CN113844667A - Unmanned aerial vehicle lift transport platform convenient to delivery - Google Patents
Unmanned aerial vehicle lift transport platform convenient to delivery Download PDFInfo
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- CN113844667A CN113844667A CN202111105221.1A CN202111105221A CN113844667A CN 113844667 A CN113844667 A CN 113844667A CN 202111105221 A CN202111105221 A CN 202111105221A CN 113844667 A CN113844667 A CN 113844667A
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- 230000000087 stabilizing effect Effects 0.000 claims abstract description 11
- 238000006243 chemical reaction Methods 0.000 claims description 12
- 238000005096 rolling process Methods 0.000 claims description 3
- 239000000203 mixture Substances 0.000 claims 1
- 239000002994 raw material Substances 0.000 claims 1
- 230000003028 elevating effect Effects 0.000 description 13
- 238000000034 method Methods 0.000 description 11
- 230000008569 process Effects 0.000 description 9
- 238000010586 diagram Methods 0.000 description 6
- 239000003381 stabilizer Substances 0.000 description 4
- 230000008859 change Effects 0.000 description 3
- 238000009434 installation Methods 0.000 description 3
- 230000001681 protective effect Effects 0.000 description 3
- 230000008901 benefit Effects 0.000 description 2
- 238000007689 inspection Methods 0.000 description 2
- 238000000926 separation method Methods 0.000 description 2
- 238000003860 storage Methods 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000002360 explosive Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
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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
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- 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
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- 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
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- 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
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- 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 invention discloses an unmanned aerial vehicle lifting transportation platform convenient to carry, which comprises a bearing unit, a lifting component and a limiting component, wherein the bearing unit comprises a bottom plate component, the lifting component and the limiting component are arranged on the bottom plate component, and the limiting component is positioned on two sides of the lifting component; the lifting assembly comprises a lifting rod and a stabilizing piece, and the stabilizing piece is connected with the end part of the lifting rod in a matching way; the lifting unit is positioned at the top of the lifting assembly and comprises a lifting platform and a driving piece arranged at the end part of the lifting platform; 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 limits the unmanned aerial vehicle to be placed so as to be stably transported; 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
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 convenient to carry.
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: the utility model provides an unmanned aerial vehicle lift transport platform convenient to delivery, this transport platform includes bearing unit, lift 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 push lifting rod and a stabilizing piece, and the stabilizing piece is connected with the end part of the push lifting rod in a matching way; the lifting unit is positioned at the top of the lifting assembly and comprises a lifting platform and a driving piece arranged at the end part of the lifting platform; and the protection unit is arranged on the outer side of the lifting unit and comprises a protection component and a hinged seat arranged on the side wall of the protection component.
As an optimal scheme of the unmanned aerial vehicle lifting transportation platform convenient for carrying, the invention 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 formed at 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 sliding groove; the hinge seat can be matched with the hinge table in a hinge mode.
As an optimal scheme of the unmanned aerial vehicle lifting transportation platform convenient for carrying, the invention comprises the following steps: the stabilizing piece comprises a connecting plate, first deflecting rods 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 deflecting rod, and a second deflecting rod with one end hinged to the sliding block, and the other end of the second deflecting rod is hinged to the side wall of the bottom of the lifting platform; the bottom of the sliding block slides in the sliding groove; one end of the lifting rod is connected to the connecting plate, and the other end of the lifting rod is connected to the side wall of the bottom of the lifting platform.
As an optimal scheme of the unmanned aerial vehicle lifting transportation platform convenient for carrying, the invention 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 an optimal scheme of the unmanned aerial vehicle lifting transportation platform convenient for carrying, the invention 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 an optimal scheme of the unmanned aerial vehicle lifting transportation platform convenient for carrying, the invention 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 an optimal scheme of the unmanned aerial vehicle lifting transportation platform convenient for carrying, the invention 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 an optimal scheme of the unmanned aerial vehicle lifting transportation platform convenient for carrying, the invention 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 an optimal scheme of the unmanned aerial vehicle lifting transportation platform convenient for carrying, the invention 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 an optimal scheme of the unmanned aerial vehicle lifting transportation platform convenient for carrying, the invention 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 stably lift the lifting unit to a proper height, and the limiting unit limits the unmanned aerial vehicle to be placed so as to be stably transported; 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 an overall external structural view of the present invention.
Fig. 2 is a schematic diagram of the overall explosive separation structure of the present invention.
FIG. 3 is a schematic diagram of a cross-sectional plane structure in the width direction of the present invention.
Fig. 4 is a schematic view of a longitudinal sectional three-dimensional structure of the present invention.
Fig. 5 is a schematic structural view of the limiting assembly of the present invention.
Fig. 6 is a schematic structural diagram of the protection assembly of the present invention.
Fig. 7 is a schematic diagram of the connection of the charging system according to the present invention.
Fig. 8 is a schematic diagram of the unmanned aerial vehicle placement process state of the present invention.
Fig. 9 is a schematic diagram of the state of the storage drone 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, for a first embodiment of the present invention, an unmanned aerial vehicle lifting transportation platform convenient for carrying is provided, and the transportation platform comprises a carrying unit 100, a lifting 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 a bottom plate, and is not only used for installing the lifting assembly 102 and the limiting assembly 103, but also used for fixing the whole transportation platform 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 4, 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 the bottom 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; the bottom of the groove cavity of the mounting groove 101c is provided with a sliding groove 101 c-1; the hinge base 302 can be in hinged engagement with the hinge table 101 d.
