CN115196029A - Unmanned aerial vehicle with multi-rotor structure - Google Patents
Unmanned aerial vehicle with multi-rotor structure Download PDFInfo
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- CN115196029A CN115196029A CN202210682257.4A CN202210682257A CN115196029A CN 115196029 A CN115196029 A CN 115196029A CN 202210682257 A CN202210682257 A CN 202210682257A CN 115196029 A CN115196029 A CN 115196029A
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- unmanned aerial
- aerial vehicle
- vehicle body
- base station
- wireless base
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- 238000000034 method Methods 0.000 abstract description 17
- 230000001681 protective effect Effects 0.000 abstract description 12
- 239000008187 granular material Substances 0.000 abstract 1
- 230000002633 protecting effect Effects 0.000 abstract 1
- 230000000694 effects Effects 0.000 description 11
- 238000004891 communication Methods 0.000 description 6
- 230000000007 visual effect Effects 0.000 description 6
- 239000002245 particle Substances 0.000 description 5
- 230000007613 environmental effect Effects 0.000 description 4
- 238000009434 installation Methods 0.000 description 4
- 230000008447 perception Effects 0.000 description 4
- 230000006978 adaptation Effects 0.000 description 2
- 230000003139 buffering effect Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 description 1
- 230000004075 alteration Effects 0.000 description 1
- 230000002567 autonomic effect Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000012634 fragment Substances 0.000 description 1
- 229910052744 lithium Inorganic materials 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 229920000642 polymer Polymers 0.000 description 1
- 230000003014 reinforcing effect Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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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
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
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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
- B64D45/04—Landing aids; Safety measures to prevent collision with earth's surface
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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
- B64D47/00—Equipment not otherwise provided for
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- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Forklifts And Lifting Vehicles (AREA)
Abstract
The invention relates to the technical field of unmanned aerial vehicles with multiple rotor wing structures, and discloses an unmanned aerial vehicle with multiple rotor wing structures, which comprises an unmanned aerial vehicle body, wherein a connecting frame is arranged on the surface of the unmanned aerial vehicle body, rotor wings are arranged on the side surface of the connecting frame, a camera device is arranged at the top of the unmanned aerial vehicle body, a bearing and placing device is arranged at the bottom of the unmanned aerial vehicle body, and an auxiliary device is arranged at the bottom of the unmanned aerial vehicle body. This unmanned aerial vehicle with multi-rotor structure, the throwing line ware is used for the carry and control places wireless base station, protective equipment such as cooperation guard plate, can install the guard plate in the both sides of high performance computing equipment and wireless base station, can form the protection, make the protecting effect that unmanned aerial vehicle possessed good, can carry out effectual protection to wireless base station, can avoid the small granule piece to take place to collide with the damage that causes wireless base station with wireless base station in the flight process, can guarantee wireless base station's life, it is effectual when using.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicles with multi-rotor structures, in particular to an unmanned aerial vehicle with a multi-rotor structure.
Background
When natural disasters such as earthquake, flood, debris flow, ice and snow take place, can cause communication equipment damage in the short-term, the disaster area often faces the condition of large tracts of land communication interrupt, power interruption, road interruption, and communication can't be resumeed fast to ordinary emergent communication means, and in recent years, along with the breakthrough of key technologies such as high-efficient brushless motor, high energy lithium polymer battery, many rotors cooperative control, middle-size and small-size many rotors unmanned aerial vehicle is gradually ripe. Therefore, the portable communication base station and the intelligent carrier unmanned aerial vehicle are utilized, and the communication base station is deployed on the basis of a multi-rotor unmanned aerial vehicle platform, so that an important solution is provided.
Current unmanned aerial vehicle is for the information transfer between reinforcing and the ground, can be provided with the throwing line ware in the unmanned aerial vehicle bottom and be used for the carry and control to place wireless base station, but current unmanned aerial vehicle's protective effect is not good, can't carry out effectual protection to wireless base station, there is the tiny particle piece to take place to collide with the damage that causes wireless base station with wireless base station in flight process, influence wireless base station's life, effect when using is not good, need improve to this.
Disclosure of Invention
The invention aims to provide an unmanned aerial vehicle with a multi-rotor structure, so as to solve the problems in the background technology.
