Protective overclothes for unmanned aerial vehicle

Abstract

The utility model provides an unmanned aerial vehicle protection overclothes which comprises a plurality of fuselage overclothes parts connected in sequence, first connecting parts are arranged on the two sides of each fuselage overclothes part respectively, the fuselage overclothes parts are connected into a barrel shape or a cone shape through the first connecting parts, and a second connecting part is arranged at one end of each fuselage overclothes part; waterproof pressing stubbles and connecting pressing stubbles are arranged on the edges of every two adjacent machine body overclothes parts correspondingly, the second connecting parts are connected with the connecting pressing stubbles, and the waterproof pressing stubbles can be overlapped on gaps of the connecting positions; each wing cover part is in a cylinder shape with one closed end, and the open end of each wing cover part can be connected with one fuselage cover part. According to the utility model, the overclothes of the unmanned aerial vehicle are designed in sections, so that the overclothes can be better attached to the unmanned aerial vehicle on the basis of convenient cutting and processing, and the unmanned aerial vehicle can be conveniently sleeved with the overclothes; through two-layer connection of all the fuselage overclothes parts, water can be prevented while connection is achieved, and the situation that rainwater or muddy water splashed in the running process enters the overclothes along gaps of the overclothes, and consequently the unmanned aerial vehicle is affected is avoided.

Description

TECHNICAL FIELD

[0001] The utility model belongs to the unmanned plane protective cover field especially, it relates to an unmanned plane protective cover clothing. BACKGROUND

[0002] With the rapid development of electronic communication and machinery fields, the application of unmanned plane in various fields is gradually widespread, in the unmanned plane transportation process, in order to see unmanned plane structure directly by the way of people, also in order to protect unmanned plane, prevent the stone rainwater that can splash in the transportation process causes harm to unmanned plane, need to utilize protective cover clothing to wrap unmanned plane.

[0003] The existing protective cover clothing cannot avoid the position of the landing gear when facing the unmanned plane with the landing gear, and is not convenient to wrap outside the unmanned plane. UTILITY MODEL CONTENT

[0004] Therefore, the utility model aims at providing an unmanned plane protective cover clothing to protect the unmanned plane in the transportation process.

[0005] To achieve the above purpose, the technical scheme of the utility model is as follows:

[0006] An unmanned plane protective cover clothing comprises

[0007] A plurality of fuselage clothing parts connected in sequence, the two sides of each fuselage clothing part are respectively provided with a first connecting part, each fuselage clothing part can be connected into a cylindrical shape or a conical shape through the first connecting part, and one end of the fuselage clothing part is provided with a second connecting part;

[0008] The edges of each adjacent two fuselage clothing parts are respectively provided with a waterproof ridge and a connecting ridge, the second connecting part is connected with the connecting ridge, and the waterproof ridge can overlap the gap between the connecting ridge and the second connecting part;

[0009] Two wing clothing parts in a cylindrical shape, one end of the wing clothing part is closed, the other end is open, and the open end can be connected with one of the fuselage clothing parts.

[0010] Further, the two side corners of one of the fuselage clothing parts are respectively provided with avoiding notches, and when the fuselage clothing part is bent into a cylindrical shape or a conical shape, the landing gear of the unmanned plane can pass through the avoiding notches.

[0011] Further, the two sides of one of the fuselage clothing parts are respectively provided with connecting notches, and the open end of the wing clothing part is connected with the edges of the connecting notches.

[0012] Further, the width of the connecting ridge and the width of the rainproof ridge are greater than 11CM.

[0013] Further, the fuselage cover part and the wing cover part sequentially comprise an anti-static layer, an anti-collision layer, a fireproof layer and a waterproof layer from the direction away from the unmanned aerial vehicle.

[0014] Further, the edge of the waterproof layer is provided with a hemmed outer edge, which is outside the anti-static layer, the anti-collision layer and the fireproof layer, and the hemmed outer edge can be folded inward so that the edges of the anti-static layer, the anti-collision layer and the fireproof layer are wrapped in the hemmed outer edge.

[0015] Further, the anti-static layer is two layers of shumei silk.

[0016] Further, the first connecting part of the fuselage cover part is sewn with a strap and / or a magic tape.

[0017] Further, the second connecting part of the fuselage cover and the connecting press are connected by a magic tape.

[0018] Compared with the prior art, the protective cover of the unmanned aerial vehicle has the following advantages:

[0019] The unmanned aerial vehicle cover is designed in sections, which is convenient for cutting and processing, and makes each cover more fit the unmanned aerial vehicle and more convenient to put on the unmanned aerial vehicle; two layers of press are arranged at the splicing part of each fuselage cover part, so that the waterproof effect is achieved at the connecting part, and rainwater or mud splashed during driving is prevented from entering the cover interior through the gap of the cover and affecting the unmanned aerial vehicle.

