CN109131850A - A kind of flying robot - Google Patents
A kind of flying robot Download PDFInfo
- Publication number
- CN109131850A CN109131850A CN201811055370.XA CN201811055370A CN109131850A CN 109131850 A CN109131850 A CN 109131850A CN 201811055370 A CN201811055370 A CN 201811055370A CN 109131850 A CN109131850 A CN 109131850A
- Authority
- CN
- China
- Prior art keywords
- fuselage
- support plate
- outside
- holder
- fixed block
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/006—Safety devices
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60F—VEHICLES FOR USE BOTH ON RAIL AND ON ROAD; AMPHIBIOUS OR LIKE VEHICLES; CONVERTIBLE VEHICLES
- B60F5/00—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media
- B60F5/02—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media convertible into aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
- B64C25/62—Spring shock-absorbers; Springs
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/20—Rotors; Rotor supports
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
Abstract
The invention discloses a kind of flying robots, including fuselage, the fuselage roof is provided with hood, the fuselage bottom is provided with holder, and the fuselage bottom is provided with fixed block, and the fixed block side is hinged with support plate, telescopic rod is provided between the support plate bottom and fixed block, the first spring is provided on the outside of the telescopic rod, there are two undercarriage, two undercarriages are set as hinged for the support plate bottom end setting.The present invention is by being equipped with fixed block; two undercarriage support ground when robot lands, by gravity and effect of inertia, robot is made two undercarriages be pressurized by biggish impact force; support plate is by torsion; in the case where two torque springs act on, support plate bottom and top damping twice mitigate impact force; first spring and telescopic rod cooperate support plate damping three times; robot security's landing is protected, electric pushrod is released universal wheel and allowed the robot in ground running, and damper keeps robot motion more stable.
Description
Technical field
The present invention relates to unmanned plane field, in particular to a kind of flying robot.
Background technique
With the development of science and technology, robot receives pursuing for people, robot can adapt to severe environment, instead of people
Complete dangerous work, development prospect is wide, and the area of activities of robot includes sky, land and waters, for aerial machine
Device people is also referred to as unmanned plane, and during unmanned plane rises and falls, undercarriage is frequently subjected to biggish impact force, usually stops shakiness, leads
Undercarriage serious wear is caused, the normal flight of unmanned plane is influenced, unmanned plane crash is will lead to when serious, causes heavy losses.
Therefore, it is necessary to solve the above problems to invent a kind of flying robot.
Summary of the invention
The purpose of the present invention is to provide a kind of flying robots, by being equipped with fixed block, fixed block and the fixed company of fuselage
It connecing, fixed block is hinged with support plate, and two undercarriages are hinged, when robot lands, two undercarriage support ground, by gravity and inertia
Effect, robot are made two undercarriages be pressurized by biggish impact force, and support plate is acted on by torsion in two torque springs
Under, support plate bottom and top damping twice mitigate impact force, and the first spring and telescopic rod cooperate support plate damping three times, protect
Robot security's landing is protected, electric pushrod is released universal wheel and allowed the robot in ground running, and damper makes robot motion
It is more stable, to solve the problems mentioned in the above background technology.
The purpose of the present invention is to provide following technical solutions: a kind of flying robot, including fuselage, the fuselage roof
It is provided with hood, the fuselage bottom is provided with holder, and the fuselage bottom is provided with fixed block, the fixed block side hinge
It is connected to support plate, telescopic rod is provided between the support plate bottom and fixed block, is provided with the first bullet on the outside of the telescopic rod
Spring, the support plate bottom end setting is there are two undercarriage, and two undercarriages are set as hingedly, the support plate and fixed block
Hinged place be provided with torque spring, the hinged place of two undercarriages is provided with torque spring, the fuselage interior setting
There is electric pushrod, the output end of electric push rod is provided with connection frame, and the connection frame bottom is provided with universal wheel, the connection
Frame two sides are provided with damper.
Preferably, micromotor is provided in the fuselage, the Miniature electric machine output shaft is provided with shaft, the shaft
Outside is provided with propeller, is provided with sleeve on the outside of the propeller, the sleeve is fixedly connected with fuselage by fixed frame, institute
It states and is provided with second spring between sleeve and hood, connecting rod, setting at the top of the connecting rod are provided on the outside of the fixed frame
There is roller.
Preferably, the holder side, which is provided with, blocks door, and the quantity for blocking door is set as two, described in two
Middle part is provided with partition in holder, and the partition two sides are provided with collecting bin, and the header that blocks is hinged with holder,
It is described to block a bottom and holder bottom is provided with magnet block.
Preferably, the bottom of blocking is arranged on the inside of holder, and the holder two sides are provided with manipulator, and two
The manipulator is matched with blocking.
Preferably, the fuselage shape setting is square, and each side of the fuselage is disposed as concave arc shape, described
The quantity of propeller is set as four, and four propellers are uniformly arranged at the top of fuselage quadrangle, the fuselage tetrapod
It is provided with camera.
Preferably, the fuselage outer side is provided with ventilation hole, and the ventilation hole matches with micromotor.
Preferably, it is set as arc-shaped at the top of the hood, is provided with lightning rod at the top of the hood, the lightning rod is set
It is set to stretching structure.
Preferably, it is provided with LED light on the outside of the hood, the quantity of the LED light is set as multiple, multiple LED
Lamp is uniformly arranged on hood surface.
Preferably, it is provided with rubber layer on the outside of the roller, the quantity of the roller is set as multiple, multiple rollers
It is uniformly arranged on the outside of roller, the undercarriage is shaped to trapezoidal.
Technical effect and advantage of the invention:
1, by being equipped with fixed block, fixed block is fixedly connected with fuselage, and fixed block is hinged with support plate, two undercarriage hinges
It connects, when robot lands, two undercarriage support ground, by gravity and effect of inertia, robot is made two by biggish impact force
Undercarriage is pressurized, and support plate is by torsion, and in the case where two torque springs act on, support plate bottom and top damping twice mitigate
Impact force, the first spring and telescopic rod cooperate support plate damping three times, and protection robot security's landing, electric pushrod is released universal
Wheel is allowed the robot in ground running, and damper keeps robot motion more stable, is conducive to the docking conversion in unmanned plane sky land
Stability, guarantee the safety of unmanned plane, realize the amphibious movement in empty land of unmanned plane；
2, by being equipped with sleeve, micromotor rotation drives shaft rotation, so that propeller be made to stablize hoisting machine people, spiral shell
It is provided with sleeve on the outside of rotation paddle, sleeve is fixedly connected by fixed frame with fuselage, is provided with connecting rod, connecting rod on the outside of fixed frame
Top is provided with roller, and roller is matched with sleeve, is provided with rubber layer on the outside of roller, and when unmanned plane during flying is hit, sleeve
It protects propeller injury-free, keeps unmanned mechanomotive force, roller is arranged on the outside of sleeve, improves the resistance power of sleeve, the second bullet
Spring is fixedly connected with sleeve and hood, makes sleeve damping, advantageously ensures that the stabilization safe flight of unmanned plane；
3, by being equipped with holder, holder is divided into two collecting bins by partition, and collecting bin side, which is hinged with, blocks door,
It blocks door to connect by magnet block with holder, holder two sides are provided with manipulator, and fuselage bottom is provided with camera, lead to
Camera observation extraneous circumstance is crossed, manipulator crawl object classification puts two collecting bins into, blocks a bottom and be arranged in holder
Inside, after object enters collecting bin, magnet block makes to block door and holder is closed, and prevents object from falling, and is advantageously implemented long-range
Sampling；
Detailed description of the invention
Fig. 1 is overall structure diagram of the invention.
Fig. 2 is overall top view of the invention.
Fig. 3 is the portion the A schematic enlarged-scale view of Fig. 1 of the present invention.
Fig. 4 is the portion the B schematic enlarged-scale view of Fig. 1 of the present invention.
Fig. 5 is the attachment structure schematic diagram that the present invention blocks door and holder.
Fig. 6 is undercarriage main view of the invention.
