CN219487730U - Unmanned aerial vehicle with prevent falling function - Google Patents
Unmanned aerial vehicle with prevent falling function Download PDFInfo
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- CN219487730U CN219487730U CN202320078858.4U CN202320078858U CN219487730U CN 219487730 U CN219487730 U CN 219487730U CN 202320078858 U CN202320078858 U CN 202320078858U CN 219487730 U CN219487730 U CN 219487730U
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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
- Y02T50/00—Aeronautics or air transport
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Abstract
The utility model discloses an unmanned aerial vehicle with an anti-falling function, which comprises an unmanned aerial vehicle body, wherein an auxiliary component is detachably arranged at one end of a support, and a protection component is detachably arranged on the upper surface of the unmanned aerial vehicle body.
Description
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicles, and particularly relates to an unmanned aerial vehicle with an anti-falling function.
Background
Unmanned aircraft is called unmanned aircraft for short, is unmanned aircraft operated by radio remote control equipment and a self-contained program control device, or is operated by a vehicle-mounted computer completely or intermittently and autonomously, and compared with unmanned aircraft, unmanned aircraft is more suitable for the tasks of being too dull, fool or dangerous, unmanned aircraft can be classified into military and civil, and in military aspects, unmanned aircraft is classified into a reconnaissance aircraft and a target aircraft, in civil aspects, unmanned aircraft and industrial application, and is really just needed by unmanned aircraft; application in fields of aerial photography, agriculture, plant protection, miniature self-timer, express delivery transportation, disaster relief, wild animal observation, infectious disease monitoring, mapping, news report, electric power inspection, disaster relief, film and television shooting, romantic manufacturing and the like greatly expands application of the unmanned aerial vehicle, and developed countries are also actively expanding industry application and unmanned aerial vehicle development technologies, and publication numbers: CN214356721U discloses an unmanned aerial vehicle with prevent falling function, including the unmanned aerial vehicle body, the bottom of unmanned aerial vehicle body is provided with the fixed block, stopper and fixed block interconnect, this unmanned aerial vehicle with prevent falling function, the fixed block, the spout, the slider, the movable block, the inside groove, first spring, the movable rod, the bracing piece, the dead slot, the telescopic link, mutually support of second spring and bottom plate, when making unmanned aerial vehicle body plane drop, can be protected by parts such as baffle and second spring, avoid unmanned aerial vehicle body damage, when unmanned aerial vehicle body side drops, can be protected by parts such as movable rod and first spring, the damage that the omnidirectional unmanned aerial vehicle body that avoids dropping to cause is provided with mutually support of parts such as gag lever post, stopper and round pin axle, when making rotation gag lever post, can with the stopper block, avoid preventing falling the device.
The problems with the above techniques are: at present unmanned aerial vehicle opportunity uses in express delivery transportation, can require unmanned aerial vehicle's speed to be fast, but in order to prevent that the speed from being too fast to lead to unmanned aerial vehicle to collide with foreign object, make unmanned aerial vehicle fall, receive the damage, can install prevent falling mechanism, protection machanism on the current prevent falling unmanned aerial vehicle, it is too heavy, make unmanned aerial vehicle's speed reduce, lead to work efficiency to descend, and when unmanned aerial vehicle falls to the ground, operating personnel mishandling leads to unmanned aerial vehicle to fall to the ground fast, make unmanned aerial vehicle's support receive the damage, therefore we propose an unmanned aerial vehicle with prevent falling function.
Disclosure of Invention
Aiming at the problems existing in the prior art, the utility model provides the unmanned aerial vehicle with the anti-falling function, which has the advantages that when the unmanned aerial vehicle falls down, damage caused by collision of the unmanned aerial vehicle with foreign objects can be prevented, the unmanned aerial vehicle is protected by the screw and is damped, the problems that the unmanned aerial vehicle can be used in express delivery transportation at present, the unmanned aerial vehicle is required to be fast, but in order to prevent collision of the unmanned aerial vehicle with the foreign objects caused by the too fast speed, the unmanned aerial vehicle falls down and is damaged, an anti-falling mechanism is installed, the existing protection mechanism on the anti-falling unmanned aerial vehicle is too heavy, the speed of the unmanned aerial vehicle is reduced, the working efficiency is reduced, and when the unmanned aerial vehicle falls down, operators operate improperly, the unmanned aerial vehicle falls down quickly, and the support of the unmanned aerial vehicle is damaged are solved.
