CN113844667B - Unmanned aerial vehicle lift transport platform convenient to delivery - Google Patents

Unmanned aerial vehicle lift transport platform convenient to delivery Download PDF

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Publication number
CN113844667B
CN113844667B CN202111105221.1A CN202111105221A CN113844667B CN 113844667 B CN113844667 B CN 113844667B CN 202111105221 A CN202111105221 A CN 202111105221A CN 113844667 B CN113844667 B CN 113844667B
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CN
China
Prior art keywords
lifting
limiting
assembly
unmanned aerial
aerial vehicle
Prior art date
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Active
Application number
CN202111105221.1A
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Chinese (zh)
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CN113844667A (en
Inventor
李荣春
游洁
谢榕
陈水波
杨涛
魏乾
陆韦刚
周力
龙文亮
张卿科
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Guizhou Power Grid Co Ltd
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Guizhou Power Grid Co Ltd
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Filing date
Publication date
Application filed by Guizhou Power Grid Co Ltd filed Critical Guizhou Power Grid Co Ltd
Priority to CN202111105221.1A priority Critical patent/CN113844667B/en
Publication of CN113844667A publication Critical patent/CN113844667A/en
Application granted granted Critical
Publication of CN113844667B publication Critical patent/CN113844667B/en
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Classifications

    • 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
    • B64F1/007—Helicopter portable landing pads
    • 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
    • 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
    • B64F1/005—Protective coverings for aircraft not in use
    • 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
    • B60L2200/00—Type of vehicles
    • B60L2200/10—Air crafts
    • 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
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/60—Other road transportation technologies with climate change mitigation effect
    • Y02T10/70—Energy storage systems for electromobility, e.g. batteries
    • 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
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/60—Other road transportation technologies with climate change mitigation effect
    • Y02T10/7072—Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
    • 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
    • Y02T90/12—Electric charging stations

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Power Engineering (AREA)
  • Transportation (AREA)
  • Forklifts And Lifting Vehicles (AREA)

Abstract

The application discloses an unmanned aerial vehicle lifting transport platform convenient to carry, which comprises a bearing unit, wherein the bearing unit comprises a bottom plate assembly, a lifting assembly and a limiting assembly, wherein the lifting assembly and the limiting assembly are arranged on the bottom plate assembly, and the limiting assembly is positioned on two sides of the lifting assembly; the lifting component comprises a lifting rod and a stabilizing piece, and the stabilizing piece is matched and connected with the end part of the lifting rod; the lifting unit is positioned at the top of the lifting assembly and comprises a lifting table and a driving piece arranged at the end part of the lifting table; the protection unit is arranged on the outer side of the lifting unit and comprises a protection assembly and a hinge seat arranged on the side wall of the protection assembly; the bearing unit is used for installing the lifting unit and the protection unit, the lifting assembly can stably lift the lifting unit to a proper height, and the limiting unit is used for limiting the placed unmanned aerial vehicle so as to facilitate stable transportation; the lifting unit is used for parking and charging the unmanned aerial vehicle; the protection unit is used for protecting the lifting unit and the unmanned aerial vehicle.

Description

Unmanned aerial vehicle lift transport platform convenient to delivery
Technical Field
The application relates to the technical field of unmanned aerial vehicle carrying, in particular to an unmanned aerial vehicle lifting and transporting platform convenient to carry.
Background
In the power industry, power equipment located in the field needs to be overhauled from time to time, so that overhaulers in the power industry are required to visit the field at random. In the field inspection process, unmanned aerial vehicles are used in a large amount to help maintenance personnel to inspect high places or places which are difficult to reach; because the place of work is in the field, many places do not possess unmanned aerial vehicle elevating condition, and need decompose unmanned aerial vehicle and put into unmanned aerial vehicle after the unmanned aerial vehicle has been used at every turn and deposit the case and transport and install again after the next point of use, this process is troublesome promptly, and the time is wasted again.
Disclosure of Invention
This section is intended to outline some aspects of embodiments of the application and to briefly introduce some preferred embodiments. Some simplifications or omissions may be made in this section as well as in the description of the application and in the title of the application, which may not be used to limit the scope of the application.
The present application has been made in view of the above problems with lifting and transporting existing unmanned aerial vehicles.
Therefore, the application aims to provide an unmanned aerial vehicle lifting transportation platform, which aims to solve the problems that in a field environment, the unmanned aerial vehicle is inconvenient to take off and land, and the unmanned aerial vehicle is required to be disassembled and put into a storage box for transportation after being used up each time, and is required to be installed again when being used again.
