CN213524245U

CN213524245U - Unmanned aerial vehicle knapsack

Info

Publication number: CN213524245U
Application number: CN202021485835.8U
Authority: CN
Inventors: 杨思强
Original assignee: Nanjing Dassault Aviation Technology Co Ltd
Current assignee: Nantong Guoyi Aviation Technology Co.,Ltd.
Priority date: 2020-07-24
Filing date: 2020-07-24
Publication date: 2021-06-25
Anticipated expiration: 2030-07-24

Abstract

The utility model discloses an unmanned aerial vehicle knapsack belongs to unmanned air vehicle technical field. Including the inclusion, fixed connection is shouldered at the inclusion back, swing joint is in lid on the inclusion, the inclusion divide into skin and inlayer, the inlayer is inside to be equipped with four and to accomodate the chamber, fixed connection be in accomodate chamber one of the inside upper end of inlayer, fixed connection be in accomodate chamber two of the inside lower extreme of inlayer, fixed connection be in accomodate chamber three of the inside left end of inlayer, fixed connection be in accomodate chamber four of the inside right-hand member of inlayer, accomodate chamber three, accomodate chamber four with accomodate chamber two the same structure, accomodate chamber one, accomodate chamber two, accomodate chamber three, accomodate chamber four subsection with inboard UNICOM and with the skin forms hollow seal's inflation layer, fixed connection be in outer inflation inlet on the skin. The utility model discloses simple structure utilizes and aerifys aerifing the layer, lets form a plurality of cavitys in the inlayer and places each spare part of unmanned aerial vehicle, convenient to use.

Description

Unmanned aerial vehicle knapsack

Technical Field

The utility model relates to an unmanned air vehicle technique field specifically is an unmanned aerial vehicle knapsack.

Background

Unmanned aerial vehicle comes more and more in daily life, utilizes unmanned aerial vehicle to take photo by plane, plays the auto heterodyne and has been accepted by masses, and is great because of the unmanned aerial vehicle size, and the part is numerous moreover, in order to prevent to receive external force damage carrying the in-process, adopts materials such as foam to separate the part usually, has nevertheless used a large amount of spaces temporarily, has still increased weight moreover, is not convenient for the open air and carries.

SUMMERY OF THE UTILITY MODEL

The utility model discloses an it is not enough to exist among the prior art, has provided an unmanned aerial vehicle knapsack, is used for placing the unmanned aerial vehicle part through being equipped with a plurality of support airbags inside the inclusion, the utility model discloses simple structure, convenient to use to solve the problem that proposes among the above-mentioned background art.

In order to achieve the above object, the utility model provides a following technical scheme: an unmanned aerial vehicle backpack, wherein a shoulder strap is fixedly connected to the back surface of the backpack body, a cover body is movably connected to the backpack body, the backpack body is divided into an outer layer and an inner layer, four containing cavities are arranged outside the inner layer, the upper end of the inner layer is fixedly connected with a first containing cavity, the lower end of the inner layer is fixedly connected with a second containing cavity, the left end of the inner layer is fixedly connected with a third containing cavity, the right end of the inner layer is fixedly connected with a fourth containing cavity, the second containing cavity comprises a first supporting air bag, a second supporting air bag and a third supporting air bag, the second supporting air bag is vertically arranged in the center of the second containing cavity, one side of the second supporting air bag is provided with a second supporting air bag, the first supporting air bag and the second supporting air bag form an included angle of 30 degrees, the other side of the second supporting air bag is provided with a third supporting air, the storage cavity I, the storage cavity II, the storage cavity III and the storage cavity IV are communicated with the inner layer and form a hollow sealed inflation layer with the outer layer, and the outer layer is fixedly connected with an inflation inlet.

Preferably, the bag further comprises a first fixing rod fixedly connected with the lower end of the cover body, a second fixing rod is fixedly connected to the bag body, the first fixing rod is movably connected with the second fixing rod, and the cover body and the bag body are movably matched with the second fixing rod through the first fixing rod.

Preferably, the cover body and the outer layer are made of CURV materials.

Preferably, the inner layer and the containing cavity are made of PVC materials.

Preferably, the bag further comprises a fixing buckle fixedly connected to the center of the upper end of the bag body, and the bag body fixedly connects the cover body through the fixing buckle, so that the inner layer forms a closed space.

Preferably, the lifting handle is fixedly connected to the center of the upper end of the outer layer.

Has the advantages that: aerify the inflatable layer through the inflation inlet on the skin, make four of inclusion inlayer accomodate the chamber and aerify and swell, the unmanned aerial vehicle part is placed and is being accomodate the intracavity, need not to carry out the separation through materials such as foam between to the part, prevents that the inclusion from giving off the collision between the part under receiving external force's impact, through carrying out the mode of aerifing to the inflatable layer, the weight of the inclusion of reduction that can be great, portable outdoors.

Drawings

Fig. 1 is a schematic view of the overall structure of the present invention;

fig. 2 is a schematic view of the internal structure of the present invention.

In the figure: the bag comprises a bag body 1, shoulder straps 2, a cover body 3, a first fixing rod 4, a second fixing rod 5, an outer layer 6, an inner layer 7, an inflation inlet 8, a first storage cavity 9, a second storage cavity 10, a third storage cavity 11, a fourth storage cavity 12, a fifth storage cavity 13, an inflation layer 14, a fixing buckle 15, a first supporting air bag 101, a second supporting air bag 102 and a third supporting air bag 103.

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.