In order to achieve the purpose, the invention provides the following technical scheme:
the utility model provides an unmanned aerial vehicle with many rotor structures, includes the unmanned aerial vehicle body, the surface of unmanned aerial vehicle body is provided with the link, the side of link is provided with the rotor, the top of unmanned aerial vehicle body is provided with camera device, the bottom of unmanned aerial vehicle body is provided with holds puts the device, the bottom of unmanned aerial vehicle body is provided with auxiliary device.
Auxiliary device includes connecting plate, high performance computing equipment, guard plate, mounting panel, bolt, screw hole and throwing line ware, connecting plate fixed connection is in the bottom of throwing line ware, high performance computing equipment fixed connection is in the bottom of connecting plate, the inside at the connecting plate is seted up to the screw hole.
Preferably, camera device includes support frame, rack, inertia regulation and control equipment and camera, support frame fixed connection is in the top of unmanned aerial vehicle body, rack fixed connection is in the top of support frame, inertia regulation and control equipment fixed connection is in the top of rack.
Preferably, the device is put to holding includes supporting rack, supporting link, blotter and chassis, supporting rack fixed connection is in the bottom of unmanned aerial vehicle body, supporting link fixed connection is in the side of supporting rack, chassis fixed connection is in the bottom of supporting link, blotter fixed connection is in the surface of chassis.
Preferably, the quantity of link and rotor is six, six the equidistant distribution of link and rotor is on the surface of unmanned aerial vehicle body.
Preferably, the camera is connected in inertia regulation and control equipment, the camera comprises binocular degree of depth camera and wide angle camera lamp visual equipment, obtains detailed space point cloud environmental information, perception ground conditions through being provided with the camera of constituteing with binocular degree of depth camera and wide angle camera, makes it safer at the autonomous flight in-process, can further strengthen unmanned aerial vehicle security performance when flying, cooperation inertia regulation and control equipment utilizes the visual characteristic in the environment, even at unknown space, also can accurately track its route, security performance when using is stronger.
Preferably, the connecting screw hole that equals with screw hole aperture is seted up to the inside of mounting panel, bolt threaded connection can play the effect of erection joint mounting panel in the inside of screw hole and connecting screw hole through being provided with the bolt, cooperation screw hole and connecting screw to install the guard plate in the both sides of high performance computing equipment and wireless base station, can form the protection, make the protective effect that unmanned aerial vehicle possessed good, can carry out effectual protection to wireless base station, can guarantee wireless base station's life, effectual when using.
Preferably, the mounting groove has been seted up to the bottom of connecting plate, the mounting panel is pegged graft in the inside of mounting groove, the big or small adaptation of mounting panel and mounting groove through being provided with the mounting groove, can conveniently peg graft the mounting panel in the inside of connecting plate when the installation, can accomplish the effect that reaches the location fast, and cooperation bolt and screw hole can be in the same place mounting panel and connecting plate installation are fixed.
Preferably, the wire thrower is fixedly connected to the bottom of the support frame, the number of the support connecting frames and the number of the bottom frames are two, the two support connecting frames and the two bottom frames are symmetrically distributed on the left side and the right side of the support frame, and the wire thrower is used for mounting and controlling the placement of the wireless base station.
Compared with the prior art, the unmanned aerial vehicle with the multi-rotor structure provided by the invention has the following beneficial effects:
1. this unmanned aerial vehicle with many rotor structures, through being provided with auxiliary device, bottom at the unmanned aerial vehicle body is provided with the throwing line ware, the throwing line ware is used for the carry and controls and places wireless basic station, protective equipment such as cooperation guard plate, can install the both sides at high performance computing equipment and wireless basic station with the guard plate, can form the protection, make the protective effect that unmanned aerial vehicle possessed good, can carry out effectual protection to wireless basic station, can avoid the tiny particle piece to take place to collide with the damage that causes wireless basic station with wireless basic station at the flight in-process, can guarantee wireless basic station's life, it is effectual when using.
2. This unmanned aerial vehicle with multi-rotor structure, through being provided with camera device, wherein, support frame and rack play the effect that the camera was placed in the support, cooperation inertia regulation and control equipment, utilize the visual characteristics in the environment, even in unknown space, its route also can accurately be tracked, and through being provided with the camera of constituteing with binocular degree of depth camera and wide angle camera and acquire detailed space point cloud environmental information, perception ground conditions, make it safer at the autonomous flight in-process, can further strengthen the security performance of unmanned aerial vehicle when the flight.
3. This unmanned aerial vehicle with many rotor structures through being provided with and holding the device, when falling to the ground, can let the blotter and the ground contact on chassis surface, can play the effect of buffering to reduce the wearing and tearing to the chassis, increase the life of device, and can be more stable when falling to the ground, effectual when using.
