to an anti-collision aerial photography unmanned aerial vehicle, which comprises an unmanned aerial vehicle main body, wherein two sides of the bottom of the unmanned aerial vehicle main body are fixedly provided with an underframe, a basal plane of the unmanned aerial vehicle main body is embedded with an infrared obstacle avoidance sensor, a bottom center of the unmanned aerial vehicle main body is embedded with a rotating pan-tilt, the bottom of the rotating pan-tilt is provided with an electric roll-over stand, the bottom of the electric roll-over stand is provided with an aerial photography camera, the top of the inner wall of the unmanned aerial vehicle main body is provided with a control processor, two sides of the unmanned aerial vehicle main body are provided with rotor mounting frames, the whole device has simple structure, is convenient for automatic infrared monitoring and obstacle avoidance use, is convenient for ensuring the stable structure of power rotor mounting and weakening the use of vibration during operation and protecting the power rotor from collision, has the advantages of solar energy storage, prolonged endurance and power supply use and higher stability and practicability, has certain popularization value.
Description
Technical Field
The utility model relates to an unmanned air vehicle technical field specifically is an anticollision type unmanned air vehicle that takes photo by plane.
Background
The unmanned aerial vehicle is an unmanned aerial vehicle controlled by a radio remote control device or an onboard computer program control system, the unmanned aerial vehicle is simple in structure and low in use cost, not only can complete tasks executed by piloted aircraft, but also is more suitable for tasks which cannot be executed by piloted aircraft, emergency and early warning are realized in emergencies, aerial photography of the unmanned aerial vehicle takes the piloted aircraft as an aerial platform, onboard remote sensing equipment such as a high-resolution CCD (charge coupled device) digital camera, a light optical camera and an infrared scanner is used for acquiring information, a laser scanner and a magnetic measuring instrument are used for processing image information, and images are manufactured according to certain precision requirements.
The unmanned aerial vehicle that takes photo by plane that has now is not convenient for automatic infrared monitoring and avoids the anticollision of barrier and uses, and the stable in structure who guarantees the power rotor installation simultaneously is not convenient for use with the vibration of weakening the operation and is not convenient for protect the power rotor and prevent the collision and use to do not have solar energy electric power storage extension continuation of the journey power supply and use.
Therefore, there is a need for an anti-collision type aerial photography unmanned aerial vehicle that improves upon the above problems.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an anticollision type unmanned aerial vehicle that takes photo by plane to solve the problem that proposes in the above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme:
an anti-collision aerial photography unmanned aerial vehicle comprises an unmanned aerial vehicle main body, wherein two sides of the bottom of the unmanned aerial vehicle main body are fixedly provided with an underframe, an infrared obstacle avoidance sensor is embedded in the base surface of the unmanned aerial vehicle main body, a rotating holder is embedded in the center of the bottom of the unmanned aerial vehicle main body, the bottom of the rotating tripod head is provided with an electric roll-over stand, the bottom of the electric roll-over stand is provided with an aerial camera, the top of the inner wall of the unmanned aerial vehicle main body is provided with a control processor, two sides of the unmanned aerial vehicle main body are provided with rotor wing mounting racks, the two ends of the top of the rotor wing mounting rack are provided with power rotor wings, a first spring telescopic rod is arranged between one sides of the rotor wing mounting rack close to the main body of the unmanned aerial vehicle, one side of keeping away from first spring telescopic link on the rotor mounting bracket installs second spring telescopic link, the anticollision cover is installed to one side that rotor mounting bracket was kept away from to second spring telescopic link.
As the preferable scheme of the utility model, a solar electronic board is embedded and mounted at the top of the unmanned aerial vehicle main body; the battery is installed to the inside one side of pressing close to rotatory cloud platform of unmanned aerial vehicle main part, just electric connection between solar energy electronic plate and the battery.
