CN217533266U

CN217533266U - Combined unmanned aerial vehicle

Info

Publication number: CN217533266U
Application number: CN202220730742.XU
Authority: CN
Inventors: 殷孝忠
Original assignee: Fuxin Ecological Space Survey And Design Institute Co ltd
Current assignee: Fuxin Ecological Space Survey And Design Institute Co ltd
Priority date: 2022-03-31
Filing date: 2022-03-31
Publication date: 2022-10-04
Anticipated expiration: 2032-03-31

Abstract

The utility model provides a modular unmanned aerial vehicle relates to unmanned air vehicle technical field, including the fuselage, the camera is equipped with to the lower surface of fuselage, and camera and light filling lamp are equipped with to the front end of camera, and the extension board is equipped with to the surface of fuselage, and the upper surface of extension board is equipped with the deckle board, and the upper surface of extension board is equipped with the gag lever post. The utility model discloses, through having set up the fuselage, the camera, the extension board, the deckle board, the gag lever post, the wing, including a motor, an end cap, a controller, and a cover plate, the flabellum, the dead lever, the nut, can be through the cooperation of motor and flabellum, flight for the fuselage provides power source, cooperation through camera and camera, realize this unmanned aerial vehicle's earth's surface exploration function, through the extension board, deckle board and gag lever post realize the limited function to wing position and angle, cooperation through screw rod and nut, realize the fixed position function of wing, and through the structure of this kind of removable, when the damage appears in the wing, it provides convenience to maintain the work for the change of wing.

Description

Combined unmanned aerial vehicle

Technical Field

The utility model relates to an unmanned air vehicle technique field especially relates to a modular unmanned aerial vehicle.

Background

Unmanned aerial vehicle, a small-size remote control formula helicopter, its principle is through the free removal function of air kinetic energy realization fuselage in the air, in unmanned aerial vehicle's in-service use, because among the aerial photography work, it is great to the exploration work load on earth's surface, also compare frequently to unmanned aerial vehicle's frequency of use, lead to unmanned aerial vehicle's wing part probably to receive the damage because of unexpected factors such as misoperation, change and maintenance work are all relatively complicated, need improve.

SUMMERY OF THE UTILITY MODEL

The utility model aims at solving the shortcoming that exists among the prior art, and the modular unmanned aerial vehicle who provides.

In order to achieve the above purpose, the utility model adopts the following technical scheme: the utility model provides a modular unmanned aerial vehicle, includes the fuselage, the camera is equipped with to the lower surface of fuselage, camera and light filling lamp are equipped with to the front end of camera, the extension board is equipped with to the surface of fuselage, the upper surface of extension board is equipped with the deckle board, the upper surface of extension board is equipped with the gag lever post, the surface cover of gag lever post is equipped with the wing, the motor is equipped with to the one end of wing, the flabellum is equipped with to the output of motor, the upper surface of gag lever post is equipped with the dead lever, the surface cover of dead lever is equipped with the nut.

In order to realize the protect function to the flabellum, the utility model discloses an improvement has, the surface of motor is equipped with the protection frame, the annular frame is equipped with between the protection frame, the protection frame cover is established at the surface of flabellum.

In order to carry out preliminary spacing to the position of wing, the utility model discloses an improvement has, the wing is laminated with the extension board mutually, the surface at the wing is established to the deckle board cover.

In order to realize the dismouting function of nut, the utility model discloses an improvement has, the surface of dead lever is seted up threadedly, the dead lever passes through the screw thread and is connected with the nut rotation, the nut is laminated with the wing mutually.

In order to inject electric telescopic handle's output position, the utility model discloses an improvement has, electric telescopic handle is equipped with to the inboard of fuselage, electric telescopic handle's one end runs through to the lower surface of fuselage.

In order to realize the position shift function of connecting rod and semi-ring frame, the utility model discloses an improvement has, be equipped with the connecting rod between electric telescopic handle's the bottom, semi-ring frame is equipped with to the surface of connecting rod.

Compared with the prior art, the utility model discloses an advantage lies in with positive effect:

1. the utility model discloses, through having set up the fuselage, the camera, the extension board, the deckle board, the gag lever post, the wing, including a motor, an end cap, a controller, and a cover plate, the flabellum, the dead lever, the nut, can be through the cooperation of motor and flabellum, flight for the fuselage provides power source, cooperation through camera and camera, realize this unmanned aerial vehicle's earth's surface exploration function, through the extension board, deckle board and gag lever post realize the limited function to wing position and angle, cooperation through screw rod and nut, realize the fixed position function of wing, and through the structure of this kind of removable, when the damage appears in the wing, it provides convenience to maintain the work for the change of wing.

