CN212354396U

CN212354396U - High survey and drawing unmanned aerial vehicle who lasts duration

Info

Publication number: CN212354396U
Application number: CN202021056567.8U
Authority: CN
Inventors: 杜鹏
Original assignee: Qingdao Zhonghai Changyang Environmental Technology Co ltd
Current assignee: Qingdao Zhonghai Changyang Environmental Technology Co ltd
Priority date: 2020-06-10
Filing date: 2020-06-10
Publication date: 2021-01-15
Anticipated expiration: 2030-06-10

Abstract

The utility model discloses a survey and drawing unmanned aerial vehicle of high continuation of journey, including structure and circuit, the top central point fixedly connected with solar cell panel of unmanned aerial vehicle casing, the inner wall bottom central point fixedly connected with battery of unmanned aerial vehicle casing, and be located corresponding position between the corresponding both sides of unmanned aerial vehicle casing inner wall and all rotate and be connected with the axis of rotation, the surperficial bottom one side of support bar is rotated and is connected with the supporting legs, electric telescopic handle's work end is rotated with the surperficial one side of supporting legs and is connected, the corresponding position in unmanned aerial vehicle casing top all is provided with rotary wing, the bottom central point of unmanned aerial vehicle casing puts and is provided with camera mechanism, the utility model relates to a. This survey and drawing unmanned aerial vehicle of high continuation of journey has reached the energy storage, reduces the effect of volume, and the energy storage is convenient fast, can contract, reduces air resistance, reduces energy resource consumption, and sustainable continuation of journey has improved work efficiency and performance.

Description

High survey and drawing unmanned aerial vehicle who lasts duration

Technical Field

The utility model relates to a survey and drawing unmanned aerial vehicle technical field specifically is a survey and drawing unmanned aerial vehicle of high continuation of journey.

Background

Along with the continuous development of society, the technological level is continuously improved, also more and more to unmanned aerial vehicle's use, unmanned aerial vehicle is the unmanned aerial vehicle that utilizes radio remote control equipment and the program control device of self-contained to control, unmanned aerial vehicle is also called many rotor crafts, it has portablely, light in weight, flight is stable, characteristics such as noise low, carry image equipment and monitoring equipment can provide powerful means for secret reconnaissance, especially the region that the people is difficult for approaching, can provide aerial first hand image data, also can play huge effect in the event of group sex equally, can carry small-size tear gas even in addition to reconnaissance and throw in the air, in surveying and mapping trade, unmanned aerial vehicle also plays this important effect simultaneously. At present, prior art unmanned aerial vehicle can only carry out short distance and work of lower intensity, can't keep the work of continuation, leads to actual operating time short, and total operating time is longer, has great limitation, and at the during operation, bulky moreover, can't shrink, leads to the resistance that receives great to the energy consumption of accelerating has further reduced operating time, can't last flight, has reduced performance.

SUMMERY OF THE UTILITY MODEL

Technical problem to be solved

Not enough to prior art, the utility model provides a survey and drawing unmanned aerial vehicle of high continuation of journey has solved that unmanned aerial vehicle can only carry out short distance and work of lower intensity, can't keep the work of continuation, lead to actual operating time short, and total operating time is longer, there is great limitation, and at the during operation, it is bulky, can't shrink, lead to the resistance that receives great, thereby the energy consumption of acceleration, the operating time has further been reduced, can't last flight, the problem of performance is reduced.

(II) technical scheme

In order to achieve the above purpose, the utility model discloses a following technical scheme realizes: the utility model provides a survey and drawing unmanned aerial vehicle of high continuation of journey, includes structure and circuit, the structure includes the unmanned aerial vehicle casing, the top central point fixedly connected with solar cell panel of unmanned aerial vehicle casing, the inner wall bottom central point fixedly connected with battery of unmanned aerial vehicle casing, it is connected with the axis of rotation all to lie in corresponding position between the corresponding both sides of unmanned aerial vehicle casing inner wall, the fixed surface of axis of rotation is connected with the support bar, the one end that the axis of rotation was kept away from to the support bar runs through the inner wall of unmanned aerial vehicle casing and extends to its outside, surface bottom one side of support bar is rotated and is connected with the supporting legs, surface one side of support bar is rotated and is connected with electric telescopic handle, electric telescopic handle's working end is rotated with surface one side of supporting legs and is connected, the corresponding, and a camera shooting mechanism is arranged at the central position of the bottom of the unmanned aerial vehicle shell.

Preferably, the surface of the rotating shaft is fixedly connected with a first gear, the position of the bottom of the inner wall of the unmanned aerial vehicle shell, which is close to the first gear, is fixedly connected with a servo motor, the output shaft of the servo motor is fixedly connected with a second gear, and the second gear is meshed with the first gear.

