CN111959810A - Unmanned aerial vehicle intelligence platform of taking off and land - Google Patents

Unmanned aerial vehicle intelligence platform of taking off and land Download PDF

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Publication number
CN111959810A
CN111959810A CN202010897844.6A CN202010897844A CN111959810A CN 111959810 A CN111959810 A CN 111959810A CN 202010897844 A CN202010897844 A CN 202010897844A CN 111959810 A CN111959810 A CN 111959810A
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CN
China
Prior art keywords
unmanned aerial
aerial vehicle
horizontally arranged
fixed
wall
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Withdrawn
Application number
CN202010897844.6A
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Chinese (zh)
Inventor
秦立宝
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Nanjing New Changdian Information Technology Co ltd
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Nanjing New Changdian Information Technology Co ltd
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Publication date
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Priority to CN202010897844.6A priority Critical patent/CN111959810A/en
Publication of CN111959810A publication Critical patent/CN111959810A/en
Withdrawn legal-status Critical Current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
    • B60L53/10—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles characterised by the energy transfer between the charging station and the vehicle
    • B60L53/12—Inductive energy transfer
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
    • B63B35/00—Vessels or similar floating structures specially adapted for specific purposes and not otherwise provided for
    • B63B35/50—Vessels or floating structures for aircraft
    • B63B35/52—Nets, slipways or the like, for recovering aircraft from the water
    • 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
    • B64F1/12—Ground or aircraft-carrier-deck installations for anchoring aircraft
    • B64F1/125—Mooring or ground handling devices for helicopters
    • 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
    • Y02T90/14—Plug-in electric vehicles

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Ocean & Marine Engineering (AREA)
  • Power Engineering (AREA)
  • Transportation (AREA)
  • Forklifts And Lifting Vehicles (AREA)

Abstract

The invention belongs to the technical field of unmanned aerial vehicles, and particularly relates to an intelligent lifting platform of an unmanned aerial vehicle, aiming at the problem that the existing lifting platform of the unmanned aerial vehicle is easy to topple due to huge reaction force when taking off, the intelligent lifting platform of the unmanned aerial vehicle comprises a main case, wherein an installation groove is formed in the inner wall of the top of the main case, a horizontal fixing bottom plate is fixed at the bottom of the installation groove, four first holes are formed in the top of the fixing bottom plate, a vertically arranged electric push rod I is sleeved on each first hole, and a horizontally arranged lifting top seat is fixed between the tops of the four electric push rods I. According to the invention, the electric push rod II drives the bottom fixing base to rise, the compressor controls the inflation of the air pump to enable the sealing drill rod groove to be inflated, the fixing drill rod is inserted into the bottom position of the ground, the air hole valve controls the air suction pipe to suck air, the arc-shaped suction disc groove in the bottom position is firmly attracted to the ground, and the lifting platform is effectively prevented from toppling over due to impact force generated when the unmanned aerial vehicle takes off.