2. The utility model discloses, through having set up electronic flexible, connecting rod, semi-ring frame, can realize the position control function of connecting rod, semi-ring frame through electric telescopic handle to through the cooperation of connecting rod and semi-ring frame, establish more stable bearing structure, through this kind of mode, can provide the stable stay at the in-process that the fuselage fell, and can reduce the air resistance through electric telescopic handle's shrink at the in-process that the fuselage removed.

Drawings

Fig. 1 is a schematic view of the overall components of a combined unmanned aerial vehicle according to the present invention;

fig. 2 is an exploded view of a depression angle part of a structure of a combined unmanned aerial vehicle according to the present invention;

fig. 3 is a schematic view of a contraction state of an electric telescopic rod of the combined unmanned aerial vehicle;

fig. 4 is the utility model provides a modular unmanned aerial vehicle figure 2's a department enlargies the schematic diagram.

Illustration of the drawings:

1. a body; 2. a camera; 3. a camera; 4. a light supplement lamp; 5. a support plate; 6. a frame plate; 7. a limiting rod; 8. an airfoil; 9. a motor; 10. a fan blade; 11. a protective frame; 12. fixing the rod; 13. a nut; 14. an electric telescopic rod; 15. a connecting rod; 16. a semi-ring frame.

Detailed Description

In order to make the above objects, features and advantages of the present invention more clearly understood, the present invention will be further described with reference to the accompanying drawings and examples. It should be noted that the embodiments and features of the embodiments of the present application may be combined with each other without conflict.

In the following description, numerous specific details are set forth in order to provide a thorough understanding of the present invention, however, the present invention may be practiced in other ways than those specifically described herein, and therefore the present invention is not limited to the limitations set forth in the following description of the specific embodiments.

Example one

Referring to fig. 1, 2 and 4, the present invention provides a technical solution: a combined unmanned aerial vehicle comprises a machine body 1, a camera 2 is arranged on the lower surface of the machine body 1, a camera 3 and a light supplementing lamp 4 are arranged at the front end of the camera 2, stable support can be provided for the camera 2 through the machine body 1, the earth surface exploration function of the unmanned aerial vehicle is realized through the camera 3, certain light source supplement is provided when the light supplementing lamp 4 is insufficient in the light source of the surrounding environment, so that the effective implementation of earth surface exploration work is ensured, a support plate 5 is arranged on the outer surface of the machine body 1, a frame plate 6 is arranged on the upper surface of the support plate 5, the stable support can be provided for the support plate 5 through the machine body 1, the frame plate 6 is further supported, a limiting rod 7 is arranged on the upper surface of the support plate 5, a wing sleeve 8 is arranged on the outer surface of the limiting rod 7, the position of a wing 8 can be preliminarily limited through the limiting rod 7, the wing 8 is attached to the support plate 5, the frame plate 6 is sleeved on the outer surface of the wing 8, the support plate 5 can provide basic support for the wing 8, the limiting function of the position and the angle of the wing 8 is realized through the frame plate 6, the fixing rod 12 is arranged on the upper surface of the limiting rod 7, the nut 13 is sleeved on the outer surface of the fixing rod 12, the outer surface of the fixing rod 12 is provided with threads, the fixing rod 12 is rotatably connected with the nut 13 through the threads, the nut 13 is attached to the wing 8, the design aims to realize the dismounting function of the nut 13, the position fixing function of the wing 8 is realized when the nut 13 is dismounted through the position arrangement of the nut 13, the motor 9 is arranged at one end of the wing 8, the fan blade 10 is arranged at the output end of the motor 9, the fan blade 10 can be driven to rotate through the operation of the motor 9, so that a power source is provided for the movement of the unmanned aerial vehicle, the protective frame 11 is arranged on the outer surface of the motor 9, and the annular frame is arranged between the protective frames 11, can make protection frame 11's structure more stable through the annular frame, protection frame 11 cover is established at the surface of flabellum 10, can protect flabellum 10's structure through preventing the balladeur train, avoids flabellum 10 to receive the condition emergence of damaging at rotatory in-process.

