CN211208783U

CN211208783U - Unmanned aerial vehicle supply socket sets up structure with waterproof dustproof effect

Info

Publication number: CN211208783U
Application number: CN201922477984.3U
Authority: CN
Inventors: 杨建�
Original assignee: Shenzhou Tenglong Technology Shenzhen Co ltd
Current assignee: Shenzhou Tenglong Technology Shenzhen Co ltd
Priority date: 2019-12-31
Filing date: 2019-12-31
Publication date: 2020-08-07
Anticipated expiration: 2029-12-31

Abstract

The utility model discloses an unmanned aerial vehicle supply socket setting structure with waterproof and dustproof effects, which comprises a shell on the unmanned aerial vehicle body and a socket, wherein the shell is provided with a hole groove for inserting the socket, the hole groove is communicated with the inside and the outside of the unmanned aerial vehicle, the socket extends into and is arranged in the hole groove, and the outer end of the socket is downwards inclined relative to the shell; the upper surface of the shell forms a slope surface which inclines towards the outer end of the socket. The utility model discloses a reset and expose supply socket's setting structure, specifically stretch into the inside of unmanned aerial vehicle casing with supply socket through the hole groove of shape adaptation to utilize protruding muscle and groove structure to stabilize, the slope sets up supply socket simultaneously, and the corresponding casing of cooperation unmanned aerial vehicle forms domaticly, so that unmanned aerial vehicle fly with receive wash in-process dust and liquid can not enter into unmanned aerial vehicle inside, and then avoided because dust and liquid get into the safety problem that causes.

Description

Unmanned aerial vehicle supply socket sets up structure with waterproof dustproof effect

Technical Field

The utility model relates to an unmanned air vehicle technique field, in particular to unmanned aerial vehicle supply socket sets up structure with waterproof dustproof effect.

Background

Unmanned aerial vehicle products, as a new thing, have been used to develop boxing feet in the practical application fields such as farm pesticide spraying, geographic mapping and aerial photography, and as for the application in other more fields, urgent needs to be tried and explored. Also, since the unmanned aerial vehicle is an emerging product, there are many defects in the design of the relevant parts of the product, which causes troubles and obstacles in practical application.

From the actual conditions that unmanned aerial vehicle connects the electricity, need set up supply socket in unmanned aerial vehicle's fuselage relevant position to be used for the grafting of cable conductor. From the needs of in-service use, supply socket often need set up the outside at the unmanned aerial vehicle fuselage, for exposing the socket, and will satisfy inside the unmanned aerial vehicle power cord inserts the unmanned aerial vehicle fuselage, consequently will produce gap and hole etc. in relevant position, current unmanned aerial vehicle supply socket sets up the mechanism reasonable inadequately, the design is coarse, structure including unmanned aerial vehicle socket self is perfect inadequately yet, consequently, just cause fly and wash overshoot at unmanned aerial vehicle (produce relative movement), dust and liquid enter into unmanned aerial vehicle's inside through above-mentioned gap and hole etc., cause the influence to unmanned aerial vehicle's safety.

SUMMERY OF THE UTILITY MODEL

In view of above-mentioned current unmanned aerial vehicle exposes supply socket structure and design defect, cause dust and liquid to enter into unmanned aerial vehicle inside and cause the problem of influence to unmanned aerial vehicle safety, the utility model provides an unmanned aerial vehicle supply socket with waterproof dustproof effect sets up the structure, through the structure that sets up of resetting supply socket and unmanned aerial vehicle casing, stretch into inside unmanned aerial vehicle with supply socket, and utilize protruding muscle and groove structure's cooperation to make supply socket fasten to unmanned aerial vehicle casing inside, and prolong supply socket in the inside part of unmanned aerial vehicle, the slope setting that utilizes the domatic structure of casing and supply socket simultaneously is in order to realize that dust and liquid can not just enter into unmanned aerial vehicle's inside, and then avoided because dust and liquid get into the unmanned aerial vehicle safety problem that causes.

The technical scheme of the utility model as follows: an unmanned aerial vehicle power socket setting structure with waterproof and dustproof effects comprises a shell on an unmanned aerial vehicle body and a socket, wherein the shell is provided with a hole groove used for inserting the socket, the hole groove is communicated with the inside and the outside of the unmanned aerial vehicle, the socket extends into and is arranged in the hole groove, the shape of the hole groove is matched with that of the socket, the hole groove is tightly matched with the socket, convex ribs used for clamping and limiting are arranged on the upper surface and the lower surface of the socket, a groove matched with the convex ribs is correspondingly arranged in the shell, and the convex ribs are clamped into the groove to realize limiting and clamping; the outer end of the socket is arranged obliquely downwards relative to the shell; the upper surface of the shell is provided with a slope surface which inclines towards the outer end of the socket.