Description

Unmanned aerial vehicle intelligence platform of taking off and land
Technical Field
The invention relates to the technical field of unmanned aerial vehicles, in particular to an intelligent take-off and landing platform of an unmanned aerial vehicle.
Background
An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer.
Through the retrieval, chinese patent application number is CN 108082517A's patent, discloses a lift for unmanned aerial vehicle, which comprises a frame, the left and right sides symmetry of frame bottom is equipped with first mount and second mount, the top of frame is through first spring fixedly connected with backup pad, the top of backup pad is equipped with the blotter, the bottom of backup pad is rotated through the engaging lug and is connected with the bracing piece, the bottom fixedly connected with gyro wheel axle of bracing piece, the both ends of gyro wheel axle all are connected with the gyro wheel. Unmanned aerial vehicle elevating platform in the above-mentioned patent has following not enough: in the use of this unmanned aerial vehicle elevating platform, the bottom part is fixed shakiness, and unmanned aerial vehicle's reaction force is very big, makes the bottom elevating platform topple over very easily.
Disclosure of Invention
Based on the technical problem that the existing unmanned aerial vehicle lifting platform is prone to toppling under huge reaction force during take-off, the invention provides an intelligent take-off and landing platform for an unmanned aerial vehicle.
The invention provides an intelligent unmanned aerial vehicle lifting platform which comprises a main case, wherein an installation groove is formed in the inner wall of the top of the main case, a horizontal fixing bottom plate is fixed at the bottom of the installation groove, four first holes are formed in the top of the fixing bottom plate, a vertically arranged electric push rod I is sleeved in the first holes, a horizontally arranged lifting top seat is fixed between the tops of the four electric push rods I, vertically arranged lifting grooves are formed in both ends of the bottom of the main case, a vertically arranged electric push rod II is fixed on the inner wall of the top of the lifting groove, a horizontally arranged fixing base is connected with the bottom of the electric push rod II through bolts, horizontally inwards concave arc-shaped suction disc grooves are formed in both ends of the bottom of the fixing base, and a horizontally arranged suction pipe is sleeved at the top of the arc-shaped suction disc grooves, the utility model discloses a chip machine, including solid fixed base, arc sucking disc groove, blast pipe, gas pocket, gas vent valve, trachea, the bottom inner wall of mainframe box, the sealed borer groove of putting to one side is seted up to solid fixed base's bottom inner wall both ends position, and the blast pipe that the top intercommunication of sealed borer groove has the level to set up, the circumference inner wall seal cover in sealed borer groove has the solid fixed drill rod of putting to one side, the circumference inner wall top position of arc sucking disc groove is fixed with the filter plate that the level set up, gu fixed base's top inner wall is fixed with the gas pocket valve that the level set up, and the gas pocket valve cup joints with the one end of exhaust tube and blast pipe mutually, the trachea of vertical setting has been cup jointed at the top of gas pocket valve, the bottom inner wall of mainframe box is fixed with the battery that the level.
Preferably, the top positions of both ends of the mainframe box are respectively provided with a lifting groove which is horizontally arranged.
Preferably, the compressor that the bottom inner wall one end of mainframe box was fixed with the level and sets up, and mainframe box bottom inner wall other end is fixed with the air pump that the level set up, and the air pump is connected with the compressor, cup joints with the trachea through the connecting pipe mutually of air pump.
Preferably, a horizontally arranged supporting middle plate is fixed at the middle position between the inner walls of the two sides of the main case through a bolt.
Preferably, a horizontally arranged limiting clamping groove is formed in the middle of the bearing middle plate.
