CN114197933B - Unmanned aerial vehicle nest - Google Patents

Unmanned aerial vehicle nest Download PDF

Info

Publication number
CN114197933B
CN114197933B CN202111589571.XA CN202111589571A CN114197933B CN 114197933 B CN114197933 B CN 114197933B CN 202111589571 A CN202111589571 A CN 202111589571A CN 114197933 B CN114197933 B CN 114197933B
Authority
CN
China
Prior art keywords
arc
shaped upper
aerial vehicle
unmanned aerial
sealing ring
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.)
Active
Application number
CN202111589571.XA
Other languages
Chinese (zh)
Other versions
CN114197933A (en
Inventor
黄立
陈红胜
张超峰
凃永义
余志勇
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Wuhan Gaode Aircraft Technology Co ltd
Original Assignee
Wuhan Gaode Aircraft Technology 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 Wuhan Gaode Aircraft Technology Co ltd filed Critical Wuhan Gaode Aircraft Technology Co ltd
Priority to CN202111589571.XA priority Critical patent/CN114197933B/en
Publication of CN114197933A publication Critical patent/CN114197933A/en
Application granted granted Critical
Publication of CN114197933B publication Critical patent/CN114197933B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04H—BUILDINGS OR LIKE STRUCTURES FOR PARTICULAR PURPOSES; SWIMMING OR SPLASH BATHS OR POOLS; MASTS; FENCING; TENTS OR CANOPIES, IN GENERAL
    • E04H6/00—Buildings for parking cars, rolling-stock, aircraft, vessels or like vehicles, e.g. garages
    • E04H6/44—Buildings for parking cars, rolling-stock, aircraft, vessels or like vehicles, e.g. garages for storing aircraft
    • 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
    • B60L53/14—Conductive energy transfer
    • B60L53/16—Connectors, e.g. plugs or sockets, specially adapted for charging electric vehicles
    • 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
    • B60L53/302—Cooling of charging equipment
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F1/00—Ground or aircraft-carrier-deck installations
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/10—Propulsion
    • B64U50/19—Propulsion using electrically powered motors
    • E—FIXED CONSTRUCTIONS
    • E01—CONSTRUCTION OF ROADS, RAILWAYS, OR BRIDGES
    • E01F—ADDITIONAL WORK, SUCH AS EQUIPPING ROADS OR THE CONSTRUCTION OF PLATFORMS, HELICOPTER LANDING STAGES, SIGNS, SNOW FENCES, OR THE LIKE
    • E01F3/00—Landing stages for helicopters, e.g. located above buildings
    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04B—GENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
    • E04B7/00—Roofs; Roof construction with regard to insulation
    • E04B7/08—Vaulted roofs
    • E04B7/10—Shell structures, e.g. of hyperbolic-parabolic shape; Grid-like formations acting as shell structures; Folded structures
    • E04B7/102—Shell structures
    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04B—GENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
    • E04B7/00—Roofs; Roof construction with regard to insulation
    • E04B7/16—Roof structures with movable roof parts
    • E04B7/163—Roof structures with movable roof parts characterised by a pivoting movement of the movable roof parts
    • E—FIXED CONSTRUCTIONS
    • E04—BUILDING
    • E04H—BUILDINGS OR LIKE STRUCTURES FOR PARTICULAR PURPOSES; SWIMMING OR SPLASH BATHS OR POOLS; MASTS; FENCING; TENTS OR CANOPIES, IN GENERAL
    • E04H6/00—Buildings for parking cars, rolling-stock, aircraft, vessels or like vehicles, e.g. garages
    • E04H6/42—Devices or arrangements peculiar to garages, not covered elsewhere, e.g. securing devices, safety devices, monitoring and operating schemes; centering devices
    • 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
    • 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
    • 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
    • Y02T90/16—Information or communication technologies improving the operation of electric vehicles
    • 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
    • Y02T90/16—Information or communication technologies improving the operation of electric vehicles
    • Y02T90/167—Systems integrating technologies related to power network operation and communication or information technologies for supporting the interoperability of electric or hybrid vehicles, i.e. smartgrids as interface for battery charging of electric vehicles [EV] or hybrid vehicles [HEV]
    • 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
    • Y04—INFORMATION OR COMMUNICATION TECHNOLOGIES HAVING AN IMPACT ON OTHER TECHNOLOGY AREAS
    • Y04S—SYSTEMS INTEGRATING TECHNOLOGIES RELATED TO POWER NETWORK OPERATION, COMMUNICATION OR INFORMATION TECHNOLOGIES FOR IMPROVING THE ELECTRICAL POWER GENERATION, TRANSMISSION, DISTRIBUTION, MANAGEMENT OR USAGE, i.e. SMART GRIDS
    • Y04S30/00—Systems supporting specific end-user applications in the sector of transportation
    • Y04S30/10—Systems supporting the interoperability of electric or hybrid vehicles
    • Y04S30/12—Remote or cooperative charging

