CN113844666A - Unmanned aerial vehicle lift transportation platform - Google Patents

Unmanned aerial vehicle lift transportation platform Download PDF

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Publication number
CN113844666A
CN113844666A CN202111105215.6A CN202111105215A CN113844666A CN 113844666 A CN113844666 A CN 113844666A CN 202111105215 A CN202111105215 A CN 202111105215A CN 113844666 A CN113844666 A CN 113844666A
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CN
China
Prior art keywords
lifting
limiting
unmanned aerial
aerial vehicle
groove
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
CN202111105215.6A
Other languages
Chinese (zh)
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
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 Guizhou Power Grid Co Ltd filed Critical Guizhou Power Grid Co Ltd
Priority to CN202111105215.6A priority Critical patent/CN113844666A/en
Publication of CN113844666A publication Critical patent/CN113844666A/en
Pending legal-status Critical Current

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    • 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

Abstract

The invention discloses an unmanned aerial vehicle lifting transportation platform which comprises a bearing unit, a lifting unit and a protection 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; a lifting unit located above the lifting assembly; the protection device comprises a lifting platform, a driving piece arranged at the end part of the lifting platform, and a protection unit arranged at the outer side of the lifting unit, and the protection unit comprises a protection component and a hinge seat arranged on the side wall of the protection component; the bearing unit is used for installing the lifting unit and the protection unit, the lifting assembly can lift the lifting unit to a proper height, and the limiting unit limits the unmanned aerial vehicle to be placed so as to be convenient for stable transportation; the lifting unit is used for parking and charging the unmanned aerial vehicle; the protection unit is then used for the protection to lift unit and unmanned aerial vehicle.

Description

Unmanned aerial vehicle lift transportation platform
Technical Field
The invention relates to the technical field of unmanned aerial vehicle carrying, in particular to an unmanned aerial vehicle lifting and transporting platform.
Background
In the power industry, power equipment located in the field needs to be overhauled frequently, so that maintainers in the power industry need to go to the field for inspection irregularly. In the field inspection process, a large number of unmanned aerial vehicles can be used to help maintainers to inspect high places or places which are difficult to reach; because of the place of work is in the field, unmanned aerial vehicle lift condition does not possess in a lot of places, and need decompose unmanned aerial vehicle after having used up unmanned aerial vehicle at every turn and put into unmanned aerial vehicle and deposit the case and transport and install once more after next point of use, and this process is troublesome promptly, waste time again.
Disclosure of Invention
This section is for the purpose of summarizing some aspects of embodiments of the invention and to briefly introduce some preferred embodiments. In this section, as well as in the abstract and the title of the invention of this application, simplifications or omissions may be made to avoid obscuring the purpose of the section, the abstract and the title, and such simplifications or omissions are not intended to limit the scope of the invention.
The invention is provided in view of the problems of the existing unmanned aerial vehicle in lifting and transporting.
Therefore, the invention aims to provide an unmanned aerial vehicle lifting and transporting platform, and aims to solve the problems that the unmanned aerial vehicle is inconvenient to take off and land in a field environment, needs to be disassembled and put into a storage box for transportation after being used up each time, and needs to be installed again when being used again.
In order to solve the technical problems, the invention provides the following technical scheme: an unmanned aerial vehicle lifting transportation platform comprises a bearing unit, a lifting unit and a protection unit, wherein the bearing unit comprises a bottom plate assembly, a lifting assembly and a limiting assembly, 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; a lifting unit located above the lifting assembly; it includes the elevating platform with set up in the driving piece of elevating platform tip to and, protection unit, set up in the outside of elevating unit, it includes protection component and set up in articulated seat on the protection component lateral wall.