In order to solve the technical problems, the application provides the following technical scheme: an unmanned aerial vehicle lifting transportation platform convenient to carry, this transportation platform includes load-bearing unit, elevating unit and protection unit. The bearing unit comprises a bottom plate assembly, a lifting assembly and a limiting assembly, wherein the lifting assembly and the limiting assembly are arranged on the bottom plate assembly, and the limiting assembly is positioned on two sides of the lifting assembly; the lifting assembly comprises a lifting rod and a stable piece, wherein the stable piece is matched and connected with the end part of the lifting rod; the lifting unit is positioned at the top of the lifting assembly and comprises a lifting table and a driving piece arranged at the end part of the lifting table; and the protection unit is arranged on the outer side of the lifting unit and comprises a protection component and a hinge seat arranged on the side wall of the protection component.
As a preferable scheme of the unmanned aerial vehicle lifting transportation platform convenient to carry, the application comprises the following steps: the bottom plate assembly comprises a bottom plate, a boss positioned at the top of the bottom plate, a mounting groove arranged at the top of the boss, and hinge tables arranged on side walls at two sides of the boss; a chute is formed in the bottom of the groove cavity of the mounting groove; the hinge seat can be in hinge fit with the hinge table.
As a preferable scheme of the unmanned aerial vehicle lifting transportation platform convenient to carry, the application comprises the following steps: the stable piece comprises a connecting plate, a first deflection rod symmetrically hinged to the side wall of the end part of the connecting plate, a sliding block hinged to the other end of the first deflection rod, and a second deflection rod with one end hinged to the sliding block, wherein the other end of the second deflection rod is hinged to the bottom side wall of the lifting table; the bottom of the sliding block slides in the sliding groove; one end of the pushing rod is connected to the connecting plate, and the other end of the pushing rod is connected to the bottom side wall of the lifting table.
As a preferable scheme of the unmanned aerial vehicle lifting transportation platform convenient to carry, the application comprises the following steps: the limiting assembly comprises limiting plates arranged on the bottom plate and located on two sides of the mounting groove and limiting pieces arranged in the limiting plates.
As a preferable scheme of the unmanned aerial vehicle lifting transportation platform convenient to carry, the application comprises the following steps: a placement notch is formed in the side wall of the limiting plate and is positioned at one side close to the mounting groove; an assembly groove is further formed in the plate body of the limiting plate, a notch of the assembly groove is positioned on the side wall of the plate body at one side of the mounting groove, and the limiting piece is mounted in the assembly groove; one end of the notch of the assembly groove is positioned on the placement notch, and the other end of the notch is positioned on the side wall of the lower end of the limiting plate.
As a preferable scheme of the unmanned aerial vehicle lifting transportation platform convenient to carry, the application comprises the following steps: the limiting piece comprises a supporting frame, guide wheels sleeved at the bending part of the supporting frame, limiting springs sleeved at two sides of the supporting frame, sliding blocks sliding at two end parts of the supporting frame, and ropes connected to the end parts of the two sliding blocks and in rolling contact with the two guide wheels; the sliding block can be contained in the assembly groove or extend out of the notch of the assembly groove.
As a preferable scheme of the unmanned aerial vehicle lifting transportation platform convenient to carry, the application comprises the following steps: the lifting platform comprises a platform body and a charging system positioned in the platform body, wherein the charging system comprises a control module, a conversion module, a rectifying module and a charging module, wherein the conversion module, the rectifying module and the charging module are electrically connected with the control module; the input end of the conversion module is connected with the acquisition module through the converging module, and the output end of the conversion module is connected with the power module; the input end of the rectifying module is connected with the output end of the power supply module, and the output end of the rectifying module is connected with the charging module; the power module provides power for each module.
As a preferable scheme of the unmanned aerial vehicle lifting transportation platform convenient to carry, the application comprises the following steps: the driving piece comprises a driving rod and a limiting rod which are symmetrically arranged at two ends of the length side wall of the lifting platform, the driving rod and the limiting rod are parallel to each other, and the driving rod is positioned below the limiting rod; the end parts of the rod bodies of the driving rod and the limiting rod are respectively provided with a cam.
As a preferable scheme of the unmanned aerial vehicle lifting transportation platform convenient to carry, the application comprises the following steps: the protection component comprises a first half shell and a second half shell which can be matched with each other and are coated on the periphery of the lifting platform; the side walls of the end parts of the inner cavities of the first half shell and the second half shell in the length direction are respectively provided with a driving groove and a limiting groove; the end cam of the driving rod can slide in the driving groove in a matched mode, and the end cam of the limiting rod can slide in the limiting groove in a matched mode.
As a preferable scheme of the unmanned aerial vehicle lifting transportation platform convenient to carry, the application comprises the following steps: the hinge seat is positioned on the opposite inner cavity side walls of the first half shell and the second half shell.