Abstract

The invention discloses an unmanned aerial vehicle nest, which relates to the technical field of unmanned aerial vehicle hangars, and comprises a flying platform body, wherein the table surface of the flying platform body is used for stopping an unmanned aerial vehicle, a cover body is arranged at the upper part of the flying platform body, a charging motor cabin is formed between the cover body and the flying platform body, the cover body is formed by buckling two arc-shaped upper covers, a waterproof sealing assembly is arranged at the buckling position of the two arc-shaped upper covers, the waterproof sealing assembly comprises a water guide groove, a first sealing ring, a third sealing ring and a water shielding cover, the first sealing ring is arranged between opposite abutting edges of the two arc-shaped upper covers, the water guide groove is arranged between the two arc-shaped upper covers, and the third sealing ring is arranged on the water guide groove and is used for sealing a gap between the water guide groove and the arc-shaped upper covers. According to the invention, the hangar rain cover is opened and closed through the rotary unmanned aerial vehicle hangar mechanism, the unmanned aerial vehicle is rapidly charged on the hangar parking platform, and the sealing waterproofness is improved by adopting multiple sealing.

Description

Unmanned aerial vehicle nest
Technical Field
The invention relates to the technical field of unmanned aerial vehicle libraries, in particular to an unmanned aerial vehicle nest.
Background
The unmanned aerial vehicle is an unmanned aerial vehicle which is operated by using a radio remote control device and a self-contained program control device. The machine has no cockpit, but is provided with an automatic pilot, a program control device and other devices. Personnel on the ground, ships or on a master remote control station track, position, remotely control, telemeter and digitally transmit the remote control station through radar and other equipment. Can take off like a common plane under radio remote control or launch and lift off by using a boosting rocket, and can also be brought into the air by a master machine to put in flight. When recovered, the aircraft can automatically land in the same way as a normal aircraft landing process.
The current unmanned aerial vehicle hangar rain-proof lid adopts slide rail formula metal structure and the mode of charging to realize wireless charging or shut down free state on the platform more, and it is difficult to accomplish sealedly and lead to receiving the rainwater influence easily to wet and influence the charging.
Disclosure of Invention
The invention aims to provide an unmanned aerial vehicle nest for solving the problems in the background technology.
In order to achieve the above purpose, the present invention provides the following technical solutions:
the utility model provides an unmanned aerial vehicle aircraft nest, includes the flight platform body, the flight platform body is the semicylindrical structure, and the mesa of flight platform body is used for supplying unmanned aerial vehicle to stop, and the flight platform body upper portion is equipped with the cover body, forms a motor charging cabin between the cover body and the flight platform body, the cover body is closed and is detained by two arc upper covers, an arc upper cover corner is connected with the rotation of flight platform body end wall through the axis of rotation, and the knot department of closing of two arc upper covers is equipped with waterproof seal assembly, waterproof seal assembly includes guiding gutter, first sealing washer, third sealing washer and covers water, it can cover the strip seam that two arc upper covers closed and detained and produce along the edge that one of them arc upper cover closed and detained to cover water, first sealing washer is established between two arc upper covers relatively supporting the holding limit and is connected with one of them arc upper cover supporting limit, the guiding gutter is established between two arc upper covers and one end is connected with one of them arc upper cover lateral part, the third is established and is used to seal up with the guiding gutter between the sealing washer.
Based on the technical scheme, the invention also provides the following optional technical schemes:
in one alternative: the waterproof sealing assembly further comprises a second sealing ring, and the second sealing ring is arranged along the edge of the bottom of the arc-shaped upper cover; the second sealing ring can be propped against the edge of the flying platform body to seal when the two arc-shaped upper covers are buckled.
In one alternative: the unmanned aerial vehicle lifting device is characterized in that two centering mechanisms and push rod pieces which are symmetrical with each other by taking the unmanned aerial vehicle stopping area as the center are arranged on the table surface of the flying table body, the centering mechanisms can move from two sides to the center of the unmanned aerial vehicle stopping area on the flying table body, and the push rod pieces are arranged on the centering mechanisms.
