CN212829087U - Unmanned aerial vehicle's year thing case - Google Patents
Unmanned aerial vehicle's year thing case Download PDFInfo
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- CN212829087U CN212829087U CN202021256543.7U CN202021256543U CN212829087U CN 212829087 U CN212829087 U CN 212829087U CN 202021256543 U CN202021256543 U CN 202021256543U CN 212829087 U CN212829087 U CN 212829087U
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- aerial vehicle
- unmanned aerial
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Abstract
The utility model discloses an unmanned aerial vehicle's year thing case, it includes: the box body comprises a body and a cover body, wherein the body is provided with an accommodating cavity with one open end, and the cover body is used for sealing the open end of the accommodating cavity; the locking assembly comprises a locking part and a locking part, and the locking part are arranged on the body and the cover body; and the control box is arranged on the top surface of the body and is electrically connected with at least one of the locking part and the locking part so as to control the locking part and the locking part to be locked or unlocked. The utility model discloses technical scheme makes unmanned aerial vehicle's the focus of carrying the thing case upwards squint, so can reduce the loss of unmanned aerial vehicle's kinetic energy, is favorable to improving the dispatch of unmanned aerial vehicle group delivery express delivery parcel and sends efficiency.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field, in particular to unmanned aerial vehicle carries thing case.
Background
An unmanned aerial vehicle is simply referred to as a drone (UAV), which is an unmanned aerial vehicle that is operated by a radio remote control device and self-contained program control means, or is autonomously operated by an onboard computer, either completely or intermittently. Unmanned aerial vehicle can divide into for military use unmanned aerial vehicle and civilian unmanned aerial vehicle according to its application, and civilian unmanned aerial vehicle has obtained extensive development in the trade field of difference, wherein can utilize civilian unmanned aerial vehicle to carry out the transportation of express delivery parcel usually. In the prior art, the purpose of transporting express packages is realized by spirally connecting one carrying box on the frame of the civil unmanned aerial vehicle.
But at the in-process that utilizes unmanned aerial vehicle transportation express delivery parcel, carry the thing case and pass through the screw fixation on unmanned aerial vehicle, because the quality of carrying the thing case is overweight, unmanned aerial vehicle need provide more kinetic energy and just can accomplish the dispatch task, leads to unmanned aerial vehicle to carry a large amount of kinetic energies of consumption when the thing operation.
SUMMERY OF THE UTILITY MODEL
The utility model aims at providing an unmanned aerial vehicle's year thing case aims at solving the too big problem of energy consumption when unmanned aerial vehicle sends the express delivery parcel.
In order to achieve the above object, the utility model provides an unmanned aerial vehicle carries thing case, it includes:
the box body comprises a body and a cover body, wherein the body is provided with an accommodating cavity with one open end, and the cover body is used for covering the open end of the accommodating cavity;
the locking assembly comprises a locking part and a locking part, and the locking part are arranged on the body and the cover body;
and the control box is arranged on the top surface of the body and is electrically connected with at least one of the locking part and the locking part so as to control the locking part and the locking part to be locked or unlocked. In an embodiment of the present invention, the control box is installed at a top center position of the body.
The utility model discloses an in the embodiment, the control box includes box body, PCB board and apron, the box body install in the top surface of body, it is back to the concave installation cavity that is equipped with in surface of body, the PCB board install in the installation cavity of box body, it with locking portion electricity is connected, the apron is used for the closing cap the installation cavity of box body.
In an embodiment of the present invention, the box body and the body are integrally formed.
In an embodiment of the present invention, one side of the cover body is pivotally connected to one side of the body;
the locking part comprises a locking shell, a power part and a locking column, the locking shell is arranged on one side of the body, which is pivoted with the cover body relative to the locking shell, the locking shell is concavely provided with a abdication opening, the power part is arranged on the locking shell, the locking column is in transmission connection with the power part, and the locking column can move along the directions in which two side walls, which are oppositely arranged, of the abdication opening are close to or far away from each other under the driving of the power part;
the locking part is arranged on one side of the cover body, which is pivoted with the shell, opposite to the cover body, the locking part comprises a fixing part fixedly connected with the cover body and a locking ring connected with the fixing part, and the locking ring can extend into or out of the abdicating opening.
