CN214165292U

CN214165292U - Long-range large-mounting surveying and mapping unmanned aerial vehicle

Info

Publication number: CN214165292U
Application number: CN202022542495.4U
Authority: CN
Inventors: 刘双双; 宁波; 尚尔龙
Original assignee: Individual
Current assignee: Individual
Priority date: 2020-11-06
Filing date: 2020-11-06
Publication date: 2021-09-10
Anticipated expiration: 2030-11-06

Abstract

The utility model discloses a long-range large-mount surveying and mapping unmanned aerial vehicle, which comprises a main body, a plurality of extension wings, a plurality of rotor wings and a plurality of driving motors, the main body and a plurality of the extension wings are integrally formed, a plurality of the extension wings are arranged in an annular array by taking the center of the main body as an array, a plurality of the driving motors are embedded on the wing tips of a plurality of the extension wings, a plurality of the rotor wings are arranged on a plurality of the driving motors, the utility model relates to the technical field of surveying and mapping, the long-range large-mount surveying and mapping unmanned aerial vehicle has a simple and firm structure, adopts a wing-body integrated body design, increases the internal storage space of the main machine body, is matched with an external power supply mode, integrates the power supply outside the main machine body to increase the capacity of the power supply, a pair of parallel mounting grooves on two sides is used for increasing carrying capacity, the overall structure design is excellent, and a large range and mounting capacity can be obtained in the flying process.

Description

Long-range large-mounting surveying and mapping unmanned aerial vehicle

Technical Field

The utility model relates to a survey and drawing technical field specifically is a survey and drawing unmanned aerial vehicle of long voyage big carry.

Background

In the existing surveying and mapping technology, unmanned aerial vehicle surveying and mapping is a very advanced technology, more and more unmanned aerial vehicle products are applied to various technical fields along with the development of the unmanned aerial vehicle technology in China, wherein the unmanned aerial vehicle surveying and mapping is included, the application of the unmanned aerial vehicle in the surveying and mapping field not only accelerates the surveying and mapping efficiency and enables the surveying and mapping space to be three-dimensional, but also enables surveying and mapping personnel to have more overall view and benefits due to the overlooking form of the unmanned aerial vehicle surveying and mapping;

however, the existing unmanned aerial vehicle often needs to land to perform oil supplement or charge in the surveying and mapping process, so that the cruising ability of the unmanned aerial vehicle is still acceptable in a short term, but once the unmanned aerial vehicle is operated outside, the cruising ability of the unmanned aerial vehicle is greatly limited, even the unmanned aerial vehicle cannot complete the work within one day, the portable energy supply of the unmanned aerial vehicle is limited due to the small shape of the unmanned aerial vehicle, the range, the continuous operation ability and the mounting ability of the unmanned aerial vehicle are further limited, and some devices cannot be operated.

SUMMERY OF THE UTILITY MODEL

Not enough to prior art, the utility model provides a survey and drawing unmanned aerial vehicle of big carry of long voyage has solved current background technical problem.

In order to achieve the above purpose, the utility model discloses a following technical scheme realizes: a long-range large-mount surveying and mapping unmanned aerial vehicle comprises a main machine body, a plurality of extension wings, a plurality of rotor wings and a plurality of driving motors, wherein the main machine body and the extension wings are integrally formed, the extension wings are distributed in an annular array mode through the center of the main machine body, the driving motors are embedded on wing tips of the extension wings, the rotor wings are installed on the driving motors, a mounting groove is formed in one end of the main machine body, a camera is installed on the mounting groove, the mounting groove is wrapped by the camera in a half mode, and a power supply replacing structure is arranged below the main machine body and on one side of the mounting groove;

the power supply replacement structure includes: the power supply comprises a track groove, a power supply shell, a slot, a plug strip, a storage battery, a controller, a plug and a socket;

the host computer body bottom surface just is located the opposite one side of mounting groove and is equipped with the track groove, a pair of slot has been seted up to track bottom of the groove both sides, power casing both sides are equipped with a pair of cutting that matches with the slot, and is a pair of cutting cartridge is in a pair of in the slot, the embedded battery that is equipped with of power casing, be equipped with the plug on the battery, be equipped with the interface on the host computer body that matches with it, the internal top surface of host computer is equipped with the controller and is connected with the interface, and is a pair of be equipped with a pair of spacing subassembly on the slot, it is a pair of with it matches the spacing groove that a pair of and it matches is seted up to the cutting tip.