In one alternative: the pushing rod piece is provided with a charging seat and a lamp belt, the charging seat corresponds to a charging interface of the unmanned aerial vehicle, and the lamp belt can be electrified to illuminate the charging cabin.
In one alternative: the inside fan and the heater of still being provided with of charging cabin, the fan is used for leading in the radiating air current to charging cabin inside and the heater is used for heating charging cabin inside temperature.
In one alternative: and a UPS power supply is further arranged in the charging cabin and is used for temporarily charging under the condition of power failure in the whole charging cabin.
Compared with the prior art, the invention has the following beneficial effects:
1. by using the quick charging mode on the rotary unmanned aerial vehicle hangar and the shutdown platform, the overall dimension of the hangar can be reduced, the charging area can be sealed, charging can be carried out on any weather, the operation efficiency is improved, and the cost of the hangar can be reduced. And the occupied area is smaller when two or more expansion is carried out;
2. the arc upper cover seals the charging motor cabin of the machine nest in a mode of combining the water guide grooves, the sealing rings and the water shielding cover, and the sealing is tight and effectively plays a role in water prevention.
3. According to the invention, the hangar rain cover is opened and closed through the rotary unmanned aerial vehicle hangar mechanism, the unmanned aerial vehicle is rapidly charged on the hangar parking platform, and the sealing waterproofness is improved by adopting multiple sealing.
Drawings
Fig. 1 is a schematic view of the nest cover structure in an embodiment of the invention.
Fig. 2 is a schematic diagram of the structure of the cover of the machine nest according to an embodiment of the present invention.
Fig. 3 is a schematic view of a waterproof seal assembly according to an embodiment of the present invention.
Fig. 4 is a schematic view of a partial enlarged structure in fig. 3.
Fig. 5 is a schematic view showing an internal structure of a flight deck in one embodiment of the present invention.
Reference numerals annotate: the device comprises an arc-shaped upper cover 1, a base 3, a flying platform body 4, a centering mechanism 5, a push rod piece 51, a charging seat 52, a lamp belt 53, an unmanned aerial vehicle 6, a camera 7, a fan 8, a heater 9, a UPS power supply 10, a rotating shaft 12, a water guide groove 13, a first sealing ring 14, a second sealing ring 23, a third sealing ring 24 and a water shielding cover 25.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more apparent, the present invention will be described in further detail with reference to the accompanying drawings and examples; in the drawings or description, similar or identical parts are provided with the same reference numerals, and in practical applications, the shape, thickness or height of each part may be enlarged or reduced. The examples set forth herein are intended to be illustrative of the invention and are not intended to limit the scope of the invention. Any obvious modifications or alterations to the invention, as would be apparent, are made without departing from the spirit and scope of the present invention.
Example 1:
as shown in fig. 1-4, this embodiment provides an unmanned aerial vehicle nest, including a flight platform body 4, the flight platform body 4 is in a semi-cylindrical structure, the table top of the flight platform body 4 is used for stopping an unmanned aerial vehicle 6, a cover body is arranged at the upper part of the flight platform body 4, a charging motor cabin is formed between the cover body and the flight platform body 4, the cover body is formed by buckling two arc-shaped upper covers 1, a corner of the arc-shaped upper covers 1 is rotationally connected with the end wall of the flight platform body 4 through a rotating shaft 12, a waterproof sealing assembly is arranged at the buckling position of the two arc-shaped upper covers 1, the waterproof sealing assembly comprises a water guiding groove 13, a first sealing ring 14, a third sealing ring 24 and a water shielding cover 25, the water shielding cover 25 is arranged along the buckling edge of one arc-shaped upper cover 1, when the two arc-shaped upper covers 1 are buckled, the water shielding cover 25 can cover a strip seam generated by buckling the two arc-shaped upper covers 1, the first sealing ring 14 is arranged between the opposite propping edges of the two arc-shaped upper covers 1 and is connected with one of the two arc-shaped upper covers 1, the two arc-shaped upper covers 1 are connected with one another arc-shaped upper covers 13, and the two arc-shaped upper covers 1 are connected with one another arc-shaped upper cover 13, and one end is connected with the water guiding groove 13 by the arc-shaped upper covers 1, and the other arc-shaped upper covers are sealed with one another arc-shaped upper cover 13;
