CN108820213A - A kind of unmanned plane launches umbrella shape robot device in the air - Google Patents
A kind of unmanned plane launches umbrella shape robot device in the air Download PDFInfo
- Publication number
- CN108820213A CN108820213A CN201810766460.3A CN201810766460A CN108820213A CN 108820213 A CN108820213 A CN 108820213A CN 201810766460 A CN201810766460 A CN 201810766460A CN 108820213 A CN108820213 A CN 108820213A
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- Prior art keywords
- air
- unmanned plane
- umbrella shape
- fuselage
- cabin
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- 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.)
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- 238000013016 damping Methods 0.000 claims description 26
- 238000003780 insertion Methods 0.000 claims description 3
- 230000037431 insertion Effects 0.000 claims description 3
- 238000005259 measurement Methods 0.000 claims description 3
- 238000012806 monitoring device Methods 0.000 claims description 3
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims description 3
- 238000009434 installation Methods 0.000 claims description 2
- 238000000465 moulding Methods 0.000 claims description 2
- 238000000034 method Methods 0.000 abstract description 10
- 238000004804 winding Methods 0.000 abstract description 4
- 230000000694 effects Effects 0.000 description 7
- 238000010586 diagram Methods 0.000 description 5
- 206010057071 Rectal tenesmus Diseases 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 230000002035 prolonged effect Effects 0.000 description 2
- 208000012271 tenesmus Diseases 0.000 description 2
- 238000013475 authorization Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000000116 mitigating effect Effects 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/14—Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers
-
- 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
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
-
- 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
-
- E—FIXED CONSTRUCTIONS
- E06—DOORS, WINDOWS, SHUTTERS, OR ROLLER BLINDS IN GENERAL; LADDERS
- E06B—FIXED OR MOVABLE CLOSURES FOR OPENINGS IN BUILDINGS, VEHICLES, FENCES OR LIKE ENCLOSURES IN GENERAL, e.g. DOORS, WINDOWS, BLINDS, GATES
- E06B9/00—Screening or protective devices for wall or similar openings, with or without operating or securing mechanisms; Closures of similar construction
- E06B9/02—Shutters, movable grilles, or other safety closing devices, e.g. against burglary
- E06B9/08—Roll-type closures
-
- E—FIXED CONSTRUCTIONS
- E06—DOORS, WINDOWS, SHUTTERS, OR ROLLER BLINDS IN GENERAL; LADDERS
- E06B—FIXED OR MOVABLE CLOSURES FOR OPENINGS IN BUILDINGS, VEHICLES, FENCES OR LIKE ENCLOSURES IN GENERAL, e.g. DOORS, WINDOWS, BLINDS, GATES
- E06B9/00—Screening or protective devices for wall or similar openings, with or without operating or securing mechanisms; Closures of similar construction
- E06B9/56—Operating, guiding or securing devices or arrangements for roll-type closures; Spring drums; Tape drums; Counterweighting arrangements therefor
- E06B9/68—Operating devices or mechanisms, e.g. with electric drive
- E06B9/70—Operating devices or mechanisms, e.g. with electric drive comprising an electric motor positioned outside the roller
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structural Engineering (AREA)
- Mechanical Engineering (AREA)
- Architecture (AREA)
- Civil Engineering (AREA)
- Manipulator (AREA)
Abstract
The invention discloses a kind of unmanned planes to launch umbrella shape robot device in the air, including drone body, fuselage is provided at the top of the drone body, and the bottom end of drone body is connected with supporting leg, four horns circumferentially dispersed are provided on the outside of the fuselage, and the lower surface of fuselage is provided with and launches cabin, is equipped with propeller above the horn.Structure of the invention is scientific and reasonable, it is easy to operate, it can be realized the unlatching and closure of hatch door by motor, shaft is driven to rotate using motor, to realize the winding work of hatch door, when needing to launch robot, directly hatch door is controlled by wireless remote control device to open, pass through pushing meanss, the push work that push plate can be realized using the piston rod in pusher cylinder, the Forward of push plate is driven by the stretching of piston rod, to generate motive force to robot, it disengages it from and launches cabin, realize air-drop process.
Description
Technical field
The present invention relates to air vehicle technique field, specifically a kind of unmanned plane launches umbrella shape robot device in the air.