Preferably, the top positions of the inner walls of the two sides of the mainframe box are both provided with horizontally arranged sliding side grooves, and a horizontally arranged sealing top plate is clamped between the two sliding side grooves in a sliding manner.
Preferably, the other end of mainframe box has the interface that charges that the level set up through bolted connection, and the interface that charges passes through wire and controller electric connection.
Preferably, the middle position of the inner wall of the bottom of the main case is connected with a horizontally arranged wireless charging seat through a bolt.
Preferably, the bottom position all around of mainframe box all sets up the recess of accomodating of vertical setting, and the buoyancy curb plate of vertical setting has been cup jointed through the bearing to the bottom between the both sides inner wall of accomodating the recess, and accomodate one side inner wall of recess and install the driving motor that the level set up, and driving motor's output shaft is connected with one side bottom of buoyancy curb plate.
Preferably, the bottom position of the buoyancy side plate is fixed with a horizontally arranged inflatable air bag, the top of the inflatable air bag, which is positioned on the fixed drill rod, is connected with an air pipe, and the air pipe is communicated with an air pump.
Compared with the prior art, the invention provides an intelligent take-off and landing platform of an unmanned aerial vehicle, which has the following beneficial effects:
1. this unmanned aerial vehicle intelligence platform that takes off and land drives bottom unable adjustment base through setting up bottom electric putter two and rises, and inflation of compressor control air pump can make sealed borer groove aerify for fixed drill rod inserts the bottom position to ground, and the gas pocket valve control exhaust tube is breathed in, makes the actuation that the arc sucking disc groove of bottom position is firm ground, and the effectual impact force that produces when preventing unmanned aerial vehicle from taking off makes the platform that takes off and land empty.
2. This unmanned aerial vehicle intelligence platform that takes off and land places the top position at the lift footstock through the bottom position that sets up unmanned aerial vehicle, and the decline of electric putter one can make unmanned aerial vehicle descend, fixes unmanned aerial vehicle's profile through spacing draw-in groove for unmanned aerial vehicle is fixed stable, and the wireless charging seat of bottom position can carry out the process of charging to unmanned aerial vehicle's bottom position.
3. This unmanned aerial vehicle intelligence platform that takes off and land all has seted up through setting up the outer wall bottom all around at the mainframe box and has accomodate the recess, opens buoyancy curb plate all around through driving motor at the in-process that the waters was surveyed, and the rethread air pump is aerifyd, aerifys inflating the gasbag for whole elevating platform floats, and the unmanned aerial vehicle of the user of being convenient for in the waters goes up and down to use.
Drawings
Fig. 1 is a schematic view of an overall structure of an intelligent take-off and landing platform of an unmanned aerial vehicle, which is provided by the invention;
fig. 2 is a schematic front sectional view of an intelligent take-off and landing platform of an unmanned aerial vehicle according to the present invention;
fig. 3 is a schematic structural view of a fixed base of an intelligent take-off and landing platform of an unmanned aerial vehicle, which is provided by the invention;
fig. 4 is a schematic structural view of a buoyancy side plate of the intelligent take-off and landing platform of the unmanned aerial vehicle.
In the figure: 1 electric push rod I, 2 mainframe boxes, 3 limiting clamping grooves, 4 closed top plates, 5 lifting top seats, 6 bearing middle plates, 7 sliding side grooves, 8 lifting grooves, 9 charging interfaces, 10 fixing bottom plates, 11 fixing bases, 12 lifting grooves, 13 electric push rods II, 14 chip chambers, 15 controllers, 16 wireless charging seats, 17 air pipes, 18 air pumps, 19 compressors, 20 fixing drill rods, 21 sealing drill rod grooves, 22 exhaust pipes, 23 exhaust pipes, 24 pneumatic control valves, 25 arc suction disc grooves, 26 filter screen plates, 27 driving motors, 28 storage grooves, 29 inflatable air bags and 30 buoyancy side plates.
