CN109644581B - Shielding device and unmanned vehicles - Google Patents
Shielding device and unmanned vehicles Download PDFInfo
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- CN109644581B CN109644581B CN201680087991.9A CN201680087991A CN109644581B CN 109644581 B CN109644581 B CN 109644581B CN 201680087991 A CN201680087991 A CN 201680087991A CN 109644581 B CN109644581 B CN 109644581B
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- housing
- shielding device
- aerial vehicle
- unmanned aerial
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- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 2
- 229910000570 Cupronickel Inorganic materials 0.000 description 2
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- 229910052782 aluminium Inorganic materials 0.000 description 2
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Images
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05K—PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
- H05K9/00—Screening of apparatus or components against electric or magnetic fields
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- Engineering & Computer Science (AREA)
- Microelectronics & Electronic Packaging (AREA)
- Aviation & Aerospace Engineering (AREA)
- Shielding Devices Or Components To Electric Or Magnetic Fields (AREA)
- Toys (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
The invention discloses a shielding device (50) and an unmanned aerial vehicle (100). Wherein the shielding device (50) is used for an unmanned aerial vehicle (100). The unmanned aerial vehicle (100) includes a global positioning system module (40). The shield device (50) includes a cover portion (52) and a mounting portion (54). The cover portion (52) accommodates the global positioning system module (40). The mounting portion (54) extends from the cover portion (52) and surrounds the cover portion (52). The shielding device (50) and the unmanned aerial vehicle (100) can effectively shield the interference of electronic components in the unmanned aerial vehicle (100) on the global positioning system module (40) so as to ensure that the global positioning system module (40) can be accurately positioned and navigated in the flight process of the unmanned aerial vehicle (100).
Description
Technical Field
The invention relates to the aircraft technology, in particular to a shielding device and an unmanned aerial vehicle.
Background
The unmanned aerial vehicle has the advantages of flexibility, quick response, unmanned flight, low operation requirement and the like, and is widely applied to three fields of military affairs, scientific research and civil affairs to execute tasks of transportation, delivery, monitoring, investigation, exploration, shooting and the like in application of each field. Unmanned vehicles carries out location and navigation through the Global Positioning System (GPS) module, and in the location and navigation processes, the GPS module easily receives the interference of other electronic components such as batteries in the unmanned vehicles, and influences the working performance of the GPS module, leads to inaccurate, even failure of location and navigation.
Disclosure of Invention
The present invention is directed to solving at least one of the problems of the prior art. Therefore, the invention needs to provide a shielding device and an unmanned aerial vehicle.
A shielding device for an unmanned aerial vehicle, the unmanned aerial vehicle including a global positioning system module, the shielding device comprising:
the covering part accommodates the global positioning system module; and
the installation department, the installation department certainly cover portion extension and encircle cover portion, cover portion reaches the installation department is made by metal material, and integrated into one piece.
In some embodiments, the cover portion is spaced apart from the gps module.
In some embodiments, the cover portion is perforated with a through hole.
In some embodiments, the mounting portion defines a plurality of engaging holes.
In some embodiments, the mounting portion is formed with a plurality of protrusions, each of which defines a receiving slot.
An unmanned aerial vehicle, unmanned aerial vehicle includes first casing, fixes global positioning system module and shield assembly on the first casing, shield assembly includes:
the covering part accommodates the global positioning system module; and
the installation department, the installation department certainly cover portion extends and encircles cover portion, the installation department is installed on the first casing, cover portion reaches the installation department is made by metal material, and integrated into one piece.
In some embodiments, the cover portion is spaced apart from the gps module.
In some embodiments, the covering portion has a through hole, and the unmanned aerial vehicle further includes a battery module and a wire, wherein the wire passes through the through hole and connects the gps module and the battery module.
In some embodiments, the unmanned aerial vehicle further comprises a filler for filling a gap formed by the wire passing through the through hole.
In some embodiments, the shape of the mounting portion matches the shape of the first housing to conform to the first housing.
In some embodiments, the mounting portion is fixed to the first housing by one or more of adhesive bonding, screwing, snapping, and welding.
In some embodiments, the mounting portion has a plurality of engaging holes, the first housing includes a plurality of engaging blocks, and the mounting portion is fixed to the first housing by engaging with the plurality of engaging blocks through the plurality of engaging holes.
