CN108791850A - Novel unmanned vehicle - Google Patents
Novel unmanned vehicle Download PDFInfo
- Publication number
- CN108791850A CN108791850A CN201810617795.9A CN201810617795A CN108791850A CN 108791850 A CN108791850 A CN 108791850A CN 201810617795 A CN201810617795 A CN 201810617795A CN 108791850 A CN108791850 A CN 108791850A
- Authority
- CN
- China
- Prior art keywords
- unmanned vehicle
- aircraft
- connection
- aircraft body
- flying wing
- 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.)
- Withdrawn
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Classifications
-
- 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
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/54—Floats
- B64C25/56—Floats inflatable
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/02—Arrangements or adaptations of signal or lighting devices
- B64D47/06—Arrangements or adaptations of signal or lighting devices for indicating aircraft presence
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
Abstract
The present invention discloses a kind of novel unmanned vehicle, and one end of multiple solid rings is connected to flying wing end in turn, and the other end bypasses flight paddle and comes together in the same tie point after being upwardly formed outwardly projecting arc, and tie point is on the central axis of aircraft body.Novel unmanned vehicle further includes that at least three support legs, support leg is disposed in an evenly spaced relation on the bottom face of aircraft body along circumferential direction, and an annular inflatable air cushion is interconnected to form between support leg.Containing cavities are formed on the side wall of aircraft body, inside is filled with signal flare or aerosol bomb, also, containing cavities pass through sealing of sealing cover.It can take off and forced landing with very strong flight stability on land and the water surface so that logistics transportation more quick and safe；Meanwhile once unexpected air crash occurs for unmanned vehicle, it can in time be found convenient for salvor with the specific orientation of automatic prompt.
Description
Technical field
The present invention relates to unmanned vehicle fields, and in particular, to a kind of novel unmanned vehicle.
Background technology
With more and more unmanned planes, model plane, aerial photography aircraft is applied in civil field, such unmanned vehicle due to
Function is continuously increased with ceiling voyage, and the weight and volume of unmanned vehicle itself is also being continuously increased, and it is such nobody fly
The undercarriage of row device has been difficult to bear such weight, during leading to the landing after flown, occur undercarriage lose into
And aircraft is made the damage of structure and appearance occur.
Existing unmanned vehicle has multiple flying wings, and after slight deformation occurs for a flying wing wherein, flight
Device meeting disequilibrium in flight course, is easy air crash；And the more fragile position of unmanned vehicle and hard ground after air crash
Collision easily cracking failure, leads to not use, increases maintenance cost.Meanwhile unmanned vehicle is in night or light line
Flight safety is low in the environment of part difference, while inconvenient naked eyes position.Once accident occurs in flight course for unmanned vehicle
Air crash is difficult to find and succour in time only by visually observing when falling into region with a varied topography.
Therefore, urgent need, which will provide one kind, can prompt crash-position, save the novel unmanned flight of relief unmanned plane time
Device.
Invention content
The object of the present invention is to provide a kind of novel unmanned vehicle, which has very strong flight steady
It is qualitative, it can take off on land and the water surface and forced landing so that logistics transportation more quick and safe；Meanwhile once nobody
It is unexpected that air crash occurs for aircraft, can in time be found convenient for salvor with the specific orientation of automatic prompt.