In an embodiment of the present invention, the locking housing is provided with an accommodating cavity and a relief hole formed through a cavity wall of the accommodating cavity; one end of the locking column extends into the cavity, and a limiting bulge is convexly arranged on the outer peripheral wall of the locking column outside the cavity;
the power part comprises an electromagnet and a spring, the electromagnet is installed in the containing cavity and can magnetically adsorb the locking column, the spring is sleeved on the locking column, one end of the spring is abutted to the limiting protrusion, and the other end of the spring is abutted to the outer surface of the locking shell.
In an embodiment of the present invention, the body and the cover are made of flexible materials.
In an embodiment of the present invention, the outer surface of the body is provided with a protective layer, and the protective layer is made of a carbon fiber material.
In an embodiment of the present invention, the protective layer on the outer surface of the body is concavely provided with a plurality of positioning holes connected with the positioning mechanical arm.
The utility model discloses an in the embodiment, the body is the tetragonal body setting, all be provided with a plurality of locating holes that are the symmetry setting on the protective layer that the body is relative two surfaces that set up.
The utility model discloses technical scheme installs in the top of box through the control box with unmanned aerial vehicle's year thing case for unmanned aerial vehicle's the whole skew that upwards inclines of the focus of carrying the thing case, the utility model discloses an unmanned aerial vehicle carry the thing case and when current unmanned aerial vehicle's year thing case risees the same height, the utility model discloses an unmanned aerial vehicle carries the thing case because of its focus is higher than current unmanned aerial vehicle's the focus of carrying the thing case, just so can reduce the loss of unmanned aerial vehicle's kinetic energy, and then is favorable to improving the speed that unmanned aerial vehicle sent the parcel.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings needed to be used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to the structures shown in the drawings without creative efforts.
Fig. 1 is a cross-sectional view of an embodiment of a carrier box of the unmanned aerial vehicle of the present invention;
FIG. 2 is a cross-sectional view of an embodiment of the locking portion of FIG. 1;
FIG. 3 is a cross-sectional view of one embodiment of the locking portion of FIG. 1;
fig. 4 is the utility model discloses unmanned aerial vehicle's carries the structure schematic diagram of another embodiment of thing case.
The reference numbers illustrate:
| reference numerals | Name (R) | Reference numerals | Name (R) |
| 100 | Unmanned aerial vehicle's |
211 | Locking shell |
| 10 | |
212 | Power part |
| 20 | |
213 | |
| 30 | |
2111 | Abdication opening |
| 11 | |
221 | Fixing |
| 12 | |
222 | |
| 21 | |
2112 | Hole of stepping down |
| 22 | |
2131 | Spacing protrusion |
| 31 | Box body | 2121 | |
| 32 | PCB board | 2122 | |
| 33 | |
50 | |
| 40 | Hinge (C) | 51 | Locating hole |
The objects, features and advantages of the present invention will be further described with reference to the accompanying drawings.
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 efforts belong to the protection scope of the present invention.
It should be noted that all the directional indicators (such as upper, lower, left, right, front and rear … …) in the embodiment of the present invention are only used to explain the relative position relationship between the components, the motion situation, etc. in a specific posture (as shown in the drawings), and if the specific posture is changed, the directional indicator is changed accordingly.
In addition, the descriptions related to "first", "second", etc. in the present invention are for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicit ly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include at least one such feature. In addition, the technical solutions in the embodiments may be combined with each other, but it must be based on the realization of those skilled in the art, and when the technical solutions are contradictory or cannot be realized, the combination of the technical solutions should not be considered to exist, and is not within the protection scope of the present invention.
The utility model provides an unmanned aerial vehicle's year thing case, please refer to fig. 1, this unmanned aerial vehicle's year thing case 100 includes box 10, locking Assembly 20 and control box 30.
