CN217649314U

CN217649314U - Unmanned aerial vehicle wireless charging cabin

Info

Publication number: CN217649314U
Application number: CN202221247736.5U
Authority: CN
Inventors: 陈宇; 张河山
Original assignee: Chongqing Huachuang Intelligent Technology Research Institute Co ltd
Current assignee: Chongqing Huachuang Intelligent Technology Research Institute Co ltd
Priority date: 2022-05-24
Filing date: 2022-05-24
Publication date: 2022-10-25
Anticipated expiration: 2032-05-24

Abstract

The utility model relates to an unmanned aerial vehicle cabin technical field discloses an unmanned aerial vehicle wireless charging cabin, including the open cabin body in top and installing a pair of hatch door at the open end of the cabin body, the cabin still includes two mechanisms of opening door that are used for two hatches of switching respectively, the mechanism of opening door includes the driving piece, first connecting piece and two second connecting pieces, the hatch door is through two second connecting pieces and cabin body swing joint, and two second connecting pieces set up respectively in the both sides of hatch door, first connecting piece is installed between two second connecting pieces and is used for driving two second connecting piece synchronous motion, the driving piece is installed on the cabin body and is used for driving the motion of first connecting piece. The utility model discloses a set up the cabin body, hatch door, driving piece, first connecting piece, second connecting piece isotructure, can realize that the automation of hatch door is opened and the automation is closed, also make the switching process of hatch door more harmonious, smooth and easy simultaneously.

Description

Unmanned aerial vehicle wireless charging cabin

Technical Field

The utility model relates to an unmanned aerial vehicle cabin technical field especially relates to an unmanned aerial vehicle wireless charging cabin.

Background

An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer. Unmanned aerial vehicles can be classified into military and civil applications according to the application field. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle + the industry application is really just needed by the unmanned aerial vehicle; the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, and developed countries actively expand the industrial application and develop the unmanned aerial vehicle technology.

At present most unmanned aerial vehicle all is equipped with wireless charging engine room, and when unmanned aerial vehicle after accomplishing the navigation task, can return the cabin in and charge, for next navigation task makes preparation. But when some cabins receive the unmanned aerial vehicle that returns to the journey, still need artifical switching hatch door, reduced the degree of automation of cabin.

SUMMERY OF THE UTILITY MODEL

In view of this, the utility model aims at providing a wireless charging cabin in unmanned aerial vehicle has solved the partial cabin that the background art center pointed out and still needs artifical switching hatch door when receiving the unmanned aerial vehicle of returning a journey, has reduced the problem of the degree of automation in cabin.

The utility model discloses an above-mentioned technical problem is solved to following technical means.

The utility model provides a wireless charging cabin of unmanned aerial vehicle, includes the open cabin body in top and installs a pair of hatch door at the open end of cabin body, the cabin still includes two mechanism of opening door that are used for two hatch doors of switching respectively, the mechanism of opening door includes driving piece, first connecting piece and two second connecting pieces, the hatch door is through two second connecting pieces and cabin body swing joint, and two the second connecting piece sets up respectively in the both sides of hatch door, first connecting piece is installed between two second connecting pieces and is used for driving two second connecting piece synchronous motion, the driving piece is installed on the cabin body and is used for driving the motion of first connecting piece.

Further, the second connecting piece includes the mount pad, in-connection arm and outer joint arm down, it fixes on the inner wall of hatch door to go up the mount pad, the mount pad is fixed and is served at the uncovered of the cabin body down, the upper end of in-connection arm and outer joint arm all articulates on last mount pad, the lower extreme of in-connection arm and outer joint arm all articulates under on the mount pad.

Furthermore, all have the portion of bending on internal link arm and the outer joint arm, just one side of internal link arm indent is towards the outer joint arm, one side of outer joint arm indent is towards the internal link arm.

Furthermore, the inner connecting arm and the outer connecting arm are provided with lightening holes at the upper side and the lower side of the bending part.