Referring to fig. 1 to fig. 2, the present invention provides a technical solution: an unmanned aerial vehicle knapsack comprises a knapsack body 1, a shoulder strap 2 fixedly connected to the back of the knapsack body 1, a cover body 3 movably connected to the knapsack body 1, a first fixing rod 4 fixedly connected to the lower end of the cover body 3, a second fixing rod 5 fixedly connected to the knapsack body 1, the first fixing rod 4 movably connected to the second fixing rod, the cover body 3 and the knapsack body 1 are movably matched with the second fixing rod 5 through the first fixing rod 4 to ensure that the cover body 3 and the knapsack body 1 are opened at a fixed angle, the cover body 3 and the outer layer 6 are made of a CURV material, the knapsack further comprises a handle fixedly connected to the center of the upper end of the outer layer 6, the knapsack body 1 is divided into an outer layer 6 and an inner layer 7, four containing cavities are arranged inside the inner layer 7, the first containing cavity 9 is fixedly connected to the inside of the inner layer 7, and the second containing cavity 10 is fixedly connected to the, a third receiving cavity 11 fixedly connected to the left end inside the inner layer 7, a fourth receiving cavity 12 fixedly connected to the right end inside the inner layer 7, a fifth receiving cavity 13 formed among the first receiving cavity 9, the second receiving cavity 10, the third receiving cavity 11 and the fourth receiving cavity 12, the fifth receiving cavity 13 being of a type, the second receiving cavity 10 including a first supporting airbag 101, a second supporting airbag 102 and a third supporting airbag 103, the second supporting airbag 102 being vertically arranged in the center of the second receiving cavity, the second supporting airbag 102 being arranged on the side of the first supporting airbag 101, the first supporting airbag 101 forming an included angle of 30 degrees with the second supporting airbag 102, the third supporting airbag 103 being arranged on the other side of the second supporting airbag 102 and mirroring the first supporting airbag 101, the third receiving cavity 11, the fourth receiving cavity 12 and the second receiving cavity 10 being structurally identical, the first receiving cavity 9, the second receiving cavity 10, the third receiving cavity 11, the fourth receiving cavity 12 being communicated with the inner layer 7 and forming a hollow and sealed inflatable layer 14 with the outer layer 6, inner 7 with the institute accomodate chamber 9, accomodate two 10 in the chamber, accomodate three 11 in the chamber, accomodate four 12 in the chamber and all adopt the PVC material, fixed connection is in inflation inlet 8 on outer 6 is through aerifing inflation inlet 8, makes four accomodate the chamber and aerify and swell, makes inner 7 with accomodate chamber 9, accomodate two 10 in the chamber, accomodate three 11 in the chamber, accomodate and form the elasticity separation between four 12 in the chamber, accomodate five 13 in the chamber, each spare part of unmanned aerial vehicle forms the elasticity separation, prevents that each spare part of unmanned aerial vehicle from taking place the striking and being damaged under the external force striking, still includes fixed connection the fixed buckle 15 of 1 upper end central point of inclusion, inclusion 1 passes through fixed buckle 15 will lid 3 fixed connection makes inner 7 form the enclosure space.

Based on above-mentioned structure and relation of connection, the utility model discloses a theory of operation as follows:

when each spare part of unmanned aerial vehicle is packed into in the unmanned aerial vehicle knapsack as required, aerify the knapsack through inflation inlet 8, be that the inside chamber of accomodating of inlayer 7 9, accomodate chamber two 10, accomodate chamber three 11, accomodate chamber four 12 and swell and form the elastic separation, put into support airbag with each spare part of unmanned aerial vehicle, cover lid 3 back and fix lid 3 and inclusion 1 through fixed buckle 15.

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 unmanned aerial vehicle knapsack, its characterized in that, includes the inclusion, fixedly connected with baldric on the inclusion back, swing joint has the lid on the inclusion, the inclusion divide into skin and inlayer, the inlayer outside is equipped with four and accomodates the chamber, chamber one is accomodate to inlayer inside upper end fixed connection, chamber two is accomodate to inlayer inside lower extreme fixed connection, chamber three is accomodate to inlayer inside left end fixed connection, chamber four is accomodate to inlayer inside right-hand member fixed connection, accomodate chamber two including support gasbag one, support gasbag two and support gasbag three, support gasbag two sets up perpendicularly in accomodate chamber two central authorities, support gasbag one side is equipped with support gasbag two, support gasbag one with support gasbag two become 30 contained angles, support gasbag two opposite sides are equipped with the support gasbag three with support gasbag one mirror image, accomodate chamber three, The storage cavity IV is structurally the same as the storage cavity II, the storage cavity I, the storage cavity II, the storage cavity III and the storage cavity IV are communicated with the inner layer and form a hollow sealed inflation layer with the outer layer, and the outer layer is fixedly connected with an inflation inlet.

2. The drone backpack of claim 1, wherein: the bag body is fixedly connected with a first fixing rod, the first fixing rod is movably connected with the second fixing rod, and the cover body and the bag body are movably matched with the second fixing rod through the first fixing rod.

3. The drone backpack of claim 1, wherein: the cover body and the outer layer are made of CURV materials.

4. The drone backpack of claim 1, wherein: the inner layer and the containing cavity are made of PVC materials.

5. The drone backpack of claim 1, wherein: the bag body is fixedly connected with the cover body through the fixing buckle, so that the inner layer forms a closed space.

6. The drone backpack of claim 1, wherein: the lifting handle is fixedly connected to the center of the upper end of the outer layer.