Detailed Description
The technical solution of the present patent will be described in further detail with reference to the following embodiments.
Reference will now be made in detail to embodiments of the present patent, examples of which are illustrated in the accompanying drawings, wherein like or similar reference numerals refer to the same or similar elements or elements having the same or similar function throughout. The embodiments described below with reference to the drawings are exemplary only for the purpose of explaining the present patent and are not to be construed as limiting the present patent.
In the description of this patent, it is to be understood that the terms "center," "upper," "lower," "front," "rear," "left," "right," "vertical," "horizontal," "top," "bottom," "inner," "outer," and the like are used in the orientations and positional relationships indicated in the drawings for the convenience of describing the patent and for the simplicity of description, and are not intended to indicate or imply that the referenced devices or elements must have a particular orientation, be constructed and operated in a particular orientation, and are not to be considered limiting of the patent.
In the description of this patent, it is noted that unless otherwise specifically stated or limited, the terms "mounted," "connected," and "disposed" are to be construed broadly and can include, for example, fixedly connected, disposed, detachably connected, disposed, or integrally connected and disposed. The specific meaning of the above terms in this patent may be understood by those of ordinary skill in the art as appropriate.
Example 1:
an intelligent lifting platform of an unmanned aerial vehicle is disclosed, as shown in fig. 1-3, comprising a main case 2, wherein the inner wall of the top of the main case 2 is provided with an installation groove, the bottom of the installation groove is fixed with a horizontal fixed bottom plate 10, the top of the fixed bottom plate 10 is provided with four first holes, the first holes are sleeved with vertically arranged electric push rods 1, a horizontally arranged lifting footstock 5 is fixed between the tops of the four electric push rods 1, the two ends of the bottom of the main case 2 are both provided with vertically arranged lifting grooves 12, the inner wall of the top of the lifting grooves 12 is fixed with vertically arranged electric push rods 13, the bottom of the electric push rods 13 is connected with a horizontally arranged fixed base 11 through bolts, the two ends of the bottom of the fixed base 11 are both provided with horizontally inwards concave arc-shaped suction cup grooves 25, the top of the arc-shaped suction cup grooves 25 is sleeved with a horizontally arranged suction pipe 22, the utility model discloses a chip chamber 14 of vertical setting is seted up to unable adjustment base 11's bottom inner wall both ends position seted up inclined sealed borer groove 21, and the blast pipe 23 that the top intercommunication of sealed borer groove 21 has the level to set up, the circumference inner wall seal cover of sealed borer groove 21 has inclined fixed drill rod 20, the circumference inner wall top position of arc sucking disc groove 25 is fixed with the filter plate 26 that the level set up, unable adjustment base 11's top inner wall is fixed with the gas pocket valve 24 that the level set up, and gas pocket valve 24 cup joints mutually with the one end of exhaust tube 22 and blast pipe 23, the trachea 17 of vertical setting has been cup jointed at gas pocket valve 24's top, the bottom inner wall of mainframe box 2 is fixed with the battery of level setting, the chip chamber 14 of vertical setting is seted up to the one end inner wall of mainframe box 2, and the controller 15 of vertical setting is installed to the one.