To achieve the goals above, the present invention provides a kind of novel unmanned vehicles, including are used to store transport cargo
Aircraft body, flying wing, connection ring and three-dimensional ring；
One end of flying wing is fixed on the lateral wall of aircraft body, the other end along aircraft body radial direction to
Outer extension；The quantity of flying wing is at least three and is arranged along the circumferential direction uniform intervals of aircraft body；
The diameter of flying wing is gradually reduced from inside to outside and end is equipped with flight paddle, connection ring along circumferential direction according to
The secondary end for connecting each flying wing, also, connection ring and aircraft body are concentric；
One end of multiple solid rings is connected to flying wing end in turn, and the other end bypasses flight paddle and is upwardly formed outward
The same tie point is come together in after arc outstanding, tie point is on the central axis of aircraft body；
Multiple clearance lamps are equipped at intervals on connection ring and three-dimensional ring, the equal parallel connection of clearance lamps is electrically connected to aircraft body
Photovoltaic panel, also, photovoltaic panel bottom end is hinged in aircraft body, and light sensor is also associated on clearance lamps；
Novel unmanned vehicle further includes that at least three support legs, support leg is disposed in an evenly spaced relation in flight along circumferential direction
An annular inflatable air cushion is interconnected to form on the bottom face of device main body, between support leg；Wherein,
Containing cavities are formed on the side wall of aircraft body, inside is filled with signal flare or aerosol bomb, also, containing cavities
Pass through sealing of sealing cover.
Preferably, connection ring and three-dimensional ring are that elastoplastic or rubber are made.
Preferably, the connection between connection ring and flying wing is detachable connection.
Preferably, detachable connection is to be threadedly coupled, and is equipped with internal thread hole on connection ring and flying wing, passes through spiral shell
Bolt sequentially passes through internal thread hole and connection ring can be solidly connected on flying wing.
Preferably, the connection between three-dimensional ring and flying wing is detachable connection.
Preferably, detachable connection is to be threadedly coupled or snap connection.
Preferably, flight paddle is double bladed paddle or three leaf paddles.
According to above-mentioned technical proposal, one end of flying wing is fixed on the lateral wall of aircraft body by the present invention, is utilized
Connection ring links together the other end of multiple flying wings, can make multiple flying wings by the involve power of connection ring in this way
It remains original position, maintains original angle between each other so that entire aircraft can be always in flight course
Keep balance, stabilized flight.Meanwhile one end of multiple three-dimensional rings is connected to flying wing end in turn, the other end bypasses flight
Paddle simultaneously comes together in the same tie point, central axis of the tie point in aircraft body after being upwardly formed outwardly projecting arc
On.It is that multiple three-dimensional eyes are first touched with ground when unmanned vehicle lands in this way, even if unexpected air crash occurs in flight course
It hits, since three-dimensional ring has certain elasticity, good buffering effect can be played, it can also be by rolling come effectively after landing
The secondary injury to fall after secondary bounce is prevented, ensures the integrality of each component, security performance is high, and service life is long, saves
Maintenance cost.
Also, multiple clearance lamps are equipped at intervals on connection ring and three-dimensional ring, the equal parallel connection of clearance lamps is electrically connected to aircraft master
Photovoltaic panel on body, also, photovoltaic panel bottom end is hinged in aircraft body, and light sensor is also associated on clearance lamps.This
Sample, when The night screen has hung down or uses unmanned vehicle under rather dark environment, after light sensor induction is less than light
It is shinny to trigger clearance lamps unlatching so that unmanned vehicle is remained able to smoothly take off in such environment and be indicated according to clearance lamps
Flight range can also confirm the profile of the aircraft in dark surrounds and avoid in time, reduce accidental impact and bring machine
Damage, extends its service life.
When aircraft drop to rugged jump area, in order to avoid aircraft body, flying wing bottom end and ground
It collides with, extends the service life of aircraft, it is preferable that novel unmanned vehicle further includes at least three support legs, support
Foot is disposed in an evenly spaced relation on the bottom face of aircraft body along circumferential direction.Meanwhile one is interconnected to form between support leg
The inflatable air cushion of a annular can use remote control air valve to be inflated to inflatable air cushion, inflate so in actual use
Inflatable air cushion afterwards is heaved can generate larger buoyancy to support entire aircraft to be done on the water surface under case of emergency in water
Take off or landing operation, ensure that logistics goods still normal transport under extreme terrain environment so that logistics transport is pressed
When reach, substantially increase the safety of logistics goods.