In figure: 1 fuselage, 2 hoods, 3 holders, 4 fixed blocks, 5 support plates, 6 telescopic rods, 7 first springs, 8 undercarriages, 9
Torque spring, 10 electric pushrods, 11 connection frames, 12 universal wheels, 13 dampers, 14 micromotors, 15 shafts, 16 propellers, 17
Door, 23 partitions, 24 magnet blocks, 25 manipulators, 26 are blocked in sleeve, 18 fixed frames, 19 second springs, 20 connecting rods, 21 rollers, 22
Camera, 27 ventilation holes, 28 lightning rods, 29 LED light.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
Embodiment 1:
A kind of flying robot according to shown in Fig. 1-6, including fuselage 1 are provided with hood 2 at the top of the fuselage 1, described
1 bottom of fuselage is provided with holder 3, and 1 bottom of fuselage is provided with fixed block 4, and 4 side of fixed block is hinged with support plate
5, it is provided with telescopic rod 6 between 5 bottom of support plate and fixed block 4, the first spring 7, institute are provided on the outside of the telescopic rod 6
The setting of 5 bottom end of support plate is stated there are two undercarriage 8, two undercarriages 8 are set as hingedly, the support plate 5 and fixed block 4
Hinged place be provided with torque spring 9, the hinged place of two undercarriages 8 is provided with torque spring 9, inside the fuselage 1
It is provided with electric pushrod 10,10 output end of electric pushrod is provided with connection frame 11, and 11 bottom of connection frame is provided with ten thousand
To wheel 12,11 two sides of connection frame are provided with damper 13；
By being equipped with fixed block 4, fixed block 4 is fixedly connected with fuselage 1, and fixed block 4 and support plate 5 are hinged, and two are risen and fallen
Frame 8 is hinged, and when robot lands, two support of undercarriage 8 ground, by gravity and effect of inertia, robot is by biggish impact force
Two undercarriages 8 are made to be pressurized, support plate 5 is by torsion, and in the case where two torque springs 9 act on, 5 bottom and top of support plate are twice
Damping mitigates impact force, and the first spring 7 and telescopic rod 6 cooperate the damping three times of support plate 5, and protection robot security's landing is electronic
Push rod 10 is released universal wheel 12 and is allowed the robot in ground running, and damper 13 keeps robot motion more stable, is conducive to nothing
The stability of man-machine sky land docking conversion, guarantees the safety of unmanned plane, realizes the amphibious movement in empty land of unmanned plane.
Embodiment 2:
Micromotor 14 is provided in the fuselage 1,14 output shaft of micromotor is provided with shaft 15, the shaft
15 outsides are provided with propeller 16, and sleeve 17 is provided on the outside of the propeller 16, and the sleeve 17 passes through fixed frame with fuselage 1
18 are fixedly connected, and second spring 19 is provided between the sleeve 17 and hood 2, is provided with connecting rod on the outside of the fixed frame 18
20, roller 21 is provided at the top of the connecting rod 20, the rotation of micromotor 14 drives shaft 15 to rotate, to keep propeller 16 steady
Determine hoisting machine people, sleeve 17 is provided on the outside of propeller 16, sleeve 17 is fixedly connected by fixed frame 18 with fuselage 1, fixed
It is provided with connecting rod 20 on the outside of frame 18, roller 21 is provided at the top of connecting rod 20, roller 21 is matched with sleeve 17,21 outside of roller
It is provided with rubber layer, when unmanned plane during flying, is hit, and sleeve 17 protects propeller 26 injury-free, unmanned mechanomotive force is kept,
The setting of roller 21 improves the resistance power of sleeve 17, second spring 19 is fixedly connected with sleeve 17 and hood 2, makes in 17 outside of sleeve
17 damping of sleeve advantageously ensures that the stabilization safe flight of unmanned plane；
3 side of holder, which is provided with, blocks door 22, and the quantity for blocking door 22 is set as two, puts described in two
It sets middle part in box 3 and is provided with partition 23,23 two sides of partition are provided with collecting bin, described to block 22 top of door and holder
3 is hinged, and described to block 22 bottom of door and 3 bottom of holder is provided with magnet block 24, two magnet blocks, which match, makes holder 3
It is closed with door 22 is blocked；
Described to block the setting of 22 bottom of door in the inside of holder 3,3 two sides of holder are provided with manipulator 25, and two
The manipulator 25 with block door 22 and match, holder 3 is divided into two collecting bins by partition 23, and collecting bin side is hinged with
Door 22 is blocked, door 22 is blocked and is connect by magnet block 24 with holder 3,3 two sides of holder are provided with manipulator 25, fuselage 1
Bottom is provided with camera 26, observes extraneous circumstance by camera 26, manipulator 25 grabs object classification and puts two collections into
The setting of 22 bottom of door is blocked in 3 inside of holder in storehouse, and after object enters collecting bin, magnet block 24 makes to block door 22 and holder 3
Closing, prevents object from falling, is advantageously implemented long-range sampling；
The fuselage 1 is shaped to square, and each side of the fuselage 1 is disposed as concave arc shape, the spiral
The quantity of paddle 16 is set as four, and four propellers 16 are uniformly arranged on 1 four jiaos of tops of fuselage, guarantees robot flight
Balance and stability, 1 tetrapod of fuselage are provided with camera 26, eyes of the camera 26 as robot, convenient for ground
Face observation and control；
Ventilation hole 27 is provided on the outside of the fuselage 1, the ventilation hole 27 matches with micromotor 14, and ventilation hole 27 makes
Micromotor 14 is aeration-cooling；
It is set as arc-shaped at the top of the hood 2, lightning rod 28 is provided at the top of the hood 2, the lightning rod 28 is set
It is set to stretching structure, in thunderstorm weather lightning protection；
LED light 29 is provided on the outside of the hood 2, the quantity of the LED light 29 is set as multiple, multiple LED light
29 are uniformly arranged on 2 surface of hood, and LED light 29 is convenient for using in the bad local display position coordinate of light and illumination；
Rubber layer is provided on the outside of the roller 21, the quantity of 21 antiskid, shock-absorbing of rubber cylinder, the roller 21 is set as
Multiple, multiple rollers 21 are uniformly arranged on the outside of roller 21, and the undercarriage 8 is shaped to trapezoidal, make to rise and fall
Frame 8 stablizes support.