The application has the beneficial effects that: the bearing unit is used for installing the lifting unit and the protection unit, the lifting assembly can stably lift the lifting unit to a proper height, and the limiting unit is used for limiting the placed unmanned aerial vehicle so as to facilitate stable transportation; the lifting unit is used for parking and charging the unmanned aerial vehicle; the protection unit is used for protecting the lifting unit and the unmanned aerial vehicle.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present application, the drawings that are needed in the description of the embodiments will be briefly described below, it being obvious that the drawings in the following description are only some embodiments of the present application, and that other drawings may be obtained according to these drawings without inventive effort for a person skilled in the art. Wherein:
fig. 1 is a schematic view of the overall external structure of the present application.
Fig. 2 is a schematic diagram of the overall explosive separation structure of the present application.
Fig. 3 is a schematic view of a cross-sectional plane structure in the width direction of the present application.
Fig. 4 is a schematic view of a longitudinal sectional perspective structure of the present application.
Fig. 5 is a schematic structural diagram of a limiting component according to the present application.
Fig. 6 is a schematic structural diagram of a protection component according to the present application.
Fig. 7 is a schematic diagram of a charging system according to the present application.
Fig. 8 is a schematic view of a state of a placement process of the unmanned aerial vehicle according to the present application.
Fig. 9 is a schematic diagram of a storage drone state of the present application.
Detailed Description
In order that the above-recited objects, features and advantages of the present application will become more readily apparent, a more particular description of the application will be rendered by reference to specific embodiments thereof which are illustrated in the appended drawings.
In the following description, numerous specific details are set forth in order to provide a thorough understanding of the present application, but the present application may be practiced in other ways other than those described herein, and persons skilled in the art will readily appreciate that the present application is not limited to the specific embodiments disclosed below.
Further, reference herein to "one embodiment" or "an embodiment" means that a particular feature, structure, or characteristic can be included in at least one implementation of the application. The appearances of the phrase "in one embodiment" in various places in the specification are not necessarily all referring to the same embodiment, nor are separate or alternative embodiments mutually exclusive of other embodiments.
Further, in describing the embodiments of the present application in detail, the cross-sectional view of the device structure is not partially enlarged to a general scale for convenience of description, and the schematic is only an example, which should not limit the scope of protection of the present application. In addition, the three-dimensional dimensions of length, width and depth should be included in actual fabrication.
Example 1
Referring to fig. 1 and 2, for a first embodiment of the present application, there is provided a portable unmanned aerial vehicle lifting transport platform including a carrying unit 100, a lifting unit 200, and a guard unit 300. Wherein the carrying unit 100 is a plate for mounting the lifting unit 100 and the guard unit 300; the lifting unit 200 is used for parking and charging the unmanned aerial vehicle; the protection unit 300 is used for protecting the platform of the unmanned plane and the lifting unit 200, so as to ensure the safety during transportation.
Specifically, the carrying unit 100 includes a base plate assembly 101, a lifting assembly 102 and a limiting assembly 103 disposed on the base plate assembly 101, and the limiting assemblies 103 are located at two sides of the lifting assembly 102; wherein the base plate component 101 is a plate of the base plate, which is not only used for installing the lifting component 102 and the limiting component 103, but also used for fixing the whole lifting transportation platform when the lifting transportation platform is installed on a carrier (such as a carriage of a truck); the lifting assembly 102 is used for integrally lifting the lifting unit 200, so as to facilitate the lifting process of the unmanned aerial vehicle on the lifting unit 200; the limiting component 103 is used for limiting the position of the unmanned aerial vehicle when the unmanned aerial vehicle is parked, and keeping the unmanned aerial vehicle stably parked on the platform of the lifting unit 200, so as to prevent the unmanned aerial vehicle from being damaged by collision during transportation.
A lifting unit 200 located above the lifting assembly 102; which comprises a lifting table 201 and a driving piece 202 arranged at the end part of the lifting table 201; the lifting platform 201 is a parking platform of the unmanned aerial vehicle, and can be used for charging the unmanned aerial vehicle; the driving member 202 located on the lifting table 201 is used to drive the unfolding and folding of the protection unit 300.
The protection unit 300 is arranged on the outer side of the lifting unit 200 and comprises a protection component 301 and a hinge seat 302 arranged on the side wall of the protection component 301; wherein, the protection component 301 is wrapped on the outer side of the lifting unit 200, and is driven by the driving piece 202; the hinge base 302 is used for connecting the protection component 301 and the base plate component 101.
Example 2
Referring to fig. 2 to 4, a second embodiment of the present application is different from the first embodiment in that: the base plate assembly 101 comprises a base plate 101a, a boss 101b positioned at the top of the base plate 101a, a mounting groove 101c formed at the top of the boss 101b, and hinge tables 101d arranged on the side walls of the two sides of the boss 101 b; a chute 101c-1 is formed in the bottom of the groove cavity of the mounting groove 101 c; the hinge base 302 can be hinge-fitted with the hinge table 101 d.