As a preferred scheme of the unmanned aerial vehicle lifting and transporting platform, the unmanned aerial vehicle lifting and transporting platform comprises the following steps: the bottom plate assembly comprises a bottom plate, a boss positioned at the top of a bottom plate body, a mounting groove formed in the side wall of the top of the boss, and hinge tables arranged on the side walls of two sides of the boss; the bottom of the groove cavity of the mounting groove is provided with a placing groove; the hinge seat can be matched with the hinge table in a hinge mode.
As a preferred scheme of the unmanned aerial vehicle lifting and transporting platform, the unmanned aerial vehicle lifting and transporting platform comprises the following steps: the lifting assembly comprises a lifting oil cylinder and a balance piece, wherein the lifting oil cylinder is arranged on the lifting assembly; the bottom of the lifting oil cylinder is placed in the placing groove, and the top telescopic end of the lifting oil cylinder is connected with the bottom side wall of the lifting platform; the balance piece is located in the mounting groove and comprises a first balance plate, a second balance plate and a synchronous plate, wherein the first balance plate and the second balance plate are symmetrically distributed on two sides of the placing groove, the synchronous plate is connected with the end portions of the two balance plates, and the connecting ends of the two balance plates are respectively connected to the inside of the mounting groove and the side wall of the bottom of the lifting platform.
As a preferred scheme of the unmanned aerial vehicle lifting and transporting platform, the unmanned aerial vehicle lifting and transporting platform comprises the following steps: the limiting assembly comprises a limiting plate arranged on the bottom plate and positioned on two sides of the mounting groove and a limiting part arranged in the limiting plate.
As a preferred scheme of the unmanned aerial vehicle lifting and transporting platform, the unmanned aerial vehicle lifting and transporting platform comprises the following steps: a placing notch is formed in the side wall of the limiting plate and is positioned at one side close to the mounting groove; a plate body of the limiting plate is also provided with a molded assembling groove, a notch of the assembling 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 assembling groove; one end of a groove opening of the assembling groove is located on the placing notch, and the other end of the groove opening of the assembling groove is located on the side wall of the lower end of the limiting plate.
As a preferred scheme of the unmanned aerial vehicle lifting and transporting platform, the unmanned aerial vehicle lifting and transporting platform comprises the following steps: the limiting part comprises a type supporting frame, guide wheels sleeved at the bending part of the type supporting frame, limiting springs sleeved at two sides of the type supporting frame, sliding blocks sliding at two end parts of the type 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 assembling groove or extend out of the notch of the assembling groove.
As a preferred scheme of the unmanned aerial vehicle lifting and transporting platform, the unmanned aerial vehicle lifting and transporting platform 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, and a conversion module, a rectification module and a charging module which are electrically connected with the control module; the input end of the conversion module is connected with the acquisition module through the confluence module, and the output end of the conversion module is connected with the power supply module; the input end of the rectification module is connected with the output end of the power supply module, and the output end of the rectification module is connected with the charging module; the power module provides electric energy for each module.
As a preferred scheme of the unmanned aerial vehicle lifting and transporting platform, the unmanned aerial vehicle lifting and transporting platform 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 provided with cams.
As a preferred scheme of the unmanned aerial vehicle lifting and transporting platform, the unmanned aerial vehicle lifting and transporting platform comprises the following steps: the protection assembly comprises a first half shell and a second half shell which can be matched with each other and coated on the periphery of the lifting platform; the side walls of the end parts of the first half shell and the second half shell in the length direction of the inner cavities are 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 preferred scheme of the unmanned aerial vehicle lifting and transporting platform, the unmanned aerial vehicle lifting and transporting platform comprises the following steps: the hinged seats are located on opposing sidewalls of the cavity of the first and second half-shells.
The invention has the beneficial effects that:
the bearing unit is used for installing the lifting unit and the protection unit, the lifting assembly can lift the lifting unit to a proper height, and the limiting unit limits the unmanned aerial vehicle to be placed so as to be convenient for stable transportation; the lifting unit is used for parking and charging the unmanned aerial vehicle; the protection unit is then used for the protection to lift unit and unmanned aerial vehicle.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings needed to be used in the description of the embodiments will be briefly introduced below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and it is obvious for those skilled in the art to obtain other drawings based on these drawings without inventive exercise. Wherein:
fig. 1 is a schematic diagram of the overall external structure of the unmanned aerial vehicle lifting and transporting platform.
