CN213443079U

CN213443079U - Impact-proof exploration unmanned aerial vehicle

Info

Publication number: CN213443079U
Application number: CN202021520670.3U
Authority: CN
Inventors: 林素芬; 王宁
Original assignee: Individual
Current assignee: Individual
Priority date: 2020-07-28
Filing date: 2020-07-28
Publication date: 2021-06-15
Anticipated expiration: 2030-07-28

Abstract

The utility model discloses an impact-proof exploration unmanned aerial vehicle, including the unmanned aerial vehicle organism, the equal fixedly connected with mount in both sides of unmanned aerial vehicle organism, one side fixedly connected with mount pad of unmanned aerial vehicle organism is kept away from to the mount, the top of mount pad is provided with helical blade, one side fixedly connected with sleeve pipe of mount is kept away from to the mount pad, one side fixedly connected with attenuator of cover tube cavity. The utility model discloses an unmanned aerial vehicle organism, mount pad, helical blade, sleeve pipe, attenuator, connecting plate, spliced pole, guard plate, first spring, pillar and the cooperation of landing frame are used, thereby can effectually solve traditional unmanned aerial vehicle of exploring because the wing lacks the problem that the protection reduces the security in the use, this unmanned aerial vehicle of exploring can effectually protect the wing part to the effectual security that improves unmanned aerial vehicle avoids receiving the damage phenomenon that the impact produced.

Description

Impact-proof exploration unmanned aerial vehicle

Technical Field

The utility model relates to an unmanned air vehicle technique field specifically is an impact-proof exploration unmanned aerial vehicle.

Background

Unmanned aerial vehicle is called unmanned aerial vehicle for short, unmanned aerial vehicle operated by radio remote control equipment and self-contained program control device, or autonomous operation completely or intermittently by vehicle-mounted computer, unmanned aerial vehicle can be divided into military and civil according to application field, for military use, unmanned aerial vehicle is divided into reconnaissance plane and target drone, for civil use, industrial application of unmanned aerial vehicle is real just needed by unmanned aerial vehicle, when in use, unmanned aerial vehicle needs to fly in comparatively abominable environment, the possibility of damage is very high, especially rotor wing part, if some damage, imbalance can be caused, and unmanned aerial vehicle is damaged.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide an impact-proof exploration unmanned aerial vehicle possesses the effectual advantage of protection, has solved when using, and unmanned aerial vehicle need fly in comparatively abominable environment, and the possibility of its damage is very big, especially rotor part, if damage a bit, will cause the unbalance, and damage unmanned problem.

In order to achieve the above object, the utility model provides a following technical scheme: an anti-impact exploration unmanned aerial vehicle comprises an unmanned aerial vehicle body, wherein fixing frames are fixedly connected to two sides of the unmanned aerial vehicle body, one side, away from the unmanned aerial vehicle body, of each fixing frame is fixedly connected with a mounting seat, the top of each mounting seat is provided with a helical blade, one side, away from each fixing frame, of each mounting seat is fixedly connected with a sleeve, one side, away from the inner wall of each sleeve, of each sleeve is fixedly connected with a connecting plate, one side, away from each connecting plate, of each connecting plate extends to the outside of each sleeve, one side, located at the outside of each sleeve, of each connecting plate is fixedly connected with a protection plate, the surface, located at the damper, of each inner cavity of each sleeve is sleeved with a first spring, one side of each first spring is fixedly connected with each connecting plate, one side of, the bottom of the pillar is sleeved with a falling frame.

Preferably, the top and the bottom of the inner cavity of the sleeve are both provided with sliding grooves, the top and the bottom of the connecting plate are both fixedly connected with sliding blocks, one side, far away from the connecting plate, of each sliding block extends to the inner cavity of each sliding groove, and each sliding groove is connected with the corresponding sliding block in a sliding mode.

Preferably, the top of the falling frame is provided with a groove, the bottom of the inner cavity of the groove is fixedly connected with a second spring, the bottom of the support column is fixedly connected with a backing plate, and the top of the backing plate is fixedly connected with the top of the second spring.