In some embodiments, the housing includes a plurality of ribs, the mounting portion is formed with a plurality of protrusions, each protrusion defines a receiving slot, and each receiving slot is configured to receive one of the ribs.
According to the shielding device and the unmanned aerial vehicle, the interference of electronic components in the unmanned aerial vehicle on the global positioning system module can be effectively shielded, so that the global positioning system module can be accurately positioned and navigated in the flight process of the unmanned aerial vehicle.
Additional aspects and advantages of the invention will be set forth in part in the description which follows and, in part, will be obvious from the description, or may be learned by practice of the invention.
Drawings
The above and/or additional aspects and advantages of the present invention will become apparent and readily appreciated from the following description of the embodiments, taken in conjunction with the accompanying drawings of which:
fig. 1 is a perspective assembly schematic view of an unmanned aerial vehicle according to an embodiment of the present invention.
Fig. 2 is an exploded perspective view of the unmanned aerial vehicle of fig. 1.
Fig. 3 is a perspective exploded schematic view of a portion of the structure from another perspective of the UAV of fig. 2.
Fig. 4 is a perspective view of the shielding device of the unmanned aerial vehicle of fig. 3.
Description of the main element symbols:
the unmanned aerial vehicle 100, the first housing 10, the receiving space 10a, the first main body portion 12, the rib 122, the latch 124, the first arm portion 14, the rotor assembly 16, the second housing 20, the second main body portion 22, the second arm portion 24, the coupling portion 26, the battery module 30, the global positioning system module 40, the shielding device 50, the covering portion 52, the covering end 521, the through hole 522, the receiving groove 523, the receiving end 524, the side wall 526, the mounting portion 54, the latching hole 542, the protrusion 544, and the receiving groove 545.
Detailed Description
Reference will now be made in detail to embodiments of the present invention, examples of which are illustrated in the accompanying drawings, wherein like 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 accompanying drawings are illustrative only for the purpose of explaining the present invention, and are not to be construed as limiting the present invention.
In the description of the present invention, it is to be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise", and the like, indicate orientations and positional relationships based on those shown in the drawings, and are used only for convenience of description and simplicity of description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and thus, should not be considered as limiting the present invention. Furthermore, the terms "first", "second" and "first" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, features defined as "first", "second", may explicitly or implicitly include one or more of the described features. In the description of the present invention, "a plurality" means two or more unless specifically defined otherwise.
In the description of the present invention, it should be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, e.g., as meaning either a fixed connection, a removable connection, or an integral connection; may be mechanically connected, may be electrically connected or may be in communication with each other; either directly or indirectly through intervening media, either internally or in any other relationship. The specific meanings of the above terms in the present invention can be understood by those skilled in the art according to specific situations.
In the present invention, unless otherwise expressly stated or limited, "above" or "below" a first feature means that the first and second features are in direct contact, or that the first and second features are not in direct contact but are in contact with each other via another feature therebetween. Also, the first feature being "on," "above" and "over" the second feature includes the first feature being directly on and obliquely above the second feature, or merely indicating that the first feature is at a higher level than the second feature. A first feature being "under," "below," and "beneath" a second feature includes the first feature being directly under and obliquely below the second feature, or simply meaning that the first feature is at a lesser elevation than the second feature.
The following disclosure provides many different embodiments or examples for implementing different features of the invention. To simplify the disclosure of the present invention, the components and arrangements of specific examples are described below. Of course, they are merely examples and are not intended to limit the present invention. Furthermore, the present invention may repeat reference numerals and/or letters in the various examples, such repetition is for the purpose of simplicity and clarity and does not in itself dictate a relationship between the various embodiments and/or configurations discussed. In addition, the present invention provides examples of various specific processes and materials, but one of ordinary skill in the art may recognize applications of other processes and/or uses of other materials.