Further, the first connecting piece comprises a connecting rod, and two ends of the connecting rod are respectively fixed with the lower rotating centers of the inner connecting arms of the two second connecting pieces or the lower rotating centers of the outer connecting arms of the two second connecting pieces.

Furthermore, the first connecting piece also comprises a rotating handle, and one end of the rotating handle is fixed on the connecting rod.

Furthermore, the driving piece is an electric push rod, one end of the electric push rod, far away from the output shaft, is hinged to the open end of the cabin body, and one end of the output shaft of the electric push rod is hinged to one end of the rotating handle, far away from the connecting rod.

Furthermore, the electric push rods of the two door opening mechanisms are respectively positioned at two sides of the open end of the cabin body.

Furthermore, four corners of the bottom of the cabin body are provided with universal wheels with brakes.

Has the advantages that: the utility model discloses a set up the cabin body, hatch door, driving piece, first connecting piece, second connecting piece isotructure, can realize that the automation of hatch door is opened and the automation is closed, also make the switching process of hatch door more harmonious, smooth and easy simultaneously.

Drawings

Fig. 1 is a schematic structural view of the double-sided hatch in the open state of the present invention.

Fig. 2 is a schematic structural view of the door opening mechanism of the present invention.

Fig. 3 is a schematic structural view of the single-sided cabin of the present invention in a closed state.

Wherein, 1, a cabin body; 2. a cabin door; 3. a drive member; 4. a first connecting member; 41. a connecting rod; 42. rotating the handle; 5. a second connecting member; 51. an upper mounting seat; 52. a lower mounting seat; 53. an inner connecting arm; 531. a bending part; 532. lightening holes; 54. an outer connecting arm; 6. a universal wheel.

Detailed Description

The following description is given by way of specific embodiments, and those skilled in the art will appreciate the advantages and effects of the present invention from the disclosure provided in the present specification. It should be noted that the drawings provided in the following embodiments are for illustrative purposes only, and are only schematic drawings rather than actual drawings, which should not be construed as limiting the present invention, and in order to better illustrate the embodiments of the present invention, some components in the drawings may be omitted, enlarged or reduced, and do not represent the size of an actual product; it will be understood by those skilled in the art that certain well-known structures in the drawings and descriptions thereof may be omitted.

In the description of the present invention, it should be understood that if there are the terms "upper", "lower", "left", "right", "front", "back", etc. indicating the orientation or position relationship based on the orientation or position relationship shown in the drawings, it is only for convenience of description and simplification of description, but not for indicating or implying that the indicated device or element must have a specific orientation, be constructed in a specific orientation, and be operated, therefore, the terms describing the position relationship in the drawings are used only for exemplary illustration, and should not be construed as limiting the present invention, and those skilled in the art can understand the specific meaning of the terms according to the specific situation.

As shown in fig. 1, fig. 2 and fig. 3, the utility model discloses a wireless charging cabin of unmanned aerial vehicle, including the open cabin body 1 in top and install a pair of hatch door 2 at the open end of cabin body 1, this pair of hatch door 2 can be toward the direction motion of keeping away from each other or being close to each other. When the two cabin doors 2 move to the preset positions in the direction away from each other, the open end of the cabin body 1 can be completely opened, so that the unmanned aerial vehicle can conveniently land on a parking apron in the cabin body 1; when the two doors 2 are moved closer together until the two doors 2 are fully closed, the open end of the cabin 1 can be completely closed.

The cabin also comprises two door opening mechanisms, the two door opening mechanisms respectively correspond to the two cabin doors 2, and the door opening mechanisms are used for automatically opening or closing the corresponding cabin doors 2.