Preferably, the limiting assembly comprises: embedding grooves, springs and sliding blocks;

the inserting groove is characterized in that the tail end of the inserting groove is provided with an inwards concave embedded groove, a spring is arranged in the embedded groove, the end part of the spring is provided with a sliding block, one end of the sliding block is connected with the spring, the other end of the sliding block is of a spherical structure, and the inserting strip is provided with a spherical groove matched with the sliding block.

Preferably, a pair of mounting grooves parallel to the rail grooves are formed in two sides of the main body, and a plurality of hooks are arranged on the mounting grooves.

Preferably, a plurality of the extension wings are two pairs of trapezoidal hollow blocks with the same structure, and the radian of the top surfaces of the extension wings is greater than that of the bottom surfaces.

Preferably, the host computer body is the rectangle structure and the top surface is the arc arch, power chassis bottom surface flushes with host computer body bottom surface, the mounting groove is the wrapping up in the camera outside of half-cylinder type groove.

Preferably, the connection part of the wing root and the main body of a plurality of the extension wings adopts wing body fusion transition.

Advantageous effects

The utility model provides a survey and drawing unmanned aerial vehicle of big carry of long voyage. The method has the following beneficial effects: the unmanned aerial vehicle for surveying and mapping designed according to the scheme has the characteristics of good pneumatic appearance, long endurance time, convenience in energy source replacement and strong mounting capacity;

firstly, designing the pneumatic appearance of the existing unmanned aerial vehicle, wherein a rotor motor of the unmanned aerial vehicle is installed on the wingtips of extension wings in an embedding mode, and the wing structure is enhanced through hollow extension wings, so that preparation is provided for installing a rotor with a larger diameter and a high-power driving motor;

secondly, optimizing a mounting scheme, fixing a camera in a semi-wrapping mode, protecting the pneumatic appearance, reducing the unnecessary structural weight of the machine body, forming grooves in the bottom surfaces of two sides to serve as mounting grooves, and arranging hooks or mounting racks on the mounting grooves to mount different task modules;

the last battery as the energy adopts the modularized design, adopts cartridge and spacing mode installation battery, and the convenient change can select polylith battery to match an unmanned aerial vehicle when using to further increase the journey.

Drawings

Fig. 1 is a long-range big mounting surveying and mapping unmanned aerial vehicle's of looking up section structure schematic diagram.

Fig. 2 is a survey and drawing unmanned aerial vehicle's of big carry of long voyage looks sideways at schematic structure.

Fig. 3 is a long-range big mounting surveying and mapping unmanned aerial vehicle overlook the schematic structural diagram.

In the figure: 1. a main body; 2. extending the wing; 3. a rotor; 4. a drive motor; 5. a track groove; 6. a power supply housing; 7. a slot; 8. cutting; 9. a storage battery; 10. a controller; 11. a plug; 12. an interface; 13. embedding a groove; 14. a spring; 15. a slider; 16. and a mounting groove.

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.

All the electrical components in the present application are connected with the power supply adapted to the electrical components through a wire, and an appropriate controller and an appropriate encoder should be selected according to actual conditions to meet control requirements, and specific connection and control sequences should be obtained.