Preferably, the circuit includes microcontroller, microcontroller's interface electricity in proper order is connected with wireless transmission module, speedtransmitter and power module, power module's interface electricity in proper order is connected with power detection module, battery, the interface electricity of battery is connected with solar control module, electricity is connected between solar control module's interface and solar cell panel's the interface.

Preferably, the top of the unmanned aerial vehicle shell and the solar cell panel are both arranged to be arc curved surfaces.

Preferably, the rotation breach with the one end looks adaptation of support bar is all seted up to the corresponding both sides in unmanned aerial vehicle casing surface bottom, the rectangle recess has been seted up to the surperficial one side of support bar and the position that is located electric telescopic handle.

(III) advantageous effects

The utility model provides a survey and drawing unmanned aerial vehicle of high continuation of journey. The method has the following beneficial effects:

(1) the high-continuous-endurance surveying and mapping unmanned aerial vehicle is characterized in that a solar cell panel is fixedly connected to the central position of the top of the unmanned aerial vehicle shell, a storage battery is fixedly connected to the central position of the bottom of the inner wall of the unmanned aerial vehicle shell, rotating shafts are rotatably connected between two corresponding sides of the inner wall of the unmanned aerial vehicle shell and located at corresponding positions, supporting bars are fixedly connected to the surfaces of the rotating shafts, one ends, far away from the rotating shafts, of the supporting bars penetrate through the inner wall of the unmanned aerial vehicle shell and extend to the outside of the unmanned aerial vehicle shell, supporting legs are rotatably connected to one sides of the surfaces of the supporting bars, electric telescopic rods are rotatably connected to the working ends of the electric telescopic rods and one sides of the surfaces of the supporting legs, rotary wing bodies are arranged at corresponding positions of the top of, the energy storage device has the advantages of reasonable and simple structure, convenience in use, quickness and convenience in energy storage, capability of contracting, volume reduction, air resistance reduction, energy consumption reduction, sustainable endurance and improvement on working efficiency and service performance.

Drawings

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

FIG. 2 is a schematic view of the shrinking structure in flight of the present invention;

fig. 3 is a circuit block diagram.

In the figure: the solar camera comprises an unmanned aerial vehicle shell 1, a solar cell panel 2, a storage battery 3, a rotating shaft 4, a supporting bar 5, supporting legs 6, an electric telescopic rod 7, a rotating wing 8, a camera shooting mechanism 9, a first gear 10, a servo motor 11 and a second gear 12.

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. 1-3, the present invention provides a technical solution: the utility model provides a survey and drawing unmanned aerial vehicle of high continuation of journey, includes structure and circuit, and the circuit includes microcontroller, and microcontroller is the singlechip, and the model of singlechip is: AT80C51, for prior art, commercially available, the interface of microcontroller electricity in proper order is connected with wireless transmission module, speed sensor and power module, the interface of power module electricity in proper order is connected with power detection module, battery 3, the interface electricity of battery 3 is connected with solar control module, the interface of solar control module is connected with the interface electricity between solar cell panel 2, the structure includes unmanned aerial vehicle casing 1, the top central point of unmanned aerial vehicle casing 1 fixedly connects with solar cell panel 2, solar cell panel 2 can turn light energy into electric energy, make the energy storage quick and convenient, provide energy for high continuation of journey, the top of unmanned aerial vehicle casing 1 and solar cell panel 2 all set up as the circular arc curved surface, can reduce the resistance, the inner wall bottom central point of unmanned aerial vehicle casing 1 fixedly connects with battery 3, battery 3 can provide the electric energy for whole device, a rotating shaft 4 is rotatably connected between two corresponding sides of the inner wall of the unmanned aerial vehicle shell 1 and at corresponding positions, a supporting bar 5 is fixedly connected to the surface of the rotating shaft 4, rotating notches matched with one end of the supporting bar 5 are respectively arranged at two corresponding sides of the bottom of the surface of the unmanned aerial vehicle shell 1, one end of the supporting bar 5, far away from the rotating shaft 4, penetrates through the inner wall of the unmanned aerial vehicle shell 1 and extends to the outside of the inner wall, a supporting leg 6 is rotatably connected to one side of the bottom of the surface of the supporting bar 5, an electric telescopic rod 7 is rotatably connected to one side of the surface of the supporting bar 5, a rectangular groove is arranged at one side of the surface of the supporting bar 5 and at the position of the electric telescopic rod 7, the working end of the electric telescopic rod 7 is rotatably connected to one side of the surface of the, the surface of the rotating shaft 4 is fixedly connected with a first gear 10, the position of the bottom of the inner wall of the unmanned aerial vehicle shell 1, which is close to the first gear 10, is fixedly connected with a servo motor 11, the output shaft of the servo motor 11 is fixedly connected with a second gear 12, and the second gear 12 is meshed with the first gear 10.