The utility model discloses an unmanned aerial vehicle with an anti-falling function, which comprises an unmanned aerial vehicle body, wherein a protection component is detachably arranged on the upper surface of the unmanned aerial vehicle body, propellers are fixedly arranged at four corners of the outer surface of the unmanned aerial vehicle body, the protection component corresponds to the propellers, a transportation mounting plate is fixedly arranged on the lower surface of the unmanned aerial vehicle body, a camera is rotatably arranged on the lower surface of the transportation mounting plate, a mounting piece is detachably arranged on the lower surface of the unmanned aerial vehicle body, a support is fixedly arranged on one side of the mounting piece, and an auxiliary component is detachably arranged at one end of the support.
As the preferable mode of the utility model, the protection component comprises a protection sleeve, a second connecting rod is fixedly arranged on one side of the protection sleeve, a connecting sleeve is fixedly arranged at one end of the second connecting rod, a first screw is connected with the lower end of the connecting sleeve in a threaded manner, and the protection sleeve is fixed on the unmanned aerial vehicle body through the connecting sleeve.
As the preferable mode of the utility model, one side of the second connecting rod is fixedly provided with the first connecting rod, one end of the first connecting rod is fixedly provided with the protective cover, the protective cover corresponds to the propeller, and the outer surface of the protective cover is provided with the auxiliary hole.
As preferable in the utility model, the lower surface of the first connecting rod is fixedly provided with an auxiliary sleeve, and the lower end of the auxiliary sleeve is connected with a second screw in a threaded manner.
As the preferable mode of the utility model, the auxiliary assembly comprises a mounting block, a notch is formed in the mounting block, a damping spring is fixedly arranged in the notch, a placing plate is fixedly arranged on the upper surface of the damping spring, and the placing plate corresponds to the bracket.
As preferable in the utility model, a first fixed block is fixedly arranged on one side of the installation block, a connecting piece is fixedly arranged on the upper surface of the first fixed block, a second fixed block is fixedly arranged on the other side of the installation block, a slotted hole is formed in the upper surface of the second fixed block, and one end of the connecting piece corresponds to the slotted hole.
In the present utility model, preferably, a bolt is inserted into the second fixing block, the bolt corresponds to the connecting piece, and one end of the bolt is connected with a nut in a threaded manner.
Compared with the prior art, the utility model has the following beneficial effects:
1. according to the utility model, through the design of the unmanned aerial vehicle body, the protection component, the screw, the transportation mounting plate, the camera, the mounting part, the support and the auxiliary component, the protection component is detachably mounted on the upper surface of the unmanned aerial vehicle body, the effect that the unmanned aerial vehicle can be prevented from being damaged when falling down and colliding with foreign objects is achieved when the unmanned aerial vehicle falls down, the protection component comprises the protection sleeve and the protection cover, the second connecting rod is fixedly mounted at four corners of the outer surface of the protection sleeve, the connecting sleeve is fixedly mounted at one end of the second connecting rod, so that the protection sleeve is matched with the connecting sleeve through the second connecting rod, the first connecting rod is fixedly mounted at one end of the second connecting rod, the protection cover is fixedly mounted at one end of the first connecting rod, the protection cover is mounted at the periphery of the screw, the protection cover is simultaneously mounted at the periphery of the screw, the effect of protecting the screw is achieved, the auxiliary hole is formed in the outer surface of the protection cover, the effect that the screw is prevented from being reduced when the unmanned aerial vehicle is used, the mounting part is detachably mounted on the lower surface of the unmanned aerial vehicle body, the support is fixedly mounted at one side of the support, the auxiliary component is detachably mounted at one end of the protection component, and the auxiliary component is detachably mounted at the time of the unmanned aerial vehicle.
2. According to the utility model, through the design of the protective sleeve, the second connecting rod, the connecting sleeve, the first screw and the unmanned aerial vehicle body, the connecting sleeve is fixedly arranged on one side of the protective sleeve, one end of the second connecting rod is fixedly provided with the connecting sleeve, and the first screw is connected with the lower end of the connecting sleeve in a threaded manner, so that the connecting sleeve is arranged on the horn of the unmanned aerial vehicle body, and the effect of convenient fixing is achieved by screwing the first screw.
