CN212401552U

CN212401552U - Exploration unmanned aerial vehicle with gather function

Info

Publication number: CN212401552U
Application number: CN202020753485.2U
Authority: CN
Inventors: 欧丽梅; 汤方其
Original assignee: Individual
Current assignee: Individual
Priority date: 2020-05-09
Filing date: 2020-05-09
Publication date: 2021-01-26
Anticipated expiration: 2030-05-09

Abstract

The utility model discloses an exploration unmanned aerial vehicle with gather function, including the unmanned aerial vehicle body, the bottom fixedly connected with camera of unmanned aerial vehicle body, the equal fixedly connected with sleeve pipe in both sides of unmanned aerial vehicle body, sheathed tube inner chamber is provided with the wing, the card hole has all been seted up to sheathed tube top and bottom, the spring chamber has been seted up on the surface that is located sleeve pipe inner chamber one end of wing, the inner chamber fixedly connected with backup pad in spring chamber, the top and the equal fixedly connected with reset spring in bottom of backup pad. The utility model discloses a press the fixture block, the fixture block removes to the inner chamber in spring chamber, when the fixture block breaks away from the joint with the card hole on sleeve pipe surface to conveniently take the wing out to the sheathed tube outside, convenient to detach conveniently carries, has solved current unmanned aerial vehicle because the volume is great, and is comparatively inconvenient when carrying, causes the part to damage easily, thereby shortens unmanned aerial vehicle life's problem.

Description

Exploration unmanned aerial vehicle with gather function

Technical Field

The utility model relates to an unmanned air vehicle technique field specifically is an exploration unmanned aerial vehicle with gather function.

Background

Unmanned aerial vehicle is the unmanned aircraft that utilizes radio remote control equipment and self-contained program control device to control, or by the vehicle-mounted computer completely or intermittently independently operate, compare with manned aircraft, unmanned aerial vehicle often more is fit for those too foolproof, dirty or dangerous tasks, unmanned aerial vehicle is according to application, can be divided into military use and civilian use, for military use aspect, unmanned aerial vehicle divide into scout and target plane, at present in the field wide application such as aerial photography, agriculture, plant protection, miniature autodyne, express delivery transportation, rescue disaster, observe wild animal, control infectious disease, survey and drawing, news report, electric power inspection, relief disaster, movie & TV is shot, make romantic, greatly expand unmanned aerial vehicle's use itself, current unmanned aerial vehicle is comparatively inconvenient when carrying because of being bulky, cause the part to damage easily, thereby shorten unmanned aerial vehicle life.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide an exploration unmanned aerial vehicle with gather function possesses the advantage that conveniently carries, has solved current unmanned aerial vehicle because the volume is great, comparatively inconvenient when carrying, causes the part to damage easily to shorten unmanned aerial vehicle life's problem.

In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides an exploration unmanned aerial vehicle with gather function, includes the unmanned aerial vehicle body, the bottom fixedly connected with camera of unmanned aerial vehicle body, the equal fixedly connected with sleeve pipe in both sides of unmanned aerial vehicle body, sheathed tube inner chamber is provided with the wing, the card hole has all been seted up to sheathed tube top and bottom, the spring chamber has been seted up on the surface that is located sleeve pipe inner chamber one end of wing, the inner chamber fixedly connected with backup pad in spring chamber, the equal fixedly connected with reset spring in top and the bottom of backup pad, reset spring's other end fixedly connected with fixture block, and the fixture block extends to the outside in card hole.

Preferably, the fixed cover of equal fixedly connected with all around of unmanned aerial vehicle body bottom, the equal fixedly connected with buffer spring in both sides at fixed cover inner chamber top.

Preferably, the bottom of the buffer spring is fixedly connected with a limiting plate, and the bottom of the limiting plate is fixedly connected with a supporting leg.

Preferably, the bottom of the supporting leg extends to the outside of the fixing sleeve and is fixedly connected with a rubber pad.

Preferably, the two sides of the inner cavity of the fixed sleeve are both provided with a limiting groove, and the two sides of the limiting plate extend to the inner cavity of the limiting groove and are in sliding connection with the inner cavity of the limiting groove.

Compared with the prior art, the beneficial effects of the utility model are as follows:

1. the utility model discloses a press the fixture block, the fixture block removes to the inner chamber in spring chamber, when the fixture block breaks away from the joint with the card hole on sleeve pipe surface to conveniently take the wing out to the sheathed tube outside, convenient to detach conveniently carries, has solved current unmanned aerial vehicle because the volume is great, and is comparatively inconvenient when carrying, causes the part to damage easily, thereby shortens unmanned aerial vehicle life's problem.

2. The utility model discloses a set up buffer spring, limiting plate and landing leg, played when landing leg and ground contact, buffer spring atress deformation to the effect of buffering is carried out to the impact force that the descending produced.

Drawings

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

FIG. 2 is a schematic view of the sectional structure of the sleeve of the present invention;

fig. 3 is a schematic view of the cross-section structure of the fixing sleeve of the present invention.

In the figure: 1. an unmanned aerial vehicle body; 2. a camera; 3. a sleeve; 4. an airfoil; 5. a clamping hole; 6. a spring cavity; 7. a support plate; 8. a return spring; 9. a clamping block; 10. fixing a sleeve; 11. a buffer spring; 12. a limiting plate; 13. a support leg; 14. a limiting 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.

