CN112793800A - Multi-functional unmanned aerial vehicle flight platform - Google Patents
Multi-functional unmanned aerial vehicle flight platform Download PDFInfo
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- CN112793800A CN112793800A CN202110148502.9A CN202110148502A CN112793800A CN 112793800 A CN112793800 A CN 112793800A CN 202110148502 A CN202110148502 A CN 202110148502A CN 112793800 A CN112793800 A CN 112793800A
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- China
- Prior art keywords
- unmanned aerial
- aerial vehicle
- cover plate
- platform
- frame
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Classifications
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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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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
- F16F15/02—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems
- F16F15/03—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using magnetic or electromagnetic means
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
- F16F15/02—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems
- F16F15/04—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using elastic means
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
- F16F15/02—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems
- F16F15/04—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using elastic means
- F16F15/08—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using elastic means with rubber springs ; with springs made of rubber and metal
- F16F15/085—Use of both rubber and metal springs
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Acoustics & Sound (AREA)
- Electromagnetism (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Vibration Dampers (AREA)
- Vibration Prevention Devices (AREA)
Abstract
The invention provides a multifunctional unmanned aerial vehicle flight platform, which belongs to the technical field of unmanned aerial vehicles and comprises a platform body, wherein an inner cavity is arranged in the platform body, a notch is formed in the upper part of the platform body, a cover plate is hinged in the notch, a second groove is formed in the middle of the upper surface of the cover plate, and a buffer assembly is arranged on the upper part of the cover plate; the buffer assembly comprises a frame arranged around the second groove and a flexible layer arranged at the bottom of the frame. The embodiment of the invention has the advantages of simple structure, convenience in use and good buffering effect, the unmanned aerial vehicle can be supported from the bottom in the descending process of the unmanned aerial vehicle through the arrangement of the flexible layer, the unmanned aerial vehicle is greatly damped, the unmanned aerial vehicle is protected from being damaged by vibration in the parking process, in addition, the first magnetic part and the second magnetic part are arranged, upward supporting force can be provided for the unmanned aerial vehicle, the descending speed of the unmanned aerial vehicle is slowed down, and the further buffering of the unmanned aerial vehicle is realized.
Description
Technical Field
The invention belongs to the technical field of unmanned aerial vehicles, and particularly relates to a multifunctional unmanned aerial vehicle flight platform.
Background
Unmanned aircraft, also known as "drones," are unmanned aircraft that are operated by radio remote control devices and self-contained program control devices, or are operated autonomously, either completely or intermittently, by an onboard computer, and are often more suited to tasks that are too "fool, dirty, or dangerous" than are manned aircraft.
At present, unmanned aerial vehicle is parking the decline in-process, for preventing it from producing rigid structure with ground, lead to unmanned aerial vehicle to take place to damage because of suffering vibrations, be equipped with dedicated parking platform for unmanned aerial vehicle usually, and park the corresponding damper of platform upper portion configuration in order to provide the shock attenuation buffering to unmanned aerial vehicle, current damper upwards launches the parachute through launching the mechanism mostly, utilize the parachute to provide the support to unmanned aerial vehicle's bottom, but the parachute launches the in-process and has certain impact force, this impact force can the unmanned aerial vehicle vibrations that arouse of certain degree, and then lead to buffering effect not good.
Disclosure of Invention
Aiming at the defects of the prior art, the technical problem to be solved by the embodiment of the invention is to provide a multifunctional unmanned aerial vehicle flight platform.