Fig. 2 is a schematic diagram of the overall explosion separation structure of the unmanned aerial vehicle lifting and transporting platform.
Fig. 3 is a schematic diagram of a length-direction section three-dimensional structure of the unmanned aerial vehicle lifting and transporting platform.
Fig. 4 is a schematic view of a cross-sectional plane structure in the width direction of the unmanned aerial vehicle lifting and transporting platform.
Fig. 5 is a schematic structural view of a limiting assembly of the unmanned aerial vehicle lifting and transporting platform.
Fig. 6 is a schematic structural view of a protective assembly of the unmanned aerial vehicle lifting and transporting platform of the present invention.
Fig. 7 is a schematic connection diagram of a charging system of the unmanned aerial vehicle lifting and transporting platform of the present invention.
Fig. 8 is a schematic diagram of the unmanned aerial vehicle placement process state of the unmanned aerial vehicle lifting and transporting platform of the invention.
Fig. 9 is a schematic diagram of a state of a storage drone of the unmanned plane lifting and transporting platform of the present invention.
Detailed Description
In order to make the aforementioned objects, features and advantages of the present invention comprehensible, embodiments accompanied with figures are described in detail below.
In the following description, numerous specific details are set forth in order to provide a thorough understanding of the present invention, but the present invention may be practiced in other ways than those specifically described and will be readily apparent to those of ordinary skill in the art without departing from the spirit of the present invention, and therefore the present invention is not limited to the specific embodiments disclosed below.
Furthermore, reference herein to "one embodiment" or "an embodiment" means that a particular feature, structure, or characteristic described in connection with the embodiment is included in at least one implementation of the invention. 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.
Furthermore, the present invention is described in detail with reference to the drawings, and in the detailed description of the embodiments of the present invention, the cross-sectional view illustrating the structure of the device is not enlarged partially according to the general scale for convenience of illustration, and the drawings are only exemplary and should not be construed as limiting the scope of the present invention. In addition, the three-dimensional dimensions of length, width and depth should be included in the actual fabrication.
Example 1
Referring to fig. 1 and 2, in a first embodiment of the present invention, there is provided an unmanned aerial vehicle elevating transport platform, which includes a carrying unit 100, an elevating unit 200, and a protection unit 300. Wherein, the carrying unit 100 is a plate for installing the lifting unit 100 and the shielding 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 unmanned aerial vehicle and the platform of the lifting unit 200 so as to ensure the safety in the transportation process.
Specifically, the carrying unit 100 includes a bottom plate assembly 101, a lifting assembly 102 and a limiting assembly 103, which are disposed on the bottom plate assembly 101, and the limiting assembly 103 is located at two sides of the lifting assembly 102; the bottom plate assembly 101 is a plate of the bottom plate, and is not only used for installing the lifting assembly 102 and the limiting assembly 103, but also used for integrally fixing the bottom plate assembly 101 when the lifting transportation platform is installed on a vehicle (such as a carriage of a truck); the lifting assembly 102 is used for lifting the whole lifting unit 200, so that the taking off and landing process of the unmanned aerial vehicle on the lifting unit 200 is facilitated; spacing subassembly 103 then is used for when parking unmanned aerial vehicle's position to be injectd, keeps unmanned aerial vehicle stable parking on the platform of lift unit 200 to produce the collision when preventing the transportation and damage unmanned aerial vehicle.
A lift unit 200 positioned above the lift assembly 102; the device comprises a lifting platform 201 and a driving piece 202 arranged at the end part of the lifting platform 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 on the lifting platform 201 is used for driving the unfolding and folding of the protection unit 300.