Drawings
In order to more clearly illustrate the technical solutions in the embodiments of the present invention, the drawings needed to be used in the description of the embodiments are briefly introduced below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to the drawings without inventive labor:
fig. 1 is a schematic view of a three-dimensional appearance structure of an unmanned aerial vehicle according to an embodiment of the present invention;
fig. 2 is a schematic view of an internal main view structure of an unmanned aerial vehicle according to an embodiment of the present invention;
FIG. 3 is an enlarged view of the structure at A in FIG. 2 according to the present invention;
fig. 4 is a schematic partial sectional structure view of an auxiliary device, a supporting frame and the like of the unmanned aerial vehicle according to the embodiment of the invention;
FIG. 5 is an enlarged view of the structure at B in FIG. 4 according to the present invention.
In the figure: 1. an unmanned aerial vehicle body; 2. a rotor; 3. a connecting frame; 4. a camera device; 401. a support frame; 402. placing a rack; 403. an inertia control device; 404. a camera; 5. a bearing device; 501. a support frame; 502. a support link; 503. a cushion pad; 504. a chassis; 7. an auxiliary device; 701. a connecting plate; 702. a high performance computing device; 703. a protection plate; 704. mounting a plate; 705. a bolt; 706. a threaded hole; 707. and (7) a line throwing device.
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.
In the present invention, unless otherwise expressly stated or limited, the terms "mounted," "connected," "secured," and the like are to be construed broadly and can, for example, be fixedly connected, detachably connected, or integrally formed; can be mechanically or electrically connected; 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.
The first embodiment is as follows:
referring to fig. 1-5, the unmanned aerial vehicle with a multi-rotor structure provided by the invention comprises an unmanned aerial vehicle body 1, wherein a connecting frame 3 is arranged on the surface of the unmanned aerial vehicle body 1, a rotor 2 is arranged on the side surface of the connecting frame 3, and an auxiliary device 7 is arranged at the bottom of the unmanned aerial vehicle body 1.
The auxiliary device 7 comprises a connecting plate 701, high-performance computing equipment 702, a protective plate 703, a mounting plate 704, a bolt 705, a threaded hole 706 and a line throwing device 707, the connecting plate 701 is fixedly connected to the bottom of the line throwing device 707, the high-performance computing equipment 702 is fixedly connected to the bottom of the connecting plate 701, the threaded hole 706 is formed in the connecting plate 701, a connecting threaded hole with the same diameter as that of the threaded hole 706 is formed in the mounting plate 704, the bolt 705 is in threaded connection with the threaded hole 706 and the connecting threaded hole, a mounting groove is formed in the bottom of the connecting plate 701, the mounting plate 704 is inserted into the mounting groove, the mounting plate 704 is matched with the mounting groove in size, the line throwing device 707 is fixedly connected to the bottom of the supporting frame 501, the number of the supporting connecting frames 502 and the number of the bottom frames 504 are two, and the two supporting connecting frames 502 and the bottom frames 504 are symmetrically distributed on the left side and the right side of the supporting frame 501.
Through being provided with auxiliary device 7, bottom at the unmanned aerial vehicle body is provided with throwing line ware 707, throwing line ware 707 is used for the mount and control places wireless base station, protective equipment such as cooperation guard plate 703, can install the both sides at high performance computing equipment 702 and wireless base station with guard plate 703, can form the protection, make the protective effect that unmanned aerial vehicle possessed good, can carry out effectual protection to wireless base station, can avoid the tiny particle piece to take place to collide with wireless base station and cause wireless base station's damage at the flight in-process, can guarantee wireless base station's life, it is effectual when using.
The second embodiment:
on the basis of embodiment one, the unmanned aerial vehicle with multi-rotor structure that this embodiment provided, including unmanned aerial vehicle body 1, the surface of unmanned aerial vehicle body 1 is provided with link 3, the side of link 3 is provided with rotor 2, the top of unmanned aerial vehicle body 1 is provided with camera device 4, the bottom of unmanned aerial vehicle body 1 is provided with holds puts device 5, the bottom of unmanned aerial vehicle body 1 is provided with auxiliary device 7, the quantity of link 3 and rotor 2 is six, six links 3 and the equidistant distribution of rotor 2 are on the surface of unmanned aerial vehicle body 1.
