CN112173152A - Composite wing unmanned aerial vehicle shuts down strorage device - Google Patents
Composite wing unmanned aerial vehicle shuts down strorage device Download PDFInfo
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- CN112173152A CN112173152A CN201910596785.6A CN201910596785A CN112173152A CN 112173152 A CN112173152 A CN 112173152A CN 201910596785 A CN201910596785 A CN 201910596785A CN 112173152 A CN112173152 A CN 112173152A
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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
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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
- B60L53/10—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
- 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
- Y02T90/14—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
- 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]
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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
- 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
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Power Engineering (AREA)
- Transportation (AREA)
- Aviation & Aerospace Engineering (AREA)
- Charge And Discharge Circuits For Batteries Or The Like (AREA)
Abstract
The invention discloses a composite wing unmanned aerial vehicle stopping and storing device which comprises a fixed storing device and a controller, wherein a movable door is arranged at the top of the fixed storing device, the movable door is movably connected to the top of the fixed storing device, a stopping platform is arranged in the fixed storing device, a platform lifting device is connected to the bottom of the stopping platform, the stopping platform comprises a charging system, the charging system is electrically connected with the controller, the charging system comprises a charging connector and a charging connector driving mechanism, the charging connector is arranged at the center of the surface of the stopping platform, the charging connector driving mechanism is arranged in the stopping platform, and the output end of the charging connector driving mechanism is connected with the charging connector. The unmanned aerial vehicle emergency charging system can be deployed near the operation site of the composite wing unmanned aerial vehicle for a long time, the timeliness and the area coverage capability of emergency operation of the composite wing unmanned aerial vehicle are improved, the automatic charging of the unmanned aerial vehicle is realized by arranging the charging system, the external maintenance and inspection can be carried out on the unmanned aerial vehicle by arranging the camera, and unmanned remote management is realized.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicles, in particular to a composite wing unmanned aerial vehicle parking and storing device.
Background
Fixed-wing multi-rotor composite unmanned aerial vehicle is a novel aircraft different from traditional fixed-wing and rotor unmanned aerial vehicles. The multi-rotor system is additionally arranged on the fixed-wing flying platform, so that the vertical take-off and landing and hovering capabilities are obtained, and the cruise speed and range advantages of the fixed-wing unmanned aerial vehicle are achieved. Compared with other unmanned aerial vehicle systems, the composite wing unmanned aerial vehicle has obvious advantages. Compared with a helicopter, the composite wing unmanned aerial vehicle has the advantages of simple structure, low cost, high safety and long endurance time; compared with a multi-rotor wing, the composite wing unmanned aerial vehicle has long flight time, large flight range, high cruising speed and good stable flight performance under complex meteorological conditions; compared with a fixed wing, the composite wing unmanned aerial vehicle has no special runway, and is wide in application field, low in use difficulty and flexible in launching position.
The composite wing unmanned aerial vehicle is generally used for emergency operation, and is usually an area which is difficult for people to reach, and the timeliness and the area coverage capability in the operation are one of key points for ensuring the operation efficiency of the unmanned aerial vehicle. At present, because of lacking the unmanned aerial vehicle arresting gear of long-term deployment, flight each time all needs the staff to take unmanned aerial vehicle to arrive near scene and take off, has weakened the efficiency that unmanned aerial vehicle was on duty greatly. Therefore, a composite wing unmanned aerial vehicle stopping and storing device is urgently needed.
Disclosure of Invention
The invention aims to provide a composite wing unmanned aerial vehicle parking and storing device which can be deployed near an operation site for a long time so as to improve the timeliness and the area coverage capability of emergency operation of the composite wing unmanned aerial vehicle.
In order to achieve the purpose, the invention provides a composite wing unmanned aerial vehicle stopping and storing device which comprises a fixed storing device and a controller, wherein a movable door is arranged at the top of the fixed storing device and is movably connected to the top of the fixed storing device, a stopping platform is arranged in the fixed storing device, a platform lifting device is connected to the bottom of the stopping platform, the movable door is electrically connected with the controller,
the shutdown platform comprises a charging system, the charging system is electrically connected with the controller, the charging system comprises a charging connector and a charging connector driving mechanism, the charging connector is arranged at the center of the surface of the shutdown platform, the charging connector driving mechanism is arranged inside the shutdown platform, and the output end of the charging connector driving mechanism is connected with the charging connector.
Further, the charging connector driving mechanism is an electric push rod.