The box 10 is a carrier capable of accommodating objects, and includes a body 11 and a cover 12, the body 11 is provided with an accommodating cavity (not labeled) for accommodating objects, and the cover 12 is used for covering the accommodating cavity. It should be noted that the size of the cover 12 may be larger than or equal to the size of the open end of the accommodating cavity, so as to ensure that the open end of the accommodating cavity can be completely closed when the cover 12 covers the open end of the accommodating cavity, thereby preventing the object placed in the accommodating cavity from falling.
The locking assembly 20 is a device for locking the cover 12 to the body 11, the locking assembly 20 includes a locking portion 21 and a locking portion 22, the locking portion 21 and the locking portion 22 are respectively disposed on the body 11 and the cover 12, that is, the locking portion 21 is disposed on the body 11, the locking portion 22 is correspondingly disposed on the cover 12, or the locking portion 21 is disposed on the cover 12, and the locking portion 22 is correspondingly disposed on the body 11. The locking portion 21 and the locking portion 22 can be connected by magnetic attraction, the locking portion 21 and the locking portion 22 can also be connected by snap, and the locking portion 21 and the locking portion 22 can also be connected by other methods, which are not limited in this respect.
The control box 30 is mounted on the top surface of the body 11, the top surface of the body 11 is the surface of the body 11 that faces away from the ground or a load when the body 11 is placed on the ground or the load, and the connection modes of the control box 30 and the body 11 are various, and the control box can be connected and fixed through screw connection, snap connection and other connection modes.
The control box 30 is electrically connected to the locking assembly 20, that is, it is electrically connected to one or both of the locking portion 21 and the locking portion 22 in the locking assembly 20, and the electrically connecting manner includes a wired connection, that is, an electrical connection through a wire, and a wireless connection, that is, an electrical connection through a wireless bluetooth module. The control box 30 controls the locking part 21 to be locked or unlocked with the lock catch according to the control command.
The utility model discloses an unmanned aerial vehicle's year thing case 100 is through setting up in the 11 top surfaces of body of box 10 with control box 30, so that unmanned aerial vehicle's the whole skew that makes progress of the focus of carrying thing case 100, unmanned aerial vehicle's the focus of carrying thing case 100 shifts up, make unmanned aerial vehicle shift up at the holistic focus of flight in-process, the pulling force that has reduced the year thing case 100 that promotes unmanned aerial vehicle, the kinetic energy that needs has also been reduced simultaneously, just so can reduce the loss of unmanned aerial vehicle's kinetic energy, and then be favorable to improving the speed that unmanned aerial vehicle send the parcel. In addition, the kinetic energy required by the carrying case carried by the unmanned aerial vehicle is reduced, so that the service life of a battery of the unmanned aerial vehicle can be prolonged.
In an embodiment of the present invention, please refer to fig. 1, the control box 30 includes a box body 31, a PCB 32 and a cover plate 33, the box body 31 is installed on the top surface of the body 11, the surface of the box body opposite to the body 11 is concave and provided with an installation cavity, the PCB 32 is installed in the installation cavity of the box body 31 and electrically connected to the locking portion 21, and the cover plate 33 is used for sealing the installation cavity of the box body 31.
The connection between the box 31 and the body 11 can be various, and it can be fixed by screw connection, adhesion, snap connection and other connection methods. The box 31 may be formed by a single injection molded part, and the box 31 may also be formed by splicing a plurality of plate-shaped structures, which is not limited herein.
The connection mode of lid 12 and box body 31 has the multiple, and both can be connected fixedly through screw connection, buckle connection and other modes, and lid 12 and box body 31's fixed connection can be with the open end closing cap of installation cavity, so can avoid PCB board 32 to receive external factors's interference.
Further, this box body 31 and body 11 integrated into one piece set up, and box body 31 can be established by body 11 part protruding and form promptly, so set up, and the top surface of this body 11 can form the chamber bottom of the installation cavity of box body 31, is favorable to simplifying the structure of this box body 31. Meanwhile, the box body 31 and the body 11 can be formed by one-step injection molding, so that the production and the manufacture are convenient.