Referring to fig. 1 to 3, an unmanned aerial vehicle 100 according to an embodiment of the present invention is a quad-rotor vehicle, i.e., a vehicle having four rotor assemblies. It is understood that unmanned aerial vehicle 100 can also be a six-rotor aircraft, an eight-rotor aircraft, a twelve-rotor aircraft, etc., and even that unmanned aerial vehicle 100 can be a single-rotor aircraft; additionally, in certain embodiments, unmanned aerial vehicle 100 may be a fixed-wing aircraft, or a fixed-wing-rotor hybrid aircraft. Rotor assembly 16 includes an electric motor (not shown) and a propeller (not shown) coupled to the electric motor (not shown), and in the illustrated embodiment, the propeller of rotor assembly 16 is not shown, but rotor assembly 16 may be omitted. A motor (not shown) can drive the propeller to rotate to provide power for the flight of the unmanned aerial vehicle 100.
The unmanned aerial vehicle 100 includes a first housing 10, and a second housing 20 connected to the first housing 10, a battery module 30, a Global Positioning System (GPS) module 40, and a shielding device 50. The first housing 10 and the second housing 20 are combined to form an accommodating space 10a, and the battery module 30, the GPS module 40 and the shielding device 50 are accommodated in the accommodating space 10 a.
The first housing 10 includes a first main body portion 12 and a first arm portion 14. The first main body 12 is recessed inward, and a plurality of protruding ribs 122 and a plurality of locking blocks 124 are disposed on the recessed bottom surface, and the plurality of protruding ribs 122 are uniformly and radially distributed around the center of the first main body 12. The number of first arms 14 corresponds to the number of rotor assemblies 16 of unmanned aerial vehicle 100 for cooperating with second housing 20 to position corresponding rotor assemblies 16 in a predetermined position. In the present embodiment, the first arm portion 14 extends radially from the first main body portion 12, and more specifically, the first arm portion 14 is provided symmetrically with respect to the center of the first main body portion 12.
The second housing 20 includes a second main body portion 22, a second arm portion 24, and a joint portion 26. The second body portion 22 is recessed inwardly. The number of second arms 24 corresponds to the number of rotor assemblies 16 of unmanned aerial vehicle 100 and the number of first arms 14 for cooperating with first arms 14 to position corresponding rotor assemblies 16 in a predetermined position. In the present embodiment, the second arm portion 24 extends radially from the second main body portion 22, and more specifically, the second arm portion 24 is provided symmetrically with respect to the center of the second main body portion 22. Each joint 26 extends from each first arm portion 14 in a direction away from the housing space 10a for joining with a foot stand (not shown) of the unmanned aerial vehicle 100 so that the unmanned aerial vehicle can stand on the ground. The second housing 20 may be combined with the first housing 10 by any one or more of gluing, screwing, clamping, welding, etc., and the recess of the first body 12 and the recess of the first body 22 together form the receiving space 10 a.
In addition to providing power for the unmanned aerial vehicle 100, the battery module 30 further integrates a sensor (not shown) and a processing chip (not shown) for implementing functions of obstacle avoidance, positioning, speed measurement, navigation, and the like on the battery module 30.
The GPS module 40 and the shielding device 50 are fixed on the first housing 10, the GPS module 40 and the battery module 30 are respectively disposed at two sides of the shielding device 50 and electrically connected through a wire (not shown), and the shielding device 50 accommodates the GPS module 40.
Referring to fig. 2 to 4, the shielding device 50 includes a covering portion 52 and a mounting portion 54 extending from the covering portion 52 and surrounding the covering portion 52. The covering portion 52 is a cover structure, and includes a covering end 521, a containing end 524 opposite to the covering end, and a sidewall 526 connecting the covering end and the containing end. The shape of the cover structure may be circular, triangular, elliptical, rectangular, or other regular or irregular shapes, and in this embodiment, the cover structure is circular. The cover end 521 is provided with a through hole 522 for passing a wire connecting the GPS module 40 and the battery module 30. The accommodating end 524 is formed with an accommodating groove 523 for accommodating the GPS module 40. The mounting portion 54 extends from the sidewall 526 of the covering portion 52 to surround the covering portion 52, the mounting portion 54 is formed with a plurality of engaging holes 542 corresponding to the plurality of engaging blocks 124 and a plurality of protrusions 544 corresponding to the plurality of protruding ribs 122, each protrusion 544 is provided with a receiving groove 545, and each receiving groove 545 is used for receiving one protruding rib 122. The mounting portion 54 is fixed to the first housing 10 by engaging the plurality of engaging holes 542 with the plurality of engaging pieces 124, and at this time, the plurality of ribs 122 are received in the corresponding plurality of receiving grooves 545. The shape of the mounting part 54 matches the shape of the first housing 10 to be attached to the first housing 10, and preferably, the shape of the mounting part 54 matches the shape of the first housing 10 to be completely attached to the first housing 10, in other words, there is no gap between the mounting part 54 and the first housing 10.