In order to solve the technical problems, the invention provides the following technical scheme:
a multifunctional unmanned aerial vehicle flight platform comprises a platform body, wherein an inner cavity is formed in the platform body, a notch is formed in the upper portion of the platform body, a cover plate is hinged in the notch, a second groove is formed in the middle of the upper surface of the cover plate, and a buffering assembly is arranged on the upper portion of the cover plate; the buffer assembly comprises a frame arranged around the second groove and a flexible layer arranged at the bottom of the frame, one end, far away from the frame, of the flexible layer is connected with the upper surface of the cover plate, and the flexible layer can be unfolded to form a bucket-shaped structure; the inside activity of second recess is provided with the backup pad, and second recess bottom has been seted up and has been link up extremely the through-hole of inner chamber, backup pad upper portion is provided with first magnetism portion, the fixed bracing piece that is provided with in backup pad bottom, the bracing piece certainly the through-hole extends to the inner chamber, and the fixed first conducting strip that is provided with in bracing piece bottom, a plurality of second conducting strips are installed to the inner chamber bottom, the apron upper wall still is provided with a plurality of effects in the shoring subassembly of frame bottom, the shoring subassembly with the second conducting strip passes through the wire and connects, first conducting strip and external power source electric connection.
As a further improvement of the invention: the top bracing subassembly is including articulating the guide cylinder on apron upper portion and articulating the ejector pin of frame bottom, the ejector pin extends to inside and with the flexible cooperation of guide cylinder, the ejector pin lower extreme is provided with the second electro-magnet, guide cylinder inner chamber bottom is provided with first electro-magnet, the wire with first electro-magnet and second electro-magnet are connected respectively.
As a further improvement of the invention: the flexible layer is made of rubber or nylon cloth.
As a further improvement of the invention: the support rod is made of an insulating material.
As a still further improvement of the invention: platform body lateral wall has been seted up unmanned aerial vehicle and has been got and put the mouth, unmanned aerial vehicle gets and installs sealing door in putting the mouth.
As a still further improvement of the invention: the side wall of the supporting rod is fixedly provided with a stop block, the stop block is positioned in the inner cavity, and the upper part of the stop block is connected with the top wall of the inner cavity through an elastic body.
As a still further improvement of the invention: the elastic body is a spring.
Compared with the prior art, the invention has the beneficial effects that:
the embodiment of the invention has the advantages of simple structure, convenience in use and good buffering effect, the unmanned aerial vehicle can be supported from the bottom in the descending process of the unmanned aerial vehicle through the arrangement of the flexible layer, the unmanned aerial vehicle is greatly damped, the unmanned aerial vehicle is protected from being damaged by vibration in the parking process, in addition, the first magnetic part and the second magnetic part are arranged, upward supporting force can be provided for the unmanned aerial vehicle, the descending speed of the unmanned aerial vehicle is slowed down, and the further buffering of the unmanned aerial vehicle is realized.
Drawings
Fig. 1 is a schematic diagram of an internal structure of a multifunctional unmanned aerial vehicle flight platform;
FIG. 2 is a schematic structural diagram of a multifunctional unmanned aerial vehicle flight platform;
FIG. 3 is a schematic structural diagram of a top bracing assembly in a multifunctional unmanned aerial vehicle flight platform;
in the figure: 1-platform body, 2-inner cavity, 3-cover plate, 4-notch, 5-first groove, 6-top support component, 7-buffer component, 8-first magnetic part, 9-support plate, 10-second groove, 11-through hole, 12-support rod, 13-elastic body, 14-stop block, 15-first conducting strip, 16-second conducting strip, 17-lead, 18-frame, 19-flexible layer, 20-guide cylinder, 21-first electromagnet, 22-second electromagnet and 23-ejector rod.