When the device is used, firstly, the device is placed at a specified position, when the device needs to work, the whole device is driven by the rotation of the rotary wing 8, the servo motor 11 is started immediately to work, the output shaft of the servo motor 11 drives the second gear 12 to rotate, the second gear 12 is meshed with the first gear 10 to drive the first gear 10 to rotate, the rotating shaft 4 is driven to rotate, the supporting bar 5 is retracted, the electric telescopic rod 7 is started simultaneously when the servo motor 11 is started, the electric telescopic rod 7 is retracted, the working end of the electric telescopic rod 7 pulls the supporting legs 6 to rotate, the supporting legs 6 are tightly attached to the surfaces of the supporting bar 5, the retraction is realized, the size is reduced, the air resistance is reduced, and meanwhile, the top of the unmanned aerial shell 1 and the solar cell panel 2 are both arranged to be arc curved surfaces, also can reduce the resistance, reduce energy consumption, sustainable continuation of the journey, work efficiency and performance have been improved, in-process at the flight, solar cell panel 2 can be with solar energy transformation electric energy, and store in battery 3, battery 3 can provide the electric energy for whole device, and then high ability of lasting continuation of the journey has been realized, when work is accomplished, when preparing the whereabouts, rotate to opposite direction through servo motor 11 this moment, rotate support bar 5 to unmanned aerial vehicle casing 1's bottom, open electric telescopic handle 7 simultaneously, and make its extension, electric telescopic handle 7's work end promotes supporting legs 6 and rotates this moment, when support bar 5's bottom and supporting legs 6 one end contact ground, triangular supports has been formed this moment, stability is improved.

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 use of the phrase "comprising one of the elements does not exclude the presence of other like 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

1. The utility model provides a survey and drawing unmanned aerial vehicle of high continuation of journey, includes structure and circuit, its characterized in that: the structure comprises a unmanned aerial vehicle shell (1), a solar cell panel (2) is fixedly connected to the top central position of the unmanned aerial vehicle shell (1), a storage battery (3) is fixedly connected to the central position of the bottom of the inner wall of the unmanned aerial vehicle shell (1), a rotating shaft (4) is rotatably connected to the positions between the two corresponding sides of the inner wall of the unmanned aerial vehicle shell (1), a supporting strip (5) is fixedly connected to the surface of the rotating shaft (4), one end, far away from the rotating shaft (4), of the supporting strip (5) penetrates through the inner wall of the unmanned aerial vehicle shell (1) and extends to the outside of the unmanned aerial vehicle shell, one side of the bottom of the surface of the supporting strip (5) is rotatably connected with a supporting foot (6), one side of the surface of the supporting strip (5) is rotatably connected with an electric telescopic rod (7), the working end of the, the unmanned aerial vehicle is characterized in that rotary wings (8) are arranged at corresponding positions of the top of the unmanned aerial vehicle shell (1), and a camera shooting mechanism (9) is arranged at the center of the bottom of the unmanned aerial vehicle shell (1).

2. The high duration mapping unmanned aerial vehicle of claim 1, wherein: the surface fixed connection of axis of rotation (4) has first gear (10), the inner wall bottom of unmanned aerial vehicle casing (1) and the position fixed connection who is close to first gear (10) have servo motor (11), the output shaft fixed connection of servo motor (11) has second gear (12), meshing connection between second gear (12) and first gear (10).

3. The high duration mapping unmanned aerial vehicle of claim 1, wherein: the circuit comprises a microcontroller, the interface of the microcontroller is electrically connected with a wireless transmission module, a speed sensor and a power supply module in sequence, the interface of the power supply module is electrically connected with a power supply detection module and a storage battery (3) in sequence, the interface of the storage battery (3) is electrically connected with a solar control module, and the interface of the solar control module is electrically connected with the interface of a solar cell panel (2).

4. The high duration mapping unmanned aerial vehicle of claim 1, wherein: the top of the unmanned aerial vehicle shell (1) and the solar cell panel (2) are both arranged to be arc curved surfaces.

5. The high duration mapping unmanned aerial vehicle of claim 1, wherein: the corresponding both sides in unmanned aerial vehicle casing (1) surface bottom all set up with the rotation breach of the one end looks adaptation of support bar (5), the rectangle recess has been seted up to the surface one side of support bar (5) and the position that is located electric telescopic handle (7).