Working principle of the present invention:
Referring to Figure of description 1-6, fixed block 4 is fixedly connected with fuselage 1, and fixed block 4 and support plate 5 are hinged, and two are risen
It is hinged to fall frame 8, when robot lands, two support of undercarriage 8 ground, by gravity and effect of inertia, robot is by biggish impact
Power makes two undercarriages 8 be pressurized, and support plate 5 is by torsion, in the case where two torque springs 9 act on, 5 bottom and top two of support plate
Secondary damping, mitigates impact force, and the first spring 7 and telescopic rod 6 cooperate the damping three times of support plate 5, protection robot security's landing, electricity
Dynamic push rod 10 is released universal wheel 12 and is allowed the robot in ground running, and damper 13 keeps robot motion more stable, is conducive to
The stability of unmanned plane sky land docking conversion, guarantees the safety of unmanned plane, realizes the amphibious movement in empty land of unmanned plane；
Referring to Figure of description 1-4, the rotation of micromotor 14 drives shaft 15 to rotate, and is promoted so that propeller 16 be made to stablize
Robot is provided with sleeve 17 on the outside of propeller 16, and sleeve 17 is fixedly connected by fixed frame 18 with fuselage 1, outside fixed frame 18
Side is provided with connecting rod 20, and roller 21 is provided at the top of connecting rod 20, and roller 21 is matched with sleeve 17, is provided on the outside of roller 21
Rubber layer, when unmanned plane during flying, are hit, and sleeve 17 protects propeller 26 injury-free, keep unmanned mechanomotive force, roller 21
Setting improves the resistance power of sleeve 17, second spring 19 is fixedly connected with sleeve 17 and hood 2, makes sleeve 17 in 17 outside of sleeve
Damping advantageously ensures that the stabilization safe flight of unmanned plane；
Referring to Figure of description 1, holder 3 is divided into two collecting bins by partition 23, and collecting bin side, which is hinged with, blocks
Door 22 blocks door 22 and is connect by magnet block 24 with holder 3, and 3 two sides of holder are provided with manipulator 25,1 bottom of fuselage
It is provided with camera 26, extraneous circumstance is observed by camera 26, manipulator 25 grabs object classification and puts two collecting bins into, hides
The setting of 22 bottom of door is kept off in 3 inside of holder, after object enters collecting bin, magnet block 24 makes to block door 22 and holder 3 is closed,
It prevents object from falling, is advantageously implemented long-range sampling.
Finally, it should be noted that the foregoing is only a preferred embodiment of the present invention, it is not intended to restrict the invention,
Although the present invention is described in detail referring to the foregoing embodiments, for those skilled in the art, still may be used
To modify the technical solutions described in the foregoing embodiments or equivalent replacement of some of the technical features,
All within the spirits and principles of the present invention, any modification, equivalent replacement, improvement and so on should be included in of the invention
Within protection scope.
Claims (9)
1. a kind of flying robot, including fuselage (1), it is characterised in that: it is provided with hood (2) at the top of the fuselage (1), it is described
Fuselage (1) bottom is provided with holder (3), and fuselage (1) bottom is provided with fixed block (4), fixed block (4) the side hinge
It is connected to support plate (5), is provided with telescopic rod (6) between support plate (5) bottom and fixed block (4), the telescopic rod (6) is outside
Side is provided with the first spring (7), and there are two undercarriage (8), two undercarriages (8) are set for support plate (5) the bottom end setting
It is set to hingedly, the hinged place of the support plate (5) and fixed block (4) is provided with torque spring (9), two undercarriages (8)
Hinged place be provided with torque spring (9), the fuselage (1) is internally provided with electric pushrod (10), the electric pushrod (10)
Output end is provided with connection frame (11), and connection frame (11) bottom is provided with universal wheel (12), connection frame (11) two sides
It is provided with damper (13).