As the utility model discloses preferred scheme, vibration damping mount is installed to the bottom of chassis, vibration damping mount adopts spring damper and crashproof heelpiece to constitute, and wherein spring damper's top fixed connection is in the top of chassis, and spring damper's bottom fixed connection is in the top of crashproof heelpiece.
As the utility model discloses preferred scheme, the rotation angle of rotatory cloud platform is the degree, just the internally mounted that the unmanned aerial vehicle main part was installed in the top embedding of rotatory cloud platform has the rotation driving motor.
As the utility model discloses preferred scheme, the rotation angle of electronic roll-over stand is the degree, just miniature upset driving motor is installed to the one end of electronic roll-over stand.
As the utility model discloses preferred scheme, be equipped with control module, power module and wireless module in proper order along length direction on control processor's the base face, wherein control processor passes through electric connection between power module and the battery, control processor passes through electric connection between control module and the infrared obstacle avoidance sensor, rotatory cloud platform, electronic roll-over stand, the camera of taking photo by plane and the power rotor, just control processor passes through wireless module and external control end wireless connection.
As the utility model discloses preferred scheme, first spring telescopic link all is equipped with the multiunit with second spring telescopic link.
Compared with the prior art, the beneficial effects of the utility model are that:
1. in the utility model, the infrared obstacle avoidance sensor embedded and installed on the base surface of the main body of the unmanned aerial vehicle is used for utilizing the infrared ray to meet the model of the obstacle object to be reflected, the infrared ray meets the obstacle in a certain range, the infrared ray is reflected and received and detected by the infrared obstacle avoidance sensor to cooperate with the control processor to process, analyze and control the power rotor wing to avoid the obstacle to be collided, the first spring telescopic rod arranged between the two sides of the main body of the unmanned aerial vehicle and the rotor wing mounting rack is used for ensuring the stable structure of the power rotor wing installation and weakening the vibration in operation, meanwhile, the anti-collision cover arranged on the outer side of the rotor wing mounting rack through the second spring telescopic rod is used for protecting the power rotor wing from collision, and the damping base consisting of the spring shock absorber and the anti-collision bottom cushion is arranged on the bottom of the chassis of the main body of the unmanned aerial vehicle, when the whole main body descends and lands, play buffering shock attenuation anticollision and use, the solar energy electronic plate cooperation battery of unmanned aerial vehicle main part top embedding installation simultaneously, be convenient for carry on solar energy conversion electric energy electric power storage and supply with whole unmanned aerial vehicle continuation of the journey power consumption and use, simple structure and the automatic infrared monitoring of being convenient for dodge the obstacle anticollision and use, be convenient for guarantee the stable in structure of power rotor installation simultaneously and weaken the vibration use of operation and be convenient for protect the power rotor and prevent the collision and use, and have the use of solar energy electric power storage extension continuation of the journey power supply.
Drawings
FIG. 1 is an overall front view of the present invention;
FIG. 2 is a schematic view of the overall internal structure of the present invention;
fig. 3 is an overall plan view of the present invention.
In the figure: 1. an unmanned aerial vehicle main body; 101. a chassis; 102. a rotor mount; 2. an infrared obstacle avoidance sensor; 3. rotating the holder; 4. an electric roll-over stand; 5. an aerial camera; 6. a control processor; 7. a storage battery; 8. a damping mount; 9. a first spring telescopic rod; 10. a second spring telescopic rod; 11. an anti-collision cover; 12. a power rotor; 13. solar electronic panels.
Detailed Description
The technical solution in the embodiments of the present invention will be clearly and completely described below in conjunction with the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, rather than all embodiments, and all other embodiments obtained by a person of ordinary skill in the art without creative work belong to the scope of the present invention based on the embodiments of the present invention.
In order to facilitate understanding of the present invention, the present invention will be described more fully hereinafter with reference to the accompanying drawings. Several embodiments of the present invention are presented. The invention may, however, be embodied in many different forms and should not be construed as limited to the embodiments set forth herein. Rather, these embodiments are provided so that this disclosure will be thorough and complete.