The protective unit 300 is arranged on the outer side of the lifting unit 200 and comprises a protective assembly 301 and a hinge seat 302 arranged on the side wall of the protective assembly 301; wherein, the protection component 301 covers the outer side of the lifting unit 200 and is driven by the driving component 202; the hinge base 302 is used to connect the shield assembly 301 to the base plate assembly 101.
Example 2
Referring to fig. 2 to 5, a second embodiment of the present invention is different from the first embodiment in that: the bottom plate assembly 101 comprises a bottom plate 101a, a boss 101b positioned at the top of a plate body of the bottom plate 101a, a mounting groove 101c formed in the side wall of 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 placing groove 101c-1 is formed in the bottom of the groove cavity of the mounting groove 101 c; the hinge base 302 can be in hinged engagement with the hinge table 101 d.
The lift assembly 102 includes a lift cylinder 102a and a counterbalance 102b, wherein; the bottom of the lifting oil cylinder 102a is placed in the placing groove 101c-1, and the top telescopic end of the lifting oil cylinder is connected with the bottom side wall of the lifting platform 201; the balance member 102b is disposed in the mounting groove 101c, and includes a first balance plate 102b-1 and a second balance plate 102b-2 symmetrically disposed on both sides of the placement groove 101c-1, and a synchronization plate 101b-3 connected to the ends of the two balance plates, and the connection ends of the two balance plates are respectively connected to the inside of the mounting groove 101c and the bottom sidewall of the lifting platform 201.
The limiting component 103 comprises a limiting plate 103a arranged on the bottom plate 101a and positioned at two sides of the mounting groove 101c, and a limiting member 103b arranged in the limiting plate 103 a.
A placing notch 103a-1 is formed in the side wall of the limiting plate 103a, and the placing notch 103a-1 is positioned at one side close to the mounting groove 101 c; a U-shaped assembling groove 103a-2 is further formed in the plate body of the limiting plate 103a, the notch of the assembling groove 103a-2 is located on the side wall of the plate body on one side of the installing groove 101c, and the limiting piece 103b is installed in the assembling groove 103 a-2; one end of a U-shaped notch of the assembly groove 103a-2 is positioned on the placing notch 103a-1, and the other end is positioned on the side wall of the lower end of the limit plate 103 a.
The limiting part 103b comprises a U-shaped supporting frame 103b-1, a guide wheel 103b-2 sleeved at the bent part of the U-shaped supporting frame 103b-1, a limiting spring 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 cable 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 in the fitting groove 103a-2 or extend out of the notch of the fitting groove 103 a-2.
Compared with the embodiment 1, further, the upper plate surface of the bottom plate 101a in the bottom plate assembly 101 has a boss 101b protruding out of the plate body, the top of the boss 101b is provided with an installation groove 101c recessed into the top plate surface, the groove surface of the installation groove 101c is smaller than the plate surface of the boss 101b, and the hinge platforms 101d on the two side walls of the boss 101b are used for connecting the hinge seats 302 on the side walls of the protection assembly 301. A placing groove 101c-1 is formed at the bottom of the center of the groove cavity of the mounting groove 101c, and the lifting assembly 102 is mounted in the mounting groove 101c and the placing groove 101 c-1. It should be noted that the bottom plate 101a has a large surface, and a connecting hole may be formed in a side wall of the plate body for mounting the transportation platform on a vehicle.