In this embodiment, the right door opening mechanism and the hatch door 2 are taken as an example, and the structure and principle of the door opening mechanism will be described in detail. The door opening mechanism comprises a driving member 3, a first connecting member 4 and two second connecting members 5. The hatch door 2 is movably connected with the cabin body 1 through two second connecting pieces 5, the two second connecting pieces 5 are respectively arranged on two sides of the hatch door 2, and the hatch door 2 can move relative to the cabin body 1 through the two second connecting pieces 5, so that the aim of opening and closing the hatch door 2 is fulfilled. The first connecting piece 4 is arranged between the two second connecting pieces 5, the first connecting piece 4 is used for driving the two second connecting pieces 5 to move synchronously, and the second connecting pieces 5 on the two sides can be more coordinated and smoother when the movement of opening or closing the cabin door 2 is completed by the first connecting piece 4. The driving piece 3 is installed on the cabin body 1, and the driving piece 3 is used for driving the first connecting piece 4 to move, and when the driving piece 3 drives the first connecting piece 4 to move, the two second connecting pieces 5 can be driven to move synchronously through the first connecting piece 4, so that the actions of opening or closing the cabin door 2 can be completed more coordinately, more smoothly and more automatically.

In this embodiment, each of the second connecting members 5 includes an upper mounting seat 51, a lower mounting seat 52, an inner connecting arm 53 and an outer connecting arm 54, the upper mounting seat 51 is fixed to the inner wall of the cabin door 2 by bolts, and the lower mounting seat 52 is fixed to the open end of the cabin body 1 by bolts. The inner connecting arm 53 is located at the left side of the outer connecting arm 54, the upper ends of the inner connecting arm 53 and the outer connecting arm 54 are hinged on the upper mounting seat 51, and the lower ends of the inner connecting arm 53 and the outer connecting arm 54 are hinged on the lower mounting seat 52. The upper mount 51, the lower mount 52, the inner connecting arm 53 and the outer connecting arm 54 enclose the entire second link 5 in a parallelogram-like hinge mechanism which can be deformed. When the second connecting pieces 5 on the two sides deform, the cabin door 2 can be driven to move along an arc-shaped track, so that the action of opening or closing the cabin door 2 is completed.

In this embodiment, the inner connecting arm 53 and the outer connecting arm 54 have bent portions 531, and the inner connecting arm 53 faces the outer connecting arm 54 at its concave side, and the outer connecting arm 54 faces the inner connecting arm 53 at its concave side. Through the arrangement, in the process of opening or closing the cabin door 2 by the second connecting piece 5, the stress of the inner connecting arm 53 and the outer connecting arm 54 is more uniform and reasonable, so that the service life of the inner connecting arm 53 and the outer connecting arm 54 is prolonged.

In this embodiment, the inner connecting arm 53 and the outer connecting arm 54 have lightening holes 532 on both upper and lower sides of the bending portion 531. By so arranging, the weight of the inner link arm 53 and the outer link arm 54 can be reduced, and the entire nacelle can be made lighter in weight.

In this embodiment, the first connecting member 4 includes a connecting rod 41, and both ends of the connecting rod 41 are respectively fixed to the lower rotation centers of the inner connecting arms 53 of the two second connecting members 5 or the lower rotation centers of the outer connecting arms 54 of the two second connecting members 5. When the connecting rod 41 rotates, the two inner connecting arms 53 or the two outer connecting arms 54 can be driven to rotate synchronously, so that the two second connecting pieces 5 are deformed synchronously, and the purpose of opening or closing the cabin door 2 is achieved. In order to drive the connecting rod 41 to rotate, in another embodiment, the driving member 3 may be a motor, and an output shaft of the motor may be directly fixed to the connecting rod 41 through a coupling, or may drive the connecting rod 41 to rotate through a gear transmission, a belt rotation, or the like.

In this embodiment, the first connecting member 4 further includes a rotating handle 42, and one end of the rotating handle 42 is fixed to the connecting rod 41. When the connecting rod 41 needs to be driven to rotate, the rotating handle 42 can be directly driven to rotate around the connecting rod 41, so that the connecting rod 41 is driven to rotate, the aim of opening or closing the cabin door 2 is fulfilled, and the operation is more labor-saving than the operation of directly driving the connecting rod 41 to rotate.