[0020] An anti-static layer is arranged in the protective cover to avoid static electricity generated by the mutual friction between the cover and the unmanned aerial vehicle during transportation, and to avoid damage to the unmanned aerial vehicle caused by static electricity. BRIEF DESCRIPTION OF DRAWINGS

[0021] The drawings constituting a part of the present application are used to provide a further understanding of the present application, and the illustrative embodiments of the present application and the description thereof are used to explain the present application, and do not constitute an improper limitation on the present application. In the drawings:

[0022] Figure 1 It is a whole structure schematic view of the unmanned aerial vehicle cover;

[0023] Figure 2 It is a schematic view of the cooperation between the second connecting part and each press.

[0024] Explanation of reference signs:

[0025] 1-Fuselage cover; 11-First connecting part; 12-Second connecting part; 13-Avoidance notch; 1a-Nose cover; 1b-Fuselage cover; 1c-Wing connecting part; 1c1-Main body; 1c2-Slit assembly band; 1d-Tail cover; 2-Wing cover; 31-Waterproof layer; 311-Connecting joint; 312-Waterproof joint; 32-Fireproof layer; 33-Impact layer; 34-Antistatic layer. Detailed Implementation

[0026] It should be noted that, unless otherwise specified, the embodiments and features described in these embodiments can be combined with each other.

[0027] In the description of this utility model, it should be understood that the terms "center," "longitudinal," "lateral," "upper," "lower," "front," "rear," "left," "right," "vertical," "horizontal," "top," "bottom," "inner," and "outer," etc., indicating orientation or positional relationships based on the orientation or positional relationships shown in the accompanying drawings, are only for the convenience of describing this utility model and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, or be constructed and operated in a specific orientation, and therefore should not be construed as a limitation of this utility model. Furthermore, the terms "first," "second," etc., are used for descriptive purposes only and should not be construed as indicating or implying relative importance or implicitly specifying the number of indicated technical features. Thus, features defined with "first," "second," etc., may explicitly or implicitly include one or more of that feature. In the description of this utility model, unless otherwise stated, "a plurality of" means two or more.

[0028] In the description of this utility model, it should be noted that, unless otherwise explicitly specified and limited, the terms "installation," "connection," and "joining" should be interpreted broadly. For example, they can refer to a fixed connection, a detachable connection, or an integral connection; they can refer to a mechanical connection or an electrical connection; they can refer to a direct connection or an indirect connection through an intermediate medium; and they can refer to the internal connection of two components. Those skilled in the art can understand the specific meaning of the above terms in this utility model based on the specific circumstances.

[0029] The present invention will now be described in detail with reference to the accompanying drawings and embodiments.

[0030] The utility model discloses an unmanned plane protective cover clothes, including the multiple fuselage cover clothing department 1b1 and two wing cover clothing department 2 of connection in proper order, in this embodiment, the fuselage cover clothing department 1b1 is four, and it is machine nose cover clothing department 1a, fuselage cover clothing department 1b1, wing connecting portion 1c and tail cover clothing department 1d respectively, wing cover clothing department 2 is placed in wing connecting portion 1c both sides respectively. Every fuselage cover clothing department 1b1 and wing cover clothing department 2 are layer structure, and after being wrapped on unmanned plane, it includes antistatic layer 34, anti -impact layer 33, fire -retardant layer 32 and waterproof layer 31 in proper order along from inside to outside, in this embodiment, antistatic layer 34 is made into by two layers of shumei silk interlaced, anti -impact layer 33 is elastic felt layer, fire -retardant layer 32 is made into by aluminium foil foam insulation cotton, and it plays the effect of anti -collision while preventing fire, waterproof layer 31 is made into by tarpaulin or waterproof cloth. In this embodiment, waterproof cloth edge is equipped with edge overlock, and after antistatic layer 34, anti -impact layer 33, fire -retardant layer 32 and waterproof layer 31 interlaced, the edge overlock of waterproof layer 31 is outside other three layers, and the edge overlock can be folded inwards, and the edge of other three layers is wrapped inwards through the edge overlock, and is connected as a whole through sewing, and the needle hole of sewing is in proper order through the edge overlock, antistatic layer 34, anti -impact layer 33 and fire -retardant layer 32, avoids forming needle hole on waterproof layer 31, prevents the needle hole from causing water leakage.

[0031] The double -deck structure of two -layer edge overlock can be bonded together through hot -pressing after folding. In the process of bonding, the two ends of each fuselage cover clothing department 1b1 are bonded to be stepped, more specifically, the stepped surface of one end is close to the side of antistatic layer 34 as connecting pressure stub 311, and the stepped surface of the other end is close to the side of waterproof layer 31 as waterproof pressure stub 312. The end of the fuselage cover clothing department 1b1 is provided with a second connecting portion 12, specifically, the second connecting portion 12 is sewn with a magic tape face, and the needle face of the magic tape is sewn on the side of the waterproof layer 31 facing the connecting pressure stub 311, more specifically, the face is sewn on the antistatic layer 34. For the adjacent connecting pressure stub 311 and the second connecting portion 12 connected by the magic tape, the waterproof pressure stub covers between the connecting pressure stub 311 and the second connecting portion 12 to prevent rainwater from entering the cover inside from the gap between the two fuselage cover clothing department 1b1, which affects the unmanned plane. In order to ensure the reliability of the connection, the width of the connecting pressure stub 311 is greater than 11CM, and in order to play the effect of waterproof, the width of the waterproof pressure stub 312 is greater than 11CM.