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
Referring to fig. 1-3, the embodiment provides a multifunctional unmanned aerial vehicle flight platform, which includes a platform body 1, an inner cavity 2 is arranged inside the platform body 1, a notch 4 is formed in the upper portion of the platform body 1, a cover plate 3 is hinged inside the notch 4, a second groove 10 is formed in the middle of the upper surface of the cover plate 3, a buffer assembly 7 is arranged on the upper portion of the cover plate 3, specifically, the buffer assembly 7 includes a frame 18 surrounding the second groove 10 and a flexible layer 19 arranged at the bottom of the frame 18, one end of the flexible layer 19, which is far away from the frame 18, is connected with the upper surface of the cover plate 3, and the flexible layer 19 can be unfolded into a bucket-shaped structure; the inside activity of second recess 10 is provided with backup pad 9, and second recess 10 bottom has been seted up and has been link up extremely through-hole 11 of inner chamber 2, backup pad 9 upper portion is provided with first magnetism portion 8, and backup pad 9 bottom is fixed and is provided with bracing piece 12, bracing piece 12 certainly through-hole 11 extends to in the inner chamber 2, and bracing piece 12 bottom is fixed and is provided with first conducting strip 15, a plurality of second conducting strips 16 are installed to inner chamber 2 bottom, apron 3 upper wall still is provided with a plurality of effects in the shoring subassembly 6 of frame 18 bottom, shoring subassembly 6 with second conducting strip 16 passes through wire 17 and connects, first conducting strip 15 and external power source (not shown) electric connection.
In the embodiment, a second magnetic part mutually repulsive to the first magnetic part 8 is arranged on the belly of the unmanned aerial vehicle body, in the parking process of the unmanned aerial vehicle, the unmanned aerial vehicle can fly and hover above the cover plate 3, at the moment, the second magnetic part and the first magnetic part 8 generate a repelling effect to drive the support plate 9 to move downwards along the second groove 10, so as to drive the supporting rod 12 and the first conductive sheet 15 to move downwards until the first conductive sheet 15 is attached to the upper portion of the second conductive sheet 16, thereby realizing the electric conduction between the first conductive sheet 15 and the second conductive sheet 16, and an external power supply can supply power to the top bracing assembly 6, so as to drive the top bracing assembly 6 to drive the frame 18 to move upwards, thereby, the flexible layer 19 is pulled, the flexible layer 19 is unfolded to form a bucket-shaped structure, the unmanned aerial vehicle is controlled to descend, the flexible layer 19 is used for providing flexible support for the bottom of the unmanned aerial vehicle, the buffering of the unmanned aerial vehicle is realized, and the unmanned aerial vehicle can stably descend and the upper part of the cover plate 3 is ensured; and, through the repulsion effect of first magnetism portion 18 with second magnetism portion, still can provide ascending holding power to unmanned aerial vehicle for slow down unmanned aerial vehicle's falling speed, realize unmanned aerial vehicle's further buffering.
Specifically, the top bracing assembly 6 comprises a guide cylinder 20 hinged to the upper portion of the cover plate 3 and a mandril 23 hinged to the bottom of the frame 18, the mandril 23 extends to the inside of the guide cylinder 20 and is in telescopic fit with the guide cylinder 20, a second electromagnet 22 is arranged at the lower end of the mandril 23, a first electromagnet 21 is arranged at the bottom of the inner cavity of the guide cylinder 20, and the wire 17 is connected with the first electromagnet 21 and the second electromagnet 22 respectively.
When the first conductive sheet 15 and the second conductive sheet 16 are attached to each other, the current output from the external power source can be transmitted to the first electromagnet 21 and the second electromagnet 22 through the first conductive sheet 15, the second conductive sheet 16 and the wire 17, so that the first electromagnet 21 and the second electromagnet 22 have magnetism, the first electromagnet 21 and the second electromagnet 22 generate a repelling effect, and the ejector rod 23 is driven to move towards the outside of the guide cylinder 20, so as to drive the frame 18 to move upwards, thereby realizing the unfolding of the flexible layer 19.
In this embodiment, flexible layer 19 is made for rubber or nylon cloth to provide the buffering for unmanned aerial vehicle's decline.
In this embodiment, the supporting rod 12 is made of an insulating material to ensure that the current outputted from the external power supply can smoothly act on the first electromagnet 21 and the second electromagnet 22.
In this embodiment, the upper portion of the cover plate 3 is provided with a first groove 5 for accommodating the top bracing assembly 6.
In this embodiment, 1 lateral wall of platform body has been seted up unmanned aerial vehicle and has been got and put mouth (not shown), unmanned aerial vehicle gets and installs sealing door (not shown) in putting the mouth, when not using, can put into inner chamber 2 with unmanned aerial vehicle and deposit to carry flight platform and unmanned aerial vehicle.