The bottom of a lifting oil cylinder 102a in the lifting assembly 102 is installed in the placing groove 101c-1, the top of the lifting oil cylinder is connected to the side wall of the bottom of the lifting platform 201, the lifting oil cylinder 102a is used for lifting the lifting platform 201 integrally, and a balancing piece 102b is used for stabilizing the stable lifting of the lifting platform 201 integrally; specifically, the balance member 102b comprises two balance plates and a synchronization plate 101b-3 for synchronizing the deflection of the two balance plates, the first balance plate 102b-1 and the second balance plate 102b-2 have the same plate body structure, as shown in fig. 2 and 3, and are formed by hinging and connecting two plate members, the lower end of the balance plate connecting body is hinged on the side wall of the bottom of the cavity of the installation groove 101c, and the upper end of the balance plate connecting body is hinged on the side wall of the bottom of the lifting platform 201. When the lifting oil cylinder 102a extends or shortens, the synchronous plate 101b-3 keeps the first balance plate 102b-1 and the second balance plate 102b-2 to deflect and bend synchronously because the middle part of the synchronous plate 101b-3 is sleeved on the cylinder body of the lifting oil cylinder 102a, and therefore the lifting consistency of the two sides of the lifting platform 201 is kept.
The limiting component 103 includes a limiting plate 103a and a limiting member 103b, specifically, the limiting plate 103a is symmetrical to the bosses 101b on both sides of the mounting groove 101c, and the length thereof may be smaller than the length of the bosses 101 b. The whole position that can be used for injecing elevating platform 201 of limiting plate 103a avoids it to produce the dislocation slope at the lift process, also is used for the installation of locating part 103b, and locating part 103b is used for carrying on spacingly to placing the unmanned aerial vehicle on elevating platform 201 to avoid the unstable problem of unmanned aerial vehicle when placing on elevating platform 201.
Specifically, the side wall of the two side limiting plates 103a close to one side of the mounting groove 101c is provided with a placing notch 103a-1, the notch is used for placing the bottom support of the unmanned aerial vehicle, and the depth and the size of the notch can be determined by the size of the bottom support of the unmanned aerial vehicle which is actually placed. The limiting piece 103 is provided with a limiting piece 103b by forming a U-shaped assembling groove 103a-2 in the side wall of the plate body, and the notches of the U-shaped cavity groove are respectively positioned on the side wall of the lower end of the limiting piece 103a and the side wall of the position where the notch 103a-1 is positioned and face one side of the mounting groove 101 c.
Specifically, as shown in 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 cable 103b-5, wherein the U-shaped supporting frame 103b-1 is structurally fixed and can be placed in the U-shaped assembling 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 limiting spring 103b-3 is sleeved on the rod bodies at two sides of the U-shaped support frame 103b-1, the sliding block 103b-4 is respectively slid on the rod body at the U-shaped end part of the U-shaped support frame 103b-1 and is connected with one end of the limiting spring 103b-3, and the other end of the limiting spring 103b-3 is fixed on the two rod bodies at the bottom of the U-shaped support frame 103 b-1; the cable 103b-5 is connected to the side walls of the two sliders 103b-4 in a U-shape, and the middle portions of the cables are in rotational contact with the outer side walls of the two guide wheels 103 h-2. It should be noted that the elastic coefficient of the limiting spring 103b-3 at the lower end is greater than the elastic coefficient of the limiting spring 103b-3 at the upper end, i.e. the lower slider 103b-4 extends out of the lower notch of the mounting groove 103a-2 in the initial state without external force, and the extending distance is the width of the placement gap 103 a-1. It should be noted that the free end of the slider 103b-4 is formed in a circular arc shape 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 invention, which differs from the second embodiment, is: the lifting platform 201 comprises a platform body 201a and a charging system 203 positioned in the platform body 201a, wherein the charging system 203 comprises a control module 203a, and a conversion module 203b, a rectification module 203c and a charging module 203d which are electrically connected with the control module 203 a; the input end of the conversion module 203b is connected with the acquisition module 203f through the confluence module 203e, and the output end of the conversion module is connected with the power supply 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 203c is connected with the charging module 203 d; the power module 203g provides power to the modules.
The driving member 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 limiting rod 202b are both provided with cams T.