3. According to the utility model, through the design of the second connecting rod, the first connecting rod, the protective cover, the propeller and the auxiliary hole, the first connecting rod is fixedly arranged on one side of the second connecting rod, and the protective cover is fixedly arranged at one end of the first connecting rod, so that the effect of conveniently arranging the protective cover around the propeller can be achieved through the cooperation of the first connecting rod and the protective cover.
4. According to the utility model, through the design of the first connecting rod, the auxiliary sleeve and the second screw, the auxiliary sleeve is fixedly arranged on the lower surface of the first connecting rod, and the second screw is connected to the lower end of the auxiliary sleeve in a threaded manner, so that after the second connecting rod is fixed, the first connecting rod is matched with the second screw through the auxiliary sleeve, and the effect of stabilizing the second connecting rod is achieved.
5. According to the utility model, through the design of the mounting block, the damping spring, the placement plate and the support, the slotted hole is formed in the mounting block, the damping spring is fixedly arranged in the slotted hole, and the placement plate is fixedly arranged on the upper surface of the damping spring, so that when the mounting block is fixed at one end of the support, the unmanned aerial vehicle can perform damping effect on the unmanned aerial vehicle when falling or landing.
6. According to the utility model, through the design of the mounting block, the first fixing block, the connecting piece and the second fixing block, the first fixing block is fixedly arranged on one side of the mounting block, the connecting piece is fixedly arranged on the upper surface of the first fixing block, and the second fixing block is fixedly arranged on the other side of the mounting block, so that when the bracket is arranged in the mounting block, the effect of conveniently fixing the bracket is achieved through the cooperation of the first fixing block, the connecting piece and the second fixing block.
7. According to the utility model, through the design of the second fixed block, the bolt, the connecting piece and the nut, the bolt is connected in the second fixed block in a penetrating way, and one end of the bolt is connected with the nut in a threaded way, so that when one end of the connecting piece is installed in the second fixed block, the effect of fixing the connecting piece is achieved through the cooperation of the bolt and the nut.
Drawings
Fig. 1 is a schematic perspective view of the whole structure of an unmanned aerial vehicle according to an embodiment of the present utility model;
fig. 2 is a schematic perspective view of a partial structure of a unmanned aerial vehicle according to an embodiment of the present utility model;
FIG. 3 is a schematic perspective view of a guard assembly according to an embodiment of the present utility model;
FIG. 4 is a schematic perspective view of an auxiliary group structure provided by an embodiment of the present utility model;
fig. 5 is an enlarged schematic perspective view of fig. 3 at a provided in accordance with an embodiment of the present utility model.
In the figure: 1. an unmanned aerial vehicle body; 2. a protective assembly; 3. a propeller; 4. a bracket; 5. an auxiliary component; 6. a camera; 7. a transport mounting plate; 8. a mounting member; 201. a protective sleeve; 202. a protective cover; 203. a first connecting rod; 204. a second connecting rod; 205. connecting sleeves; 206. a first screw; 207. an auxiliary sleeve; 208. a second screw; 209. an auxiliary hole; 501. a mounting block; 502. a first fixed block; 503. a connecting piece; 504. a second fixed block; 505. placing a plate; 506. a damping spring; 507. a bolt; 508. and (3) a nut.
Detailed Description
For a further understanding of the utility model, its features and advantages, reference is now made to the following examples, which are illustrated in the accompanying drawings.
The structure of the present utility model will be described in detail with reference to the accompanying drawings.
As shown in fig. 1 to 5, the unmanned aerial vehicle with anti-falling function provided by the embodiment of the utility model comprises an unmanned aerial vehicle body 1, wherein a protection component 2 is detachably arranged on the upper surface of the unmanned aerial vehicle body 1, a propeller 3 is fixedly arranged at four corners of the outer surface of the unmanned aerial vehicle body 1, the protection component 2 corresponds to the propeller 3, a transportation mounting plate 7 is fixedly arranged on the lower surface of the unmanned aerial vehicle body 1, a camera 6 is rotatably arranged on the lower surface of the transportation mounting plate 7, a mounting piece 8 is detachably arranged on the lower surface of the unmanned aerial vehicle body 1, a support 4 is fixedly arranged on one side of the mounting piece 8, and an auxiliary component 5 is detachably arranged at one end of the support 4.