Example 2
Referring to fig. 1, in the present embodiment, compared with embodiment 1, a stop 14 is fixedly disposed on a side wall of the supporting rod 12, the stop 14 is located in the inner cavity 2, and an upper portion of the stop 14 is connected to a top wall of the inner cavity 2 through an elastic body 13.
When the unmanned aerial vehicle flies outside, under the effect of elastomer 13, can pull bracing piece 12 for first conducting strip 15 is in the separation state with second conducting strip 16, and first electro-magnet 21 is in the outage state with second electro-magnet 22 this moment, and under the action of gravity, frame 18 is kept flat in apron 3 upper portion, and flexible layer 19 is in fold condition, avoids frame 18 and flexible layer 19 protrusion in apron 3 upper portion all the time, in order to reduce shared space.
Specifically, the elastic body 13 is a spring.
The embodiment of the invention has the advantages of simple structure, convenience in use and good buffering effect, the unmanned aerial vehicle can be supported from the bottom in the descending process of the unmanned aerial vehicle through the arrangement of the flexible layer 19, the unmanned aerial vehicle is greatly damped, the unmanned aerial vehicle is protected from being damaged by vibration in the parking process, in addition, the first magnetic part 8 and the second magnetic part are arranged, upward supporting force can be provided for the unmanned aerial vehicle, the descending speed of the unmanned aerial vehicle is slowed down, and the further buffering of the unmanned aerial vehicle is realized.
Although the preferred embodiments of the present patent have been described in detail, the present patent is not limited to the above embodiments, and various changes can be made without departing from the spirit of the present patent within the knowledge of those skilled in the art.
Claims (7)
1. The multifunctional unmanned aerial vehicle flight platform is characterized by comprising a platform body (1), wherein an inner cavity (2) is formed in the platform body (1), a notch (4) is formed in the upper portion of the platform body (1), a cover plate (3) is hinged in the notch (4), a second groove (10) is formed in the middle of the upper surface of the cover plate (3), and a buffer assembly (7) is arranged on the upper portion of the cover plate (3); the buffer assembly (7) comprises a frame (18) arranged around the second groove (10) and a flexible layer (19) arranged at the bottom of the frame (18), one end, far away from the frame (18), of the flexible layer (19) is connected with the upper surface of the cover plate (3), and the flexible layer (19) can be unfolded into a bucket-shaped structure; second recess (10) inside activity is provided with backup pad (9), and second recess (10) bottom has been seted up and has been link up to through-hole (11) of inner chamber (2), backup pad (9) upper portion is provided with first magnetism portion (8), and backup pad (9) bottom is fixed and is provided with bracing piece (12), bracing piece (12) certainly through-hole (11) extend to in inner chamber (2), and bracing piece (12) bottom is fixed and is provided with first conducting strip (15), a plurality of second conducting strips (16) are installed to inner chamber (2) bottom, apron (3) upper wall still is provided with a plurality of effects in shoring subassembly (6) of frame (18) bottom, shoring subassembly (6) with second conducting strip (16) pass through wire (17) and connect, first conducting strip (15) and external power electric connection.
2. The multifunctional unmanned aerial vehicle flying platform of claim 1, wherein the top bracing assembly (6) comprises a guide cylinder (20) hinged to the upper portion of the cover plate (3) and a top rod (23) hinged to the bottom of the frame (18), the top rod (23) extends into the guide cylinder (20) and is in telescopic fit with the guide cylinder (20), a second electromagnet (22) is arranged at the lower end of the top rod (23), a first electromagnet (21) is arranged at the bottom of the inner cavity of the guide cylinder (20), and the lead (17) is respectively connected with the first electromagnet (21) and the second electromagnet (22).
3. A multifunctional unmanned aerial vehicle flight platform according to claim 1, wherein the flexible layer (19) is made of rubber or nylon cloth.