When the shielding device 50 is mounted on the first housing 10, the GPS module 40 is received in the receiving slot and spaced apart from the covering portion 52, i.e. there is a gap therebetween.
The unmanned aerial vehicle 100 provided by the invention utilizes the covering part 52 of the shielding device 50 to accommodate the 6PS module 40, so that the GPS module 40 is isolated from other electronic components such as the battery module 30, the interference of other electronic components on the GPS module 40 is effectively shielded, the working performance of the GPS module is prevented from being influenced, and the positioning and navigation are ensured to be accurate. In addition, the unmanned aerial vehicle 100 is fixed on the first housing 10 by the mounting portion 54 in a clamping manner, so that the shielding device 50 is installed in cooperation with the first housing 10, the shielding device 50 is convenient to install and detach, and the operation is simple. Moreover, in the process of the unmanned aerial vehicle 100 falling and rising, the first housing 10, the second housing 20 and the internal components vibrate, and the space between the covering part 52 and the GPS module 40 can provide a moving space, so that on one hand, when the unmanned aerial vehicle 100 is dismounted, the shielding device 50 can be prevented from colliding with the GPS module 40 to damage the GPS module 40, the positioning and navigation accuracy of the unmanned aerial vehicle 100 is ensured, and the service life of the GPS module 4() is also prolonged; on the other hand, the movement space provided by the space between the covering portion 52 and the GPS module 40 effectively prevents the vibration generated by the shielding device 50 from directly acting on the GPS module 40, which may cause the GPS module 40 to loosen or fall off, thereby affecting the positioning and navigation accuracy of the unmanned aerial vehicle 100; similarly, the movement space provided by the space between the covering portion 52 and the GPS module 40 can also effectively prevent the vibration generated by the GPS module 40 from directly acting on the shielding device 50, which may cause the shielding device 50 to loosen or fall off, thereby reducing the shielding effect, and also affecting the positioning and navigation accuracy of the unmanned aerial vehicle 100. Moreover, since the mounting portion 54 is fixed on the first housing 10 and completely attached to the first housing 10, on one hand, the shielding device 50 can effectively shield electromagnetic interference generated by other electronic components, thereby ensuring the working performance of the GPS module 40; on the other hand, the fitting design of the mounting portion 54 and the first housing 10 can save the internal space and facilitate the layout of the components. The rib 122 in the first housing 10 can be used to reinforce the structure of the first housing 10, and the mounting portion 54 forms a protrusion 544 for receiving the rib 122, so as to ensure that the mounting portion 54 is well attached to the first housing 10.
In some embodiments, the rib 122 on the first housing 10 may be omitted, and correspondingly, the protrusion on the mounting portion 54 may also be omitted, that is, the structures of the first housing 10 and the mounting portion 54 may be arbitrarily set, and it is only necessary that the shape of the mounting portion 54 matches the shape of the first housing 10 to fit the first housing 10.
In some embodiments, the distance separating the covering portion 52 from the GPS module 40 may be set according to the specific size of the components in the first housing 10, for example, there may be no space between the covering portion 52 and the GPS module 40, such as just touching/completely fitting.
In some embodiments, the cover portion 52 is integrally formed with the mounting portion 54.
In this way, the manufacturing process of the shielding device 50 can be simplified, and the cost can be saved, for example, a metal plate with a suitable size can be selected for stamping and forming, and the assembly can be completed by matching with the specific structure of the first housing 10.
In some embodiments, unmanned aerial vehicle 100 further comprises a filler for filling the gap formed by the wire passing through via 522. The filler may be made of metal, for example, the filler may be made of any one or more of very thin gold, silver, copper, cupronickel, iron, aluminum.