Preferably, the bottom of the opposite side of the falling frame is fixedly connected with a connecting frame, and the connecting frame is of an arc-shaped structure.

Preferably, the bottom fixedly connected with watch-dog of unmanned aerial vehicle organism, the both ends of guard plate are a structure of turning over.

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

1. the utility model discloses an unmanned aerial vehicle organism, mount pad, helical blade, sleeve pipe, attenuator, connecting plate, spliced pole, guard plate, first spring, pillar and the cooperation of landing frame are used, thereby can effectually solve traditional unmanned aerial vehicle of exploring because the wing lacks the problem that the protection reduces the security in the use, this unmanned aerial vehicle of exploring can effectually protect the wing part to the effectual security that improves unmanned aerial vehicle avoids receiving the damage phenomenon that the impact produced.

2. The utility model discloses a set up spout and slider, can guarantee the stability of connecting plate, when receiving the impact, the atress is even to guaranteed equipment stability, through setting up recess, second spring and backing plate, can improve this exploration unmanned aerial vehicle and play the ability of buffer protection when descending, strengthen equipment security, through setting up the link, can connect the frame that falls, guarantee the stability that equipment connects, through setting up the watch-dog, can realize the purpose of exploration.

Drawings

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

FIG. 2 is a schematic cross-sectional view of the internal structure of the casing according to the present invention;

fig. 3 is a schematic sectional view of the connection structure of the support and the landing frame of the present invention.

In the figure: 1. an unmanned aerial vehicle body; 2. a fixed mount; 3. a mounting seat; 4. a helical blade; 5. a sleeve; 6. a damper; 7. a connecting plate; 8. connecting columns; 9. a protection plate; 10. a first spring; 11. a pillar; 12. a descending frame; 13. a chute; 14. a slider; 15. a groove; 16. a second spring; 17. a base plate; 18. a connecting frame; 19. and a monitor.

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.

In the description of the present invention, it should be noted that the terms "upper", "lower", "inner", "outer", "front end", "rear end", "both ends", "one end", "the other end", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplification of description, but do not indicate or imply that the device or element to be referred must have a specific orientation, be constructed in a specific orientation, and be operated, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first" and "second" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.

In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted", "provided", "connected", and the like are to be construed broadly, such as "connected", which may be fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.

The components adopted by the utility model are all universal standard components or components known by the technicians in the field, and the structure and the principle of the components are known by the technicians through technical manuals or conventional experimental methods.

Referring to fig. 1-3, an anti-impact exploration unmanned aerial vehicle comprises an unmanned aerial vehicle body 1, a monitor 19 is fixedly connected to the bottom of the unmanned aerial vehicle body 1, two ends of a protection plate 9 are of a turnover structure, fixing frames 2 are fixedly connected to both sides of the unmanned aerial vehicle body 1, a mounting seat 3 is fixedly connected to one side of the fixing frame 2 away from the unmanned aerial vehicle body 1, a helical blade 4 is arranged at the top of the mounting seat 3, a sleeve 5 is fixedly connected to one side of the mounting seat 3 away from the fixing frame 2, sliding grooves 13 are formed in the top and the bottom of the inner cavity of the sleeve 5, sliding blocks 14 are fixedly connected to the top and the bottom of a connecting plate 7, one side of the sliding block 14 away from the connecting plate 7 extends to the inner cavity of the sliding groove 13, the sliding grooves 13 are in sliding connection with the sliding blocks 14, a damper 6, one side of the connecting plate 7 is fixedly connected with a connecting column 8, one side of the connecting column 8, which is far away from the connecting plate 7, extends to the outside of the sleeve 5, one side of the connecting column 8, which is positioned at the outside of the sleeve 5, is fixedly connected with a protection plate 9, the inner cavity of the sleeve 5 and the surface of the damper 6 are sleeved with a first spring 10, one side of the first spring 10 is fixedly connected with the connecting plate 7, one side of the bottom of the fixing frame 2 is fixedly connected with a supporting column 11, the bottom of the supporting column 11 is sleeved with a falling frame 12, the top of the falling frame 12 is provided with a groove 15, the bottom of the inner cavity of the groove 15 is fixedly connected with a second spring 16, the bottom of the supporting column 11 is fixedly connected with a backing plate 17, the top of the backing plate 17 is fixedly connected with the top of the second spring 16, the bottom of the opposite side, when the unmanned aerial vehicle is impacted, the stress is uniform, the stability of equipment is ensured, the capacity of buffer protection of the exploration unmanned aerial vehicle during landing can be improved by arranging the groove 15, the second spring 16 and the base plate 17, the safety of the equipment is enhanced, the landing frame 12 can be connected by arranging the connecting frame 18, the stability of equipment connection is ensured, the exploration purpose can be realized by arranging the monitor 19, the problem that the safety is reduced due to lack of protection of wings in the using process of the traditional exploration unmanned aerial vehicle can be effectively solved by matching the unmanned aerial vehicle body 1, the fixing frame 2, the mounting seat 3, the helical blades 4, the sleeve 5, the damper 6, the connecting plate 7, the connecting column 8, the guard plate 9, the first spring 10, the strut 11 and the landing frame 12, the unmanned aerial vehicle can effectively protect the wing part, so that the safety of the unmanned aerial vehicle is effectively improved, the damage phenomenon caused by impact is avoided.