The lift assembly 102 includes a lift bar 102a and a stationary member 102b, the stationary member 102b being cooperatively associated with an end of the lift bar 102 a.
The stationary member 102b comprises a connecting plate 102b-1, a first deflection rod 102b-2 symmetrically hinged to the side wall of the end of the connecting plate 102b-1, a sliding block 102b-3 hinged to the other end of the first deflection rod 102b-2, and a second deflection rod 102b-4 hinged to the sliding block 102b-3 at one end, the other end of the second deflection rod 102b-4 being hinged to the bottom side wall of the lifting platform 201; the bottom of the sliding block 102b-3 slides in the sliding groove 101c-1; one end of the push rod 102a is connected to the connecting plate 102b-1, and the other end is connected to the bottom side wall of the lift table 201.
The limiting assembly 103 includes limiting plates 103a disposed on the bottom plate 101a and located at both sides of the mounting groove 101c, and limiting members 103b disposed in the limiting plates 103 a.
The side wall of the limiting plate 103a is provided with a placement notch 103a-1, and the placement notch 103a-1 is positioned at one side close to the mounting groove 101 c; the plate body of the limiting plate 103a is also provided with a U-shaped assembly groove 103a-2, the notch of the assembly groove 103a-2 is positioned on the side wall of the plate body at one side of the mounting groove 101c, and the limiting piece 103b is mounted in the assembly groove 103 a-2; one end of the U-shaped notch of the assembly groove 103a-2 is positioned on the placement notch 103a-1, and the other end is positioned on the lower end side wall of the limiting plate 103 a.
The limiting piece 103b comprises a U-shaped supporting frame 103b-1, guide wheels 103b-2 sleeved at the bending position of the U-shaped supporting frame 103b-1, limiting springs 103b-3 sleeved at two sides of the U-shaped supporting frame 103b-1, sliding blocks 103b-4 sliding at two end parts of the U-shaped supporting frame 103b-1, and a rope 103b-5 connected to the end parts of the two sliding blocks 103b-4 and in rolling contact with the two guide wheels 103 b-2; the slider 103b-4 can be received within the fitting groove 103a-2 or extend out of the notch of the fitting groove 103 a-2.
In comparison with the embodiment 1 and with reference to fig. 2, further, the upper plate surface of the bottom plate 101a of the bottom plate assembly 101 has a boss 101b protruding from the plate body, a mounting groove 101c recessed into the top plate surface is formed at the top of the boss 101b, the groove surface of the mounting groove 101c is smaller than the plate surface of the boss 101b, and hinge bases 101d on two side walls of the boss 101b are used for connecting hinge bases 302 on the side walls of the protection assembly 301. A chute 101c-1 is arranged at the bottom of the groove cavity of the mounting groove 101c, and the chute 101c-1 is long and can be distributed with a plurality of groups in parallel along the length and/or width direction of the mounting groove 101 c; the advantage of the multiple group distribution is that the overall lifting stability of the lifting table 201 can be ensured. The bottom plate 101a has a large plate surface, and may have fixing holes on the outer edge side wall of the plate for mounting the transport platform on a vehicle.
In the lifting assembly 102, the stationary member 102b is used to maintain the entire lifting table 201 stably raised or lowered, and the lift rod 102a is used to drive the motion of the stationary member 102 b. Specifically, the connecting plate 102b-1 in the stationary member 102b is located at the middle portion, and on the peripheral side wall thereof, is hinged to one end of the first deflecting lever 102b-2, while the other end of the first deflecting lever 102b-2 is hinged to the sliding block 102b-3, the bottom of which slides in the sliding slot 101c-1, and the top of the sliding block 102b-3 is also hinged to one end of the second deflecting lever 102b-4, while the other end of the second deflecting lever 102b-4 is hinged to the bottom side wall of the lifting table 201. The pushing rod 102a is a rod body with telescopic pushing, in particular a hydraulic rod or an oil cylinder, which is installed between the connecting plate 102b-1 and the lifting platform 201, and pushes the sliding block 102b-3 to slide in the sliding groove 101c-1 through the change of the length thereof, so as to change the supporting angle of the second deflection rod 102b-4, and thus change the supporting height of the lifting platform 201.
The limiting assembly 103 includes a limiting plate 103a and a limiting member 103b, and specifically, the limiting plate 103a is symmetrical to the boss 101b at two sides of the mounting groove 101c, and its length may be smaller than the length of the boss 101 b. The whole limiting plate 103a can be used for limiting the position of the lifting platform 201, so that dislocation inclination of the lifting platform is avoided in the lifting process, the limiting plate is also used for installing the limiting piece 103b, and the limiting piece 103b is used for limiting an unmanned aerial vehicle placed on the lifting platform 201, so that the problem that the unmanned aerial vehicle is unstable when placed on the lifting platform 201 is solved.