The lift assembly 102 includes a lift rod 102a and a stabilizer 102b, the stabilizer 102b being matingly attached to an end of the lift rod 102 a.
The stabilizing piece 102b comprises a connecting plate 102b-1, a first deflecting rod 102b-2 symmetrically hinged on the side wall of the end part of the connecting plate 102b-1, a sliding block 102b-3 hinged on the other end of the first deflecting rod 102b-2, and a second deflecting rod 102b-4 with one end hinged on the sliding block 102b-3, and the other end of the second deflecting rod 102b-4 is hinged on the side wall of the bottom of the lifting platform 201; the bottom of the sliding block 102b-3 slides in the sliding groove 101 c-1; one end of the lifting rod 102a is connected to the connecting plate 102b-1, and the other end is connected to the bottom side wall 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 embodiment 1, with reference to fig. 2, 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. The bottom of the cavity of the mounting groove 101c is provided with a sliding groove 101c-1, the sliding groove 101c-1 is long-strip-shaped, and a plurality of groups of sliding grooves can be distributed in parallel along the length and/or width direction of the mounting groove 101 c; the advantage that the multiunit distributes lies in, can ensure the stationarity that elevating platform 201 wholly goes up and down. It should be noted that the bottom plate 101a has a larger plate surface, and fixing holes may be formed on the outer edge side walls of the plate body for mounting the transportation platform on a vehicle.
In the lift assembly 102, the stabilizer 102b serves to maintain the overall stable raising or lowering of the lift table 201, and the lift lever 102a serves to drive the action of the stabilizer 102 b. Specifically, the connecting plate 102b-1 of the stabilizing member 102b is located in the middle, and the peripheral side wall thereof is hinged to one end of the first deflecting rod 102b-2, while the other end of the first deflecting rod 102b-2 is hinged to the sliding block 102b-3 sliding in the sliding groove 101c-1 at the bottom, the top of the sliding block 102b-3 is also hinged to one end of the second deflecting rod 102b-4, and the other end of the second deflecting rod 102b-4 is hinged to the bottom side wall of the lifting platform 201. The pushing rod 102a is a rod body with telescopic propulsion, and may be a hydraulic rod or an oil cylinder, and is installed between the connecting plate 102b-1 and the lifting platform 201, and through the change of the length thereof, the sliding block 102b-3 is pushed to slide in the sliding groove 101c-1, so as to change the supporting angle of the second deflecting rod 102b-4, and thus change the supporting height of the lifting platform 201.
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 pushing away lifter 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 push-up rod 102a, extending the telescopic end of the push-up rod, slowly lifting the lifting platform 201 at the top of the push-up rod, and deflecting and unfolding the stabilizing piece 102b positioned below the lifting platform 201 in the process to stably lift up 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 charging module 203d in the lifting platform 201 can be connected with the charging interface of the unmanned aerial vehicle.
After unmanned aerial vehicle parks on elevating platform 201, withdraw elevating platform 201 that will carry unmanned aerial vehicle, shorten through control lifting rod 102a, the height of elevating platform 201 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 convenient to delivery 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);
the lifting assembly (102) comprises a lifting rod (102a) and a stabilizing piece (102b), and the stabilizing piece (102b) is connected with the end part of the lifting rod (102a) in a matching way;
the lifting unit (200) is positioned at the top of the lifting assembly (102) and comprises a lifting platform (201) and a driving piece (202) arranged at the end part of the lifting platform (201); and the number of the first and second groups,
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. An unmanned aerial vehicle lift transport platform for facilitating carrying of claim 1, wherein: the bottom plate assembly (101) comprises a bottom plate (101a), a boss (101b) positioned at the top of the bottom plate (101a), a mounting groove (101c) formed at the top of the boss (101b), and hinge tables (101d) arranged on the side walls of two sides of the boss (101 b);
the bottom of the groove cavity of the mounting groove (101c) is provided with a sliding groove (101 c-1);
the hinge base (302) can be in hinged fit with the hinge table (101 d).
3. An unmanned aerial vehicle lift transport platform for facilitating carrying of claim 2, wherein: the stabilizing piece (102b) comprises a connecting plate (102b-1), a first deflection rod (102b-2) symmetrically hinged to the side wall of the end part 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) with one end hinged to the sliding block (102b-3), and the other end of the second deflection rod (102b-4) is hinged to the side wall of the bottom of the lifting platform (201);
the bottom of the sliding block (102b-3) slides in the sliding groove (101 c-1);
one end of the lifting rod (102a) is connected to the connecting plate (102b-1), and the other end of the lifting rod is connected to the bottom side wall of the lifting platform (201).
4. An unmanned aerial vehicle lift transport platform convenient to carry according to claim 2 or 3, wherein: 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 for facilitating carrying 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 for facilitating carrying of claim 5, wherein: 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 convenient to carry according to any one of claims 1-3, 5 and 6, characterized in that: 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 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 convenient to carry according to any one of claims 1-3, 5 and 6, characterized in that: 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 for facilitating carrying 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 for facilitating carrying 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).
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