In this embodiment, the driving member 3 is an electric push rod, one end of the electric push rod far away from the output shaft is hinged to the open end of the cabin 1, and one end of the output shaft of the electric push rod is hinged to one end of the rotating handle 42 far away from the connecting rod 41. By so arranging, it is convenient to drive the rotation handle 42 to rotate about the connection rod 41.

In this embodiment, the electric push rods of the two door opening mechanisms are respectively located at two sides of the open end of the cabin 1. Through setting up like this, make mutual noninterference between two electric putter, make the mechanism in cabin more reasonable.

In this embodiment, four corners of the bottom of the cabin 1 are all provided with universal wheels 6 with brakes. By so arranging, it is convenient to move the entire nacelle.

Although the present invention has been described in detail with reference to the preferred embodiments, those skilled in the art will understand that the present invention can be modified or replaced with other embodiments without departing from the spirit and scope of the present invention, which should be construed as limited only by the appended claims. The technology, shape and construction parts which are not described in detail in the present invention are all known technology.

Claims

1. The utility model provides a wireless charging cabin of unmanned aerial vehicle, includes the open cabin body in top and installs a pair of hatch door at the open end of cabin body, its characterized in that: the cabin still includes two mechanisms of opening door that are used for two hatchdoors of switching respectively, the mechanism of opening door includes driving piece, first connecting piece and two second connecting pieces, the hatch door is through two second connecting pieces and cabin body swing joint, and two the second connecting piece sets up respectively in the both sides of hatch door, first connecting piece is installed between two second connecting pieces and is used for driving two second connecting piece synchronous motion, the driving piece is installed on the cabin body and is used for driving the motion of first connecting piece.

2. The unmanned aerial vehicle wireless charging cabin of claim 1, characterized in that: the second connecting piece includes mount pad, lower mount pad, in-connection arm and outer link arm, it fixes on the inner wall of hatch door to go up the mount pad, the mount pad is fixed and is served at the uncovered of the cabin body down, the upper end of in-connection arm and outer link arm all articulates on last mount pad, the lower extreme of in-connection arm and outer link arm all articulates under on the mount pad.

3. The unmanned aerial vehicle wireless charging cabin of claim 2, characterized in that: all have the portion of bending on internal connection arm and the outer joint arm, just one side of internal connection arm indent is towards the outer joint arm, one side of outer joint arm indent is towards the internal connection arm.

4. The unmanned aerial vehicle wireless charging cabin of claim 3, characterized in that: and the inner connecting arm and the outer connecting arm are provided with lightening holes at the upper side and the lower side of the bending part.

5. The unmanned aerial vehicle wireless charging cabin of any one of claims 2-4, wherein: the first connecting piece comprises a connecting rod, and two ends of the connecting rod are respectively fixed with the lower rotating centers of the inner connecting arms of the two second connecting pieces or the lower rotating centers of the outer connecting arms of the two second connecting pieces.

6. The unmanned aerial vehicle wireless charging cabin of claim 5, characterized in that: the first connecting piece further comprises a rotating handle, and one end of the rotating handle is fixed to the connecting rod.

7. The unmanned aerial vehicle wireless charging cabin of claim 6, characterized in that: the driving piece is an electric push rod, one end of the electric push rod, far away from the output shaft, is hinged to the open end of the cabin body, and one end of the output shaft of the electric push rod is hinged to one end, far away from the connecting rod, of the rotating handle.

8. The unmanned aerial vehicle wireless charging cabin of claim 7, wherein: and the electric push rods of the two door opening mechanisms are respectively positioned at two sides of the open end of the cabin body.

9. The unmanned aerial vehicle wireless charging cabin of any one of claims 5-8, wherein: four corners of the bottom of the cabin body are provided with universal wheels with brakes.