The scheme is adopted: through unmanned aerial vehicle body 1, protection component 2, screw 3, transport mounting panel 7, camera 6, mounting 8, support 4, auxiliary assembly 5's design, make unmanned aerial vehicle body 1 upper surface demountable installation have protection component 2, reached when unmanned aerial vehicle drops, can prevent unmanned aerial vehicle when dropping and collide with the foreign object, the effect that leads to the damage, protection component 2 includes lag 201 and protection casing 202, the equal fixed mounting in lag 201 surface four corners has second connecting rod 204, second connecting rod 204 one end fixed mounting has adapter sleeve 205, thereby lag 201 passes through the cooperation of second connecting rod 204 and adapter sleeve 205, the effect of convenient installation has been reached, second connecting rod 204 one end fixed mounting has head rod 203, head rod 203 one end fixed mounting has protection casing 202, make at installation lag 201, simultaneously install protection casing 202 around screw 3, thereby the effect of protecting screw 3 has been reached, auxiliary hole 209 has been seted up to the surface of protection casing 202, make through auxiliary hole 209, the effect that screw 3 can not reduce unmanned aerial vehicle body in use, unmanned aerial vehicle 1 surface mounting 8 has the effect that can be dismantled at 5 one side of the fixed mounting of support 4, can make the auxiliary assembly 5 one side of unmanned aerial vehicle 8, can be dismantled at 5.
Referring to fig. 3, the protection assembly 2 includes a protection sleeve 201, a second connecting rod 204 is fixedly installed at one side of the protection sleeve 201, a connecting sleeve 205 is fixedly installed at one end of the second connecting rod 204, a first screw 206 is connected to the lower end of the connecting sleeve 205 in a threaded manner, and the protection sleeve 201 is fixed on the unmanned aerial vehicle body 1 through the connecting sleeve 205.
The scheme is adopted: through the design of lag 201, second connecting rod 204, adapter sleeve 205, first screw 206 and unmanned aerial vehicle body 1 for lag 201 one side fixed mounting has second connecting rod 204, second connecting rod 204 one end fixed mounting to have adapter sleeve 205, and adapter sleeve 205 lower extreme threaded connection has first screw 206, thereby installs adapter sleeve 205 on the horn of unmanned aerial vehicle body 1, through screwing up first screw 206, thereby has reached the effect of convenient fixed.
Referring to fig. 3, a first connecting rod 203 is fixedly installed at one side of a second connecting rod 204, a protective cover 202 is fixedly installed at one end of the first connecting rod 203, the protective cover 202 corresponds to the propeller 3, and an auxiliary hole 209 is formed in the outer surface of the protective cover 202.
The scheme is adopted: through the design of second connecting rod 204, head rod 203, protection casing 202, screw 3 and auxiliary hole 209 for second connecting rod 204 one side fixed mounting has head rod 203, and head rod 203 one end fixed mounting has protection casing 202, makes through the cooperation of head rod 203 and protection casing 202, can reach the effect of making things convenient for the protection casing 202 to install around screw 3.
Referring to fig. 3, an auxiliary sleeve 207 is fixedly installed on the lower surface of the first connection rod 203, and a second screw 208 is screw-coupled to the lower end of the auxiliary sleeve 207.
The scheme is adopted: through the design of head rod 203, auxiliary sleeve 207 and second screw 208 for head rod 203 lower surface fixed mounting has auxiliary sleeve 207, and auxiliary sleeve 207 lower extreme threaded connection has second screw 208, thereby when second connecting rod 204 is fixed, head rod 203 passes through auxiliary sleeve 207 and second screw 208 cooperation, has reached the effect that can make second connecting rod 204 firm.
Referring to fig. 4, the auxiliary assembly 5 includes a mounting block 501, a slot is formed in the mounting block 501, a damper spring 506 is fixedly mounted in the slot, a placement plate 505 is fixedly mounted on the upper surface of the damper spring 506, and the placement plate 505 corresponds to the bracket 4.