The top positions of two ends of the mainframe box 2 are both provided with a horizontally arranged lifting groove 8, one end of the bottom inner wall of the mainframe box 2 is fixed with a horizontally arranged compressor 19, the other end of the bottom inner wall of the mainframe box 2 is fixed with a horizontally arranged air pump 18, the air pump 18 is connected with the compressor 19, the air pump 18 is sleeved with an air pipe 17 through a connecting pipe, a horizontally arranged bearing middle plate 6 is fixed at the middle position between the two side inner walls of the mainframe box 2 through a bolt, a horizontally arranged limiting clamping groove 3 is arranged at the middle position of the bearing middle plate 6, sliding side grooves 7 are arranged at the top positions of the two side inner walls of the mainframe box 2, a horizontally arranged sealing top plate 4 is clamped between the two sliding side grooves 7 in a sliding manner, the other end of the mainframe box 2 is connected with a horizontally arranged charging interface 9 through a bolt, and the charging interface 9 is electrically connected with a controller 15 through a wire, the middle position of the inner wall of the bottom of the mainframe box 2 is connected with a horizontally arranged wireless charging seat 16 through a bolt.
In the embodiment, when the intelligent lifting platform of the unmanned aerial vehicle is used, an operator firstly fixes and stabilizes the intelligent lifting platform and places the intelligent lifting platform at a position waiting for use, in the using process, the bottom position of the unmanned aerial vehicle is placed at the top position of the lifting top seat 5, the descending of the electric push rod I1 can enable the unmanned aerial vehicle to descend, the profile of the unmanned aerial vehicle is fixed through the limiting clamping groove 3, so that the unmanned aerial vehicle is fixed and stabilized, the wireless charging seat 16 at the bottom position can charge the bottom position of the unmanned aerial vehicle, in the using process, the electric push rod II 13 at the bottom drives the fixing base 11 to ascend, the compressor 19 controls the inflation of the air pump 18 to inflate the sealing drill rod groove 21, so that the fixing drill rod 20 is inserted into the bottom position of the ground, the air hole valve 24 controls the air suction pipe 22 to suck air, so that the arc-shaped suction disc groove 25 at the bottom position is firmly attracted, the impact force that produces when effectually preventing unmanned aerial vehicle from taking off makes the platform of taking off and land topple over, and the raising of electric putter one 1 can make unmanned aerial vehicle rise, can carry out the action of taking off through unmanned aerial vehicle's self pneumatics.
Example 2:
the utility model provides an unmanned aerial vehicle intelligence platform of taking off and land, as shown in fig. 1-4, the bottom position all around of mainframe box 2 has all been seted up the recess 28 of accomodating of vertical setting, the bottom between the both sides inner wall of accomodating recess 28 has cup jointed the buoyancy curb plate 30 of vertical setting through the bearing, and accomodate the driving motor 27 that one side inner wall of recess 28 installed the level and set up, and driving motor 27's output shaft is connected with one side bottom of buoyancy curb plate 30, the bottom rigidity of buoyancy curb plate 30 has the air bag 29 of aerifing of level setting, and the top that is located fixed drill rod 20 of aerifing air bag 29 is connected with the trachea, and the trachea is linked together with air.
This embodiment is when using, on the basis of embodiment one, has all seted up storage groove 28 in the outer wall bottom all around of mainframe box 2, opens buoyancy curb plate 30 all around through driving motor 27 at the in-process that the waters was surveyed, and rethread air pump 18 is aerifyd, inflates inflatable airbag 29 for whole elevating platform floats, and the unmanned aerial vehicle of the user of being convenient for in the waters goes up and down to use.
The above description is only for the preferred embodiment of the present invention, but the scope of the present invention is not limited thereto, and any person skilled in the art should be considered to be within the technical scope of the present invention, and the technical solutions and the inventive concepts thereof according to the present invention should be equivalent or changed within the scope of the present invention.