Aircraft in flight course be easy influenced that unexpected air crash occurs by wind-force or rainwater, once and aircraft until
Can't be exposed on earth's surface surface when region with a varied topography, it is difficult to position and be succoured only by visually observing；Cause
This is formed with containing cavities on the side wall of aircraft body, and inside is filled with signal flare or aerosol bomb, also, containing cavities are logical
Cross sealing of sealing cover.In this way, when unmanned plane air crash needs relief, can be sent out with remote control or automatic activation signal bullet
Signal, aerosol bomb exhale largely has coloured smog, prompts the specific location residing for deliverer's aircraft with this, saves
The time is searched and rescued, relief speed is accelerated.
Other features and advantages of the present invention will be described in detail in subsequent specific embodiment part.
Description of the drawings
Attached drawing is to be used to provide further understanding of the present invention, an and part for constitution instruction, with following tool
Body embodiment is used to explain the present invention together, but is not construed as limiting the invention.In the accompanying drawings：
Fig. 1 is the structural schematic diagram according to the novel unmanned vehicle in a kind of embodiment provided by the invention.
Reference sign
1- aircraft body 2- flying wings
3- connection ring 4- solid rings
5- flight paddle 6- support legs
7- inflatable air cushion 8- clearance lamps
9- photovoltaic panel 10- containing cavities
Specific implementation mode
The specific implementation mode of the present invention is described in detail below in conjunction with attached drawing.It should be understood that this place is retouched
The specific implementation mode stated is merely to illustrate and explain the present invention, and is not intended to restrict the invention.
In the present invention, in the absence of explanation to the contrary, the noun of locality that " top, bottom end " etc. is included in the term is only
Represent orientation of the term under normal service condition, or be those skilled in the art understand that be commonly called as, and be not construed as to this
The limitation of term.
Referring to Fig. 1, the present invention provides a kind of novel unmanned vehicle, includes the aircraft body for storing transport cargo
1, flying wing 2, connection ring 3 and three-dimensional ring 4；
One end of flying wing 2 is fixed on the lateral wall of aircraft body 1, and the other end is along the radial direction side of aircraft body 1
To extending outwardly；The quantity of flying wing 2 is at least three and is arranged along the circumferential direction uniform intervals of aircraft body 1；
The diameter of flying wing 2 is gradually reduced from inside to outside and end is equipped with flight paddle 5, and connection ring 3 is circumferentially square
To the end for being sequentially connected each flying wing 2, also, connection ring 3 and aircraft body 1 are concentric；
One end of multiple solid rings 4 is connected to 2 end of flying wing in turn, and the other end bypasses flight paddle 5 and is upwardly formed
The same tie point is come together in after outwardly projecting arc, tie point is on the central axis of aircraft body 1；
Multiple clearance lamps 8 are equipped at intervals on connection ring 3 and three-dimensional ring 4,8 equal parallel connection of clearance lamps is electrically connected to aircraft body
Photovoltaic panel 9 on 1, also, 9 bottom end of photovoltaic panel is hinged in aircraft body 1, and light sensor is also associated on clearance lamps 8；
Novel unmanned vehicle further includes that at least three support legs 6, support leg 6 is disposed in an evenly spaced relation in winged along circumferential direction
On the bottom face of row device main body 1, an annular inflatable air cushion 7 is interconnected to form between support leg 6；Wherein,
Containing cavities 10 are formed on the side wall of aircraft body 1, inside is filled with signal flare or aerosol bomb, also, receives
Chamber 10 of receiving passes through sealing of sealing cover.
Through the above technical solutions, one end of flying wing 2 is fixed on the lateral wall of aircraft body 1, connection is utilized
Ring 3 links together the other end of multiple flying wings 2, can make multiple flying wings 2 by the involve power of connection ring 3 in this way
It remains original position, maintains original angle between each other so that entire aircraft can be always in flight course
Keep balance, stabilized flight.Meanwhile one end of multiple three-dimensional rings 4 is connected to 2 end of flying wing in turn, the other end, which bypasses, to fly
Row paddle 5 simultaneously comes together in the same tie point, central shaft of the tie point in aircraft body 1 after being upwardly formed outwardly projecting arc
On line.In this way, even if unexpected air crash occurs in flight course, be when unmanned vehicle land multiple solid rings 4 first with ground
Face is collided, and since three-dimensional ring 4 has certain elasticity, can be played good buffering effect, can also be passed through rolling after landing
It is effectively prevent the secondary injury to fall after secondary bounce, ensures the integrality of each component, security performance is high, and service life is long,
Maintenance cost is saved.
Multiple clearance lamps 8 are equipped at intervals on connection ring 3 and three-dimensional ring 4,8 equal parallel connection of clearance lamps is electrically connected to aircraft body
Photovoltaic panel 9 on 1, also, 9 bottom end of photovoltaic panel is hinged in aircraft body 1, and light sensor is also associated on clearance lamps 8.
In this way, when The night screen has hung down or uses unmanned vehicle under rather dark environment, light sensor incudes less than light
Triggering clearance lamps is opened shinny afterwards so that unmanned vehicle remains able to smoothly take off in such environment and be referred to according to clearance lamps
Show flight range, the profile of the aircraft can also be confirmed in dark surrounds and avoid in time, reduces accidental impact and bring machine
Device damages, and extends its service life.
When aircraft drop to rugged jump area, in order to avoid aircraft body 1,2 bottom end of flying wing and ground
Face is collided with, and the service life of aircraft is extended, it is preferable that novel unmanned vehicle further includes at least three support legs 6, branch
Spike 6 is disposed in an evenly spaced relation in along circumferential direction on the bottom face of aircraft body 1.Meanwhile being connected with each other shape between support leg 6
At an annular inflatable air cushion 7, remote control air valve can be used to be inflated to inflatable air cushion 7 in actual use, this
Inflatable air cushion 7 after sample inflation heaves that can to generate larger buoyancy in water emergent to support entire aircraft to be done on the water surface
In the case of take off or landing operation, ensure that logistics goods still normal transport under extreme terrain environment so that logistics
Transport reaches on time, substantially increases the safety of logistics goods.
Aircraft in flight course be easy influenced that unexpected air crash occurs by wind-force or rainwater, once and aircraft until
Can't be exposed on earth's surface surface when region with a varied topography, it is difficult to position and be succoured only by visually observing；Cause
This, is formed with containing cavities 10 on the side wall of aircraft body, and inside is filled with signal flare or aerosol bomb, also, containing cavities
10 pass through sealing of sealing cover.In this way, when unmanned plane air crash needs relief, it can be with remote control or automatic activation signal bullet
Send out signal, aerosol bomb exhales largely has coloured smog, the specific location residing for deliverer's aircraft is prompted with this,
It saves and searches and rescues the time, accelerate relief speed.
When novel unmanned vehicle lands, once landing unstable flight device disequilibrium or ground relief hold
Connection ring 3 or three-dimensional ring 4 is caused to contact generation scratch with ground or even break, the company of substantially reducing it is easier that aircraft is crooked
The service life for connecing ring 3 or three-dimensional ring 4, in order to avoid the generation of the above situation, it is preferable that connection ring 3 and three-dimensional ring 4 are
Elastoplastic or rubber are made.
In present embodiment, for the ease of dismounting connection ring 3 to be repaired to aircraft body 1, it is preferable that connection ring
Connection between 3 and flying wing 2 is detachable connection.
Above-mentioned dismountable connection type can be any type common in this field fast and easily connection type, but
From control product cost and from the point of view of mitigating aircraft overall weight, preferably detachable connection is to be threadedly coupled,
It is equipped with internal thread hole on connection ring 3 and flying wing 2, connection ring 3 can be solidly connected to by screw bolt passes internal thread hole
On flying wing 2.
Likewise, for the ease of the three-dimensional ring 4 of dismounting to be repaired to aircraft body 1, it is preferable that three-dimensional ring 4 with fly
Connection between the row wing 2 is detachable connection.
Above-mentioned dismountable connection type can be any type common in this field fast and easily connection type, but
From the point of view of control product cost and mitigation aircraft overall weight, it is preferable that detachable connection is that screw thread connects
It connects or snaps connection.
In addition, in order to obtain stable ascending air in flight 5 high speed rotation of paddle, the stability of aircraft is kept, it is excellent
Selection of land, flight paddle 5 are double bladed paddle or three leaf paddles.
The preferred embodiment of the present invention is described in detail above in association with attached drawing, still, the present invention is not limited to above-mentioned realities
The detail in mode is applied, within the scope of the technical concept of the present invention, a variety of letters can be carried out to technical scheme of the present invention
Monotropic type, these simple variants all belong to the scope of protection of the present invention.
It is further to note that specific technical features described in the above specific embodiments, in not lance
In the case of shield, can be combined by any suitable means, in order to avoid unnecessary repetition, the present invention to it is various can
The combination of energy no longer separately illustrates.
In addition, various embodiments of the present invention can be combined randomly, as long as it is without prejudice to originally
The thought of invention, it should also be regarded as the disclosure of the present invention.
Claims (7)
1. a kind of novel unmanned vehicle, which is characterized in that include for storing the aircraft body (1) of transport cargo, flight
The wing (2), connection ring (3) and three-dimensional ring (4)；
One end of the flying wing (2) is fixed on the lateral wall of the aircraft body (1), and the other end is along the aircraft master
The radial direction of body (1) extends outwardly；The quantity of the flying wing (2) is at least three and along the aircraft body (1)
Circumferential direction uniform intervals are arranged；
The diameter of the flying wing (2) is gradually reduced from inside to outside and end is equipped with flight paddle (5), the connection ring
(3) it is sequentially connected the end of each flying wing (2), also, the connection ring (3) and the aircraft along circumferential direction
Main body (1) is concentric；
One end of multiple three-dimensional rings (4) is connected to the flying wing (2) end in turn, and the other end bypasses the flight paddle
(5) and after being upwardly formed outwardly projecting arc the same tie point is come together in, the tie point is in the aircraft body (1)
Central axis on；
Multiple clearance lamps (8) are equipped at intervals on the connection ring (3) and the three-dimensional ring (4), the clearance lamps (8) is in parallel
It is electrically connected to the photovoltaic panel (9) in the aircraft body (1), also, the photovoltaic panel (9) bottom end is hinged on the aircraft master
On body (1), light sensor is also associated on the clearance lamps (8)；
The novel unmanned vehicle further includes at least three support legs (6), the support leg (6) uniform intervals along circumferential direction
It is arranged on the bottom face of the aircraft body (1), an annular inflation is interconnected to form between the support leg (6)
Air cushion (7)；Wherein,
Containing cavities (10) are formed on the side wall of the aircraft body (1), inside is filled with signal flare or aerosol bomb, and
And the containing cavities (10) pass through sealing of sealing cover.
2. novel unmanned vehicle according to claim 1, which is characterized in that the connection ring (3) and the three-dimensional ring
(4) it is that elastoplastic or rubber are made.
3. novel unmanned vehicle according to claim 1, which is characterized in that the connection ring (3) and the flying wing
(2) connection between is detachable connection.
4. novel unmanned vehicle according to claim 3, which is characterized in that the detachable connection connects for screw thread
It connects, is equipped with internal thread hole on the connection ring (3) and the flying wing (2), passes through internal thread hole described in screw bolt passes
The connection ring (3) can be solidly connected on the flying wing (2).
5. novel unmanned vehicle according to claim 3, which is characterized in that the solid ring (4) and the flying wing
(2) connection between is detachable connection.
6. novel unmanned vehicle according to claim 5, which is characterized in that the detachable connection connects for screw thread
It connects or snaps connection.