The auxiliary device 7 comprises a connecting plate 701, a high-performance computing device 702, a protective plate 703, a mounting plate 704, bolts 705, threaded holes 706 and a wire thrower 707, wherein the connecting plate 701 is fixedly connected to the bottom of the wire thrower 707, the high-performance computing device 702 is fixedly connected to the bottom of the connecting plate 701, the threaded holes 706 are formed in the connecting plate 701, the wire thrower 707 is fixedly connected to the bottom of the support frame 501, the number of the support connecting frames 502 and the number of the base frames 504 are two, the two support connecting frames 502 and the base frames 504 are symmetrically distributed on the left side and the right side of the support frame 501, the wire thrower 707 is arranged and used for hanging and controlling placement of a wireless base station, connecting threaded holes with equal diameters of the threaded holes 706 are formed in the mounting plate 704, the bolts 705 are in threaded connection with the threaded holes 706 and the connecting threaded holes, through being provided with bolt 705, cooperation screw hole 706 and connection screw hole can play the effect of erection joint mounting panel 704, thereby install the both sides at high performance computing equipment 702 and wireless basic station with guard plate 703, can form the protection, make the protective effect that unmanned aerial vehicle possessed good, can carry out effectual protection to wireless basic station, can guarantee wireless basic station's life, effectual when using, the mounting groove has been seted up to connecting plate 701's bottom, mounting panel 704 pegs graft in the inside of mounting groove, mounting panel 704 and the big or small adaptation of mounting groove, through being provided with the mounting groove, can conveniently peg graft mounting panel 704 in connecting plate 701's inside when the installation, can accomplish the effect that reaches the location fast, cooperation bolt 705 and screw hole 706 can be in the same place mounting panel 704 and connecting plate 701 erection fixation.
The bearing device 5 comprises a bearing frame 501, a bearing connecting frame 502, a cushion pad 503 and a base frame 504, wherein the bearing frame 501 is fixedly connected to the bottom of the unmanned aerial vehicle body 1, the bearing connecting frame 502 is fixedly connected to the side surface of the bearing frame 501, the base frame 504 is fixedly connected to the bottom of the bearing connecting frame 502, and the cushion pad 503 is fixedly connected to the surface of the base frame 504.
In the actual operation process, when the device is used, the bottom of the unmanned aerial vehicle body 1 is provided with the line throwing device 707, the line throwing device 707 is used for hanging and controlling the placement of a wireless base station, when the device is used, in order to protect the wireless base station, some protective equipment is arranged at the bottom of the line throwing device 707, before the device is used, the protection plate 703 is required to be arranged at two sides of the high-performance computing equipment 702 and the wireless base station, when the device is installed, the mounting plate 704 at the top of the protection plate 703 can be aligned to the mounting groove at the bottom of the connecting plate 701, the mounting plate 704 is inserted into the mounting groove, the mounting plate 704 can be attached to the inner wall of the mounting groove, at the moment, the connecting screw hole in the mounting plate 704 is aligned to the screw hole 706 in the connecting plate 701, at the moment, the bolt 705 can be rotated by external force, the bolt 705 is in threaded connection with the connecting screw hole and the screw hole 706, so that the mounting plate 704 and the connecting plate 701 are fixed together, thereby accomplish the installation of guard plate 703, can install the both sides at high performance computing equipment 702 and wireless base station with guard plate 703, can form the protection, make the protective effect that unmanned aerial vehicle possessed good, can carry out effectual protection to wireless base station, can avoid in the flight in-process that the tiny particle piece takes place to collide with wireless base station and cause the damage of wireless base station, can guarantee wireless base station's life, it is effectual when using, be provided with camera device 4 at the top of unmanned aerial vehicle body 1, wherein, support frame 401 and rack 402 play the effect of support placing camera 404, cooperation inertia regulation and control equipment 403, visual characteristics in the utilization environment, even in unknown space, also can accurately track its route, and obtain detailed space point cloud environmental information through being provided with camera 404 that constitutes with two mesh degree of depth cameras and wide-angle camera, can form, perception ground conditions, it is safer at the autonomic flight in-process to make it, can further strengthen unmanned aerial vehicle security performance when flying, is provided with in the bottom of unmanned aerial vehicle body 1 and holds and put device 5, when falling to the ground, can let blotter 503 and the ground contact on chassis 504 surface, can play the effect of buffering to reduce the wearing and tearing to chassis 504, increase the life of device, and can be more stable when falling to the ground, effectual when using.