in the embodiment, the two rotating shafts 12 are driven to rotate by an external transmission mechanism, so that the two arc-shaped upper covers 1 rotate relatively or reversely, the two arc-shaped upper covers 1 rotate reversely and rotate to the side parts of the flying platform body 4, and the top of the flying platform body 4 is opened to facilitate the unmanned aerial vehicle 6 to stop; the two arc-shaped upper covers 1 rotate relatively to slowly realize buckling, so that the top of the flying platform body 4 is covered, the functions of water blocking and rain prevention can be achieved, secondly, when the two arc-shaped upper covers 1 buckle, the first sealing ring 14 receives the extrusion of the abutting edges of the two arc-shaped upper covers 1 to increase the tightness, the water shielding cover 25 covers the strip seams generated by buckling the two arc-shaped upper covers 1, the strip seams generated by buckling the two arc-shaped upper covers 1 can be sealed to improve the waterproof effect, and the water guide groove 13 can guide the water stain passing through the strip seams generated by buckling the two arc-shaped upper covers 1 to the bottom edge of the arc-shaped upper covers 1; simultaneously, the first sealing ring 14 seals a gap generated by the abutting of the side part of the water guide groove 13 and the bottom of the arc-shaped upper cover 1 under the action of extrusion; the bottom of the flying platform body 4 is also provided with a base 3 for supporting the whole charging cabin; a two-dimensional code or RTK positioning or infrared induction positioning is arranged in a landing area of the unmanned aerial vehicle 6 on the flying platform 4;
in one embodiment, as shown in fig. 3 and 4, the waterproof sealing assembly further comprises a second sealing ring 23, and the second sealing ring 23 is disposed along the bottom edge of the arc-shaped upper cover 1; the second sealing ring 23 can be propped against and sealed with the edge of the flying platform body 4 when the two arc-shaped upper covers 1 are buckled; rainwater is prevented from entering the flying platform body 4 from a gap between the bottom of the arc-shaped upper cover 1 and the flying platform body 4;
in one embodiment, as shown in fig. 2, two centering mechanisms 5 and push rod pieces 51 which are symmetrical with the landing area of the unmanned aerial vehicle 6 as the center are arranged on the table surface of the flying table body 4, the centering mechanisms 5 can move from two sides to the center of the landing area of the unmanned aerial vehicle 6 on the flying table body 4, and the push rod pieces 51 are arranged on the centering mechanisms 5; the foot rest of the unmanned aerial vehicle 6 is provided with the balls, and the centering mechanism 5 moves towards the landing area of the unmanned aerial vehicle 6 at the same time, so that the pushing rod piece 51 can push the unmanned aerial vehicle 6 to the center of the landing area, and quick centering is realized; the centering mechanism 5 can be a telescopic pushing rod piece or other mechanisms capable of realizing linear movement;
in one embodiment, as shown in fig. 2, the push rod piece 51 is provided with a charging seat 52 and a lamp belt 53, the charging seat 52 corresponds to a charging interface of the unmanned aerial vehicle 6, and the lamp belt 53 can be electrified to illuminate the charging cabin; when the push rod member 51 moves toward the parking area of the unmanned aerial vehicle 6, the charging seat 52 can be docked with the charging interface of the unmanned aerial vehicle 6 to facilitate charging the unmanned aerial vehicle 6.
In one embodiment, as shown in fig. 2, at least one camera 7 is further disposed on the table surface of the flying platform body 4, and the camera 7 is used for monitoring the environment inside the charging cabin;
in one embodiment, as shown in fig. 4, a fan 8 and a heater 9 are further arranged inside the charging cabin, the fan 8 is used for guiding heat dissipation air flow into the charging cabin, and the heater 9 is used for heating the temperature inside the charging cabin; the temperature inside the charging cabin is regulated by a fan 8 and a heater 9.
In one embodiment, as shown in fig. 4, a UPS power source 10 is further disposed inside the charging cabin, and the UPS power source 10 is used for temporary charging when the power is off in the entire charging cabin, so as to be used as a standby power source.
The foregoing is merely specific embodiments of the disclosure, but the protection scope of the disclosure is not limited thereto, and any person skilled in the art can easily think about changes or substitutions within the technical scope of the disclosure, and it is intended to cover the scope of the disclosure. Therefore, the protection scope of the present disclosure shall be subject to the protection scope of the claims.