It is worth noting that this control box 30 can set up in the top surface central point of body 11 and put, also can set up in the border position of top surface, and preferably, this control box 30 sets up in the top surface central point of body 11 and puts, so sets up, has avoided the heavy light problem in one side of control box 30 to appear, and then the problem that influences unmanned aerial vehicle flight appears.
In an embodiment of the present invention, one side of the cover 12 is pivotally engaged with the body 11, and the other opposite side of the cover 12 is connected to the locking portion 22 through the locking portion 21.
The cover 12 and the body 11 can be pivoted in various ways, for example, the cover 12 and the body 11 are pivoted by a rotating shaft and a shaft sleeve, and if the cover 12 and the body 11 are pivoted by a hinge 40, the cover 12 and the body 11 can also be pivoted in other ways, which are not listed here.
Preferably, referring to fig. 4, the cover 12 and the body 11 are pivotally connected by a hinge 40, the hinge 40 can be connected to an inner surface of the body 11 (i.e. a wall of the receiving cavity) and a surface of the cover 12 facing the receiving cavity, and the hinge 40 can also be connected to an outer surface of the body 11 and a surface of the cover 12 facing away from the receiving cavity.
The number of hinges 40 may be one or more, and the number of hinges 40 is determined according to the size of the container 10. In the present application, please refer to fig. 1, the number of the hinges 40 is two, and the two hinges 40 are arranged at intervals along the length direction of the corresponding side of the cover 12. The size of the hinge 40 is determined by the size of the container 10, and the size of the hinge 40 may be 3 inches, i.e., 75 mm in length, 50 mm in width and 1.5 mm in thickness. The size of the hinge 40 may be 2 inches, or may be 1.5 inches, and the size of the hinge 40 is not particularly limited.
The locking part 21 and the locking part 22 may be connected and fixed by magnetic attraction, or connected and fixed by the locking column 213 and the locking ring 222, or connected and fixed by other methods, which are not limited herein.
Preferably, the locking portion 21 and the locking portion 22 are connected and fixed by the locking post 213 and the locking ring 222. Specifically, referring to fig. 1 to 3, the locking portion 21 includes a locking housing 211, a power member 212, and a locking post 213. An abdicating opening 2111 is concavely formed on a side of the locking housing 211 adjacent to the cover 12, the abdicating opening 2111 may be formed through the locking housing 211, and the abdicating opening 2111 may also be a groove structure. The power member 212 is mounted to a locking housing 211 which is drivingly connected to a locking post 213. The power member 212 can drive the locking posts 213 to move toward or away from each other along two opposite sidewalls of the abdicating opening 2111. The locking portion 22 includes a fixing portion 221 fixedly connected to the cover 12 and a locking ring 222 connected to the fixing portion 221, wherein the locking ring 222 can extend into the relief opening 2111 to cooperate with the locking post 213.
Further, the locking housing 211 is provided with a cavity and an abdicating hole 2112 formed through the cavity wall of the cavity; one end of the locking column 213 extends into the cavity, a limiting protrusion 2131 is convexly arranged on the outer peripheral wall of the locking column 213 outside the cavity, and the locking column 213 is made of a metal material which can be adsorbed by a magnet; the power element 212 includes an electromagnet 2121 and a spring 2122, the electromagnet 2121 is installed in the cavity and can magnetically attract the locking column 213, the spring 2122 is sleeved on the locking column 213, one end of the spring is abutted against the limiting protrusion 2131, and the other end of the spring is abutted against the outer surface of the locking housing 211.
The specific working principle in the locking process of the locking assembly 20 is as follows: when the cover 12 is fastened to the body 11, the locking part 22 fixed to the cover 12 is gradually close to the locking part 21 fixed to the edge of the body 11, the locking ring 222 is inserted into the abdicating opening 2111, the control box 30 cuts off the power supply of the electromagnet 2121, so that the locking column 213 is only under the action of the spring 2122, the spring 2122 recovers elastic deformation when the magnetic force of the locking column 213 is lost, so as to drive the locking column 213 to move along the direction in which the two opposite side walls of the abdicating opening 2111 approach or separate from each other, and the locking column 213 passes through the locking ring 222 during the movement, so that the locking ring 222 is connected with the locking column 213, and the purpose of locking the cover 12 is achieved.