During the use, unmanned aerial vehicle organism 1 is when receiving the impact, the shape of guard plate 9 can effectually surround helical blade 4, avoid helical blade 4 to receive the damage, guard plate 9 receives the impact back, under the effect of 5 inside dampers of sleeve pipe 6 and first spring 10, realize buffering and the purpose of resisting the impact, very big protection helical blade 4, the stability of flight has been guaranteed, when descending, the landing frame 12 contacts ground and contracts, the effectual effect that plays the buffering of the inside second spring 16 of landing frame 12, reduce the impact that unmanned aerial vehicle organism 1 received, thereby protection unmanned aerial vehicle organism 1.

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 of protecting against shock, includes unmanned aerial vehicle organism (1), its characterized in that: the unmanned aerial vehicle comprises an unmanned aerial vehicle body (1), wherein fixing frames (2) are fixedly connected to two sides of the unmanned aerial vehicle body (1), one side of each fixing frame (2), which is far away from the unmanned aerial vehicle body (1), is fixedly connected with a mounting seat (3), the top of each mounting seat (3) is provided with a helical blade (4), one side of each mounting seat (3), which is far away from the corresponding fixing frame (2), is fixedly connected with a sleeve (5), one side of each inner cavity of each sleeve (5) is fixedly connected with a damper (6), one side of each damper (6), which is far away from the inner wall of each sleeve (5), is fixedly connected with a connecting plate (7), one side of each connecting plate (7) is fixedly connected with a connecting column (8), one side of each connecting column (8), which is far away from each connecting plate (7), extends to the outer part of each sleeve (5), one side of each connecting column (8), which is located on, one side and connecting plate (7) fixed connection of first spring (10), one side fixedly connected with pillar (11) of mount (2) bottom, the bottom cover of pillar (11) is equipped with and falls frame (12).

2. An impact-resistant exploration drone according to claim 1, characterized in that: spout (13) have all been seted up to the top and the bottom of sleeve pipe (5) inner chamber, the top and the equal fixedly connected with slider (14) in bottom of connecting plate (7), one side that connecting plate (7) were kept away from in slider (14) extends to the inner chamber of spout (13), be sliding connection between spout (13) and slider (14).

3. An impact-resistant exploration drone according to claim 1, characterized in that: the top of the falling frame (12) is provided with a groove (15), the bottom of an inner cavity of the groove (15) is fixedly connected with a second spring (16), the bottom of the strut (11) is fixedly connected with a backing plate (17), and the top of the backing plate (17) is fixedly connected with the top of the second spring (16).

4. An impact-resistant exploration drone according to claim 1, characterized in that: the bottom of one side opposite to the falling frame (12) is fixedly connected with a connecting frame (18), and the connecting frame (18) is of an arc-shaped structure.

5. An impact-resistant exploration drone according to claim 1, characterized in that: the bottom fixedly connected with watch-dog (19) of unmanned aerial vehicle organism (1), the both ends of guard plate (9) are for turning over a structure.