Specifically, the side walls of the two side limiting plates 103a, which are close to one side of the mounting groove 101c, are provided with a placement notch 103a-1, the notch is used for placing the bottom bracket of the unmanned aerial vehicle, and the depth and the size of the notch can be determined by the size of the bottom bracket of the unmanned aerial vehicle which is actually placed. The limiting plate 103 is provided with a limiting piece 103b by forming a U-shaped assembly groove 103a-2 in the side wall of the plate body, and the notch of the U-shaped cavity groove is respectively positioned on the side wall of the lower end of the limiting plate 103a and the side wall of the placement notch 103a-1 and faces one side of the mounting groove 101 c.
Specifically, referring to fig. 5, the limiting member 103b includes a U-shaped supporting frame 103b-1, a guide wheel 103b-2, a limiting spring 103b-3, a slider 103b-4 and a rope 103b-5, where the U-shaped supporting frame 103b-1 is structurally fixed and can be placed in a U-shaped assembly groove 103a-2 for installing other components in the limiting member 103 b; the guide wheel 103b-2 is rotatably arranged on two rod bodies at the bottom of the U-shaped support frame 103b-1, the limit springs 103b-3 are sleeved on two rod bodies at the two sides of the U-shape of the U-shaped support frame 103b-1, the sliding blocks 103b-4 respectively slide on the rod bodies at the U-shaped end part of the U-shaped support frame 103b-1 and are connected with one end of the limit springs 103b-3, and the other ends of the limit springs 103b-3 are fixed on the two rod bodies at the bottom of the U-shaped support frame 103 b-1; the rope 103b-5 is connected to the side walls of the two sliding blocks 103b-4 in a U shape, and the middle parts of the rope are respectively in rotary contact with the outer side walls of the two guide wheels 103 h-2. It should be noted that, the elastic coefficient of the limit spring 103b-3 at the lower end is larger than that of the limit spring 103b-3 at the upper end, that is, the lower slider 103b-4 extends out of the lower slot of the assembly slot 103a-2 in a state of not being subjected to external force initially, and the extending distance is the width of the placement notch 103 a-1. It should be noted that the free end of the slider 103b-4 is arc-shaped to facilitate the pressing contact with the sidewall of the lifting platform 201.
The rest of the structure is the same as that of embodiment 1.
Example 3
Referring to fig. 2, 4 and 7, a third embodiment of the present application is different from the second embodiment in that: the lifting table 201 comprises a table body 201a and a charging system 203 positioned in the table body 201a, wherein the charging system 203 comprises a control module 203a, a conversion module 203b electrically connected with the control module 203a, a rectifying module 203c and a charging module 203d; the input end of the conversion module 203b is connected with the acquisition module 203f through the converging module 203e, and the output end of the conversion module is connected with the power module 203 g; the input end of the rectifying module 203c is connected with the output end of the power supply module 203g, and the output end of the rectifying module is connected with the charging module 203d; the power module 203g provides power to each module.
The driving piece 202 comprises a driving rod 202a and a limiting rod 202b which are symmetrically arranged at two ends of the length side wall of the lifting platform 201, the driving rod 202a and the limiting rod 202b are parallel to each other, and the driving rod 202a is positioned below the limiting rod 202 b; the rod body ends of the driving rod 202a and the stopper rod 202b are each provided with a cam T.
Further, compared to embodiment 2, the lifting platform 201 has a table-type box structure, the whole lifting platform can be lifted by the lifting rod 102a, the interior of the platform is hollow, and a charging system 203 capable of charging the unmanned aerial vehicle is installed. Specifically, the charging system 203 is a system taking a control module 203a as a control center, and the collecting module 203d is used for photoelectric conversion to convert absorbed solar energy into electric energy, and the solar energy can be obtained by an external photovoltaic panel, and the photovoltaic panel can be installed on the outside of the carrier and the outer shell of the protection component 301; the electric energy converted by the photovoltaic cell panels is collected by the collecting module 203e and stored in the power supply module 203g after passing through the converting module 203 b; when the unmanned aerial vehicle needs to be charged, the control module 203a controls the rectification module 203c to convert the voltage output by the power module 203g into the voltage required by charging; when the unmanned aerial vehicle is parked on the top side wall of the elevating platform 201, the unmanned aerial vehicle can be charged through the charging module 203 d. The charging module 203d may be a dedicated charging connector or a contact type wireless charger of the unmanned aerial vehicle.
Further, the driving member 202 has two sets of driving rods 202a and limiting rods 202b, which are respectively located on two side walls of the lifting platform 201 in the length direction, the driving rods 202a and the limiting rods 202b are mutually parallel rods, the total length of the rods is greater than the width of the lifting platform 201, and the end of the rods is provided with a cam T, and the cam T can slide in a driving groove Q and a limiting groove X in the side wall of the half shell in the protection assembly 301 in a matching manner. Namely: when the elevating platform 201 is elevated or lowered, the deployment and closure of the guard assembly 301 can be driven by the driving rod 202a and the limit rod 202 b.