During the process of unlocking the locking assembly 20, the specific working principle is as follows: the control box 30 controls the electromagnet 2121 to be powered on, at this time, the locking column 213 is subjected to the acting force of the spring 2122 and the acting force of the electromagnet 2121 at the same time, the elastic force of the spring 2122 is opposite to the magnetic attraction force of the electromagnet 2121, and the acting force generated by the electromagnet 2121 is greater than the acting force of the spring 2122, at this time, the locking column 213 moves along the direction in which the two oppositely-arranged side walls of the abdicating opening 2111 are away from each other under the acting force of the electromagnet 2121, so that the locking column 213 and the locking ring 222 are separated from each other at this time, and.
In an embodiment of the present invention, the body 11 and the cover 12 are made of flexible materials. The flexible material can be polyethylene, rubber, silica gel and other materials capable of generating elastic deformation. The flexible material has the characteristics of light weight, not only can lighten the weight of the unmanned aerial vehicle carrying box, but also can lighten the action of external impact force on the articles in the body 11, and is favorable for ensuring the integrity of the articles in the unmanned aerial vehicle carrying box.
In an embodiment of the present invention, referring to fig. 4, a protective layer 50 is disposed on an outer surface of the body 11, and the protective layer 50 is made of a carbon fiber material. Carbon fiber material has high strength, the characteristics that density is little, and high strength can improve the holistic intensity of box 10, and protective layer 50 makes box 10 be difficult for deformation or damage when being pressed or receiving the striking, and then is favorable to guaranteeing the integrality of the inside article of box 10. The weight that box 10 self can be alleviateed to density is little, and then has the loss that reduces unmanned aerial vehicle's energy.
The connection mode of the existing carrying box 100 of the unmanned aerial vehicle and the unmanned aerial vehicle is as follows: unmanned aerial vehicle's year thing case 100 passes through the slide rail set spare and is connected with unmanned aerial vehicle's foot rest, that is to say, when the slide rail set spare withdrawal restraint, unmanned aerial vehicle's year thing case 100 can slide relative unmanned aerial vehicle's foot rest, and unmanned aerial vehicle's year thing case 100 of being convenient for just so can slide relative unmanned aerial vehicle's foot rest under the effect of robotic arm promptly.
In order to facilitate the connection of carrying case 100 and the arm of unmanned aerial vehicle the utility model discloses an in the embodiment, as shown in the figure, the protective layer 50 of the surface of this body 11 is gone up the concave a plurality of locating holes 51 that are equipped with, and the arm adsorbs on body 11 through the sucking disc and fixed connection is in locating hole 51 department.
Further, the body 11 is disposed in a square shape, and a plurality of positioning holes 51 are symmetrically disposed on the protection layers 50 on two outer surfaces of the body 11. The design that locating hole 51 set up on two opposite faces of box 10 has guaranteed that all can be connected with the arm on two opposite faces of box 10 for the arm can be more stable remove unmanned aerial vehicle's carry thing case 100.
Further, the control box 30 and the positioning hole 51 are located on different sides of the case 10. So configured, the control box 30 can be prevented from interfering with the connection between the robot arm and the housing 10.
It should be noted that the number of the positioning holes 51 may be one or more, and the number of the positioning holes 51 may be determined according to actual situations, and is not specifically limited herein. Referring to fig. 1, the number of the positioning holes 51 is four, two positioning holes 51 are uniformly distributed on two opposite side surfaces of the protection layer 50 on the outer surface of the body 11, and the positioning holes 51 on the two opposite side surfaces are opposite to each other. So set up, avoided unmanned aerial vehicle's year thing case 100 two relative arms to rotate, and then be convenient for unmanned aerial vehicle's the transportation of carrying thing case 100.