Compare in embodiment 2, further, elevating platform 201 is desk-top box structure, and its whole can be risen by lifting cylinder 102a, and its internal cavity of stage to install the charging system 203 that can charge to unmanned aerial vehicle. Specifically, the charging system 203 is a system with a control module 203a as a control center, the collection module 203d is used for photoelectric conversion, and converts absorbed solar energy into electric energy, and the solar energy can be obtained by an external photovoltaic cell panel, and the photovoltaic cell panel can be installed outside the vehicle and on an external shell of the protection component 301; the electric energy converted by the photovoltaic cell panels is collected by the collecting module 203e and is stored in the power module 203g after passing through the conversion 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 supply module 203g into the voltage required by charging; when the unmanned aerial vehicle is parked on the top side wall of the lifting platform 201, the unmanned aerial vehicle can be charged by the charging module 203 d. The charging module 203d may be a dedicated charging connector of the drone or a contact-type or wireless charger.
Further, the driving member 202 has two sets of driving rods 202a and limiting rods 202b, which are respectively located on the sidewalls of the two ends of the lifting platform 201 in the length direction, the driving rods 202a and the limiting rods 202b are parallel rods, the total length of the rods is greater than the width of the lifting platform 201, and a cam T is disposed at the end of the rod, and the cam T can be matched with and slide in the driving groove Q and the limiting groove X in the sidewall of the half shell in the protection component 301. Namely: when the lifting platform 201 is lifted or lowered, the driving rod 202a and the limiting rod 202b can drive the protection component 301 to be unfolded and closed.
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 invention, which differs from the third embodiment, is: the protection assembly 301 comprises a first half-shell 301a and a second half-shell 301b, which can be engaged with each other and cover the periphery of 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 cavities are provided with a driving groove Q and a limiting groove X; the end cam T of the driving rod 202a can be matched and slid in the driving groove Q, and the end cam T of the limiting rod 202b can be matched and slid in the limiting groove X.
Hinge mounts 302 are located on opposing sidewalls of the interior cavity of the first and second half shells 301a and 301 b.
Compare in embodiment 3, further, protection component 301 wholly is the shell structure of elevating platform 201, and it is formed by first half shell 301a and the symmetrical combination of second half shell 301b, wraps elevating platform 201 and the unmanned aerial vehicle that parks on elevating platform 201 in the inner chamber of the two to realize the protection to the two. Specifically, the first half shell 301a and the second half shell 301b have the same structure, the length, the width and the height of the two half shells are larger than those of the lifting platform 201, and a driving groove Q and a limiting groove X are distributed in the side wall of the end part of the inner cavity of the half shell, which is perpendicular to the length direction, wherein the driving groove Q is used for driving the protection component 301 in a deflection manner, and the limiting groove X is used for limiting an angle in the deflection manner. The first half-shell 301a and the second half-shell 301b are hinged to the side wall of the boss 101b by means of a hinge seat 302 located on the side wall of the lower end of the inner cavity thereof.
The rest of the structure is the same as that of example 3.
Combine to show in FIG. 1 ~ 9, this transportation platform is in the use to install for the application scene in the carriage of transport means, when unmanned aerial vehicle used up and need stop from the transportation platform on, before unmanned aerial vehicle returns, expand the transportation platform, the process is: and starting the lifting oil cylinder 102a, extending the telescopic end of the lifting oil cylinder, slowly lifting the lifting platform 201 at the top of the lifting oil cylinder, and deflecting and unfolding the balance piece 102b positioned below the lifting platform 201 in the process to stably lift the lifting platform 201. When the side wall of the lifting platform 201 does not extrude the sliding block 103b-4, under the elastic force of the lower limiting spring 103b-3, the cable 103b-5 extends towards the U-shaped lower end notch of the assembly groove 103a-2, the lower sliding block 103b-4 extends out of the lower end notch of the assembly groove 103a-2, and the upper sliding block 103b-4 is completely contracted in the upper end notch of the assembly groove 103 a-2.