Claims (4)

1. The unmanned aerial vehicle nest comprises a flying platform body, wherein the flying platform body is of a semi-cylindrical structure, a table top of the flying platform body is used for stopping an unmanned aerial vehicle, a cover body is arranged on the upper part of the flying platform body, and a charging motor cabin is formed between the cover body and the flying platform body;
a waterproof sealing component is arranged at the buckling position of the two arc-shaped upper covers;
the waterproof sealing assembly comprises a water guide groove, a first sealing ring, a second sealing ring, a third sealing ring and a water shielding cover;
the water shielding cover is arranged along the edge of one of the arc-shaped upper cover closing buckles, and when the two arc-shaped upper covers are closed, the water shielding cover can cover the strip seams generated by the two arc-shaped upper cover closing buckles;
the first sealing ring is arranged between the opposite propping edges of the two arc-shaped upper covers and is connected with one of the propping edges of the arc-shaped upper covers;
the water guide groove is arranged between the two arc-shaped upper covers, and one end of the water guide groove is connected with the side part of one of the arc-shaped upper covers;
the third sealing ring is arranged on the water guide groove and is used for sealing a gap between the water guide groove and the arc-shaped upper cover;
the second sealing ring is arranged along the bottom edge of the arc-shaped upper cover; the second sealing ring can be propped against and sealed with the edge of the flying platform body when the two arc-shaped upper covers are buckled;
the inside fan and the heater of still being provided with of charging cabin, the fan is used for leading in the radiating air current to charging cabin inside and the heater is used for heating charging cabin inside temperature.
2. The unmanned aerial vehicle nest of claim 1, wherein the table top of the flying table body is provided with two centering mechanisms and pushing rods which are symmetrical with the unmanned aerial vehicle landing area as a center;
the centering mechanism can move from two sides to the center of the unmanned aerial vehicle stopping area on the flying platform body, and the push rod piece is arranged on the centering mechanism.
3. The unmanned aerial vehicle nest of claim 2, wherein the pusher member is provided with a charging seat and a light strip, the charging seat corresponds to a charging interface of the unmanned aerial vehicle, and the light strip can be energized to illuminate the charging cabin.
4. The unmanned aerial vehicle nest of claim 1, wherein a UPS power source is further provided inside the charging cabin, the UPS power source being configured to temporarily charge the battery under power outage in the entire charging cabin.
CN202111589571.XA 2021-12-23 2021-12-23 Unmanned aerial vehicle nest Active CN114197933B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202111589571.XA CN114197933B (en) 2021-12-23 2021-12-23 Unmanned aerial vehicle nest

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202111589571.XA CN114197933B (en) 2021-12-23 2021-12-23 Unmanned aerial vehicle nest

Publications (2)

Publication Number Publication Date
CN114197933A CN114197933A (en) 2022-03-18
CN114197933B true CN114197933B (en) 2023-10-31

Family

ID=80656209

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202111589571.XA Active CN114197933B (en) 2021-12-23 2021-12-23 Unmanned aerial vehicle nest

Country Status (1)

Country Link
CN (1) CN114197933B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114537691B (en) * 2022-04-06 2023-06-30 重庆水利电力职业技术学院 Unmanned aerial vehicle nest with dampproofing function for power line inspection