The rest of the structure is the same as that of embodiment 2.
Example 4
Referring to fig. 2, 3, 6 and 8, a fourth embodiment of the present application is different from the third embodiment in that: the protection component 301 comprises a first half shell 301a and a second half shell 301b, which can be matched with each other and are wrapped around the lifting platform 201; the side walls of the end parts of the first half shell 301a and the second half shell 301b in the length direction of the inner cavity are respectively provided with a driving groove Q and a limiting groove X; the end cam T of the driving lever 202a can slide in the driving groove Q, and the end cam T of the stopper lever 202b can slide in the stopper groove X.
Hinge seats 302 are located on opposite sidewalls of the inner cavity of the first and second halves 301a and 301 b.
Compared to embodiment 3, further, the protection component 301 is a housing structure of the lifting platform 201, which is formed by symmetrically combining the first half-shell 301a and the second half-shell 301b, and the lifting platform 201 and the unmanned aerial vehicle parked on the lifting platform 201 are covered in the inner cavities of the two to realize protection of the two. Specifically, the first half shell 301a and the second half shell 301b have the same structure, and the length, width and height of the two half shells are larger than those of the lifting platform 201, and driving grooves Q and limiting grooves X are distributed in the end side walls of the inner cavities of the half shells perpendicular to the length direction, wherein the driving grooves Q are used for deflection driving of the protection component 301, and the limiting grooves X are used for limiting angles during deflection. The first half-shell 301a and the second half-shell 301b are hinged on the side wall of the boss 101b through a hinge seat 302 positioned on the side wall of the lower end of the inner cavity.
The rest of the structure is the same as that of embodiment 3.
In combination with the illustrations of fig. 1 to 9, the transport platform is used in a use process by taking a carriage installed in a transport means as an application scene, when the unmanned aerial vehicle is used up and needs to stop on the slave transport platform, the transport platform is unfolded before the unmanned aerial vehicle returns, and the process is as follows: the lifting rod 102a is started, the telescopic end of the lifting rod is extended, the lifting table 201 at the top of the lifting rod is slowly lifted, and in the process, the stable piece 102b positioned below the lifting table 201 deflects and expands, so that the lifting table 201 is stably lifted. When the side wall of the lifting platform 201 does not squeeze the sliding block 103b-4, the rope 103b-5 stretches towards the U-shaped lower end slot of the assembly slot 103a-2 under the elastic force of the lower end limiting spring 103b-3, the lower sliding block 103b-4 stretches out of the lower end slot of the assembly slot 103a-2, and the upper sliding block 103b-4 completely contracts into the upper end slot of the assembly slot 103 a-2.
Further, the driving rod 202a and the limiting rod 202b located at two ends of the lifting platform 201, the cams T at the two ends slide in the driving groove Q and the limiting groove X in the side walls of the first half shell 301a and the second half shell 301b, driving force is generated for the first half shell 301a and the second half shell 301b, so that the first half shell 301a and the second half shell 301b deflect along the respective hinge positions, and due to the existence of the limiting groove X, when the first half shell 301a and the second half shell 301b deflect to the maximum angle, the lifting platform 201 is lifted to the maximum height, at this time, the top of the lifting platform 201 is spacious and is not blocked by the protection component 301, and the unmanned aerial vehicle is convenient to park. If the parking is bad, the unmanned aerial vehicle can be manually parked at the top of the lifting platform 201, and the brackets at the two sides of the bottom of the unmanned aerial vehicle are positioned in the placement notches 103a-1 of the limiting plates 103a at the two sides of the lifting platform 201.
When the unmanned aerial vehicle needs to be charged, the charging module 203d in the lifting platform 201 can be connected with a charging interface of the unmanned aerial vehicle.
After the unmanned aerial vehicle is parked on the lifting platform 201, the lifting platform 201 carrying the unmanned aerial vehicle is retracted, the lifting platform 201 is shortened by controlling the lifting rod 102a, the height of the lifting platform 201 is gradually lowered, in the process, the first half shell 301a and the second half shell 301b are gradually reversely deflected under the action of the driving rod 202a, the separated sides of the first half shell 301a and the second half shell are close to each other again, and finally the unmanned aerial vehicle and the lifting platform 201 are completely folded, so that the unmanned aerial vehicle and the lifting platform 201 are covered in a complete shell. In the descending process of the lifting platform 201, when the side wall of the lifting platform 201 extrudes the sliding block 103b-4 extending out of the notch at the lower end of the assembly groove 103a-2, the sliding block 103b-4 is contracted inwards towards the assembly groove 103a-2, the limiting spring 103b-3 positioned below is compressed, the limiting spring 103b-3 at the upper end is extended, the sliding block 103b-4 at the upper end is pushed out of the notch at the upper end of the assembly groove 103a-2, and the sliding block 103b-4 is transversely inserted into the placement notch 103a-1 to limit the bottom bracket of the unmanned aerial vehicle. Thereby keep unmanned aerial vehicle to park steadily on elevating platform 201, guarantee at this platform removal or rock in-process, unmanned aerial vehicle can not drop.
