CN114932820A - Unmanned aerial vehicle wireless charging cabin - Google Patents

Unmanned aerial vehicle wireless charging cabin Download PDF

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Publication number
CN114932820A
CN114932820A CN202210566114.7A CN202210566114A CN114932820A CN 114932820 A CN114932820 A CN 114932820A CN 202210566114 A CN202210566114 A CN 202210566114A CN 114932820 A CN114932820 A CN 114932820A
Authority
CN
China
Prior art keywords
cabin
unmanned aerial
aerial vehicle
wireless charging
arm
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN202210566114.7A
Other languages
Chinese (zh)
Inventor
陈宇
张河山
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Chongqing Huachuang Intelligent Technology Research Institute Co ltd
Original Assignee
Chongqing Huachuang Intelligent Technology Research Institute Co ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Chongqing Huachuang Intelligent Technology Research Institute Co ltd filed Critical Chongqing Huachuang Intelligent Technology Research Institute Co ltd
Priority to CN202210566114.7A priority Critical patent/CN114932820A/en
Publication of CN114932820A publication Critical patent/CN114932820A/en
Pending legal-status Critical Current

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U70/00—Launching, take-off or landing arrangements
    • B64U70/90—Launching from or landing on platforms
    • B64U70/92—Portable platforms
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
    • B60L53/30—Constructional details of charging stations
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
    • B60L53/10—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles characterised by the energy transfer between the charging station and the vehicle
    • B60L53/12—Inductive energy transfer
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F1/00—Ground or aircraft-carrier-deck installations
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02T90/10—Technologies relating to charging of electric vehicles
    • Y02T90/14—Plug-in electric vehicles

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Power Engineering (AREA)
  • Transportation (AREA)
  • Remote Sensing (AREA)
  • Power-Operated Mechanisms For Wings (AREA)

Abstract

The invention relates to the technical field of unmanned aerial vehicle cabins, and discloses an unmanned aerial vehicle wireless charging cabin which comprises a cabin body with an open top end, a pair of cabin doors arranged at the open end of the cabin body, and two door opening mechanisms respectively used for opening and closing the two cabin doors, wherein each door opening mechanism comprises a driving piece, a first connecting piece and two second connecting pieces, each cabin door is movably connected with the cabin body through the two second connecting pieces, the two second connecting pieces are respectively arranged at two sides of each cabin door, the first connecting pieces are arranged between the two second connecting pieces and used for driving the two second connecting pieces to synchronously move, and the driving pieces are arranged on the cabin body and used for driving the first connecting pieces to move. According to the invention, by arranging the cabin body, the cabin door, the driving piece, the first connecting piece, the second connecting piece and other structures, the automatic opening and the automatic closing of the cabin door can be realized, and meanwhile, the opening and closing process of the cabin door is more coordinated and smooth.

Description

Unmanned aerial vehicle wireless charging cabin
Technical Field
The invention relates to the technical field of unmanned aerial vehicle cabins, in particular 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 the developed countries also 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 receiving the unmanned aerial vehicle that returns to navigate, some cabin still need the manual work to open and close the hatch door, has reduced the degree of automation in cabin.
Disclosure of Invention
In view of this, the present invention provides a wireless charging cabin for an unmanned aerial vehicle, which solves the problem that the automation degree of the cabin is reduced because the cabin door still needs to be opened and closed manually when a part of the cabin indicated by the center of the background art receives a returning unmanned aerial vehicle.
The present invention solves the above-described problems by the 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 mount pad, in-connection arm and outer link arm down, it fixes on the inner wall of hatch door to go up the mount pad, the open of the cabin body is served to the mount pad is fixed 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.
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.
Further, the driving piece is an electric push rod, one end, far away from the output shaft, of the electric push rod is hinged to the open end of the cabin, and one end, far away from the connecting rod, of the output shaft of the electric push rod is hinged to one end, far away from the connecting rod, of the rotating handle.
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: according to the invention, by arranging the cabin body, the cabin door, the driving piece, the first connecting piece, the second connecting piece and other structures, the automatic opening and the automatic closing of the cabin door can be realized, and meanwhile, the opening and closing process of the cabin door is more coordinated and smooth.
Drawings
Fig. 1 is a schematic structural view of a double-sided hatch of the present invention in an open state.
Fig. 2 is a schematic diagram illustrating the structure of the door opening mechanism in the present invention.
FIG. 3 is a schematic structural view of the single-sided hatch of the present invention in a closed state.
Wherein, 1, 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 of the embodiments of the present invention is provided by way of specific examples, and those skilled in the art will appreciate the advantages and utilities of the present invention from the disclosure herein. It should be noted that the drawings provided in the following embodiments are only for illustrative purposes, are schematic drawings rather than actual drawings, and are not to be construed as limiting the invention, and in order to better illustrate the embodiments of the 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 terms such as "upper", "lower", "left", "right", "front", "back", etc., indicating orientations or positional relationships based on the orientations or positional relationships shown in the drawings, it is only for convenience of description and simplicity of description, but does not indicate or imply 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 positional relationships in the drawings are only used for illustrative purposes and are not to be construed as limiting the present invention, and those skilled in the art can understand the specific meanings of the terms according to specific situations.
As shown in fig. 1, 2 and 3, the wireless charging cabin for unmanned aerial vehicles of the present invention comprises a cabin body 1 with an open top end and a pair of cabin doors 2 installed at the open end of the cabin body 1, wherein the pair of cabin doors 2 can move in a direction away from or close to each other. When the two cabin doors 2 move to the preset positions in the mutually-far direction, 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 correspond to the two cabin doors 2 respectively, 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 cabin 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 cabin door 2, and the cabin 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 cabin 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 the 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, and 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, it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted without departing from the spirit and scope of the invention as defined in the appended claims. The techniques, shapes, and configurations not described in detail in the present invention are all known techniques.

Claims (9)

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 mechanism of opening door that are used for two hatches 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 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.
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, wherein: 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. An unmanned aerial vehicle wireless charging cabin according to any one of claims 5-8, characterized in that: four corners of the bottom of the cabin body are provided with universal wheels with brakes.
CN202210566114.7A 2022-05-24 2022-05-24 Unmanned aerial vehicle wireless charging cabin Pending CN114932820A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202210566114.7A CN114932820A (en) 2022-05-24 2022-05-24 Unmanned aerial vehicle wireless charging cabin

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202210566114.7A CN114932820A (en) 2022-05-24 2022-05-24 Unmanned aerial vehicle wireless charging cabin

Publications (1)

Publication Number Publication Date
CN114932820A true CN114932820A (en) 2022-08-23

Family

ID=82863644

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202210566114.7A Pending CN114932820A (en) 2022-05-24 2022-05-24 Unmanned aerial vehicle wireless charging cabin

Country Status (1)

Country Link
CN (1) CN114932820A (en)

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