Background technique
UAV abbreviation unmanned plane is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft without cockpit on machine, but is equipped with the equipment such as automatic pilot, presetting apparatus, on ground, naval vessels or
Machine tool remote control station personnel track it, are positioned, are remotely controlled, telemetering and Digital Transmission by the equipment such as radar, can be wireless
It takes off as conventional airplane under electrical remote control or is launched with booster rocket, aerial launch can also be taken to by machine tool and flown, returned
Time receiving can use the mode automatic Landing as conventional airplane landing mission, can also be recycled by remote control parachute or block,
It can be reused several times, be widely used in aerial reconnaissance, monitoring, communication, antisubmarine, electronic interferences etc..
Through retrieving, Chinese patent discloses a kind of unmanned plane automatic release device (Authorization Notice No. CN107972873U),
The patented technology keeps the entire jettison system of aircraft more safe and reliable in processes such as transport, dispensings, solves current dispensing system
In system, fuselage and protective device do not have the defect of axial restraint, and still, unmanned plane dropping gear in the prior art is not only tied
Structure is complicated, and does not have damping device, and damping effect is poor, so that greater impact power is generated with ground when unmanned plane lands,
Damage easily is generated to fuselage, while traditional air drop robot does not have umbellate form cover, since decrease speed is too fast during air-drop,
Impact force spends the failure for being easy to cause robot greatly, and product is caused to be lost, and tradition air-drop unmanned plane does not have camera shooting
Head can not achieve the combination of unmanned plane air-drop and camera shooting, and therefore, it is empty that those skilled in the art provide a kind of unmanned plane
Middle dispensing umbrella shape robot device, to solve the problems mentioned in the above background technology.
Summary of the invention
The purpose of the present invention is to provide a kind of unmanned planes to launch umbrella shape robot device in the air, to solve above-mentioned background skill
Itd is proposed in art not only structure is complicated, but also do not have damping device, damping effect is poor so that unmanned plane land when with ground
Face generates greater impact power, easily damage is generated to fuselage, while traditional air drop robot does not have umbellate form cover, during air-drop
Since decrease speed is too fast, impact force spends the failure for being easy to cause robot greatly, and product is caused to be lost, and tradition air-drop
Not the problem of unmanned plane does not have camera, can not achieve the combination of unmanned plane air-drop and camera shooting.
To achieve the above object, the present invention provides the following technical solutions：
A kind of unmanned plane launches umbrella shape robot device, including drone body, the top of the drone body in the air
It is provided with fuselage, and the bottom end of drone body is connected with supporting leg, and four circumferentially dispersed are provided on the outside of the fuselage
A horn, and the lower surface of fuselage is provided with and launches cabin, is equipped with propeller, the bottom of the supporting leg above the horn
End is equipped with damping device, and the front side insertion for launching cabin is provided with camera, and the side for launching cabin is equipped with hatch door,
The inside for launching cabin is placed with robot body, and the rear wall for launching cabin is located at the rearward position of robot body
Pushing meanss are installed, the bottom for launching cabin, which is located at two side positions of robot body, is provided with limit plate, described
Reel is installed, one end of the reel is fixedly installed with motor, and reel is internally provided at the top of hatch door
Shaft, is provided with pusher cylinder on rear side of the pushing meanss, and the installed in front of pushing meanss has a push plate, the push plate with
The junction of pusher cylinder is equipped with piston rod, and umbellate form cover, the umbellate form cover are fixedly installed at the top of the robot body
Lower section be connected with head, the lower end on the head is equipped with pedestal, and the inside of the damping device is equipped with spring, described
When drone body works, wind speed, meteorology and height can be carried out by external monitoring devices and is monitored, to confirm outside weather
Environment is run if appropriate for drone body, while realizing best release altitude measurement, prevents robot body occur when air-drop
The phenomenon that breaking.
As a further solution of the present invention：The hatch door and motor are rotatablely connected by shaft, the motor and
External remote control equipment is electrically connected.
As further scheme of the invention：The push plate is fixedly connected with pusher cylinder by piston rod, the work
There are two stopper rod is arranged altogether, and two piston rods are arranged in parallel.
As further scheme of the invention：The limit plate is fixedly connected with cabin is launched, and limit plate is provided with altogether
Two, described two limit plates are arranged in parallel.
As further scheme of the invention：There are two the supporting leg is installed altogether, and two supporting legs are installed in parallel,
The bottom end of described two supporting legs is mounted on damping device.
As further scheme of the invention：There are two the damping device is arranged altogether, and damping device is cylinder
Structure, there are two the spring is arranged altogether.
As further scheme of the invention：The junction on the umbellate form cover and head is provided with fixed link, and umbellate form
Cover and head are fixed by fixed link, and the umbellate form cover is umbrella-shaped structure.