According to the unmanned aerial vehicle with the multi-rotor structure, the throwing line device is used for hanging, controlling and placing the wireless base station, and matching with protection devices such as the protection plate, the protection plate can be installed on two sides of the high-performance computing device and the wireless base station, protection can be formed, so that the unmanned aerial vehicle has a good protection effect, the wireless base station can be effectively protected, small particle fragments can be prevented from colliding with the wireless base station in a flight process to damage the wireless base station, the service life of the wireless base station can be ensured, and the effect is good in use.
It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. Without further limitation, an element described by the phrase "comprising a" does not exclude the presence of other identical elements in the process, method, article, or apparatus that comprises the element.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (8)
1. The utility model provides an unmanned aerial vehicle with many rotor structures, includes unmanned aerial vehicle body (1), its characterized in that: the unmanned aerial vehicle comprises an unmanned aerial vehicle body (1), and is characterized in that a connecting frame (3) is arranged on the surface of the unmanned aerial vehicle body (1), a rotor wing (2) is arranged on the side surface of the connecting frame (3), a camera device (4) is arranged at the top of the unmanned aerial vehicle body (1), a bearing and placing device (5) is arranged at the bottom of the unmanned aerial vehicle body (1), and an auxiliary device (7) is arranged at the bottom of the unmanned aerial vehicle body (1);
the auxiliary device (7) comprises a connecting plate (701), high-performance computing equipment (702), a protection plate (703), a mounting plate (704), a bolt (705), a threaded hole (706) and a wire thrower (707), wherein the connecting plate (701) is fixedly connected to the bottom of the wire thrower (707), the high-performance computing equipment (702) is fixedly connected to the bottom of the connecting plate (701), and the threaded hole (706) is formed in the connecting plate (701).
2. The drone with multi-rotor structure of claim 1, wherein: camera device (4) include support frame (401), rack (402), inertia regulation and control equipment (403) and camera (404), support frame (401) fixed connection is in the top of unmanned aerial vehicle body (1), rack (402) fixed connection is in the top of support frame (401), inertia regulation and control equipment (403) fixed connection is in the top of rack (402).
3. The unmanned aerial vehicle with multi-rotor structure of claim 1, wherein: bear and put device (5) including supporting rack (501), support link (502), blotter (503) and chassis (504), supporting rack (501) fixed connection is in the bottom of unmanned aerial vehicle body (1), support link (502) fixed connection is in the side of supporting rack (501), chassis (504) fixed connection is in the bottom of support link (502), blotter (503) fixed connection is in the surface of chassis (504).
4. The drone with multi-rotor structure of claim 1, wherein: the quantity of link (3) and rotor (2) is six, six link (3) and rotor (2) equidistant distribution are on the surface of unmanned aerial vehicle body (1).
5. The unmanned aerial vehicle with multi-rotor structure of claim 2, wherein: the camera (404) is connected to the inertia control equipment (403), and the camera (404) consists of a binocular depth camera and wide-angle camera lamp vision equipment.
6. The drone with multi-rotor structure of claim 1, wherein: the inside of mounting panel (704) is seted up and is connected the screw with screw hole (706) equal in aperture, bolt (705) threaded connection is in the inside of screw hole (706) and connection screw.
7. The drone with multi-rotor structure of claim 1, wherein: the bottom of the connecting plate (701) is provided with a mounting groove, the mounting plate (704) is inserted into the mounting groove, and the mounting plate (704) is matched with the mounting groove in size.
8. The unmanned aerial vehicle with multi-rotor structure of claim 1, wherein: the wire thrower (707) is fixedly connected to the bottom of the support frame (501), the number of the support connecting frames (502) and the number of the base frames (504) are two, and the two support connecting frames (502) and the base frames (504) are symmetrically distributed on the left side and the right side of the support frame (501).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202210682257.4A CN115196029A (en) | 2022-06-16 | 2022-06-16 | Unmanned aerial vehicle with multi-rotor structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202210682257.4A CN115196029A (en) | 2022-06-16 | 2022-06-16 | Unmanned aerial vehicle with multi-rotor structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN115196029A true CN115196029A (en) | 2022-10-18 |
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ID=83575528
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202210682257.4A Pending CN115196029A (en) | 2022-06-16 | 2022-06-16 | Unmanned aerial vehicle with multi-rotor structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN115196029A (en) |
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2022
- 2022-06-16 CN CN202210682257.4A patent/CN115196029A/en active Pending
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