It can be understood that the diameter of the wire is smaller than the diameter of the through hole 522, a gap is formed between the through hole 522 and the wire after the wire passes through, the gap will affect the shielding effect of the shielding device 50 on the electromagnetic interference, and the filler will reduce the effect on the shielding effect after the through hole 522 is formed to a certain extent.
In some embodiments, the mounting portion 54 may be further fixed to the first housing 10 by any one or more of adhesive bonding, screwing, welding, and the like. The threaded connection also facilitates the installation and removal of the shielding device 50. The first housing 10 can be directly fixed by adhesive bonding or welding without any other structure, and the process is simple and easy to operate.
In certain embodiments, the shielding device 50 is made of a metallic material.
Preferably, in some embodiments, the shielding device 50 is made of any one or more of gold, silver, copper, cupronickel, iron, aluminum.
Therefore, the shielding device 50 made of metal material can have good shielding effect on electromagnetic interference, and has certain rigidity after metal forming, is not easy to deform, and is attractive and practical.
In some embodiments, the thickness of the shielding device 50 is 0.2 millimeters or greater.
In this way, the shielding device 50 has a good shielding performance while not occupying too much inner space of the first housing 10.
In the description herein, references to the description of the terms "one embodiment," "some embodiments," "an illustrative embodiment," "an example," "a specific example," or "some examples" or the like mean that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the invention. In this specification, schematic representations of the above terms do not necessarily refer to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples.
Furthermore, the terms "first", "second" and "first" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include at least one such feature. In the description of the present invention, "a plurality" means at least two, e.g., two, three, etc., unless specifically limited otherwise.
Although embodiments of the present invention have been shown and described above, it is understood that the above embodiments are exemplary and not to be construed as limiting the present invention, and those skilled in the art can make changes, modifications, substitutions and alterations to the above embodiments within the scope of the present invention.
Claims (13)
1. A shielding device for an unmanned aerial vehicle, the unmanned aerial vehicle including a global positioning system module, the shielding device comprising:
the covering part is of a cover body structure, the cover body structure comprises a covering end, a containing end and a side wall, the containing end is opposite to the covering end, the side wall is connected with the covering end and the containing end, and the containing end is provided with a containing groove and used for containing the global positioning system module; and
the installation department, the installation department certainly cover portion extension and encircle cover portion, cover portion reaches the installation department is made by metal material, and integrated into one piece.
2. The shielding device of claim 1, wherein said cover portion is spaced from said global positioning system module.
3. The shielding device of claim 1, wherein said cover portion defines a through-hole.
4. The shielding apparatus of claim 1, wherein said mounting portion defines a plurality of engagement holes.
5. The shielding apparatus of claim 1, wherein the mounting portion defines a plurality of projections, each projection defining a receiving slot.
6. An unmanned vehicles, its characterized in that, unmanned vehicles includes first casing, fixes global positioning system module and shield assembly on the first casing, shield assembly includes:
the covering part is of a cover body structure, the cover body structure comprises a covering end, a containing end and a side wall, the containing end is opposite to the covering end, the side wall is connected with the covering end and the containing end, and the containing end is provided with a containing groove and used for containing the global positioning system module; and
the installation department, the installation department certainly cover portion extends and encircles cover portion, the installation department is installed on the first casing, cover portion reaches the installation department is made by metal material, and integrated into one piece.
7. The UAV of claim 6 wherein the cover is spaced from the GPS module.
8. The UAV of claim 6, wherein the cover defines a through hole, and further comprising a battery module and a wire, wherein the wire passes through the through hole and connects the GPS module and the battery module.
9. The UAV of claim 8 further comprising a filler to fill a gap formed by the wire passing through the via.
10. The UAV of claim 6 wherein the mount is shaped to match the shape of the first housing to conform to the first housing.
11. The UAV of claim 10 wherein the mount is secured to the first housing by one or more of adhesive bonding, threading, snapping, welding.
12. The UAV of claim 10, wherein the mounting portion defines a plurality of engaging holes, the first housing includes a plurality of clips, and the mounting portion is fixed to the first housing by engaging with the plurality of clips through the plurality of engaging holes.
13. The UAV of claim 10, wherein the first housing includes a plurality of ribs, the mounting portion defines a plurality of protrusions, each protrusion defines a slot, and each slot is configured to receive one of the ribs.