Example (b): according to the attached figures 1-3 of the specification, the long-range large-mount surveying and mapping unmanned aerial vehicle comprises a main body 1, a plurality of extending wings 2, a plurality of rotor wings 3 and a plurality of driving motors 4, wherein the main body 1 and the plurality of extending wings 2 are integrally formed, the plurality of extending wings 2 are arranged in an annular array at the center of the main body 1, the plurality of driving motors 4 are embedded on the wingtips of the plurality of extending wings 2, the plurality of rotor wings 3 are installed on the plurality of driving motors 4, one end of the main body 1 is provided with an installation groove, cameras are installed on the installation groove, the installation groove is semi-wrapped by the cameras, a power supply replacing structure is arranged below the main body 1 and on one side of the installation groove, in the specific implementation process, the main body 1 and the extending wings 2 are integrally formed, the design of a wing body fusion body is adopted, the internal storage space is enlarged, and meanwhile, the plurality of rotor wings 3 are symmetrically arranged at the wingtips of the extending wings 2, the air resistance is reduced by fusing the driving motor 4 with the wingtips of the extension wings 2, the rotor wings 3 are driven to rotate, wherein the bulge of the main machine body 1 is larger than the gradient of the bottom surface, so that the air pressure flowing through the main machine body 1 and the top surfaces of the wings is larger than the bottom surface, the lift force is increased, and the voyage is increased;

as can be seen from fig. 1 to 3 of the specification, the power supply replacement structure includes: the connection relation and the position relation of the track groove 5, the power supply shell 6, the slot 7, the inserting strip 8, the storage battery 9, the controller 10, the plug 11 and the inserting port 12 are as follows;

a track groove 5 is arranged on the bottom surface of the main machine body 1 and located on one side opposite to the mounting groove, a pair of slots 7 are formed in two sides of the bottom end of the track groove 5, a pair of inserting strips 8 matched with the slots 7 are arranged on two sides of the power supply shell 6, the pair of inserting strips 8 are inserted into the pair of slots 7, a storage battery 9 is embedded in the power supply shell 6, a plug 11 is arranged on the storage battery 9, a socket 12 is arranged on the main machine body 1 matched with the storage battery 9, a controller 10 is arranged on the top surface in the main machine body 1 and connected with the socket 12, a pair of limiting assemblies are arranged on the pair of slots, and a pair of limiting grooves matched with the limiting assemblies are formed in the end portions of the pair of inserting strips 8 matched with the slots;

in the specific implementation process, track groove 5 through the main engine body 1 bottom surface is as the cartridge platform of power, 6 both sides of power casing are equipped with respectively and insert 8 cartridge in slot 7, adopt the mode of pegging graft to install the power, battery 9 inlays the dress in power casing 6, and utilize the plug-in connector power supply of plug 11 and main engine body 1, provide continuation of the journey, and main engine body 1 is owing to adopt the design that the wing body fuses, the installation space of internal power source can be regarded as in the unnecessary place except flight control's subassembly in its inner space, further increase the voyage, it is spacing to utilize spacing subassembly to carry out when pegging graft the slip 8.

As a preferred scheme, further, as can be seen from fig. 1 to 3 of the specification, the limiting assembly comprises: the fitting groove 13, the spring 14, and the slider 15 are connected and positioned as follows;

the tail end of the slot 7 is provided with an inward embedded groove 13, a spring 14 is arranged in the embedded groove 13, the end part of the spring 14 is provided with a sliding block 15, one end of the sliding block 15 is connected with the spring 14, the other end of the sliding block 15 is of a spherical structure, and the inserting strip 8 is provided with a spherical groove matched with the sliding block 15;

in the specific implementation process, the spring 14 is fixed through the embedded groove 13, the spring 14 is used for providing outward potential energy for the sliding block 15, and when the inserting strip 8 is inserted into the inserting groove, the sliding block 15 slides out and is inserted into the limiting groove of the spherical groove structure for limiting, so that the power supply casing 6 is fixed.

Preferably, a pair of mounting grooves 16 parallel to the rail grooves 5 are formed on both sides of the main body 1, and a plurality of hooks are arranged on the mounting grooves 16 and used for mounting articles.

As a preferred scheme, furthermore, the plurality of extending wings 2 are two pairs of trapezoidal hollow blocks with the same structure, and the radian of the top surface of each extending wing 2 is greater than that of the bottom surface, so that the lift force of the whole machine is increased.