The scheme is adopted: through the design of installation piece 501, damping spring 506, place board 505 and support 4 for set up the slotted hole in the installation piece 501, fixed mounting has damping spring 506 in the slotted hole, damping spring 506 goes up fixed surface and installs places board 505, thereby when fixing installation piece 501 in support 4 one end, unmanned aerial vehicle can carry out the absorbing effect to unmanned aerial vehicle when dropping or descending.
Referring to fig. 4, a first fixing block 502 is fixedly installed on one side of a mounting block 501, a connecting piece 503 is fixedly installed on the upper surface of the first fixing block 502, a second fixing block 504 is fixedly installed on the other side of the mounting block 501, a slot hole is formed in the upper surface of the second fixing block 504, and one end of the connecting piece 503 corresponds to the slot hole.
The scheme is adopted: through the design of installation piece 501, first fixed block 502, connecting piece 503 and second fixed block 504 for installation piece 501 one side fixed mounting has first fixed block 502, and fixed surface installs connecting piece 503 on the first fixed block 502, and installation piece 501 opposite side fixed mounting has second fixed block 504, thereby installs in installation piece 501 when support 4, through the cooperation of first fixed block 502, connecting piece 503 and second fixed block 504, has reached the effect of conveniently fixing support 4.
Referring to fig. 5, a bolt 507 is inserted into the second fixing block 504, the bolt 507 corresponds to the connecting member 503, and a nut 508 is screwed to one end of the bolt 507.
The scheme is adopted: through the design of second fixed block 504, bolt 507, connecting piece 503 and nut 508 for the interlude is connected with bolt 507 in the second fixed block 504, and bolt 507 one end threaded connection has nut 508, thereby when connecting piece 503 one end was installed in second fixed block 504, through the cooperation of bolt 507 and nut 508, reached the fixed effect to connecting piece 503.
The working principle of the utility model is as follows:
when using, first unmanned aerial vehicle body 1 upper surface demountable installation has protective component 2, reached when unmanned aerial vehicle drops, can prevent that unmanned aerial vehicle from dropping and bumping with the foreign object, the effect that leads to the damage, protective component 2 includes lag 201 and protection casing 202, the equal fixed mounting in lag 201 surface four corners has second connecting rod 204, second connecting rod 204 one end fixed mounting has adapter sleeve 205, thereby lag 201 has reached the effect of easy to assemble through the cooperation of second connecting rod 204 and adapter sleeve 205, second connecting rod 204 one end fixed mounting has head rod 203, head rod 203 one end fixed mounting has protection casing 202, make at installation lag 201, install protection casing 202 around screw 3 simultaneously, thereby the effect of protecting screw 3 has been reached, auxiliary hole 209 has been seted up to the protection casing 202 surface, make through auxiliary hole 209, the effect that screw 3 can not reduce unmanned aerial vehicle flight speed when using, unmanned aerial vehicle body 1 lower surface demountable mounting has mounting 8, mounting 8 one side fixed mounting has support 4, support 4 one end demountable mounting has auxiliary assembly 5, make it can make the shock attenuation effect to the unmanned aerial vehicle when 5 is downtake place.
To sum up: this unmanned aerial vehicle with prevent falling function, through unmanned aerial vehicle body 1, protection component 2, screw 3, support 4, auxiliary assembly 5, camera 6, transport mounting panel 7, mounting 8, the lag 201, protection casing 202, head rod 203, second connecting rod 204, adapter sleeve 205, first screw 206, auxiliary sleeve 207, second screw 208, auxiliary hole 209, installation piece 501, first fixed block 502, connecting piece 503, second fixed block 504, place the board 505, damping spring 506, bolt 507 and nut 508 between the cooperation, the present unmanned aerial vehicle opportunity is used in the express delivery transportation has been solved, but can require unmanned aerial vehicle's speed to be fast, but in order to prevent that the too fast unmanned aerial vehicle from colliding with the foreign object, make unmanned aerial vehicle fall, receive the damage, can install prevent falling mechanism, the protection mechanism on the unmanned aerial vehicle of current anti-falling, it is too heavy, make unmanned aerial vehicle's speed reduce, lead to work efficiency decline, and when unmanned aerial vehicle falls to the ground, operating personnel operate improperly, lead to unmanned aerial vehicle to the quick landing, make unmanned aerial vehicle's support receive the problem of damage.