The lifting platform can be used for unmanned aerial vehicle's non-dismouting safety is placed, can realize charging to unmanned aerial vehicle, can improve the work efficiency of electric power maintainer when field work greatly.
It should be noted that the above embodiments are only for illustrating the technical solution of the present application and not for limiting the same, and although the present application has been described in detail with reference to the preferred embodiments, it should be understood by those skilled in the art that the technical solution of the present application may be modified or substituted without departing from the spirit and scope of the technical solution of the present application, which is intended to be covered in the scope of the claims of the present application.

Claims (8)

1. Unmanned aerial vehicle lift transport platform convenient to delivery, its characterized in that: comprising the steps of (a) a step of,
the bearing unit (100) comprises a bottom plate assembly (101), a lifting assembly (102) and a limiting assembly (103) which are arranged on the bottom plate assembly (101), wherein the limiting assembly (103) is positioned on two sides of the lifting assembly (102);
the bottom plate assembly (101) comprises a bottom plate (101 a), a boss (101 b) positioned at the top of the bottom plate (101 a), a mounting groove (101 c) formed at the top of the boss (101 b), and hinge tables (101 d) arranged on side walls at two sides of the boss (101 b);
a chute (101 c-1) is formed at the bottom of the groove cavity of the mounting groove (101 c);
the lifting assembly (102) comprises a lifting rod (102 a) and a stabilizing piece (102 b), wherein the stabilizing piece (102 b) is matched and connected with the end part of the lifting rod (102 a);
the stationary part (102 b) comprises a connecting plate (102 b-1), a first deflection rod (102 b-2) symmetrically hinged on the side wall of the end part of the connecting plate (102 b-1), a sliding block (102 b-3) hinged on the other end of the first deflection rod (102 b-2), and a second deflection rod (102 b-4) with one end hinged on the sliding block (102 b-3), wherein the other end of the second deflection rod (102 b-4) is hinged on the bottom side wall of the lifting platform (201);
the bottom of the sliding block (102 b-3) slides in the sliding groove (101 c-1);
one end of the pushing rod (102 a) is connected to the connecting plate (102 b-1), and the other end is connected to the bottom side wall of the lifting table (201);
a lifting unit (200) which is positioned at the top of the lifting assembly (102) and comprises a lifting table (201) and a driving piece (202) arranged at the end part of the lifting table (201); the method comprises the steps of,
the protection unit (300) is arranged on the outer side of the lifting unit (200) and comprises a protection assembly (301) and a hinge seat (302) arranged on the side wall of the protection assembly (301);
the hinge seat (302) is capable of being hinge-fitted with the hinge table (101 d).
2. The unmanned aerial vehicle lifting transport platform for facilitating carrying according to claim 1, wherein: the limiting assembly (103) comprises limiting plates (103 a) arranged on the bottom plate (101 a) and located on two sides of the mounting groove (101 c), and limiting pieces (103 b) arranged in the limiting plates (103 a).
3. The unmanned aerial vehicle lifting transport platform for facilitating carrying according to claim 2, wherein: a placement notch (103 a-1) is formed in the side wall of the limiting plate (103 a), and the placement notch (103 a-1) is positioned at one side close to the mounting groove (101 c);
the plate body of the limiting plate (103 a) is also provided with a U-shaped assembly groove (103 a-2), a notch of the assembly groove (103 a-2) is positioned on the side wall of the plate body at one side of the mounting groove (101 c), and the limiting piece (103 b) is mounted in the assembly groove (103 a-2);
one end of the U-shaped notch of the assembly groove (103 a-2) is positioned on the placement notch (103 a-1), and the other end of the U-shaped notch is positioned on the side wall of the lower end of the limiting plate (103 a).
4. The unmanned aerial vehicle lifting transport platform for facilitating carrying according to claim 3, wherein: the limiting piece (103 b) comprises a U-shaped supporting frame (103 b-1), guide wheels (103 b-2) sleeved at the bending position of the U-shaped supporting frame (103 b-1), limiting springs (103 b-3) sleeved on two sides of the U-shaped supporting frame (103 b-1), sliding blocks (103 b-4) sliding on two end parts of the U-shaped supporting frame (103 b-1), and ropes (103 b-5) connected to the end parts of the two sliding blocks (103 b-4) and in rolling contact with the two guide wheels (103 b-2);
the slider (103 b-4) can be received in the fitting groove (103 a-2) or extend out of the notch of the fitting groove (103 a-2).