Further, the shutdown platform further comprises an angle adjusting mechanism, the angle adjusting mechanism comprises a rotating disk and a rotating disk driving mechanism, the rotating disk is concentrically arranged on the outer side of the charging connector, the rotating disk driving mechanism is arranged inside the shutdown platform, the rotating disk driving mechanism is electrically connected with the controller, and the rotating disk driving mechanism drives the rotating disk to rotate on the shutdown platform.
Further, the shutdown platform comprises a position adjusting mechanism, the position adjusting mechanism comprises four push rods arranged on the periphery of the shutdown platform, each push rod is connected with a push rod driving mechanism, the push rod driving mechanisms are electrically connected with the controller, each push rod comprises a transverse push rod and a longitudinal push rod, the transverse push rods and the longitudinal push rods are not located on the same horizontal plane in the vertical direction, the transverse push rods are prevented from colliding with the longitudinal push rods, damage is avoided, and the position adjusting mechanism moves the unmanned aerial vehicle to a target position through the push rods.
Further, the push rod driving mechanism is at least one push rod cylinder.
Furthermore, the length of the push rod is the same as the side length of the shutdown platform where the push rod is located, so that the action range of the push rod can cover the whole shutdown platform.
The landing of composite wing unmanned aerial vehicle is behind shutting down the platform, and position control mechanism promotes composite wing unmanned aerial vehicle to the rotary disk on, and later the rotary disk among the angle control mechanism rotates, drives composite wing unmanned aerial vehicle and rotates, until composite wing unmanned aerial vehicle towards the target position, at this moment, the joint that charges must be the interface that charges of aiming at composite wing unmanned aerial vehicle bottom, through the joint actuating mechanism that charges promote to charge the joint and rise and be connected with the interface that charges to realize the automatic charging to composite wing unmanned aerial vehicle. It should be noted that the rotating disk and the charging connector are concentrically arranged, and the charging connector is always kept still when the rotating disk rotates.
Further, what shut down the platform is provided with a plurality of cameras that shut down the platform center towards all around, the camera is connected with the controller electricity, when shutting down the completion back, carries out visual inspection through the camera to composite wing unmanned aerial vehicle's exterior structure, looks over whether have the bad part.
Furthermore, hemispherical bulges are distributed on the surface of the shutdown platform.
Further, the relation between the diameter D of the hemispherical protrusion and the width L of the support part of the composite wing unmanned aerial vehicle is as follows: d is less than or equal to L. Wherein, the supporting part of the composite wing unmanned aerial vehicle is usually a roller or a supporting rod, and here, the width L of the supporting part is the width of the roller or the width of the supporting rod. When the push rod promotes unmanned aerial vehicle, for the stability when guaranteeing unmanned aerial vehicle and removing, avoid unmanned aerial vehicle's supporting part can not block in the recess between the hemisphere type arch, or because of the recess between the hemisphere type arch takes place to shake or slope, the bellied diameter D of hemisphere type and compound wing unmanned aerial vehicle's supporting part width L must satisfy D and be less than or equal to L.
Further, the surface of the shutdown platform is fully paved with the balls, and of course, the relationship between the diameter D 'of the balls and the width L of the support part of the composite wing unmanned aerial vehicle also needs to satisfy D' less than L.
When the advancing direction of push rod is inconsistent with the roll direction of unmanned aerial vehicle supporting part, the supporting part of unmanned aerial vehicle takes place violent friction with the platform surface of shutting down easily, cause the damage to unmanned aerial vehicle, therefore, the surface of shutting down the platform is covered with the hemisphere arch or is covered with the ball, can effectively reduce unmanned aerial vehicle and the frictional force of shutting down the platform surface, make position control mechanism remove unmanned aerial vehicle to the target location more easily, avoided the problem that the unmanned aerial vehicle supporting part and shut down the platform surface and take place violent friction and cause the damage.
Further, platform elevating gear includes lift platform, lift base, base cylinder and is located the crane between lift platform and the lift base, the crane is two mutual articulated connecting rods, lift platform's bottom surface is provided with first slide, the top sliding connection of connecting rod is in first slide, lift base's top surface is provided with the second slide, the bottom sliding connection of connecting rod is in the second slide, the base cylinder sets up the top surface at lift base, the output and the at least one of base cylinder the bottom of connecting rod is connected.