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621165021X | 2016-10-25 | ||
| CN201621165021.XU CN206118300U (en) | 2016-10-25 | 2016-10-25 | Shield assembly and unmanned vehicles |
| PCT/CN2016/108994 WO2018076468A1 (en) | 2016-10-25 | 2016-12-08 | Shielding apparatus and unmanned aerial vehicle |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN109644581A CN109644581A (en) | 2019-04-16 |
| CN109644581B true CN109644581B (en) | 2020-05-22 |
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| CN201621165021.XU Expired - Fee Related CN206118300U (en) | 2016-10-25 | 2016-10-25 | Shield assembly and unmanned vehicles |
| CN201680087991.9A Expired - Fee Related CN109644581B (en) | 2016-10-25 | 2016-12-08 | Shielding device and unmanned vehicles |
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| WO (1) | WO2018076468A1 (en) |
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| CN206118300U (en) * | 2016-10-25 | 2017-04-19 | 深圳市大疆创新科技有限公司 | Shield assembly and unmanned vehicles |
| CN118254981B (en) * | 2024-05-31 | 2024-07-26 | 国网上海市电力公司 | Unmanned aerial vehicle with electromagnetic protection structure for operation and detection of power transmission line and control method thereof |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN203844998U (en) * | 2014-01-24 | 2014-09-24 | 深圳一电科技有限公司 | Unmanned plane |
| CN104627361A (en) * | 2015-02-05 | 2015-05-20 | 深圳雷柏科技股份有限公司 | Modularized unmanned aerial vehicle |
| CN204392739U (en) * | 2014-12-26 | 2015-06-10 | 深圳市大疆创新科技有限公司 | Radiator structure and use the image transmission of this radiator structure |
| CN104787320A (en) * | 2015-04-23 | 2015-07-22 | 张�杰 | Communication anti-interference type four-rotor aircraft |
| CN205017462U (en) * | 2015-10-08 | 2016-02-03 | 深圳九星智能航空科技有限公司 | Panorama is kept watch on and is used unmanned aerial vehicle |
| CN105599895A (en) * | 2016-01-29 | 2016-05-25 | 浙江智天科技有限公司 | Multi-axis aircraft |
| CN206118300U (en) * | 2016-10-25 | 2017-04-19 | 深圳市大疆创新科技有限公司 | Shield assembly and unmanned vehicles |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20150102159A1 (en) * | 2013-10-15 | 2015-04-16 | Russ Hegarty | Waterproof multi-rotor unmanned flying apparatus |
-
2016
- 2016-10-25 CN CN201621165021.XU patent/CN206118300U/en not_active Expired - Fee Related
- 2016-12-08 WO PCT/CN2016/108994 patent/WO2018076468A1/en active Application Filing
- 2016-12-08 CN CN201680087991.9A patent/CN109644581B/en not_active Expired - Fee Related
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN203844998U (en) * | 2014-01-24 | 2014-09-24 | 深圳一电科技有限公司 | Unmanned plane |
| CN204392739U (en) * | 2014-12-26 | 2015-06-10 | 深圳市大疆创新科技有限公司 | Radiator structure and use the image transmission of this radiator structure |
| CN104627361A (en) * | 2015-02-05 | 2015-05-20 | 深圳雷柏科技股份有限公司 | Modularized unmanned aerial vehicle |
| CN104787320A (en) * | 2015-04-23 | 2015-07-22 | 张�杰 | Communication anti-interference type four-rotor aircraft |
| CN205017462U (en) * | 2015-10-08 | 2016-02-03 | 深圳九星智能航空科技有限公司 | Panorama is kept watch on and is used unmanned aerial vehicle |
| CN105599895A (en) * | 2016-01-29 | 2016-05-25 | 浙江智天科技有限公司 | Multi-axis aircraft |
| CN206118300U (en) * | 2016-10-25 | 2017-04-19 | 深圳市大疆创新科技有限公司 | Shield assembly and unmanned vehicles |
Also Published As
| Publication number | Publication date |
|---|---|
| WO2018076468A1 (en) | 2018-05-03 |
| CN109644581A (en) | 2019-04-16 |
| CN206118300U (en) | 2017-04-19 |
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