As further scheme of the invention：The dispensing cabin is fixedly connected with fuselage, and the horn and fuselage are one
Forming structure, four horn structures are consistent, and are mounted on propeller at the top of four horns.
Compared with prior art, the beneficial effects of the invention are as follows：
1, the present invention can be realized the unlatching and closure of hatch door by motor, drive shaft to rotate using motor, from
And realize the winding work of hatch door, when needing to launch robot, directly controlling hatch door unlatching by wireless remote control device is
It can.
2, the present invention can be defined the position of robot, prevent from leading in unmanned plane operation process by limit plate
The phenomenon that causing robot to be displaced, the progress to push the work forward convenient for it.
3, the present invention can be realized the push work of push plate using the piston rod in pusher cylinder, be led to by pushing meanss
The stretching for crossing piston rod drives the Forward of push plate, to generate motive force to robot, disengages it from and launches cabin, realizes air-drop
Process.
4, the present invention can be prevented impact force in descent from spending the breaking-up for causing robot greatly, be had by umbellate form cover
Effect reduces speed when robot falls, and mitigates the impact force of tenesmus, makes its safe landing, guarantees its safety.
5, the present invention can be realized air-drop unmanned plane and image effective combination of unmanned plane, increase its function by camera
Energy property, while improving the precision of air-drop.
6, the present invention can effectively improve the damping effect of equipment by damping device, when solving due to unmanned plane landing
It is excessive and fuselage is caused to damage that impact force is led to the problem of with ground, is improved equipment overall stability, is prolonged its service life.
Detailed description of the invention
Fig. 1 is the structural schematic diagram that a kind of unmanned plane launches umbrella shape robot device in the air；
Fig. 2 is that a kind of unmanned plane launches the schematic diagram of internal structure that cabin is launched in umbrella shape robot device in the air；
Fig. 3 is the structural schematic diagram that a kind of unmanned plane launches pushing meanss in umbrella shape robot device in the air；
Fig. 4 is the structural schematic diagram that a kind of unmanned plane launches robot body in umbrella shape robot device in the air；
Fig. 5 is the structural schematic diagram that a kind of unmanned plane launches damping device in umbrella shape robot device in the air.
In figure：1, drone body；2, fuselage；3, horn；4, propeller；5, cabin is launched；6, camera；7, supporting leg；
8, damping device；9, reel；10, hatch door；11, motor；12, shaft；13, robot body；14, pushing meanss；15,
Pusher cylinder；16, piston rod；17, push plate；18, umbellate form cover；19, head；20, pedestal；21, spring；22, limit plate.
Specific embodiment
Please refer to Fig. 1~5, in the embodiment of the present invention, a kind of unmanned plane launches umbrella shape robot device, including nobody in the air
Machine ontology 1, the top of drone body 1 is provided with fuselage 2, and the bottom end of drone body 1 is connected with supporting leg 7, support
The bottom end of leg 7 is equipped with damping device 8, and there are two the total installations of supporting leg 7, and two supporting legs 7 are installed in parallel, two supports
The bottom end of leg 7 is mounted on damping device 8, and there are two the total settings of damping device 8, and damping device 8 is cylindrical structure, is subtracted
The inside of shake device 8 is equipped with spring 21, and spring 21 there are two settings, can effectively improve equipment by damping device 8 altogether
Damping effect solves the problems, such as that raising is set due to excessive and fuselage is caused to damage with ground generation impact force when unmanned plane lands
Standby overall stability, prolongs its service life.
The outside of fuselage 2 is provided with four horns 3 circumferentially dispersed, and horn 3 is an integral molding structure with fuselage 2, and four
A 3 structure of horn is consistent, the lower surface of fuselage 2 be provided with launch cabin 5, launch cabin 5 be fixedly connected with fuselage 2, horn 3 it is upper
Side is equipped with propeller 4, and the top of four horns 3 is mounted on propeller 4, and the front side insertion for launching cabin 5 is provided with camera
6, air-drop unmanned plane can be realized by camera 6 and image effective combination of unmanned plane, increase its functionality, improve simultaneously
The precision of air-drop.
The side for launching cabin 5 is equipped with hatch door 10, and the top of hatch door 10 is equipped with reel 9, and one end of reel 9 is solid
Dingan County is equipped with motor 11, and reel 9 is internally provided with shaft 12, and hatch door 10 and motor 11 pass through shaft 12 and rotate
Connection, motor 11 and external remote control equipment are electrically connected, and can be realized the unlatching and closure of hatch door 10 by motor 11,
Shaft 12 is driven to rotate using motor 11, to realize the winding work of hatch door 10, when needing to launch robot, directly
Hatch door 10 is controlled by wireless remote control device to open.