The above is only the preferred embodiment of the present invention, and the patent scope of the present invention is not limited thereby, all the equivalent structure changes made by the contents of the specification and the drawings are utilized under the inventive concept of the present invention, or the direct/indirect application in other related technical fields is included in the patent protection scope of the present invention.
Claims (10)
1. An unmanned aerial vehicle's thing case, its characterized in that includes:
the box body comprises a body and a cover body, wherein the body is provided with an accommodating cavity with one open end, and the cover body is used for covering the open end of the accommodating cavity;
the locking assembly comprises a locking part and a locking part, and the locking part are arranged on the body and the cover body;
and the control box is arranged on the top surface of the body and is electrically connected with at least one of the locking part and the locking part so as to control the locking part and the locking part to be locked or unlocked.
2. The carrier case of an unmanned aerial vehicle as claimed in claim 1, wherein the control box is mounted to a central location of a top surface of the body.
3. The unmanned aerial vehicle's carrier case of claim 1, wherein the control box comprises a box body, a PCB board and a cover plate, the box body is mounted on the top surface of the body, a mounting cavity is concavely formed on the surface of the box body opposite to the surface of the body, the PCB board is mounted in the mounting cavity of the box body, the PCB board is electrically connected with the locking part, and the cover plate is used for covering the mounting cavity of the box body.
4. An unmanned aerial vehicle's carrier case of claim 3, wherein the box body is integrally formed with the body.
5. The carrier case of an unmanned aerial vehicle as claimed in claim 1, wherein one side of the cover is pivotally engaged with one side of the body;
the locking part comprises a locking shell, a locking column and a power part electrically connected with the control box, the locking shell is arranged on one side of the body pivoted with the cover body relative to the body, a abdication opening is concavely arranged on the locking shell, the power part is arranged on the locking shell, the locking column is in transmission connection with the power part, and the locking column can move along the directions in which two side walls oppositely arranged along the abdication opening are close to or far away from each other under the driving of the power part;
the locking part is arranged on one side of the cover body, which is pivoted with the shell, opposite to the cover body, the locking part comprises a fixing part fixedly connected with the cover body and a locking ring connected with the fixing part, and the locking ring can extend into or out of the abdicating opening.
6. The unmanned aerial vehicle carrying case of claim 5, wherein the locking housing is provided with a cavity and a relief hole arranged through a wall of the cavity;
one end of the locking column extends into the cavity, and a limiting bulge is convexly arranged on the outer peripheral wall of the locking column outside the cavity;
the power part comprises an electromagnet and a spring, the electromagnet is installed in the containing cavity and can magnetically adsorb the locking column, the spring is sleeved on the locking column, one end of the spring is abutted to the limiting protrusion, and the other end of the spring is abutted to the outer surface of the locking shell.
7. An unmanned aerial vehicle carrying case as claimed in any one of claims 1 to 6, wherein the body and the cover are both made of flexible material.
8. An unmanned aerial vehicle's thing case of any one of claim 1 to 6, characterized in that, the surface of body is provided with the protective layer, and the protective layer adopts carbon fiber material to make.
9. The carrier case of unmanned aerial vehicle of claim 8, wherein the protective layer of the outer surface of the body is provided with a plurality of positioning holes connected with the positioning mechanical arm in a concave manner.
10. The carrying case of unmanned aerial vehicle as claimed in claim 9, wherein the body is a square body, and the protective layers of the two outer surfaces of the body that are opposite to each other are provided with a plurality of positioning holes that are symmetrically arranged.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021256543.7U CN212829087U (en) | 2020-07-01 | 2020-07-01 | Unmanned aerial vehicle's year thing case |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021256543.7U CN212829087U (en) | 2020-07-01 | 2020-07-01 | Unmanned aerial vehicle's year thing case |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212829087U true CN212829087U (en) | 2021-03-30 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202021256543.7U Active CN212829087U (en) | 2020-07-01 | 2020-07-01 | Unmanned aerial vehicle's year thing case |
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| Country | Link |
|---|---|
| CN (1) | CN212829087U (en) |
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- 2020-07-01 CN CN202021256543.7U patent/CN212829087U/en active Active
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