It will be understood that when an element is referred to as being "secured to" another element, it can be directly on the other element or intervening elements may also be present. When an element is referred to as being "connected" to another element, it can be directly connected to the other element or intervening elements may also be present. The terms "vertical," "horizontal," "left," "right," and the like as used herein are for illustrative purposes only.
Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs. The terminology used in the description of the invention herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the invention. As used herein, the term "and/or" includes any and all combinations of one or more of the associated listed items.
Referring to fig. 1-3, the present invention provides a technical solution:
an anti-collision aerial photography unmanned aerial vehicle comprises an unmanned aerial vehicle main body 1, wherein two sides of the bottom of the unmanned aerial vehicle main body 1 are fixedly provided with an underframe 101, a basal plane of the unmanned aerial vehicle main body 1 is embedded with an infrared obstacle avoidance sensor 2, a rotary holder 3 is embedded in the center of the bottom of the unmanned aerial vehicle main body 1, the bottom of the rotary holder 3 is provided with an electric roll-over stand 4, the bottom of the electric roll-over stand 4 is provided with an aerial photography camera 5, the top of the inner wall of the unmanned aerial vehicle main body 1 is provided with a control processor 6, two sides of the unmanned aerial vehicle main body 1 are provided with rotor wing mounting frames 102, two ends of the top of each rotor wing mounting frame 102 are provided with power rotor wings 12, a first spring telescopic rod 9 is arranged on each rotor wing mounting frame 102 and between one side close to the unmanned aerial vehicle main body 1, one side, far away from the first spring telescopic rod 9, on each rotor wing mounting frame 102 is provided with a second spring telescopic rod 10, one side, far away from each rotor wing mounting frame 102, is provided with an anti-collision cover 11, the whole device is simple in structure, convenient to use for automatic infrared monitoring and obstacle avoidance, convenient to guarantee the stable structure of power rotor installation and weaken vibration use in operation and convenient to protect the power rotor from collision use, and has the advantages of solar energy power storage, prolonged endurance, higher power supply use stability and practicability, and certain popularization value.
In an embodiment, referring to fig. 1, 2 and 3, a solar electronic board 13 is embedded and mounted at the top of the main body 1 of the unmanned aerial vehicle; the battery 7 is installed to the inside one side of pressing close to rotatory cloud platform 3 of unmanned aerial vehicle main part 1, and electric connection between solar energy electronic board 13 and the battery 7, and solar energy electronic board 13 cooperation battery 7 through the 1 top embedding installation of unmanned aerial vehicle main part that sets up is convenient for carry out solar energy conversion electric energy electric power storage and supply with whole unmanned aerial vehicle continuation of journey electricity and use.
Embodiment, please refer to fig. 1, 2 and 3, vibration damping mount 8 is installed to the bottom of chassis 101, vibration damping mount 8 adopts spring damper and crashproof heelpiece to constitute, wherein spring damper's top fixed connection is in the top of chassis 101, and spring damper's bottom fixed connection is in the top of crashproof heelpiece, vibration damping mount 8 that chassis 101 bottom installation through the unmanned aerial vehicle main part 1 that sets up adopted spring damper and crashproof heelpiece to constitute, be convenient for when whole unmanned aerial vehicle main part 1 descends to land, play buffering shock attenuation anticollision and use.
In an embodiment, please refer to fig. 1 and 2, the rotation angle of the rotating tripod head 3 is 360 degrees, the top end of the rotating tripod head 3 is embedded in the unmanned aerial vehicle main body 1 and is provided with a rotation driving motor, and the aerial camera 5 mounted on the bottom electric roll-over stand 4 is driven by the rotating tripod head 3 to horizontally rotate 360 degrees for angle adjustment.