Compared with the prior art, the invention has the beneficial effects that: the invention can be deployed near the operation site of the composite wing unmanned aerial vehicle for a long time, and improves the timeliness and the area coverage capability of emergency operation of the composite wing unmanned aerial vehicle; according to the unmanned aerial vehicle remote management system, the charging system is arranged to realize automatic charging of the unmanned aerial vehicle, the camera is arranged to perform external maintenance and inspection on the unmanned aerial vehicle, and unmanned remote management is realized.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic structural view of the stopping platform of the present invention (without showing the hemispherical protrusions);
FIG. 3 is a schematic structural diagram of a charging system according to the present invention;
FIG. 4 is a schematic structural view of a hemispherical protrusion according to the present invention;
FIG. 5 is a schematic structural view of the platform lifting device of the present invention;
FIG. 6 is an electrical connection block diagram of the present invention;
in the figure: 100. fixing the storage device; 200. a controller; 300. a charging system; 310. a charging connector; 320. a charging connector driving mechanism; 400. a movable door; 500. a shutdown platform; 510. a push rod; 520. a push rod drive mechanism; 530. a hemispherical bulge; 540. a camera; 600. a platform lifting device; 610. a lifting platform; 611. a first slideway; 612. a second slideway; 620. a lifting base; 630. a base cylinder; 640. a connecting rod; 710. rotating the disc; 720. a rotating disk drive mechanism; 800. provided is a charging system.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1-6, a composite wing unmanned aerial vehicle stopping and storing device comprises a fixed storing device 100 and a controller 200, wherein a movable door 400 is arranged at the top of the fixed storing device 100, the movable door 400 is movably connected to the top of the fixed storing device 100, a stopping platform 500 is arranged in the fixed storing device 100, a platform lifting device 600 is connected to the bottom of the stopping platform 500, the movable door 400 is electrically connected with the controller 200,
as shown in fig. 2 and 3, the shutdown platform 500 includes a charging system 300, the charging system 300 is electrically connected to the controller 200, the charging system 300 includes a charging connector 310 and a charging connector driving mechanism 320, the charging connector 310 is disposed at the center of the surface of the shutdown platform 500, the charging connector driving mechanism 320 is disposed inside the shutdown platform 500, an output end of the charging connector driving mechanism 320 is connected to the charging connector 310, the charging connector driving mechanism 320 drives the charging connector 310 to move in the vertical direction, the charging connector driving mechanism 320 is electrically connected to the controller 200, so that the charging connector 310 is cooperatively connected to a charging interface of the bottom of the composite wing unmanned aerial vehicle, of course, the charging connector 310 is connected to a power source, and in this embodiment, the charging connector driving mechanism 320 is an electric push rod.
In order to adjust the angle of the composite wing unmanned aerial vehicle, so that the charging interface at the bottom of the composite wing unmanned aerial vehicle can be in fit connection with the charging connector 310, the shutdown platform 500 is further provided with an angle adjusting mechanism, as shown in fig. 3, the angle adjusting mechanism comprises a rotating disk 710 and a rotating disk driving mechanism 720, the rotating disk 710 is concentrically arranged outside the charging connector 310, the rotating disk driving mechanism 720 is arranged inside the shutdown platform 500, the rotating disk driving mechanism 720 is electrically connected with the controller 200, and the rotating disk driving mechanism 720 drives the rotating disk 710 to rotate on the shutdown platform 500. It should be noted that the rotating disc is concentric with 710 the charging connector 310, and the charging connector 310 is always kept still when the rotating disc 710 rotates.
In order to ensure that the composite wing unmanned aerial vehicle can fall onto the rotating disk 710, the shutdown platform 500 is further provided with a position adjusting mechanism, as shown in fig. 2, the position adjusting mechanism comprises four push rods 510 arranged around the shutdown platform 500, each push rod 510 is connected with a push rod driving mechanism 520, the push rod driving mechanism 520 is electrically connected with the controller 200, the push rod driving mechanism 520 is at least one push rod cylinder, the push rods 510 comprise transverse push rods and longitudinal push rods, the transverse push rods and the longitudinal push rods are not in the same horizontal plane in the vertical direction, the transverse push rods are prevented from colliding with the longitudinal push rods to cause damage, and the position adjusting mechanism moves the unmanned aerial vehicle to a target position through the push rods 510. The length of the push rod 510 is the same as the side length of the shutdown platform 500 where the push rod 510 is located, so that the action range of the push rod 510 can cover the whole shutdown platform 500.