7. novel unmanned vehicle according to claim 1, which is characterized in that the flight paddle (5) be double bladed paddle or
Three leaf paddles.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810617795.9A CN108791850A (en) | 2018-06-15 | 2018-06-15 | Novel unmanned vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810617795.9A CN108791850A (en) | 2018-06-15 | 2018-06-15 | Novel unmanned vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108791850A true CN108791850A (en) | 2018-11-13 |
Family
ID=64086239
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810617795.9A Withdrawn CN108791850A (en) | 2018-06-15 | 2018-06-15 | Novel unmanned vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108791850A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109774956A (en) * | 2018-12-24 | 2019-05-21 | 湖南警察学院 | A kind of police Drones for surveillance |
| CN110510138A (en) * | 2019-09-03 | 2019-11-29 | 深圳市道通智能航空技术有限公司 | Aircraft alarm method, device and aircraft |
| WO2020107093A1 (en) * | 2018-11-28 | 2020-06-04 | Busuioc Sever Sorin | Aerodyne with a propulsive saucer for coanda effect propulsion |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104097772A (en) * | 2014-06-13 | 2014-10-15 | 芜湖特源鑫复合材料科技有限公司 | Smoke tracking aircraft |
| CN104590554A (en) * | 2015-01-05 | 2015-05-06 | 惠州市加迈电器有限公司 | Path-finding lighting equipment |
| CN104787325A (en) * | 2015-04-21 | 2015-07-22 | 中国科学院合肥物质科学研究院 | Supporting and protection mechanism of four-rotor robot |
| CN106103275A (en) * | 2014-03-25 | 2016-11-09 | 瓦斯菲·阿希达法特 | Rescue unmanned plane |
| CN107323676A (en) * | 2017-05-20 | 2017-11-07 | 马铿钧 | A kind of aircraft with anticollision device, collision-prevention device |
| CN107380442A (en) * | 2017-09-03 | 2017-11-24 | 佛山神航科技有限公司 | A kind of swimming pool emergency relief unmanned plane device |
| CN206750130U (en) * | 2017-05-10 | 2017-12-15 | 深圳市亿联智能有限公司 | A kind of wireless security protection monitoring device for patrol of flying |
| CN206797714U (en) * | 2017-05-20 | 2017-12-26 | 马铿钧 | A kind of shatter-resistant aircraft |
-
2018
- 2018-06-15 CN CN201810617795.9A patent/CN108791850A/en not_active Withdrawn
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106103275A (en) * | 2014-03-25 | 2016-11-09 | 瓦斯菲·阿希达法特 | Rescue unmanned plane |
| CN104097772A (en) * | 2014-06-13 | 2014-10-15 | 芜湖特源鑫复合材料科技有限公司 | Smoke tracking aircraft |
| CN104590554A (en) * | 2015-01-05 | 2015-05-06 | 惠州市加迈电器有限公司 | Path-finding lighting equipment |
| CN104787325A (en) * | 2015-04-21 | 2015-07-22 | 中国科学院合肥物质科学研究院 | Supporting and protection mechanism of four-rotor robot |
| CN206750130U (en) * | 2017-05-10 | 2017-12-15 | 深圳市亿联智能有限公司 | A kind of wireless security protection monitoring device for patrol of flying |
| CN107323676A (en) * | 2017-05-20 | 2017-11-07 | 马铿钧 | A kind of aircraft with anticollision device, collision-prevention device |
| CN206797714U (en) * | 2017-05-20 | 2017-12-26 | 马铿钧 | A kind of shatter-resistant aircraft |
| CN107380442A (en) * | 2017-09-03 | 2017-11-24 | 佛山神航科技有限公司 | A kind of swimming pool emergency relief unmanned plane device |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2020107093A1 (en) * | 2018-11-28 | 2020-06-04 | Busuioc Sever Sorin | Aerodyne with a propulsive saucer for coanda effect propulsion |
| CN109774956A (en) * | 2018-12-24 | 2019-05-21 | 湖南警察学院 | A kind of police Drones for surveillance |
| CN109774956B (en) * | 2018-12-24 | 2020-11-17 | 湖南警察学院 | Police investigation unmanned aerial vehicle |
| CN110510138A (en) * | 2019-09-03 | 2019-11-29 | 深圳市道通智能航空技术有限公司 | Aircraft alarm method, device and aircraft |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20181113 |