In an embodiment, referring to fig. 1 and 2, the turning angle of the electric turning frame 4 is 270 degrees, a micro turning driving motor is installed at one end of the electric turning frame 4, and the aerial camera 5 installed through the electric turning frame 4 is conveniently driven to perform internal regulation shooting at an angle of 270 degrees in the vertical direction.
In the embodiment, referring to fig. 1 and 2, a control module, a power supply module and a wireless module are sequentially arranged on a base surface of a control processor 6 along a length direction, wherein the control processor 6 is electrically connected with a storage battery 7 through the power supply module, the control processor 6 is electrically connected with an infrared obstacle avoidance sensor 2, a rotating cradle head 3, an electric roll-over stand 4, an aerial camera 5 and a power rotor 12 through the control module, the control processor 6 is wirelessly connected with an external control end through the wireless module, the infrared obstacle avoidance sensor 2 embedded and mounted on the base surface of an unmanned aerial vehicle main body 1 is used for reflecting the infrared ray to the obstacle, the infrared ray meets the obstacle, is reflected and receives and detects a signal through the infrared obstacle avoidance sensor 2 to cooperate with the control processor 6 to process and analyze the power rotor 12 to avoid the obstacle and avoid collision, is convenient for automatic infrared monitoring and obstacle avoidance.
The embodiment, please refer to fig. 1, 2 and 3, first spring telescopic link 9 and second spring telescopic link 10 all are equipped with the multiunit, the first spring telescopic link 9 of installation between unmanned aerial vehicle main part 1 both sides and the rotor mounting bracket 102 through setting up is convenient for guarantee the stable in structure of power rotor 12 installation and the vibration when weakening the operation, the anticollision cover 11 of installation through second spring telescopic link 10 in the rotor mounting bracket 101 outside is convenient for protect power rotor 12 and prevent the collision and use simultaneously.
The working principle is as follows: when in use, the infrared obstacle avoidance sensor 2 embedded and installed on the base surface of the main body 1 of the unmanned aerial vehicle utilizes the type of infrared rays reflected when encountering an obstacle, the infrared rays encounter the obstacle within a certain range, are reflected and receive a detected signal through the infrared obstacle avoidance sensor 2 to cooperate with the control processor 6 to process, analyze and control the power rotor 12 to avoid the obstacle and avoid the collision, the first spring telescopic rods 9 installed between the two sides of the main body 1 of the unmanned aerial vehicle and the rotor installation frame 102 are used for ensuring the stable structure of the power rotor 12 and weakening the vibration during operation, meanwhile, the anti-collision cover 11 installed on the outer side of the rotor installation frame 101 through the second spring telescopic rods 10 is used for protecting the power rotor 12 from collision, the damping base 8 formed by adopting a spring damper and an anti-collision bottom cushion is installed at the bottom end of the underframe 101 of the main body 1 of the unmanned aerial vehicle, so that when the whole main body 1 of the unmanned aerial vehicle descends to the ground, play buffering shock attenuation anticollision and use, the solar energy electronic plate 13 cooperation battery 7 of the installation of the 1 top embedding of unmanned aerial vehicle main part simultaneously, be convenient for carry on solar energy conversion electric energy electric power storage supply whole unmanned aerial vehicle continuation of the journey electricity use, the overall structure is simple, the automatic infrared monitoring of being convenient for is dodged the obstacle anticollision and is used, be convenient for simultaneously guarantee the stable in structure of power rotor installation and weaken vibration use when the operation and be convenient for protect the power rotor and prevent colliding the use, and it is higher to have the use of solar energy electric power storage extension continuation of the journey power supply and stability and practicality, certain spreading value has.