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2015053523A (en) * 2014-12-02 2015-03-19 オリンパス株式会社 Waterproof apparatus
CN105221003A (en) * 2015-10-21 2016-01-06 江苏南方雄狮建设工程有限公司 A kind of flat-open door and window
WO2017029611A1 (en) * 2015-08-17 2017-02-23 H3 Dynamics Holdings Pte. Ltd. Drone box
CN209225411U (en) * 2018-08-30 2019-08-09 一飞智控(天津)科技有限公司 Rechargeable type logistics unmanned plane logistics airplane parking area platform
CN209667390U (en) * 2019-07-11 2019-11-22 广西计算中心有限责任公司 VTOL fixed-wing unmanned plane automatic storage hangar
CN110871901A (en) * 2018-08-30 2020-03-10 一飞智控(天津)科技有限公司 Commodity circulation is waterproof skylight and shut down storehouse for unmanned aerial vehicle
CN111877827A (en) * 2020-07-21 2020-11-03 广东电网有限责任公司 Unmanned aerial vehicle parking garage with gathering function and control method of arc-shaped top cover of unmanned aerial vehicle parking garage
CN212473951U (en) * 2020-05-22 2021-02-05 上海芝松航空科技有限公司 All-weather guarantee carrier for large unmanned aerial vehicle
KR20210017676A (en) * 2019-08-09 2021-02-17 주식회사 엠지아이티 Drone station

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2015053523A (en) * 2014-12-02 2015-03-19 オリンパス株式会社 Waterproof apparatus
WO2017029611A1 (en) * 2015-08-17 2017-02-23 H3 Dynamics Holdings Pte. Ltd. Drone box
CN105221003A (en) * 2015-10-21 2016-01-06 江苏南方雄狮建设工程有限公司 A kind of flat-open door and window
CN209225411U (en) * 2018-08-30 2019-08-09 一飞智控(天津)科技有限公司 Rechargeable type logistics unmanned plane logistics airplane parking area platform
CN110871901A (en) * 2018-08-30 2020-03-10 一飞智控(天津)科技有限公司 Commodity circulation is waterproof skylight and shut down storehouse for unmanned aerial vehicle
CN209667390U (en) * 2019-07-11 2019-11-22 广西计算中心有限责任公司 VTOL fixed-wing unmanned plane automatic storage hangar
KR20210017676A (en) * 2019-08-09 2021-02-17 주식회사 엠지아이티 Drone station
CN212473951U (en) * 2020-05-22 2021-02-05 上海芝松航空科技有限公司 All-weather guarantee carrier for large unmanned aerial vehicle
CN111877827A (en) * 2020-07-21 2020-11-03 广东电网有限责任公司 Unmanned aerial vehicle parking garage with gathering function and control method of arc-shaped top cover of unmanned aerial vehicle parking garage

Also Published As

Publication number Publication date
CN114197933A (en) 2022-03-18

Similar Documents

Publication Publication Date Title
CN113247289B (en) Automatic recovery of VTOL fixed wing unmanned aerial vehicle machine nest that charges
CN114197933B (en) Unmanned aerial vehicle nest
EP3749578B1 (en) Landing platform with improved charging for unmanned aerial vehicles
US20170021942A1 (en) Pod cover system for a vertical take-off and landing (vtol) unmanned aerial vehicle (uav)
US11728663B2 (en) Drone recharging station
CN214930218U (en) All-terrain mechanical dog of transformer substation
US10570636B2 (en) Hangar system for local drone storage and charging
CN209225416U (en) A kind of unmanned plane outdoor surfaces work station
CN112849422A (en) Unmanned on duty shuts down cabin
US20230013552A1 (en) Base Stations Including Integrated Systems For Servicing UAVs
CN209938989U (en) Unmanned aerial vehicle space station
CN109018409A (en) Landing charging ramp equipment for unmanned plane
CN116896135A (en) Charging safety house for underground coal mine belt inspection robot and wireless charging method
CN114537690A (en) Logistics aircraft parking platform
KR101843147B1 (en) Wireless power transmission system for drione
CN216231718U (en) Intelligent shelter for accurate positioning and battery charging and replacing of unmanned aerial vehicle
WO2023272526A1 (en) Charging base station, flight vehicle, and flight vehicle system
CN104444236A (en) Device and method for inhibiting dust raising and low-temperature oxidizing in coal field
CN210011899U (en) Unmanned aerial vehicle space station and patrol line unmanned aerial vehicle system with solar power supply system
CN212473951U (en) All-weather guarantee carrier for large unmanned aerial vehicle
CN211568332U (en) Openable landing platform of electric power line patrol unmanned aerial vehicle
CN113968350A (en) Intelligent remote parking platform for unmanned aerial vehicle
CN110362125A (en) A kind of controlling temp type reorganizes and outfit system and method automatically
KR20220031845A (en) Drone station
CN207725242U (en) A kind of unmanned plane charging case that can radiate

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant