CN112009707A - Unmanned aerial vehicle aircraft tracking device based on security protection control chip - Google Patents
Unmanned aerial vehicle aircraft tracking device based on security protection control chip Download PDFInfo
- Publication number
- CN112009707A CN112009707A CN202010907590.1A CN202010907590A CN112009707A CN 112009707 A CN112009707 A CN 112009707A CN 202010907590 A CN202010907590 A CN 202010907590A CN 112009707 A CN112009707 A CN 112009707A
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- Prior art keywords
- aerial vehicle
- unmanned aerial
- camera
- device based
- tracking device
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- 230000007246 mechanism Effects 0.000 claims abstract description 31
- 238000012544 monitoring process Methods 0.000 claims abstract description 25
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 24
- 238000009434 installation Methods 0.000 claims description 14
- 239000000428 dust Substances 0.000 claims description 13
- 239000007921 spray Substances 0.000 claims description 8
- 235000017166 Bambusa arundinacea Nutrition 0.000 claims description 3
- 235000017491 Bambusa tulda Nutrition 0.000 claims description 3
- 241001330002 Bambuseae Species 0.000 claims description 3
- 235000015334 Phyllostachys viridis Nutrition 0.000 claims description 3
- 239000011425 bamboo Substances 0.000 claims description 3
- 230000009471 action Effects 0.000 description 6
- 230000000694 effects Effects 0.000 description 6
- 238000000034 method Methods 0.000 description 4
- 230000000903 blocking effect Effects 0.000 description 3
- 230000003139 buffering effect Effects 0.000 description 2
- 230000007547 defect Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000009977 dual effect Effects 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 1
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 238000011010 flushing procedure Methods 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 230000007257 malfunction Effects 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 238000012806 monitoring device Methods 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
- 238000005086 pumping Methods 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 238000005406 washing Methods 0.000 description 1
Images
Classifications
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B08—CLEANING
- B08B—CLEANING IN GENERAL; PREVENTION OF FOULING IN GENERAL
- B08B3/00—Cleaning by methods involving the use or presence of liquid or steam
- B08B3/02—Cleaning by the force of jets or sprays
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Studio Devices (AREA)
Abstract
The invention discloses an unmanned aerial vehicle aircraft tracking device based on a security monitoring chip, which comprises an unmanned aerial vehicle body, wherein the lower surface of the unmanned aerial vehicle body is provided with a mounting mechanism, the lower surfaces of the front side and the rear side of the mounting mechanism are respectively provided with a monitoring mechanism, the front surface of the mounting mechanism is provided with a protection mechanism, the front surface of a fixed block is provided with a positioning groove, and two side surfaces of the fixed block are respectively embedded with a positioning cylinder in a sliding manner. The invention relates to the technical field of unmanned aerial vehicle application, and discloses an unmanned aerial vehicle aircraft tracking device based on a security monitoring chip.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicle application, in particular to an unmanned aerial vehicle aircraft tracking device based on a security monitoring chip.
Background
The unmanned aerial vehicle is an unmanned plane, the unmanned aerial vehicle receives a remote control signal (when the ground station is controlled, the ground station sends an autonomous flight instruction to flight control through a cloud navigation lamp or a radio station) sent by a remote controller, and after the autonomous flight instruction is processed by a flight control program, the rotating speed of each motor is controlled through electric regulation, so that the purpose of controlling the action of the unmanned aerial vehicle is achieved.
But at present with unmanned aerial vehicle carry out the security protection during operation, the installation between camera and the unmanned aerial vehicle is all fixed through the screw, consequently inconvenient carries out the dismouting to the camera, does not carry out corresponding improvement to this defect.
Disclosure of Invention
Aiming at the defects of the prior art, the invention provides an unmanned aerial vehicle aircraft tracking device based on a security monitoring chip, which solves the problem that the camera is not convenient to disassemble and assemble because the camera and the unmanned aerial vehicle are fixed through screws.
In order to achieve the purpose, the invention is realized by the following technical scheme: the utility model provides an unmanned aerial vehicle aircraft tracking means based on security protection monitoring chip, includes the unmanned aerial vehicle body, the lower surface of unmanned aerial vehicle body is provided with installation mechanism, installation mechanism's front and back side lower surface all is provided with monitoring mechanism, and installation mechanism's front surface is provided with protection machanism.
The mounting mechanism comprises a fixed block, a positioning groove is formed in the front surface of the fixed block, positioning cylinders are embedded into two side surfaces of the fixed block in a sliding manner, a containing cavity is arranged in the fixed block, a limiting block is vertically connected to the middle position of the upper surface in the containing cavity, a sliding shaft penetrates through one side of the lower end of the limiting block, two ends of the sliding shaft are respectively embedded into and slidably mounted in the opposite ends of the two positioning cylinders, first springs are respectively sleeved on the outer surfaces of the two ends of the sliding shaft in a sliding manner, two ends of each first spring are respectively fixedly connected with one end of each positioning cylinder and one side surface of the limiting block, a sliding rod is embedded into the middle position of the lower surface in the containing cavity in a sliding manner, a stop block is fixedly connected to the upper end of each sliding rod, and an adjusting rod, the outer surface of the upper end of the sliding rod is sleeved with a second spring in a sliding mode, and the upper end and the lower end of the second spring are fixedly connected with the lower surface of the stop block and the inner lower surface of the accommodating cavity respectively.
Preferably, four corners of the upper surface of fixed block all are provided with the lug, pass through bolt fixed connection between the lower surface of lug and unmanned aerial vehicle body.
Preferably, the middle position of the lower surface of the fixed block is embedded with a handle in a sliding manner, and the upper end of the handle is fixedly connected with the lower end of the sliding rod.
Preferably, the monitoring mechanism is including the camera, the one end both sides face of camera all is provided with the L shaped plate, and the other end top front surface of camera is provided with the dust board, the upper surface of dust board runs through and installs the shower nozzle, fixed surface is connected with the storage water tank on the other end of camera, the conveyer pipe is installed in the below front surface embedding of storage water tank, the other end of conveyer pipe and the upper end fixed connection of shower nozzle.
Preferably, the camera is embedded in a positioning groove in the fixed block in a sliding manner, positioning holes corresponding to the positioning cylinders are formed in the side faces of one ends of the two L-shaped plates, and the positioning cylinders are embedded in the positioning holes in a sliding manner when the first spring and the second spring are in a normal state.
Preferably, the other end of the spray head is the front surface of the other end of the directional camera, a micro pump is arranged in the water storage tank, and the water outlet end of the micro pump is fixedly connected with one end of the conveying pipe.
Preferably, the protection mechanism comprises two fixing rods, the upper ends of the two fixing rods are respectively rotatably connected to the lower surfaces of the two sides of the fixing block, the lower ends of the two fixing rods are fixedly connected with spheres, and a third spring is connected between the upper ends of the two fixing rods.
Preferably, the ball is a rubber member, and the fixing rods are splayed.
Advantageous effects
The invention provides an unmanned aerial vehicle aircraft tracking device based on a security monitoring chip, which has the following beneficial effects compared with the prior art:
(1) this unmanned aerial vehicle aircraft tracking means based on security protection monitoring chip, elasticity through utilizing first spring and second spring, when needs are installed or are dismantled the camera, the staff only needs to adjust the handle, make a location section of thick bamboo slide on the slide shaft, let a location section of thick bamboo insert or break away from in the locating hole on the L shaped plate, and then completion that can be quick is to the installation or the dismantlement work of camera, make things convenient for the staff to change or overhaul the camera, the time of dismouting has been saved.
(2) This unmanned aerial vehicle aircraft tracking means based on security protection control chip, upper end through two dead levers is rotated respectively and is connected in the both sides lower surface of fixed block, and the equal fixedly connected with spheroid of lower extreme of two dead levers, be connected with the third spring between the upper end of two dead levers, when the unmanned aerial vehicle body takes place to malfunction and falls, utilize the elasticity of spheroid and third spring, unmanned aerial vehicle falls the ground in the twinkling of an eye in the time, can play fine cushioning effect, and then played guard action to unmanned aerial vehicle and camera, economic loss has been reduced.
(3) This unmanned aerial vehicle aircraft tracking means based on security protection monitoring chip, the other end through the shower nozzle is to the inside front surface of the other end that points to the camera, the inside of storage water tank is provided with the micropump, the one end fixed connection of the play water end of micropump and conveyer pipe, micropump in the storage water tank is taken out water in the shower nozzle, then spout to the camera, can play the washing effect to the surface of camera, prevent that the surperficial dust of camera is too much and influenced the monitoring effect.
Drawings
FIG. 1 is a perspective view of the structure of the present invention;
FIG. 2 is a schematic structural view of the mounting mechanism of the present invention;
FIG. 3 is an internal view of the fixed block structure of the present invention;
FIG. 4 is a schematic diagram of the monitoring mechanism of the present invention;
fig. 5 is a schematic structural diagram of the protection mechanism of the present invention.
In the figure: 1. an unmanned aerial vehicle body; 2. an installation mechanism; 21. a fixed block; 2101. a bump; 2102. a handle; 22. positioning a groove; 23. a positioning cylinder; 24. a cavity; 25. a limiting block; 26. a slide shaft; 27. a first spring; 28. a slide bar; 29. a stopper; 210. adjusting a rod; 211. a second spring; 3. a monitoring mechanism; 31. a camera; 32. an L-shaped plate; 321. positioning holes; 33. a dust blocking plate; 34. a spray head; 35. a water storage tank; 36. a delivery pipe; 4. a protection mechanism; 41. fixing the rod; 42. a sphere; 43. and a third spring.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1, the present invention provides a technical solution: the utility model provides an unmanned aerial vehicle aircraft tracking means based on security protection monitoring chip, includes unmanned aerial vehicle body 1, and the lower surface of unmanned aerial vehicle body 1 is provided with installation mechanism 2, and installation mechanism 2's front and back side lower surface all is provided with monitoring device 3, and installation mechanism 2's front surface is provided with protection machanism 4.
Referring to fig. 2-3, the mounting mechanism 2 includes a fixing block 21, a positioning groove 22 is disposed on the front surface of the fixing block 21, positioning cylinders 23 are slidably mounted in the two side surfaces of the fixing block 21, a receiving cavity 24 is disposed in the fixing block 21, a limiting block 25 is vertically connected to the middle position of the upper surface in the receiving cavity 24, a sliding shaft 26 is disposed through one side of the lower end of the limiting block 25, two ends of the sliding shaft 26 are slidably mounted in the opposite ends of the two positioning cylinders 23, a first spring 27 is slidably mounted on the outer surfaces of the two ends of the sliding shaft 26, two ends of the first spring 27 are fixedly connected to one end of the positioning cylinders 23 and one side surface of the limiting block 25, a sliding rod 28 is slidably mounted in the middle position of the lower surface in the receiving cavity 24, a stopper 29 is fixedly connected to the upper end of the sliding rod 28, and an adjusting rod 210 is rotatably connected between, sliding rod 28's upper end surface cup joints slidable mounting has second spring 211, the upper and lower end of second spring 211 respectively with dog 29's lower surface and the inside lower surface fixed connection who holds chamber 24, four corners of the upper surface of fixed block 21 all are provided with lug 2101, pass through bolt fixed connection between lug 2101 and unmanned aerial vehicle body 1's the lower surface, in order to fix fixed block 21 on unmanned aerial vehicle body 1, the lower surface intermediate position department embedding slidable mounting of fixed block 21 has handle 2102, the upper end of handle 2102 and sliding rod 28's lower extreme fixed connection, for the convenience stimulate sliding rod 28.
Referring to fig. 4, the monitoring mechanism 3 includes a camera 31, two side surfaces of one end of the camera 31 are respectively provided with an L-shaped plate 32, a dust baffle 33 is arranged on a front surface above the other end of the camera 31, a nozzle 34 is installed on an upper surface of the dust baffle 33 in a penetrating manner, a water storage tank 35 is fixedly connected to an upper surface of the other end of the camera 31, a delivery pipe 36 is installed on a lower front surface of the water storage tank 35 in an embedded manner, the other end of the delivery pipe 36 is fixedly connected to an upper end of the nozzle 34, the other end of the nozzle 34 is directed to a front surface inside the other end of the camera 31, a micro pump is arranged inside the water storage tank 35, a water outlet end of the micro pump is fixedly connected to one end of the delivery pipe 36, in order to clean the camera 31, when the camera 31 works, the dust baffle 33 plays a role in shielding dust, if the surface of the camera 31 has, the micro pump is used for pumping water in the water storage tank 35 into the spray head 34 through the delivery pipe 36 and then spraying the water to the surface of the camera 31 from the spray head 34, so that the camera position of the camera 31 can be washed, the camera effect of the camera 31 is improved, the camera 31 is embedded into the positioning groove 22 which is slidably installed on the fixing block 21, the side surfaces of one ends of the two L-shaped plates 32 are respectively provided with a positioning hole 321 corresponding to the positioning cylinder 23, when the first spring 27 and the second spring 211 are in a normal state, the positioning cylinder 23 is embedded into the positioning hole 321 in a sliding mode, and the camera 31 is fixed.
Please refer to fig. 5, the protection mechanism 4 includes two fixing rods 41, the upper ends of the two fixing rods 41 are respectively rotatably connected to the lower surfaces of the two sides of the fixing block 21, and the lower ends of the two fixing rods 41 are respectively fixedly connected with a sphere 42, a third spring 43 is connected between the upper ends of the two fixing rods 41, the sphere 42 is a rubber component, the two fixing rods 41 are in a splayed shape, and under the dual cooperation of the sphere 42 and the third spring 43, the unmanned aerial vehicle body 1 and the camera 31 can be protected by buffering.
And those not described in detail in this specification are well within the skill of those in the art.
Disassembling and assembling: when the camera 31 needs to be disassembled, the handle 2102 is pulled downwards, under the elasticity of the second spring 211, the handle 2102 drives the sliding rod 28 to slide downwards, the sliding rod 28 drives the stopper 29 to move downwards, because the adjusting rod 210 is rotatably connected with the stopper 29 and the positioning cylinder 23, when the stopper 29 moves downwards, the adjusting rod 210 on the stopper 29 drives the positioning cylinder 23 to slide on the sliding shaft 26 by using the elasticity of the first spring 27, so that the other end of the positioning cylinder 23 is separated from the positioning hole 321 on the L-shaped plate 32, then the camera 31 is taken off, the disassembling work can be completed, when the camera 31 needs to be assembled, the handle is pulled downwards and is not placed, then one end of the camera 31 is inserted into the bump 2101 on the fixing block 21 to play a positioning role, and the two L-shaped plates 32 on the camera 31 are sleeved on the outer surface of the fixing block 21, so that the positioning hole 321 on the L-shaped plate 32 is aligned with the positioning cylinder 23, after alignment, the handle 2102 is released, the second spring 211 restores the stopper 29 to the original position, and the first spring 27 restores the positioning cylinder 23 to the original position, so that the other ends of the two positioning cylinders 23 are inserted into the positioning holes 321 of the two L-shaped plates 32, respectively, thereby completing the installation of the camera 31.
Cleaning: when the camera 31 works, the dust blocking plate 33 plays a role of blocking dust, and if the dust on the surface of the camera 31 is too much, the power supply of the micropump in the water storage tank 35 is switched on, so that the micropump pumps the water in the water storage tank 35 into the spray head 34 through the conveying pipe 36 and then sprays the water to the surface of the camera 31 from the spray head 34, and thus the flushing work can be carried out on the shooting position of the camera 31, and the shooting effect of the camera 31 is improved.
Protection work: when unmanned aerial vehicle body 1 is malfunctioning to fall and fall into ground, because two dead levers 41 are the splayed, and dead lever 41 is connected for rotating with the lower surface of fixed block 21, consequently under the elasticity of third spring 43, two dead levers 41 can open, and third spring 43 can restrain two dead levers 41 and open, again because spheroid 42 is the rubber material component, and rubber has elasticity, consequently under the dual cooperation of spheroid 42 and third spring 43, can play the buffering guard action to unmanned aerial vehicle body 1 and camera 31.
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.
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 aircraft tracking device based on security protection control chip, 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 an installation mechanism (2) is arranged on the lower surface of the unmanned aerial vehicle body (1), monitoring mechanisms (3) are arranged on the lower surfaces of the front side and the rear side of the installation mechanism (2), and a protection mechanism (4) is arranged on the front surface of the installation mechanism (2);
the installation mechanism (2) comprises a fixed block (21), a positioning groove (22) is formed in the front surface of the fixed block (21), positioning cylinders (23) are embedded into two side surfaces of the fixed block (21) in a sliding mode, an accommodating cavity (24) is arranged inside the fixed block (21), a limiting block (25) is vertically connected to the middle position of the upper surface inside the accommodating cavity (24), a sliding shaft (26) penetrates through one side of the lower end of the limiting block (25), two ends of the sliding shaft (26) are respectively embedded into and slidably installed inside the opposite ends of the two positioning cylinders (23), first springs (27) are sleeved on the outer surfaces of two ends of the sliding shaft (26) in a sliding mode, two ends of each first spring (27) are fixedly connected with one end of each positioning cylinder (23) and one side surface of each limiting block (25), a sliding rod (28) is embedded into the middle position of the lower surface inside the accommodating cavity (24), the upper end fixedly connected with dog (29) of slide bar (28), all rotate between the both ends of dog (29) and the relative one end lower surface of two location section of thick bamboo (23) and be connected with regulation pole (210), slidable mounting is cup jointed to the upper end surface of slide bar (28) has second spring (211), the upper and lower end of second spring (211) respectively with the lower surface of dog (29) and the inside lower fixed surface who holds chamber (24) be connected.
2. The unmanned aerial vehicle aircraft tracking device based on security protection monitoring chip of claim 1, characterized in that: four corners of the upper surface of fixed block (21) all are provided with lug (2101), pass through bolt fixed connection between lug (2101) and the lower surface of unmanned aerial vehicle body (1).
3. The unmanned aerial vehicle aircraft tracking device based on security protection monitoring chip of claim 1, characterized in that: a handle (2102) is embedded into the middle position of the lower surface of the fixing block (21) in a sliding mode, and the upper end of the handle (2102) is fixedly connected with the lower end of the sliding rod (28).
4. The unmanned aerial vehicle aircraft tracking device based on security protection monitoring chip of claim 1, characterized in that: monitoring mechanism (3) are including camera (31), the one end both sides face of camera (31) all is provided with L shaped plate (32), and the other end top front surface of camera (31) is provided with dust damper (33), the upper surface of dust damper (33) runs through and installs shower nozzle (34), fixed surface is connected with storage water tank (35) on the other end of camera (31), conveyer pipe (36) are installed to the below front surface embedding of storage water tank (35), the other end of conveyer pipe (36) and the upper end fixed connection of shower nozzle (34).
5. The unmanned aerial vehicle aircraft tracking device based on security protection monitoring chip of claim 1, characterized in that: the camera (31) is embedded into a positioning groove (22) which is slidably mounted on the fixing block (21), positioning holes (321) corresponding to the positioning cylinders (23) are formed in the side faces of one ends of the two L-shaped plates (32), and when the first spring (27) and the second spring (211) are in a normal state, the positioning cylinders (23) are embedded into the positioning holes (321) in a sliding manner.
6. The unmanned aerial vehicle aircraft tracking device based on security protection monitoring chip of claim 1, characterized in that: the other end of the spray head (34) points to the front surface of the inside of the other end of the camera (31), a micro pump is arranged inside the water storage tank (35), and the water outlet end of the micro pump is fixedly connected with one end of the conveying pipe (36).