Preferably, the main body 1 has a rectangular structure, the top surface of the main body is an arc-shaped protrusion, the bottom surface of the power supply casing 6 is flush with the bottom surface of the main body 1, and the mounting groove is a semi-cylindrical groove and wraps the outer side of the camera.

Preferably, the connection parts of the wing roots of the plurality of extension wings 2 and the main body 1 are in wing body fusion transition, so that the storage space inside the main body 1 is increased.

To sum up, the survey and drawing unmanned aerial vehicle of big mount of long voyage, simple structure is durable, adopts wing body integration design, has increased the inside storage space of host computer body 1, and the mode of cooperation external band power is integrated the power in the outside of host computer body 1 can increase the capacity of power, is used for increasing the carrying capacity at a pair of parallel mounting groove 16 in both sides, and overall structure design is outstanding, can obtain great voyage and mounting capacity at the flight in-process.

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 long-range large-mounted surveying and mapping unmanned aerial vehicle comprises a main machine body (1), a plurality of extension wings (2), a plurality of rotor wings (3) and a plurality of driving motors (4), and is characterized in that the main machine body (1) and the plurality of extension wings (2) are integrally formed, the plurality of extension wings (2) are arranged in an annular array mode through the center of the main machine body (1), the plurality of driving motors (4) are embedded on wing tips of the plurality of extension wings (2), the plurality of rotor wings (3) are installed on the plurality of driving motors (4), a mounting groove is formed in one end of the main machine body (1), a camera is installed on the mounting groove, the mounting groove is wrapped by the camera in a half mode, and a power supply replacing structure is arranged below the main machine body (1) and on one side of the mounting groove;

the power supply replacement structure includes: the device comprises a track groove (5), a power supply shell (6), a slot (7), a plug strip (8), a storage battery (9), a controller (10), a plug (11) and a plug interface (12);

the host computer body (1) bottom surface just is located the opposite one side of mounting groove and is equipped with track groove (5), a pair of slot (7) have been seted up to track groove (5) bottom both sides, power casing (6) both sides are equipped with a pair of cutting (8) that match with slot (7), and are a pair of cutting (8) cartridge is in a pair of in slot (7), power casing (6) embedded battery (9) of being equipped with, be equipped with plug (11) on battery (9), be equipped with interface (12) on host computer body (1) that matches with it, the top surface is equipped with controller (10) and is connected with interface (12) in host computer body (1), and is a pair of spacing subassembly is equipped with on the slot, and it is a pair of to match with it the spacing groove that matches with it is seted up to cutting (8) tip.

2. The long-range large-mount surveying and mapping unmanned aerial vehicle of claim 1, wherein the limiting assembly comprises: an embedded groove (13), a spring (14) and a sliding block (15);

the tail end of the slot (7) is provided with an inwards concave embedded groove (13), a spring (14) is arranged in the embedded groove (13), the end part of the spring (14) is provided with a sliding block (15), one end of the sliding block (15) is connected with the spring (14), the other end of the sliding block is of a spherical structure, and the inserting strip (8) is provided with a spherical groove matched with the sliding block (15).

3. The long-range large-mount surveying and mapping unmanned aerial vehicle according to claim 1, wherein a pair of mount grooves (16) parallel to the rail grooves (5) are formed on two sides of the main body (1), and a plurality of hooks are arranged on the mount grooves (16).

4. The long-range large-mount surveying and mapping unmanned aerial vehicle of claim 1, wherein the plurality of extending wings (2) are two pairs of trapezoidal hollow blocks with the same structure, and the radian of the top surface of each extending wing (2) is larger than that of the bottom surface.

5. The long-range large-mount surveying and mapping unmanned aerial vehicle of claim 1, wherein the main body (1) is rectangular and has an arc-shaped top surface, the bottom surface of the power supply housing (6) is flush with the bottom surface of the main body (1), and the mounting groove is a semi-cylindrical groove wrapped outside the camera.

6. The long-range large-mount surveying and mapping unmanned aerial vehicle according to claim 4, wherein the connection portion of the root of the extending wings (2) and the main body (1) adopts wing body fusion transition.