It is noted that relational terms such as first and second, and the like are 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. Moreover, 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.
Although embodiments of the present utility model have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made therein without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.
Claims (7)
1. Unmanned aerial vehicle with prevent falling function, including unmanned aerial vehicle body (1), its characterized in that: unmanned aerial vehicle body (1) upper surface demountable installation has protection subassembly (2), unmanned aerial vehicle body (1) surface four corners fixed mounting has screw (3), protection subassembly (2) are corresponding with screw (3), unmanned aerial vehicle body (1) lower surface mounting transportation mounting panel (7), transportation mounting panel (7) lower surface rotation installs camera (6), unmanned aerial vehicle body (1) lower surface demountable installation has installed mounting (8), installed mounting (8) one side fixed mounting has support (4), auxiliary assembly (5) are dismantled to support (4) one end.
2. The unmanned aerial vehicle with anti-drop function of claim 1, wherein: the protection assembly (2) comprises a protection sleeve (201), a second connecting rod (204) is fixedly arranged on one side of the protection sleeve (201), a connecting sleeve (205) is fixedly arranged at one end of the second connecting rod (204), a first screw (206) is connected with the lower end of the connecting sleeve (205) in a threaded mode, and the protection sleeve (201) is fixed on the unmanned aerial vehicle body (1) through the connecting sleeve (205).
3. The unmanned aerial vehicle with anti-drop function of claim 2, wherein: the novel propeller is characterized in that a first connecting rod (203) is fixedly arranged on one side of the second connecting rod (204), a protective cover (202) is fixedly arranged at one end of the first connecting rod (203), the protective cover (202) corresponds to the propeller (3), and an auxiliary hole (209) is formed in the outer surface of the protective cover (202).
4. A drone with anti-crash functionality as claimed in claim 3, wherein: an auxiliary sleeve (207) is fixedly arranged on the lower surface of the first connecting rod (203), and a second screw (208) is connected with the lower end of the auxiliary sleeve (207) in a threaded manner.
5. The unmanned aerial vehicle with anti-drop function of claim 1, wherein: the auxiliary assembly (5) comprises a mounting block (501), a notch is formed in the mounting block (501), a damping spring (506) is fixedly mounted in the notch, a placing plate (505) is fixedly mounted on the upper surface of the damping spring (506), and the placing plate (505) corresponds to the support (4).
6. The unmanned aerial vehicle with anti-drop function of claim 5, wherein: the mounting block is characterized in that a first fixed block (502) is fixedly arranged on one side of the mounting block (501), a connecting piece (503) is fixedly arranged on the upper surface of the first fixed block (502), a second fixed block (504) is fixedly arranged on the other side of the mounting block (501), a slotted hole is formed in the upper surface of the second fixed block (504), and one end of the connecting piece (503) corresponds to the slotted hole.
7. The unmanned aerial vehicle with anti-drop function of claim 6, wherein: and a bolt (507) is inserted into the second fixing block (504), the bolt (507) corresponds to the connecting piece (503), and one end of the bolt (507) is connected with a nut (508) in a threaded manner.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202320078858.4U CN219487730U (en) | 2023-01-10 | 2023-01-10 | Unmanned aerial vehicle with prevent falling function |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202320078858.4U CN219487730U (en) | 2023-01-10 | 2023-01-10 | Unmanned aerial vehicle with prevent falling function |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN219487730U true CN219487730U (en) | 2023-08-08 |
Family
ID=87480933
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202320078858.4U Active CN219487730U (en) | 2023-01-10 | 2023-01-10 | Unmanned aerial vehicle with prevent falling function |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN219487730U (en) |
-
2023
- 2023-01-10 CN CN202320078858.4U patent/CN219487730U/en active Active
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Effective date of registration: 20230824 Address after: 528200, Room 201, 2nd Floor, No. 19 Guicheng Nanxin Fifth Road, Nanhai District, Foshan City, Guangdong Province (Residence Declaration) Patentee after: Guangdong Jiabo Yuhong Information Technology Co.,Ltd. Address before: 570000 South West Point, the intersection of Nanhai Avenue and Shugang Highway, Xiuying District, Haikou City, Hainan Province Patentee before: Haikou Liuxiling Electronic Technology Co.,Ltd. |
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