7. The unmanned aerial vehicle aircraft tracking device based on security protection monitoring chip of claim 1, characterized in that: protection machanism (4) are including two dead levers (41), two the upper end of dead lever (41) rotates respectively to be connected in the both sides lower surface of fixed block (21), and the equal fixedly connected with spheroid (42) of lower extreme of two dead levers (41), two be connected with third spring (43) between the upper end of dead lever (41).
8. The unmanned aerial vehicle aircraft tracking device based on security protection monitoring chip of claim 7, characterized in that: the sphere (42) is a rubber component, and the two fixing rods (41) are splayed.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010907590.1A CN112009707A (en) | 2020-09-02 | 2020-09-02 | Unmanned aerial vehicle aircraft tracking device based on security protection control chip |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010907590.1A CN112009707A (en) | 2020-09-02 | 2020-09-02 | Unmanned aerial vehicle aircraft tracking device based on security protection control chip |
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| Publication Number | Publication Date |
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| CN112009707A true CN112009707A (en) | 2020-12-01 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN202010907590.1A Pending CN112009707A (en) | 2020-09-02 | 2020-09-02 | Unmanned aerial vehicle aircraft tracking device based on security protection control chip |
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| CN (1) | CN112009707A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114104277A (en) * | 2021-12-03 | 2022-03-01 | 西北工业大学 | Many rotors of improved generation helicopter of air bag is floated in area |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107830341A (en) * | 2017-12-20 | 2018-03-23 | 西安龙之梦网络信息有限公司 | A kind of security monitoring camera support |
| CN207926743U (en) * | 2018-03-22 | 2018-09-28 | 新乡市正和科技有限责任公司 | A kind of Multi-angle camera convenient for cleaning |
| CN108869628A (en) * | 2018-07-26 | 2018-11-23 | 赣州研顺飞科技有限公司 | A kind of easy-to-dismount artificial intelligence monitoring camera |
| CN208295487U (en) * | 2018-05-03 | 2018-12-28 | 北京瞭望神州科技有限公司 | A kind of artificial intelligence monitoring camera convenient for adjusting |
| KR102039562B1 (en) * | 2019-08-22 | 2019-11-01 | (유)동아하이테크 | An Amphibious drone and A Deck for taking off and landing therof |
| CN210027950U (en) * | 2019-03-26 | 2020-02-07 | 徐新宇 | Unmanned aerial vehicle with protection architecture has obstacle avoidance function |
-
2020
- 2020-09-02 CN CN202010907590.1A patent/CN112009707A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107830341A (en) * | 2017-12-20 | 2018-03-23 | 西安龙之梦网络信息有限公司 | A kind of security monitoring camera support |
| CN207926743U (en) * | 2018-03-22 | 2018-09-28 | 新乡市正和科技有限责任公司 | A kind of Multi-angle camera convenient for cleaning |
| CN208295487U (en) * | 2018-05-03 | 2018-12-28 | 北京瞭望神州科技有限公司 | A kind of artificial intelligence monitoring camera convenient for adjusting |
| CN108869628A (en) * | 2018-07-26 | 2018-11-23 | 赣州研顺飞科技有限公司 | A kind of easy-to-dismount artificial intelligence monitoring camera |
| CN210027950U (en) * | 2019-03-26 | 2020-02-07 | 徐新宇 | Unmanned aerial vehicle with protection architecture has obstacle avoidance function |
| KR102039562B1 (en) * | 2019-08-22 | 2019-11-01 | (유)동아하이테크 | An Amphibious drone and A Deck for taking off and landing therof |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114104277A (en) * | 2021-12-03 | 2022-03-01 | 西北工业大学 | Many rotors of improved generation helicopter of air bag is floated in area |
| CN114104277B (en) * | 2021-12-03 | 2024-02-27 | 西北工业大学 | Improved multi-rotor helicopter with floating air bag |
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Application publication date: 20201201 |