[0032] Each fuselage cover clothing part 1b1 is a piece of approximately rectangular or triangular shape, and a first connecting part 11 is arranged on each side of the piece, and the two sides of the same piece can be connected through the first connecting parts 11 on the two sides to form a cylinder or a cone, so that each fuselage cover clothing part 1b1 is wrapped outside the unmanned aerial vehicle. The connecting mode of the first connecting part 11 can be realized through magic tape and / or a binding belt. During the process of installing the protective cover clothing on the unmanned aerial vehicle, the fuselage cover clothing part 1b1 at the lower part of the fuselage can be first covered on the unmanned aerial vehicle, and then the fuselage cover clothing parts 1b1 at the two ends are sequentially connected based on this, and in this process, the first connecting part 11 of the fuselage cover clothing part 1b1 to be installed is first connected with the connecting stub 311 of the installed fuselage cover clothing part 1b1, and then the first connecting parts 11 of the fuselage cover clothing parts 1b1 to be installed are connected with each other, so that the installation of the fuselage cover clothing parts 1b1 to be installed is completed.

[0033] Two wing cover clothing parts 2 are respectively in a cylindrical shape, one end of the wing cover clothing part 2 is closed, the other end is open, and the open end can be connected with one of the fuselage cover clothing parts 1b1. Specifically, the fuselage cover clothing part 1b1 includes a main body part 1c1 and a cutout forming belt 1c2, one end of the cutout forming belt 1c2 is connected with the main body part 1c1 to form a whole, and the other end can be connected with the main body part 1c1 through a binding belt and / or magic tape, so that a cutout is formed between the cutout forming belt 1c2 and the edge of the main body part 1c1, and the wing of the unmanned aerial vehicle can be placed in the cutout. The fuselage cover clothing part 1b1 can be inserted into the cutout after wrapping the wing, and connected through magic tape. The specific connection mode can be the same as the connection mode between the fuselage cover clothing parts 1b1.

[0034] The two side corners of one of the fuselage cover clothing parts 1b1 are respectively provided with an avoiding gap 13, and when the fuselage cover clothing part 1b1 is bent to form a cylinder or a cone, the landing gear of the unmanned aerial vehicle can pass through the avoiding gap 13.

[0035] The above only describes the preferred embodiments of the present application, and is not intended to limit the present application, and any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present application shall be included in the protection scope of the present application.

Claims

1. A drone shield jacket, characterized by: Comprise A plurality of fuselage cover parts connected in sequence, each of the fuselage cover parts is provided with a first connecting part on both sides, each of the fuselage cover parts can be connected into a cylindrical shape or a conical shape through the first connecting part, and one end of each of the fuselage cover parts is provided with a second connecting part; An edge of each of the adjacent two fuselage cover parts is provided with a waterproof ridge and a connecting ridge, the second connecting part is connected with the connecting ridge, and the waterproof ridge can overlap the gap between the connecting ridge and the second connecting part; Two wing cover parts in a cylindrical shape, one end of each of the wing cover parts is closed, the other end is open, and the open end can be connected with one of the fuselage cover parts.

2. The protective coverall for drones of claim 1, wherein: Both sides of one of the fuselage cover parts are respectively provided with an avoiding gap, and when the fuselage cover part is bent into a cylindrical shape or a conical shape, the landing gear of the unmanned aerial vehicle can pass through the avoiding gap.

3. The protective coverall for drones of claim 1, wherein: Both sides of one of the fuselage cover parts are respectively provided with an avoiding gap, and when the fuselage cover part is bent into a cylindrical shape or a conical shape, the landing gear of the unmanned aerial vehicle can pass through the avoiding gap.

4. The protective coverall for drones of claim 1, wherein: The open end of the wing cover part is connected with the edge of the connecting cutout.

5. The protective coverall for drones of claim 1, wherein: The width of the connecting ridge and the width of the waterproof ridge are greater than 11 cm.

6. A protective coverall for a drone according to claim 5, wherein: The fuselage cover part and the wing cover part sequentially comprise an antistatic layer, an anti-impact layer, a fireproof layer and a waterproof layer away from the unmanned aerial vehicle.

7. The protective coverall for drones of claim 5, wherein: The edge of the waterproof layer is provided with a wrapped outer edge, the wrapped outer edge protrudes out of the antistatic layer, the anti-impact layer and the fireproof layer, and the wrapped outer edge can be folded inward so that the edges of the antistatic layer, the anti-impact layer and the fireproof layer are wrapped in the wrapped outer edge.

8. The protective coverall for drones of claim 1, wherein: The antistatic layer is two layers of shumei silk.

9. The protective coverall for drones of claim 1, wherein: The first connecting part of the fuselage cover part is sewn with a strap and / or a magic tape. The second connecting part of the fuselage cover part and the connecting ridge are connected through the magic tape.

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