When the advancing direction of push rod 510 was inconsistent with the roll direction of unmanned aerial vehicle supporting part, the supporting part of unmanned aerial vehicle took place violent friction with stopping platform 500 surface easily, led to the fact the damage to unmanned aerial vehicle, consequently, stopped platform 500's surface and be covered with the protruding 530 of hemisphere type, or paved with the ball. As shown in fig. 4, the relationship between the diameter D of the hemispherical protrusion 530 and the width L of the support portion of the composite wing drone is: d is less than or equal to L. The support part of the composite wing drone is usually a roller or a support rod, where the support part width L is the width of the roller or the width of the support rod. When push rod 510 promoted unmanned aerial vehicle, for the stability when guaranteeing unmanned aerial vehicle and removing, avoid unmanned aerial vehicle's supporting part can not block in the recess between the protruding 530 of hemisphere, or take place to shake or slope because of the recess between the protruding 530 of hemisphere, the diameter D of the protruding 530 of hemisphere and compound wing unmanned aerial vehicle's supporting part width L must satisfy D and be less than or equal to L. Of course, the relationship between the diameter D 'of the balls and the width L of the support portion of the compound wing drone should also satisfy D' ≦ L.
The surface of stopping platform 500 is covered with hemispherical bulges 530 or is covered with balls, so that the friction force between the unmanned aerial vehicle and the surface of stopping platform 500 can be effectively reduced, the position adjusting mechanism can move the unmanned aerial vehicle to a target position more easily, and the problem that the damage is caused by severe friction between the supporting part of the unmanned aerial vehicle and the surface of stopping platform 500 is avoided.
Specifically, as shown in fig. 5, the platform lifting device 600 includes a lifting platform 610, a lifting base 620, a base cylinder 630, and a lifting frame located between the lifting platform 610 and the lifting base 620, the lifting frame is two mutually hinged connecting rods 640, a first slide rail 611 is provided on the bottom surface of the lifting platform 610, the top end of the connecting rod 640 is slidably connected in the first slide rail 611, a second slide rail 612 is provided on the top surface of the lifting base 620, the bottom end of the connecting rod 640 is slidably connected in the second slide rail 612, the base cylinder 630 is provided on the top surface of the lifting base 620, and the output end of the base cylinder 630 is connected with the bottom end of at least one connecting rod 640.
Shut down platform 500 be provided with a plurality of cameras 540 that shut down the platform center towards all around, camera 540 is connected with controller electricity 200, when shutting down the completion back, carries out visual inspection through camera 540 to composite wing unmanned aerial vehicle's exterior structure, checks whether there is the damage part.
The working principle is as follows:
when the composite wing unmanned aerial vehicle is ready to land, the controller 200 opens the movable door 400, and meanwhile, the platform lifting device 600 drives the parking platform 500 to ascend, the composite wing unmanned aerial vehicle lands on the parking platform 500, the position adjusting mechanism pushes the composite wing unmanned aerial vehicle onto the rotating disk 710, then the rotating disk 710 rotates, the composite wing unmanned aerial vehicle is driven to rotate until the composite wing unmanned aerial vehicle faces a target position, at the moment, the charging connector 310 is inevitably aligned with a charging interface at the bottom of the composite wing unmanned aerial vehicle, the charging connector 310 is pushed to ascend through the charging connector driving mechanism 320 and is connected with the charging interface, so that automatic charging of the composite wing unmanned aerial vehicle is realized, meanwhile, the platform lifting device 600 drives the parking platform 500 to descend, the movable door 400 is closed, a worker remotely performs visual maintenance on the composite wing unmanned aerial vehicle through the camera 540, and unmanned remote management is realized. After charging, the controller 200 controls the charging connector driving mechanism 320 to withdraw the charging connector 310, when the unmanned aerial vehicle needs to take off, the controller 200 opens the movable door 400, the platform lifting device 600 drives the stopping platform 500 to ascend, and the unmanned aerial vehicle can be prepared to take off.
It will be evident to those skilled in the art that the invention is not limited to the details of the foregoing illustrative embodiments, and that the present invention may be embodied in other specific forms without departing from the spirit or essential attributes thereof. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
Furthermore, it should be understood that although the present description refers to embodiments, not every embodiment may contain only a single embodiment, and such description is for clarity only, and those skilled in the art should integrate the description, and the embodiments may be combined as appropriate to form other embodiments understood by those skilled in the art.