The inside for launching cabin 5, which is placed with robot body 13, can pass through external monitoring devices when drone body 1 works
It carries out wind speed, meteorology and height to monitor, to confirm that outside weather environment is run if appropriate for drone body 1, realize simultaneously
Best release altitude measurement prevents the phenomenon that robot body 13 is broken occur when air-drop, and the top of robot body 13 is fixed
Umbellate form cover 18 is installed, the lower section of umbellate form cover 18 is connected with head 19, and umbellate form cover 18 and the junction on head 19 are provided with fixation
Bar, and umbellate form cover 18 is fixed with head 19 by fixed link, umbellate form cover 18 is umbrella-shaped structure, and the lower end on head 19 is equipped with bottom
Seat 20 can prevent impact force in descent from spending the big breaking-up for causing robot, machine is effectively reduced by umbellate form cover 18
Speed when people falls, mitigates the impact force of tenesmus, makes its safe landing, guarantee its safety.
The bottom for launching cabin 5 is located at two side positions of robot body 13 and is provided with limit plate 22, limit plate 22 and
It launches cabin 5 to be fixedly connected, and there are two the total settings of limit plate 22, two limit plates 22 are arranged in parallel, and pass through 22 energy of limit plate
It is enough that the position of robot is defined, the phenomenon that causing robot to be displaced in unmanned plane operation process is prevented, it is convenient for
The progress to push the work forward.
The rear wall for launching cabin 5, which is located at the rearward position of robot body 13, is equipped with pushing meanss 14, pushing meanss
14 rear side is provided with pusher cylinder 15, and the installed in front of pushing meanss 14 has push plate 17, push plate 17 and pusher cylinder 15
Junction piston rod 16 is installed, push plate 17 is fixedly connected with pusher cylinder 15 by piston rod 16, and piston rod 16 is arranged altogether
There are two, and two piston rods 16 are arranged in parallel, it can be real using the piston rod 16 in pusher cylinder 15 by pushing meanss 14
The push work of existing push plate 17, the Forward of push plate 17 is driven by the stretching of piston rod 16, to generate promotion to robot
Power disengages it from and launches cabin 5, realizes air-drop process.
The working principle of the invention is：Firstly, driving shaft using motor 11 by 11 opened door 10 of motor
12 rotations, when needing to launch robot, are directly controlled by wireless remote control device to realize the winding work of hatch door 10
Hatch door 10 is opened, while can be defined to the position of robot by limit plate 22, and unmanned plane operation process is prevented
In the phenomenon that causing robot to be displaced convenient for the progress that it pushes the work forward then, pass through pushing meanss 14 using pushing
Piston rod 16 in cylinder 15 realizes the push work of push plate 17, and the Forward of push plate 17 is driven by the stretching of piston rod 16, from
And motive force is generated to robot, it disengages it from and launches cabin 5, realize that air-drop process further can by umbellate form cover 18
It prevents impact force in descent from spending the breaking-up for causing robot greatly, speed when robot falls is effectively reduced, under mitigation
The impact force of pendant makes its safe landing, guarantees its safety, while can be realized air-drop unmanned plane and camera shooting by camera 6
Effective combination of unmanned plane increases its functionality, while improving the precision of air-drop, finally, can have by damping device 8
Effect improves the damping effect of equipment, solves to cause fuselage to damage due to excessive with ground generation impact force when unmanned plane lands
The problem of, equipment overall stability is improved, is prolonged its service life.
Claims (8)
1. a kind of unmanned plane launches umbrella shape robot device, including drone body (1) in the air, which is characterized in that it is described nobody
It is provided at the top of machine ontology (1) fuselage (2), and the bottom end of drone body (1) is connected with supporting leg (7), the fuselage (2)
Outside be provided with four horns (3) circumferentially dispersed, and the lower surface of fuselage (2) is provided with and launches cabin (5), the horn
(3) it is equipped with above propeller (4), the bottom end of the supporting leg (7) is equipped with damping device (8), dispensing cabin (5)
Front side insertion is provided with camera (6), and the side for launching cabin (5) is equipped with hatch door (10), and the inside for launching cabin (5) is put
The rear wall for being equipped with robot body (13), and launching cabin (5), which is located to be equipped at the rearward position of robot body (13), to be pushed away
Dynamic device (14), the bottom for launching cabin (5), which is located at two side positions of robot body (13), is provided with limit plate
(22), it is equipped with reel (9) at the top of the hatch door (10), one end of the reel (9) is fixedly installed with motor
(11), and reel (9) is internally provided with shaft (12), on rear side of the pushing meanss (14) is provided with pusher cylinder
(15), and the installed in front of pushing meanss (14) has push plate (17), and the junction of the push plate (17) and pusher cylinder (15) is pacified
Equipped with piston rod (16), it is fixedly installed with umbellate form cover (18) at the top of the robot body (13), the umbellate form cover (18)
Lower section is connected with head (19), and the lower end of the head (19) is equipped with pedestal (20), the inside installation of the damping device (8)
Have spring (21), when the drone body (1) works, wind speed, meteorology and height can be carried out by external monitoring devices and is supervised
It surveys, to confirm that outside weather environment is run if appropriate for drone body (1), while realizing best release altitude measurement, prevent
Occurs the phenomenon that robot body (13) is broken when air-drop.