Claims (10)

1. An intelligent unmanned aerial vehicle lifting platform comprises a main case (2), wherein an installation groove is formed in the inner wall of the top of the main case (2), a horizontal fixing bottom plate (10) is fixed to the bottom of the installation groove, four first holes are formed in the top of the fixing bottom plate (10), a vertically arranged electric push rod I (1) is sleeved on the first holes, a horizontally arranged lifting top seat (5) is fixed between the tops of the four electric push rod I (1), the intelligent unmanned aerial vehicle lifting platform is characterized in that vertically arranged lifting grooves (12) are formed in the two ends of the bottom of the main case (2), vertically arranged electric push rod II (13) are fixed to the inner wall of the top of each lifting groove (12), a horizontally arranged fixing base (11) is connected to the bottom of each electric push rod II (13) through a bolt, an arc-shaped suction disc groove (25) which is horizontally inwards concave is formed in the two ends of the bottom of each fixing base (11), an air exhaust pipe (22) which is horizontally arranged is sleeved at the top of the arc-shaped sucker groove (25), inclined sealing drill rod grooves (21) are formed in the two ends of the inner wall of the bottom of the fixed base (11), an air exhaust pipe (23) which is horizontally arranged is communicated with the top of each sealing drill rod groove (21), inclined fixing drill rods (20) are hermetically sleeved on the inner wall of the circumference of each sealing drill rod groove (21), a horizontally arranged filter screen plate (26) is fixed at the top of the inner wall of the circumference of the arc-shaped sucker groove (25), a horizontally arranged air hole valve (24) is fixed on the inner wall of the top of the fixed base (11), the air hole valve (24) is sleeved with one end of each air exhaust pipe (22) and one end of each air exhaust pipe (23), a vertically arranged air pipe (17) is sleeved on the top of the air hole valve (24), and a horizontally arranged storage battery is fixed on the inner wall of the bottom of the, chip cavity (14) of vertical setting are seted up to the one end inner wall of mainframe box (2), and the one end inner wall of chip cavity (14) installs controller (15) of vertical setting, controller (15) pass through wire electric connection with the battery.
2. The intelligent unmanned aerial vehicle lifting platform according to claim 1, wherein the top positions of the two ends of the main cabinet (2) are provided with lifting grooves (8) which are horizontally arranged.
3. The intelligent unmanned aerial vehicle taking-off and landing platform of claim 1, wherein a horizontally arranged compressor (19) is fixed to one end of the inner wall of the bottom of the main case (2), a horizontally arranged air pump (18) is fixed to the other end of the inner wall of the bottom of the main case (2), the air pump (18) is connected with the compressor (19), and the air pump (18) is sleeved with the air pipe (17) through a connecting pipe.
4. The intelligent unmanned aerial vehicle lifting platform of claim 1, wherein a horizontally arranged supporting middle plate (6) is fixed at the middle position between the inner walls of the two sides of the main case (2) through bolts.
5. The intelligent unmanned aerial vehicle taking-off and landing platform of claim 4, wherein a horizontally arranged limiting clamping groove (3) is formed in the middle of the bearing middle plate (6).
6. The intelligent unmanned aerial vehicle lifting platform of claim 1, wherein the top positions of the inner walls of the two sides of the main cabinet (2) are provided with horizontally arranged sliding side grooves (7), and a horizontally arranged sealing top plate (4) is clamped between the two sliding side grooves (7) in a sliding manner.
7. The intelligent unmanned aerial vehicle lifting platform of claim 6, wherein the other end of the main chassis (2) is connected with a horizontally arranged charging interface (9) through a bolt, and the charging interface (9) is electrically connected with the controller (15) through a wire.
8. The intelligent unmanned aerial vehicle taking-off and landing platform of claim 6, wherein a horizontally arranged wireless charging seat (16) is connected to the middle position of the inner bottom wall of the main chassis (2) through a bolt.
9. The intelligent unmanned aerial vehicle lifting platform of claim 1, wherein the bottom of the periphery of the main cabinet (2) is provided with a vertically arranged storage groove (28), the bottom between the inner walls of the two sides of the storage groove (28) is sleeved with a vertically arranged buoyancy side plate (30) through a bearing, a horizontally arranged driving motor (27) is installed on the inner wall of one side of the storage groove (28), and the output shaft of the driving motor (27) is connected with the bottom of one side of the buoyancy side plate (30).
10. The intelligent unmanned aerial vehicle lifting platform according to claim 9, wherein a horizontally arranged air inflation bag (29) is fixed at the bottom of the buoyancy side plate (30), and an air pipe is connected to the top of the air inflation bag (29) on the fixed drill rod (20) and communicated with the air pump (18).
CN202010897844.6A 2020-08-31 2020-08-31 Unmanned aerial vehicle intelligence platform of taking off and land Withdrawn CN111959810A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202010897844.6A CN111959810A (en) 2020-08-31 2020-08-31 Unmanned aerial vehicle intelligence platform of taking off and land

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202010897844.6A CN111959810A (en) 2020-08-31 2020-08-31 Unmanned aerial vehicle intelligence platform of taking off and land

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Publication Number Publication Date
CN111959810A true CN111959810A (en) 2020-11-20

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CN202010897844.6A Withdrawn CN111959810A (en) 2020-08-31 2020-08-31 Unmanned aerial vehicle intelligence platform of taking off and land

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112874367A (en) * 2021-01-19 2021-06-01 青岛左岸传媒有限公司 Outdoor electronic communication equipment wireless charging device based on Internet of things
CN113109356A (en) * 2021-04-09 2021-07-13 徐州盛科半导体科技有限公司 Mobile platform for detecting semiconductor packaging defects

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112874367A (en) * 2021-01-19 2021-06-01 青岛左岸传媒有限公司 Outdoor electronic communication equipment wireless charging device based on Internet of things
CN112874367B (en) * 2021-01-19 2022-07-26 四川泰立智汇科技有限公司 Outdoor electronic communication equipment wireless charging device based on Internet of things
CN113109356A (en) * 2021-04-09 2021-07-13 徐州盛科半导体科技有限公司 Mobile platform for detecting semiconductor packaging defects

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