Claims (9)
1. A composite wing unmanned aerial vehicle stopping and storing device is characterized by comprising a fixed storing device and a controller, wherein a movable door is arranged at the top of the fixed storing device and movably connected to the top of the fixed storing device, a stopping platform is arranged in the fixed storing device, a platform lifting device is connected to the bottom of the stopping platform, the movable door is electrically connected with the controller,
the shutdown platform comprises a charging system, the charging system is electrically connected with the controller, the charging system comprises a charging connector and a charging connector driving mechanism, the charging connector is arranged at the center of the surface of the shutdown platform, the charging connector driving mechanism is arranged inside the shutdown platform, and the output end of the charging connector driving mechanism is connected with the charging connector.
2. The composite wing drone shutdown storage device of claim 1, wherein the shutdown platform further includes an angle adjustment mechanism, the angle adjustment mechanism including a rotating disk and a rotating disk drive mechanism, the rotating disk being concentrically disposed outside the charging connector, the rotating disk drive mechanism being disposed inside the shutdown platform, the rotating disk drive mechanism being electrically connected to the controller, the rotating disk drive mechanism driving the rotating disk to rotate on the shutdown platform.
3. The composite wing unmanned aerial vehicle shuts down strorage device of claim 1, characterized in that, the platform of shutting down includes position adjustment mechanism, position adjustment mechanism includes four push rods that set up around the platform of shutting down, each push rod all is connected with a push rod actuating mechanism, push rod actuating mechanism is connected with the controller electricity, the push rod includes horizontal push rod and vertical push rod, horizontal push rod and vertical push rod are not in same horizontal plane in the vertical direction.
4. The compound wing drone shutdown storage device of claim 3, said push rod drive mechanism being at least one push rod cylinder.
5. The compound wing drone shutdown storage device of claim 1, wherein a plurality of cameras facing the center of the shutdown platform are disposed around the shutdown platform, the cameras being electrically connected to the controller.
6. The compound wing drone of any one of claims 1-5 halts strorage device, characterized in that the surface of the platform of halting is covered with hemispherical bulges.
7. The composite wing drone of claim 6, wherein the diameter D of the hemispherical protrusion and the width L of the support portion of the composite wing drone are in relation: d is less than or equal to L.
8. The compound wing drone shutdown storage device of claims 1-5, wherein the surface of the shutdown platform is full of balls.
9. The compound wing unmanned aerial vehicle shuts down strorage device of claim 1, characterized in that, platform elevating gear includes lift platform, lift base, base cylinder and is located the crane between lift platform and the lift base, the crane is two mutual articulated connecting rods, lift platform's bottom surface is provided with first slide, the top sliding connection of connecting rod is in first slide, lift base's top surface is provided with the second slide, the bottom sliding connection of connecting rod is in the second slide, the base cylinder sets up the top surface at lift base, the output and the at least one of base cylinder the bottom of connecting rod is connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910596785.6A CN112173152A (en) | 2019-07-03 | 2019-07-03 | Composite wing unmanned aerial vehicle shuts down strorage device |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910596785.6A CN112173152A (en) | 2019-07-03 | 2019-07-03 | Composite wing unmanned aerial vehicle shuts down strorage device |
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| CN112173152A true CN112173152A (en) | 2021-01-05 |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113120252A (en) * | 2021-05-21 | 2021-07-16 | 苏州臻迪智能科技有限公司 | Unmanned aerial vehicle parking system and unmanned aerial vehicle parking method |
| CN113212781A (en) * | 2021-06-24 | 2021-08-06 | 烟台中商人工智能科技有限公司 | Unmanned aerial vehicle take-off and landing platform |
| CN113772112A (en) * | 2021-09-07 | 2021-12-10 | 万航星空科技发展有限公司 | Remote monitoring unmanned aerial vehicle battery charging system |
-
2019
- 2019-07-03 CN CN201910596785.6A patent/CN112173152A/en active Pending
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113120252A (en) * | 2021-05-21 | 2021-07-16 | 苏州臻迪智能科技有限公司 | Unmanned aerial vehicle parking system and unmanned aerial vehicle parking method |
| CN113212781A (en) * | 2021-06-24 | 2021-08-06 | 烟台中商人工智能科技有限公司 | Unmanned aerial vehicle take-off and landing platform |
| CN113772112A (en) * | 2021-09-07 | 2021-12-10 | 万航星空科技发展有限公司 | Remote monitoring unmanned aerial vehicle battery charging system |
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