Further, the driving rod 202a and the limiting rod 202b located at the two ends of the lifting platform 201, the cams T at the end portions of the driving rod 202a and the limiting rod 202b 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, and generate driving force for the first half shell 301a and the second half shell 301b, so that the driving rod and the limiting rod deflect along the respective hinged positions, 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 cannot be blocked by the protection component 301, and the unmanned aerial vehicle is convenient to park. If the unmanned aerial vehicle is not parked well, the unmanned aerial vehicle can be parked at the top of the lifting platform 201 manually, and the supports on the two sides of the bottom of the unmanned aerial vehicle are positioned in the placing notches 103a-1 of the limiting plates 103a on the two sides of the lifting platform 201.
When the unmanned aerial vehicle needs to be charged, the U-shaped support frame 103b-1, the guide wheel 103b-2, the limiting spring 103b-3, the sliding block 103b-4 and the cable 103b-5 can connect the charging module 203d in the lifting platform 201 with a charging interface of the unmanned aerial vehicle.
After unmanned aerial vehicle parks on elevating platform 201, withdraw elevating platform 201 that carries unmanned aerial vehicle, shorten through control lifting hydro-cylinder 102a, elevating platform 201 highly descends gradually, and in-process, half shell 301a and half shell 301b of second are under the effect of actuating lever 202a, reverse deflection gradually, and the separation side of the two is close to each other once more, finally folds up completely, wraps unmanned aerial vehicle and elevating platform 201 in complete casing. And 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 contracts 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 placing notch 103a-1 to limit the bottom bracket of the unmanned aerial vehicle. Thereby keep unmanned aerial vehicle steadily to park on elevating platform 201, guarantee that unmanned aerial vehicle can not drop at this platform removal or the in-process of rocking.
This lift platform can be used for unmanned aerial vehicle's no dismouting to place safely, can realize charging unmanned aerial vehicle, can improve the work efficiency of electric power maintainer when field work greatly.
It should be noted that the above-mentioned embodiments are only for illustrating the technical solutions of the present invention and not for limiting, and although the present invention has been described in detail with reference to the preferred embodiments, it should be understood by those skilled in the art that modifications or equivalent substitutions may be made on the technical solutions of the present invention without departing from the spirit and scope of the technical solutions of the present invention, which should be covered by the claims of the present invention.

Claims (10)

1. The utility model provides an unmanned aerial vehicle lift transport platform which characterized in that: comprises the steps of (a) preparing a mixture of a plurality of raw materials,
the bearing unit (100) comprises a bottom plate component (101), a lifting component (102) and a limiting component (103) which are arranged on the bottom plate component (101), wherein the limiting component (103) is positioned at two sides of the lifting component (102);
a lift unit (200) located above the lift assembly (102); which comprises a lifting platform (201) and a driving piece (202) arranged at the end part of the lifting platform (201),
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).
2. The unmanned aerial vehicle lift transport platform of claim 1, characterized in that: the bottom plate assembly (101) comprises a bottom plate (101a), a boss (101b) positioned at the top of a plate body of the bottom plate (101a), a mounting groove (101c) formed in the side wall of the top of the boss (101b), and hinge tables (101d) arranged on the side walls of two sides of the boss (101 b);
a placing groove (101c-1) is formed in the bottom of the groove cavity of the mounting groove (101 c);
the hinge base (302) can be in hinged fit with the hinge table (101 d).
3. An unmanned aerial vehicle lift transport platform of claim 2, characterized in that: the lift assembly (102) comprises a lift cylinder (102a) and a counterbalance (102b), wherein;
the bottom of the lifting oil cylinder (102a) is placed in the placing groove (101c-1), and the top telescopic end of the lifting oil cylinder is connected with the bottom side wall of the lifting platform (201);
the balance piece (102b) is positioned in the mounting groove (101c) and comprises a first balance plate (102b-1) and a second balance plate (102b-2) which are symmetrically distributed on two sides of the placing groove (101c-1), and a synchronous plate (101b-3) connected with the end parts of the two balance plates, and the connecting ends of the two balance plates are respectively connected to the inside of the mounting groove (101c) and the side wall of the bottom of the lifting platform (201).