Further, as preferred, the casing is unmanned aerial vehicle's tail lamp casing.

Preferably, the shell is provided with a group of grooves which are matched with the convex ribs on the upper surface of the socket in a clamping manner, a limiting plate is arranged below the socket, the left end and the right end of the limiting plate are connected to the shell through bolts, and the upper plate surface of the limiting plate is provided with a group of grooves which are matched with the convex ribs on the lower surface of the socket in a clamping manner.

Further, preferably, the plate surface of the stopper plate is curved to fit the shape of the lower portion of the socket.

Preferably, the socket has two ribs on the upper and lower surfaces thereof, and the two ribs on each surface are parallel to each other.

Further, preferably, the outer end of the socket is inclined horizontally downwards by 4-7 degrees.

Has the advantages that: the utility model discloses the design is novel, reasonable in design, and convenient to use, the utility model discloses a reset the structure that sets up of exposing supply socket, specifically stretch into the inside of unmanned aerial vehicle casing with supply socket through the hole groove of shape adaptation to utilize protruding muscle and groove structure to stabilize, the slope sets up supply socket simultaneously, and cooperate the corresponding casing of unmanned aerial vehicle to form domaticly, so that unmanned aerial vehicle fly with receive wash in-process dust and liquid can not enter into unmanned aerial vehicle inside, and then avoided because dust and liquid get into the safety problem that causes.

Drawings

Fig. 1 is a schematic view of an arrangement structure according to an embodiment of the present invention.

Fig. 2 is a schematic view of a structure of the rib on the housing according to an embodiment of the present invention.

Fig. 3 is a schematic view of a setting structure of the limiting plate on the housing according to an embodiment of the present invention.

Fig. 4 is a schematic diagram of an inclined state of the socket according to an embodiment of the present invention.

Detailed Description

The invention will be further explained with reference to the following figures and examples:

referring to fig. 1 to 4, an unmanned aerial vehicle power socket setting structure with waterproof and dustproof effects comprises a shell 1 on an unmanned aerial vehicle body and further comprises a socket 2, wherein the shell 1 is provided with a hole groove for inserting the socket 2, the hole groove is communicated with the inside and the outside of an unmanned aerial vehicle, the socket 2 extends into and is arranged in the hole groove, the shape of the hole groove is matched with that of the socket 2, the hole groove is tightly matched with the socket 2, convex ribs 2a for clamping and limiting are arranged on the upper surface and the lower surface of the socket 2, correspondingly, a groove matched with the convex ribs 2a is arranged in the shell 1, and the convex ribs 2a are clamped into the groove to realize limiting and clamping; the outer end of the socket 2 is arranged obliquely downwards relative to the housing 1; the upper surface of the shell 1 forms a slope surface inclined towards the outer end of the socket 2.

The utility model discloses an among the basic scheme, casing 1 is the part on the fuselage, is not limited to the fuselage main part. Socket 2 is used for connecting the power cord, and casing 1 sets up socket 2 through setting up the hole groove to satisfy socket 2's setting, and the shape and the socket 2 adaptation in hole groove, and contact through the tight fit, with the waterproof and dustproof effect that realizes well. In addition, contact department utilizes protruding muscle 2a and groove structure's cooperation, realizes both in close contact with, prevents to shift, and then makes socket 2 set up more firmly, has avoided producing the gap because of rocking, just also further strengthens waterproof and dirt-proof effect. In addition, the socket 2 is arranged in an inclined mode, and the shell 1 forms an inclined slope surface to prevent liquid from flowing backwards and prevent dust. It should be noted that, the socket 2 is disposed such that one end close to the housing 1 is higher than the other end far from the housing 1, and is disposed in an inclined manner, and the direction of gravity is downward with respect to the housing 1 which is being placed vertically, so as to facilitate the flow of liquid and avoid backflow, and similarly, the slope of the housing 1 is also disposed in such an inclined manner.

In the specific implementation process, as a preferable scheme, the housing 1 is a tail lamp housing of the unmanned aerial vehicle. In the preferred embodiment, the socket 2 is arranged in the position of the tail light, and accordingly, the housing 1 is the tail light housing.