The utility model discloses an unmanned aerial vehicle body 1, camera 2, sleeve pipe 3, wing 4, card hole 5, spring chamber 6, backup pad 7, reset spring 8, fixture block 9, fixed cover 10, buffer spring 11, limiting plate 12, landing leg 13 and spacing groove 14 part are the parts that universal standard spare or field technician know, and its structure and principle all are this technical staff all can learn through the technical manual or learn through conventional experimental method.

Referring to fig. 1-3, an exploration unmanned aerial vehicle with collection function comprises an unmanned aerial vehicle body 1, a fixed sleeve 10 is fixedly connected around the bottom of the unmanned aerial vehicle body 1, buffer springs 11 are fixedly connected to both sides of the top of the inner cavity of the fixed sleeve 10, a limiting plate 12 is fixedly connected to the bottom of the buffer springs 11, supporting legs 13 are fixedly connected to the bottom of the limiting plate 12, the bottoms of the supporting legs 13 extend to the outside of the fixed sleeve 10 and are fixedly connected with rubber pads, limiting grooves 14 are formed on both sides of the inner cavity of the fixed sleeve 10, both sides of the limiting plate 12 extend to the inner cavity of the limiting grooves 14 and are slidably connected with the inner cavity of the limiting grooves 14, a camera 2 is fixedly connected to the bottom of the unmanned aerial vehicle body 1, sleeves 3 are fixedly connected to both sides of the unmanned aerial vehicle body 1, wings 4 are arranged in the, spring chamber 6 has been seted up on the surface that is located 3 inner chamber one ends of sleeve pipe of wing 4, the inner chamber fixedly connected with backup pad 7 of spring chamber 6, the top and the equal fixedly connected with reset spring 8 in bottom of backup pad 7, reset spring 8's other end fixedly connected with fixture block 9, and fixture block 9 extends to the outside of card hole 5, through pressing fixture block 9, fixture block 9 removes to the inner chamber of spring chamber 6, when fixture block 9 breaks away from the joint with the card hole 5 on sleeve pipe 3 surface, thereby conveniently take wing 4 out to sleeve pipe 3's outside, convenient to detach, conveniently carry, current unmanned aerial vehicle has been solved because the volume is great, it is comparatively inconvenient when carrying, cause the part to damage easily, thereby shorten unmanned aerial vehicle life's problem.

During the use, through pressing fixture block 9, fixture block 9 removes to the inner chamber of spring chamber 6, when fixture block 9 breaks away from the joint with the card hole 5 on sleeve pipe 3 surface to conveniently take wing 4 out to sleeve pipe 3's outside, convenient to detach conveniently carries, has solved current unmanned aerial vehicle because the volume is great, and is comparatively inconvenient when carrying, causes the part to damage easily, thereby shortens unmanned aerial vehicle life's problem.

The standard parts used in the application document can be purchased from the market, and can be customized according to the description of the specification and the description of the attached drawings, the specific connection mode of each part adopts conventional means such as mature bolts, rivets, welding and the like in the prior art, and machines, parts and equipment adopt conventional models in the prior art.

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 an exploration unmanned aerial vehicle with gather function, includes unmanned aerial vehicle body (1), its characterized in that: the utility model discloses an unmanned aerial vehicle, including unmanned aerial vehicle body (1), the bottom fixedly connected with camera (2) of unmanned aerial vehicle body (1), the equal fixedly connected with sleeve pipe (3) in both sides of unmanned aerial vehicle body (1), the inner chamber of sleeve pipe (3) is provided with wing (4), card hole (5) have all been seted up to the top and the bottom of sleeve pipe (3), spring chamber (6) have been seted up on the surface that is located sleeve pipe (3) inner chamber one end of wing (4), the inner chamber fixedly connected with backup pad (7) of spring chamber (6), the equal fixedly connected with reset spring (8) in top and bottom of backup pad (7), the other end fixedly connected with fixture block (9) of reset spring (8), and fixture block (9) extend to the outside of card hole.

2. Exploration drone with acquisition function according to claim 1, characterized in that: the unmanned aerial vehicle is characterized in that the periphery of the bottom of the unmanned aerial vehicle body (1) is fixedly connected with a fixed sleeve (10), and two sides of the top of an inner cavity of the fixed sleeve (10) are fixedly connected with buffer springs (11).

3. Exploration drone with acquisition function according to claim 2, characterized in that: the bottom of the buffer spring (11) is fixedly connected with a limiting plate (12), and the bottom of the limiting plate (12) is fixedly connected with a supporting leg (13).

4. Exploration drone with acquisition function according to claim 3, characterized in that: the bottom of the supporting leg (13) extends to the outside of the fixing sleeve (10) and is fixedly connected with a rubber pad.

5. Exploration drone with acquisition function according to claim 3, characterized in that: the limiting groove (14) is formed in each of two sides of the inner cavity of the fixing sleeve (10), and each of two sides of the limiting plate (12) extends to the inner cavity of the corresponding limiting groove (14) and is in sliding connection with the inner cavity of the corresponding limiting groove (14).