Example two

Please refer to fig. 2-3, an electric telescopic rod 14 is installed on the inner side of the body 1, one end of the electric telescopic rod 14 penetrates the lower surface of the body 1, the purpose of the design is to limit the output position of the electric telescopic rod 14, a connecting rod 15 is installed between the bottom ends of the electric telescopic rods 14, a semi-ring frame 16 is installed on the outer surface of the connecting rod 15, the purpose of the design is to enlarge the contact area between the bottom end of the supporting rod and the ground, so as to provide more stable support for the rising and falling work of the body 1, and avoid the occurrence of the situation that the camera 3 is damaged in the rising and falling process of the body 1, in the flying process of the body 1, the connecting rod 15 and the semi-ring frame 16 are driven to move to the position attached to the body 1 through the expansion and contraction of the electric telescopic rod 14, and the air resistance in the flying process of the body 1 is reduced.

The working principle is as follows: when the fuselage 1 needs to be moved, the fan blades 10 are driven to rotate through the operation of the motor 9, the movement of the fuselage 1 is provided with aerodynamic energy, the fuselage 1 is driven to move, in the flying process, shooting work is carried out through the camera 2 and the camera 3, light source supplement is provided for the camera 3 through the light supplementing lamp 4, effective implementation of ground surface exploration work is ensured, in the lifting and falling process of the fuselage 1, the connecting rod 15 and the half ring frame 16 are driven to move through the extension of the electric telescopic rod 14, stable support is provided for the fuselage 1 through the connecting rod 15 and the half ring frame 16, the situation that the camera 3 is damaged in the lifting and falling process of the fuselage 1 is avoided, in the flying process of the fuselage 1, the connecting rod 15 and the half ring frame 16 are driven to move to be in a position attached to the fuselage 1 through the extension and the extension of the electric telescopic rod 14, the aerodynamic resistance in the flying process of the fuselage 1 is reduced, when the wing 8 is damaged, firstly, the nut 13 is detached through a rotating mode, the wing 8 is replaced, the wing 8 is sleeved on the outer surface of the limiting rod 7, the frame 6 is attached to the nut 12, and the nut 13 is attached to the wing 8, and the nut is convenient to maintain the wing 8, and the nut in a reverse direction, and the nut is attached to rotate.

The above description is only a preferred embodiment of the present invention, and is not intended to limit the present invention in other forms, and any person skilled in the art may use the above-mentioned technical contents to change or modify the equivalent embodiment into equivalent changes to be applied in other fields, but all those persons do not depart from the technical contents of the present invention, and any simple modification, equivalent change and modification made to the above embodiments according to the technical matters of the present invention still belong to the protection scope of the technical solution of the present invention.

Claims

1. The utility model provides a modular unmanned aerial vehicle, includes fuselage (1), its characterized in that: camera (2) are equipped with to the lower surface of fuselage (1), camera (3) and light filling lamp (4) are equipped with to the front end of camera (2), extension board (5) are equipped with to the surface of fuselage (1), the upper surface of extension board (5) is equipped with framed panel (6), the upper surface of extension board (5) is equipped with gag lever post (7), the surface cover of gag lever post (7) is equipped with wing (8), motor (9) are equipped with to the one end of wing (8), flabellum (10) are equipped with to the output of motor (9), the upper surface of gag lever post (7) is equipped with dead lever (12), the surface cover of dead lever (12) is equipped with nut (13).

2. The modular drone of claim 1, wherein: the outer surface of motor (9) is equipped with protection frame (11), be equipped with the annular frame between protection frame (11), protection frame (11) cover is established at the surface of flabellum (10).

3. The modular drone of claim 1, wherein: the wing (8) is attached to the support plate (5), and the frame plate (6) is sleeved on the outer surface of the wing (8).

4. The modular drone of claim 1, wherein: the outer surface of the fixing rod (12) is provided with threads, the fixing rod (12) is rotatably connected with a nut (13) through the threads, and the nut (13) is attached to the wing (8).

5. The modular drone of claim 1, wherein: electric telescopic handle (14) are equipped with to the inboard of fuselage (1), the lower surface to fuselage (1) is run through to the one end of electric telescopic handle (14).

6. The modular drone of claim 5, wherein: a connecting rod (15) is arranged between the bottom ends of the electric telescopic rods (14), and a semi-ring frame (16) is arranged on the outer surface of the connecting rod (15).