In a specific implementation process, as an optimal scheme, a group of grooves is arranged on the housing 1 and is in clamping fit with the convex ribs 2a on the upper surface of the socket 2, a limiting plate 3 is arranged below the socket 2, the left end and the right end of the limiting plate 3 are connected to the housing 1 through bolts, and a group of grooves is arranged on the upper plate surface of the limiting plate 3 and is in clamping fit with the convex ribs 2a on the lower surface of the socket 2. In this preferred scheme, a socket 2's concrete fixed structure that sets up is given, 2 one sides of socket and the contact of casing 1, and the another side is fixed through the fastening of limiting plate 3 to be provided with protruding muscle 2a and recess at corresponding contact surface and come the solid cooperation of card, in order to guarantee socket 2's fixed setting.

In a specific implementation process, as a preferable scheme, the plate surface of the limiting plate 3 is matched with the shape of the lower part of the socket 2 through bending. In the preferred scheme, the specific structural form of the limiting plate 3 is given. Limiting plate 3 will satisfy fixed socket 2 in the function, and the structure cooperation that also needs to pass through recess and protruding muscle 2a simultaneously avoids rocking of socket 2, is realized through limiting plate 3's bending on socket 2's is fixed.

In the specific implementation process, as a preferable scheme, two convex ribs 2a are respectively arranged on the upper surface and the lower surface of the socket 2, and the two convex ribs 2a on each surface are parallel to each other. Each side is better prevented from shaking by providing two ribs 2 a.

In the specific implementation process, as a preferable scheme, the outer end of the socket 2 is horizontally inclined downwards by 4-7 degrees. Because the power cord on the socket 2 is the level setting, can satisfy under this angle on the one hand that the setting of power cord is not influenced, on the other hand has also played the effect that prevents to flow backward.

The foregoing has described in detail preferred embodiments of the present invention. It should be understood that numerous modifications and variations can be devised by those skilled in the art in light of the teachings of the present invention without undue experimentation. Therefore, the technical solutions that can be obtained by a person skilled in the art through logic analysis, reasoning or limited experiments based on the prior art according to the concepts of the present invention should be within the scope of protection defined by the claims.

Claims

1. The utility model provides an unmanned aerial vehicle supply socket sets up structure with waterproof dustproof effect, includes casing (1) on the unmanned aerial vehicle fuselage, its characterized in that: the unmanned aerial vehicle is characterized by further comprising a socket (2), the shell (1) is provided with a hole groove used for inserting the socket (2), the hole groove is communicated with the inside and the outside of the unmanned aerial vehicle, the socket (2) extends into and is arranged in the hole groove, the shape of the hole groove is matched with that of the socket (2), the hole groove is tightly matched with the socket (2), convex ribs (2a) used for clamping and limiting are arranged on the upper surface and the lower surface of the socket (2), a groove matched with the convex ribs (2a) is correspondingly arranged in the shell (1), and the convex ribs (2a) are clamped into the groove to realize limiting and clamping; the outer end of the socket (2) is arranged obliquely downwards relative to the shell (1); the upper surface of the shell (1) forms a slope surface which inclines towards the outer end of the socket (2).

2. The unmanned aerial vehicle supply socket setting structure with waterproof dustproof effect of claim 1, characterized in that: casing (1) is unmanned aerial vehicle's tail lamp casing.

3. The unmanned aerial vehicle supply socket setting structure with waterproof dustproof effect of claim 2, characterized in that: the socket is characterized in that the shell (1) is provided with a group of grooves which are matched with the convex ribs (2a) on the upper surface of the socket (2) in a clamping manner, a limiting plate (3) which is positioned below the socket (2) is additionally arranged, the left end and the right end of the limiting plate (3) are connected onto the shell (1) through bolts, and the upper plate surface of the limiting plate (3) is provided with a group of grooves which are matched with the convex ribs (2a) on the lower surface of the socket (2) in a clamping manner.

4. The unmanned aerial vehicle supply socket setting structure with waterproof dustproof effect of claim 3, characterized in that: the plate surface of the limiting plate (3) is matched with the shape of the lower part of the socket (2) through bending.

5. The unmanned aerial vehicle supply socket setting structure with waterproof dustproof effect of claim 4, characterized in that: the upper surface and the lower surface of the socket (2) are respectively provided with two convex ribs (2a), and the two convex ribs (2a) on each surface are parallel to each other.

6. The unmanned aerial vehicle supply socket setting structure with waterproof dustproof effect of claim 5, characterized in that: the outer end of the socket (2) is horizontally inclined downwards by 4-7 degrees.