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 (7)
1. The utility model provides an anticollision type unmanned aerial vehicle that takes photo by plane, includes unmanned aerial vehicle main part (1), its characterized in that: bottom both sides fixed mounting of unmanned aerial vehicle main part (1) has chassis (101), infrared obstacle avoidance sensor (2) is installed in the base face embedding of unmanned aerial vehicle main part (1), rotatory cloud platform (3) are installed in the embedding of bottom center department of unmanned aerial vehicle main part (1), the bottom of rotatory cloud platform (3) is equipped with electronic roll-over stand (4), aerial camera (5) are installed to the bottom of electronic roll-over stand (4), control treater (6) are installed at the inner wall top of unmanned aerial vehicle main part (1), rotor mounting bracket (102) is installed to the both sides of unmanned aerial vehicle main part (1), power rotor (12) are installed at the top both ends of rotor mounting bracket (102), press close to on rotor mounting bracket (102) and install first spring telescopic link (9) between one side of unmanned aerial vehicle main part (1), keep away from one side of first spring telescopic link (9) and install second spring telescopic link (10) on rotor mounting bracket (102) And an anti-collision cover (11) is installed on one side, far away from the rotor wing installation frame (102), of the second spring telescopic rod (10).
2. The unmanned aerial vehicle of claim 1, wherein: a solar electronic board (13) is embedded and mounted at the top of the unmanned aerial vehicle main body (1); the unmanned aerial vehicle main part (1) is inside to be pressed close to one side of rotatory cloud platform (3) and to install battery (7), just electric connection between solar energy electronic plate (13) and battery (7).
3. The unmanned aerial vehicle of claim 1, wherein: vibration damping mount (8) are installed to the bottom of chassis (101), vibration damping mount (8) adopt spring damper and crashproof heelpiece to constitute, and wherein spring damper's top fixed connection is in the top of chassis (101), and spring damper's bottom fixed connection is in the top of crashproof heelpiece.
4. The unmanned aerial vehicle of claim 1, wherein: the rotation angle of rotatory cloud platform (3) is 360 degrees, just the internally mounted that unmanned aerial vehicle main part (1) was installed in the top embedding of rotatory cloud platform (3) has the rotation driving motor.
5. The unmanned aerial vehicle of claim 1, wherein: the turnover angle of the electric turnover frame (4) is 270 degrees, and a micro turnover driving motor is installed at one end of the electric turnover frame (4).
6. The unmanned aerial vehicle of claim 1, wherein: be equipped with control module, power module and wireless module along length direction on the base face of control treater (6) in proper order, wherein control treater (6) are through electric connection between power module and battery (7), control treater (6) are through electric connection between control module and infrared obstacle avoidance sensor (2), rotatory cloud platform (3), electronic roll-over stand (4), aerial photography camera (5) and power rotor (12), just control treater (6) are through wireless module and external control end wireless connection.
7. The unmanned aerial vehicle of claim 1, wherein: the first spring telescopic rod (9) and the second spring telescopic rod (10) are both provided with multiple groups.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120740264.6U CN215098258U (en) | 2021-04-09 | 2021-04-09 | Anticollision type unmanned aerial vehicle that takes photo by plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120740264.6U CN215098258U (en) | 2021-04-09 | 2021-04-09 | Anticollision type unmanned aerial vehicle that takes photo by plane |
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| CN215098258U true CN215098258U (en) | 2021-12-10 |
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| CN202120740264.6U Expired - Fee Related CN215098258U (en) | 2021-04-09 | 2021-04-09 | Anticollision type unmanned aerial vehicle that takes photo by plane |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114506461A (en) * | 2022-03-10 | 2022-05-17 | 国网福建省电力有限公司三明供电公司 | Electric field measurement can regulate and control unmanned aerial vehicle cloud platform |
-
2021
- 2021-04-09 CN CN202120740264.6U patent/CN215098258U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114506461A (en) * | 2022-03-10 | 2022-05-17 | 国网福建省电力有限公司三明供电公司 | Electric field measurement can regulate and control unmanned aerial vehicle cloud platform |
| CN114506461B (en) * | 2022-03-10 | 2024-03-01 | 国网福建省电力有限公司三明供电公司 | Adjustable unmanned aerial vehicle holder for electric field measurement |
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Granted publication date: 20211210 |