4. An unmanned aerial vehicle lift transport platform according to claim 2 or 3, characterized in that: the limiting component (103) comprises a limiting plate (103a) arranged on the bottom plate (101a) and positioned on two sides of the mounting groove (101c) and a limiting piece (103b) arranged in the limiting plate (103 a).
5. An unmanned aerial vehicle lift transport platform of claim 4, wherein: a placing gap (103a-1) is formed in the side wall of the limiting plate (103a), and the placing gap (103a-1) is located at one side close to the mounting groove (101 c);
a U-shaped assembling groove (103a-2) is further formed in the plate body of the limiting plate (103a), the notch of the assembling groove (103a-2) is located on the side wall of the plate body on one side of the installing groove (101c), and the limiting piece (103b) is installed in the assembling groove (103 a-2);
one end of a U-shaped notch of the assembling groove (103a-2) is positioned on the placing notch (103a-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).
6. An unmanned aerial vehicle lift transport platform of claim 5, characterized in that: the limiting part (103b) comprises a U-shaped supporting frame (103b-1), guide wheels (103b-2) sleeved at the bent part 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 cables (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 sliding block (103b-4) can be received in the assembly groove (103a-2) or extend out of the notch of the assembly groove (103 a-2).
7. An unmanned aerial vehicle lift transport platform of any one of claims 1-3, 5 and 6, wherein: the lifting platform (201) comprises a platform body (201a) and a charging system (203) positioned in the platform body (201a), wherein the charging system (203) comprises a control module (203a), a conversion module (203b), a rectification module (203c) and a charging module (203d), and the conversion module (203b), the rectification module and the charging module are electrically connected with the control module (203 a); wherein the content of the first and second substances,
the input end of the conversion module (203b) is connected with the acquisition module (203f) through the confluence module (203e), and the output end of the conversion module is connected with the power supply 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 (203 d);
the power supply module (203g) provides electric energy for each module.
8. An unmanned aerial vehicle lift transport platform of any one of claims 1-3, 5 and 6, wherein: 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 are parallel to each other, and the driving rod (202a) is positioned below the limiting rod (202 b);
the end parts of the rod bodies of the driving rod (202a) and the limiting rod (202b) are provided with cams (T).
9. An unmanned aerial vehicle lift transport platform of claim 8, wherein: the protection assembly (301) comprises a first half shell (301a) and a second half shell (301b), which can be matched with each other and coated on the periphery of 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 provided with a driving groove (Q) and a limiting groove (X);
the end cam (T) of the driving rod (202a) can be matched and slide in the driving groove (Q), and the end cam (T) of the limiting rod (202b) can be matched and slide in the limiting groove (X).
10. An unmanned aerial vehicle lift transport platform of claim 9, wherein: the hinge seats (302) are located on opposing sidewalls of the internal cavity of the first half-shell (301a) and the second half-shell (301 b).
CN202111105215.6A 2021-09-22 2021-09-22 Unmanned aerial vehicle lift transportation platform Pending CN113844666A (en)

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Application Number Priority Date Filing Date Title
CN202111105215.6A CN113844666A (en) 2021-09-22 2021-09-22 Unmanned aerial vehicle lift transportation platform

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Application Number Priority Date Filing Date Title
CN202111105215.6A CN113844666A (en) 2021-09-22 2021-09-22 Unmanned aerial vehicle lift transportation platform

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CN113844666A true CN113844666A (en) 2021-12-28

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20160364989A1 (en) * 2015-06-15 2016-12-15 ImageKeeper LLC Unmanned aerial vehicle management
KR101617594B1 (en) * 2015-09-01 2016-05-02 오영동 Landing device for drone to vehicle and control method thereof
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