4. A multifunctional unmanned aerial vehicle flight platform according to any one of claims 1 to 3, wherein the support rods (12) are made of an insulating material.
5. The multifunctional unmanned aerial vehicle flight platform of claim 1, wherein the side wall of the platform body (1) is provided with an unmanned aerial vehicle access opening, and a sealing door is installed in the unmanned aerial vehicle access opening.
6. The multifunctional unmanned aerial vehicle flying platform of claim 1, wherein the side wall of the supporting rod (12) is fixedly provided with a stopper (14), the stopper (14) is located in the inner cavity (2), and the upper part of the stopper (14) is connected with the top wall of the inner cavity (2) through an elastic body (13).
7. The multifunctional unmanned aerial vehicle flight platform of claim 6, wherein the elastomer (13) is a spring.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110148502.9A CN112793800B (en) | 2021-02-03 | 2021-02-03 | Multi-functional unmanned aerial vehicle flight platform |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110148502.9A CN112793800B (en) | 2021-02-03 | 2021-02-03 | Multi-functional unmanned aerial vehicle flight platform |
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| CN112793800A true CN112793800A (en) | 2021-05-14 |
| CN112793800B CN112793800B (en) | 2022-05-13 |
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Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104670516A (en) * | 2015-02-15 | 2015-06-03 | 南京理工大学 | Rapid taking-off and landing device of air vehicle |
| CN206841730U (en) * | 2017-05-22 | 2018-01-05 | 金陵科技学院 | A kind of rotor wing unmanned aerial vehicle with positioning landing frame |
| WO2019111251A1 (en) * | 2017-12-05 | 2019-06-13 | First Airborne Limited | Capture and storage unit and method for airborne drone |
| CN210653581U (en) * | 2019-10-30 | 2020-06-02 | 浙江舟山博斯特船舶设计研究院有限公司 | Unmanned aerial vehicle lifting platform for scientific investigation ship |
| CN210912918U (en) * | 2019-07-16 | 2020-07-03 | 国网浙江省电力有限公司衢州供电公司 | Unmanned aerial vehicle recovery unit |
| CN111439143A (en) * | 2020-05-12 | 2020-07-24 | 深圳臻像科技有限公司 | Unmanned aerial vehicle recovery system and recovery method thereof |
-
2021
- 2021-02-03 CN CN202110148502.9A patent/CN112793800B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104670516A (en) * | 2015-02-15 | 2015-06-03 | 南京理工大学 | Rapid taking-off and landing device of air vehicle |
| CN206841730U (en) * | 2017-05-22 | 2018-01-05 | 金陵科技学院 | A kind of rotor wing unmanned aerial vehicle with positioning landing frame |
| WO2019111251A1 (en) * | 2017-12-05 | 2019-06-13 | First Airborne Limited | Capture and storage unit and method for airborne drone |
| CN210912918U (en) * | 2019-07-16 | 2020-07-03 | 国网浙江省电力有限公司衢州供电公司 | Unmanned aerial vehicle recovery unit |
| CN210653581U (en) * | 2019-10-30 | 2020-06-02 | 浙江舟山博斯特船舶设计研究院有限公司 | Unmanned aerial vehicle lifting platform for scientific investigation ship |
| CN111439143A (en) * | 2020-05-12 | 2020-07-24 | 深圳臻像科技有限公司 | Unmanned aerial vehicle recovery system and recovery method thereof |
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| CN112793800B (en) | 2022-05-13 |
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Address after: 11-14 / F, tower a, Tengfei building, 88 Jiangmiao Road, yanchuangyuan, Jiangbei new district, Nanjing, Jiangsu Province 210000 Patentee after: Anyuan Technology Co.,Ltd. Address before: 11-14 / F, tower a, Tengfei building, 88 Jiangmiao Road, yanchuangyuan, Jiangbei new district, Nanjing, Jiangsu Province 210000 Patentee before: NANJING ANYUAN TECHNOLOGY Co.,Ltd. |
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