2. a kind of unmanned plane according to claim 1 launches umbrella shape robot device in the air, which is characterized in that the hatch door
(10) it is rotatablely connected with motor (11) by shaft (12), the motor (11) and external remote control equipment are electrically connected.
3. a kind of unmanned plane according to claim 1 launches umbrella shape robot device in the air, which is characterized in that the push plate
(17) it is fixedly connected with pusher cylinder (15) by piston rod (16), there are two the total settings of the piston rod (16), and two work
Stopper rod (16) is arranged in parallel.
4. a kind of unmanned plane according to claim 1 launches umbrella shape robot device in the air, which is characterized in that the limit
Plate (22) is fixedly connected with cabin (5) are launched, and there are two the total settings of limit plate (22), described two limit plates (22) set in parallel
It sets.
5. a kind of unmanned plane according to claim 1 launches umbrella shape robot device in the air, which is characterized in that the support
There are two leg (7) is installed altogether, and two supporting legs (7) are installed in parallel, and the bottom end of described two supporting legs (7) is mounted on damping
Device (8).
6. a kind of unmanned plane according to claim 1 launches umbrella shape robot device in the air, which is characterized in that the damping
There are two device (8) is arranged altogether, and damping device (8) is cylindrical structure, and the spring (21) is altogether there are two settings.
7. a kind of unmanned plane according to claim 1 launches umbrella shape robot device in the air, which is characterized in that the umbellate form
The junction of cover (18) and head (19) is provided with fixed link, and umbellate form cover (18) is fixed with head (19) by fixed link, institute
Stating umbellate form cover (18) is umbrella-shaped structure.
8. a kind of unmanned plane according to claim 1 launches umbrella shape robot device in the air, which is characterized in that the dispensing
Cabin (5) is fixedly connected with fuselage (2), and the horn (3) is an integral molding structure with fuselage (2), four horns (3) structure
Unanimously, and at the top of four horns (3) propeller (4) are mounted on.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810766460.3A CN108820213A (en) | 2018-07-13 | 2018-07-13 | A kind of unmanned plane launches umbrella shape robot device in the air |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810766460.3A CN108820213A (en) | 2018-07-13 | 2018-07-13 | A kind of unmanned plane launches umbrella shape robot device in the air |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108820213A true CN108820213A (en) | 2018-11-16 |
Family
ID=64137050
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810766460.3A Withdrawn CN108820213A (en) | 2018-07-13 | 2018-07-13 | A kind of unmanned plane launches umbrella shape robot device in the air |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108820213A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111994274A (en) * | 2020-08-20 | 2020-11-27 | 云南恒草生物科技有限公司 | Unmanned aerial vehicle puts in device with buffer function |
| CN116552788A (en) * | 2023-07-07 | 2023-08-08 | 浙江翔龙航空科技有限公司 | Rescue unmanned aerial vehicle capable of carrying inflatable boat |
-
2018
- 2018-07-13 CN CN201810766460.3A patent/CN108820213A/en not_active Withdrawn
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111994274A (en) * | 2020-08-20 | 2020-11-27 | 云南恒草生物科技有限公司 | Unmanned aerial vehicle puts in device with buffer function |
| CN116552788A (en) * | 2023-07-07 | 2023-08-08 | 浙江翔龙航空科技有限公司 | Rescue unmanned aerial vehicle capable of carrying inflatable boat |
| CN116552788B (en) * | 2023-07-07 | 2023-11-10 | 浙江翔龙航空科技有限公司 | Rescue unmanned aerial vehicle capable of carrying inflatable boat |
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| PB01 | Publication | ||
| PB01 | Publication | ||
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| WW01 | Invention patent application withdrawn after publication | ||
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Application publication date: 20181116 |