2. a kind of flying robot according to claim 1, it is characterised in that: be provided with micro electric in the fuselage (1)
Machine (14), micromotor (14) output shaft are provided with shaft (15), are provided with propeller (16) on the outside of the shaft (15),
It being provided with sleeve (17) on the outside of the propeller (16), the sleeve (17) is fixedly connected with fuselage (1) by fixed frame (18),
It is provided with second spring (19) between the sleeve (17) and hood (2), is provided with connecting rod on the outside of the fixed frame (18)
(20), roller (21) are provided at the top of the connecting rod (20).
3. a kind of flying robot according to claim 1, it is characterised in that: holder (3) side is provided with screening
It keeps off door (22), the quantity for blocking door (22) is set as two, and middle part is provided with partition in two holders (3)
(23), partition (23) two sides are provided with collecting bin, described to block door (22) top and holder (3) hingedly, the screening
Gear door (22) bottom and holder (3) bottom are provided with magnet block (24).
4. a kind of flying robot according to claim 1, it is characterised in that: it is described block door (22) bottom setting putting
Set on the inside of box (3), holder (3) two sides are provided with manipulator (25), two manipulators (25) with block door
(22) it matches.
5. a kind of flying robot according to claim 1, it is characterised in that: the fuselage (1) is shaped to pros
Shape, each side of the fuselage (1) are disposed as concave arc shape, and the quantity of the propeller (16) is set as four, four institutes
It states propeller (16) to be uniformly arranged at the top of fuselage (1) quadrangle, fuselage (1) tetrapod is provided with camera (26).
6. a kind of flying robot according to claim 1, it is characterised in that: be provided with ventilation on the outside of the fuselage (1)
Hole (27), the ventilation hole (27) match with micromotor (14).
7. a kind of flying robot according to claim 1, it is characterised in that: be set as circular arc at the top of the hood (2)
Shape, hood (2) top are provided with lightning rod (28), and the lightning rod (28) is set as stretching structure.
8. a kind of flying robot according to claim 1, it is characterised in that: be provided with LED light on the outside of the hood (2)
(29), the quantity of the LED light (29) is set as multiple, and multiple LED light (29) are uniformly arranged on hood (2) surface.
9. a kind of flying robot according to claim 1, it is characterised in that: be provided with rubber on the outside of the roller (21)
Layer, the quantity of the roller (21) are set as multiple, and multiple rollers (21) are uniformly arranged on the outside of roller (21), described
Undercarriage (8) is shaped to trapezoidal.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811055370.XA CN109131850A (en) | 2018-09-11 | 2018-09-11 | A kind of flying robot |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811055370.XA CN109131850A (en) | 2018-09-11 | 2018-09-11 | A kind of flying robot |
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| CN109131850A true CN109131850A (en) | 2019-01-04 |
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| CN201811055370.XA Pending CN109131850A (en) | 2018-09-11 | 2018-09-11 | A kind of flying robot |
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| CN109911190A (en) * | 2019-04-12 | 2019-06-21 | 龙岩学院 | Multi-rotor unmanned aerial vehicle |
| CN110203393A (en) * | 2019-06-19 | 2019-09-06 | 山西大学 | A kind of quickly mapping multi-rotor unmanned aerial vehicle and its mapping method |
| CN110550220A (en) * | 2019-09-05 | 2019-12-10 | 新昌县诺趣智能科技有限公司 | Aerial photography unmanned aerial vehicle with falling protection function |
| WO2020243925A1 (en) * | 2019-06-05 | 2020-12-10 | 中国科学院深圳先进技术研究院 | Rotor structure and rolling and crawling robot using same |
| CN114104286A (en) * | 2021-11-22 | 2022-03-01 | 国网福建省电力有限公司南平供电公司 | AI front end algorithm-based autonomous intelligent inspection device for power transmission line unmanned aerial vehicle |
| CN114524087A (en) * | 2022-02-28 | 2022-05-24 | 北京博瑞翔伦科技发展有限公司 | Unmanned aerial vehicle detection interference system's unmanned aerial vehicle protective structure |
| CN114849248A (en) * | 2021-04-29 | 2022-08-05 | 深圳市工匠社科技有限公司 | Elastic piece and robot sports hit and detect stage property |
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Application publication date: 20190104 |