5. The unmanned aerial vehicle lifting transportation platform convenient to carry according to any one of claims 1 to 4, wherein: the lifting table (201) comprises a table body (201 a) and a charging system (203) positioned in the table body (201 a), wherein the charging system (203) comprises a control module (203 a), a conversion module (203 b), a rectifying module (203 c) and a charging module (203 d), and the conversion module (203 b), the rectifying module (203 c) and the charging module are electrically connected with the control module (203 a); wherein,,
the input end of the conversion module (203 b) is connected with the acquisition module (203 f) through the converging module (203 e), and the output end of the conversion module is connected with the power module (203 g);
the input end of the rectifying module (203 c) is connected with the output end of the power supply module (203 g), and the output end of the rectifying module is connected with the charging module (203 d);
the power supply module (203 g) provides power to each module.
6. The unmanned aerial vehicle lifting transportation platform convenient to carry according to any one of claims 1 to 4, wherein: the driving piece (202) comprises a driving rod (202 a) and a limiting rod (202 b) which are symmetrically arranged at two ends of the length side wall of the lifting table (201), the driving rod and the limiting rod are parallel to each other, and the driving rod (202 a) is positioned below the limiting rod (202 b);
the end parts of the rod bodies of the driving rod (202 a) and the limiting rod (202 b) are respectively provided with a cam (T).
7. The unmanned aerial vehicle lifting transport platform for facilitating carrying of claim 6, wherein: the protection component (301) comprises a first half shell (301 a) and a second half shell (301 b), which can be matched with each other and are coated on the periphery of the lifting table (201);
the side walls of the end parts of the first half shell (301 a) and the second half shell (301 b) in the length direction of the inner cavity are respectively provided with a driving groove (Q) and a limiting groove (X);
the end cam (T) of the driving rod (202 a) can slide in the driving groove (Q) in a matching way, and the end cam (T) of the limiting rod (202 b) can slide in the limiting groove (X) in a matching way.
8. The unmanned aerial vehicle lifting transport platform for facilitating carrying of claim 7, wherein: the hinge seat (302) is located on opposite inner cavity side walls of the first half shell (301 a) and the second half shell (301 b).
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CN115258180B (en) * 2022-09-30 2023-01-31 复亚智能科技(太仓)有限公司 Linkage lifting type unilateral formula unmanned aerial vehicle storage device that uncaps

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104246101A (en) * 2012-04-23 2014-12-24 格里根门系统股份有限公司 Rotary-leaf/-casement drive device
CN108016629A (en) * 2016-10-31 2018-05-11 比亚迪股份有限公司 Unmanned plane landing platform
CN110435910A (en) * 2019-09-09 2019-11-12 深圳市科卫泰实业发展有限公司 A kind of multi-rotor unmanned aerial vehicle landing-gear
CN210162270U (en) * 2019-04-25 2020-03-20 边疆 Unmanned aerial vehicle's descending platform
CN211810295U (en) * 2020-01-02 2020-10-30 北京京东乾石科技有限公司 Cabin body and automatic airport
CN111994830A (en) * 2020-08-11 2020-11-27 南京中创智元科技有限公司 Electrical equipment box lifting and pushing device
CN112278310A (en) * 2020-11-06 2021-01-29 湖南浩天翼航空技术有限公司 Automatic lifting and retracting mechanism for tethered rotor wing and use method thereof
CN112850596A (en) * 2021-03-23 2021-05-28 广东同辉检验中心有限公司 Anti-falling safety component of construction elevator

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104246101A (en) * 2012-04-23 2014-12-24 格里根门系统股份有限公司 Rotary-leaf/-casement drive device
CN108016629A (en) * 2016-10-31 2018-05-11 比亚迪股份有限公司 Unmanned plane landing platform
CN210162270U (en) * 2019-04-25 2020-03-20 边疆 Unmanned aerial vehicle's descending platform
CN110435910A (en) * 2019-09-09 2019-11-12 深圳市科卫泰实业发展有限公司 A kind of multi-rotor unmanned aerial vehicle landing-gear
CN211810295U (en) * 2020-01-02 2020-10-30 北京京东乾石科技有限公司 Cabin body and automatic airport
CN111994830A (en) * 2020-08-11 2020-11-27 南京中创智元科技有限公司 Electrical equipment box lifting and pushing device
CN112278310A (en) * 2020-11-06 2021-01-29 湖南浩天翼航空技术有限公司 Automatic lifting and retracting mechanism for tethered rotor wing and use method thereof
CN112850596A (en) * 2021-03-23 2021-05-28 广东同辉检验中心有限公司 Anti-falling safety component of construction elevator

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