CN106892096A - A kind of Intelligent unattended machine for being easy to safe flight - Google Patents
A kind of Intelligent unattended machine for being easy to safe flight Download PDFInfo
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- CN106892096A CN106892096A CN201710134986.5A CN201710134986A CN106892096A CN 106892096 A CN106892096 A CN 106892096A CN 201710134986 A CN201710134986 A CN 201710134986A CN 106892096 A CN106892096 A CN 106892096A
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- drive shaft
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Classifications
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- 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
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- 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
- B64D17/00—Parachutes
- B64D17/62—Deployment
- B64D17/70—Deployment by springs
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- 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
- B64D17/00—Parachutes
- B64D17/80—Parachutes in association with aircraft, e.g. for braking thereof
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- 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
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Toys (AREA)
Abstract
The present invention relates to a kind of Intelligent unattended machine for being easy to safe flight,Including base,Aviation mechanism,Protection mechanism and forced landing mechanism,Protection mechanism includes fix bar,Fixed block,Guide rail,First drive component,Second drive component and guard assembly,First drive component includes the first motor,First drive shaft and drive disk,Second drive component includes the 3rd motor and the 3rd drive shaft,Guard assembly includes protection network,The forced landing mechanism includes urgent case,3rd drive component,Landing pack,Guide post and spring,3rd drive component includes the 4th motor,Connecting rod,Hinged block and cover plate,Aviation mechanism includes fixed support,The chassis interior is provided with Zhong Kong mechanisms,This is easy to the Intelligent unattended machine of safe flight,Blade is protected by protection mechanism,Prevent the impaired influence flight of blade,Improve the security of unmanned plane；Unmanned plane is force-landed safely by forced landing mechanism, improve the reliability of unmanned plane.
Description
Technical field
The present invention relates to unmanned plane field, more particularly to a kind of Intelligent unattended machine for being easy to safe flight.
Background technology
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, using radio robot and providing for oneself
The not manned vehicle that presetting apparatus is manipulated.Unmanned plane is actually the general designation of unmanned vehicle, from technical standpoint
Definition can be divided into：This is several for depopulated helicopter, unmanned fixed-wing aircraft, unmanned multi-rotor aerocraft, unmanned airship, unmanned parasol
Major class.Compared with manned aircraft, it have small volume, low cost, easy to use, low to flight environment of vehicle requirement, survival ability compared with
Strong the advantages of.
In existing unmanned plane, blade without corresponding safeguard measure, when unmanned plane during flying is by adverse circumstances such as the woods
When, the aerial object that drops can be run into unavoidably, when rotating vane is damaged so that unmanned plane is unable to normal flight, influences nobody
Machine works；Meanwhile, when running into unmanned plane failure and needing emergency landing, due to without corresponding emergency landing device, unmanned plane
Directly from aerial ground of dropping, unmanned plane damage parts are inevitable, reduce the security of unmanned plane, improve unmanned plane
Spoilage.
The content of the invention
The technical problem to be solved in the present invention is：In order to overcome the deficiencies in the prior art, there is provided one kind is easy to safe flight
Intelligent unattended machine.
The technical solution adopted for the present invention to solve the technical problems is：A kind of Intelligent unattended machine for being easy to safe flight,
Including base, aviation mechanism, protection mechanism and forced landing mechanism, the aviation mechanism and protection mechanism are arranged on base
Side, the forced landing mechanism is arranged on the top of protection mechanism；
The protection mechanism includes vertically arranged fix bar, fixed block, guide rail, the first drive component, four the second drives
Dynamic component and four guard assemblies, described fix bar one end are arranged on base, and the fix bar other end is fixed with fixed block
Connection, the fixed block is connected with guide rail, and first drive component is arranged on base middle part, first drive component
Including the first motor, the first drive shaft and drive disk, first motor is connected by the first drive shaft with drive disk, institute
State guide rail to be arranged on inside drive disk, the guide rail is circle, the center of circle of the guide rail is located at the vertical central axis of drive disk
On, four second drive components are uniformly arranged the periphery of drive disk, and second drive component includes the 3rd motor and the
Three drive shafts, the 3rd motor is arranged on the inside of drive disk, and the 3rd motor and the 3rd drive shaft are connected；
The guard assembly includes protection network, and the protection network and the 3rd drive shaft are corresponded, and the 3rd motor leads to
The 3rd drive shaft is crossed to be connected with corresponding protection network；
Wherein, in order to realize protecting aviation mechanism, the 3rd motor, the 3rd motor are controlled by motor control module
Protection network is driven by the 3rd drive shaft, the 3rd drive shaft of control makes protection network be rotated by 90 ° in horizontality, then by electricity
Machine control module controls the first motor, the first motor to drive drive disk by the first drive shaft, and drive disk edge on fixed block is led
Rail is rotated, and the first motor action is stopped when protection network is turned to directly over blade.
The forced landing mechanism includes urgent case, the 3rd drive component, landing pack, guide post and spring, described the
Three drive components are arranged on the side of urgent case, and the 3rd drive component includes the 4th motor, connecting rod, hinged block and cover plate,
4th motor is connected by the drive shaft of the 4th motor with link transmission, the driving of one end of the connecting rod and the 4th motor
Axle is hinged, and the connecting rod other end is hinged with cover plate one end, and the cover plate is hinged by hinged block with urgent case, and the cover plate sets
Put in the top of urgent case, the landing pack is arranged on inside urgent case, the guide post is arranged on landing pack lower section, institute
The periphery that spring is set in guide post is stated, the guide post lower end is fixed on urgent bottom portion, and the lower spring end is fixed on tightly
Anxious bottom portion, the spring upper end is connected with landing pack.
Wherein, the 4th motor, the 4th motor control drive shaft turns are controlled by motor control module, drive shaft drives and connects
Bar is rotated, and connecting rod causes that cover plate does arc operation by the center of circle of hinged block so that cover plate is opened, anti-due to urgent case inner spring
Active force so that parachute coating spring extruding, spring is outwards acted along guide post so that be fixed on the parachute on spring
Coating ejection is gone out, and landing pack causes the safe land of unmanned plane after opening.
Preferably, the aviation mechanism includes fixed support, the support bracket fastened quantity is four, and four described solid
Fixed rack is uniformly arranged on base outer perimeter, and described fixed support one end is provided with the 4th drive component, the 4th drive component
Including the second motor, the second drive shaft and blade, second motor is connected by the second drive shaft with vane belt, and described
Two motors are arranged on fixed support.
Wherein, the second motor is controlled by motor control module, second the second drive shaft of motor control rotates blade, leaf
Piece produces air-flow after rotating, and makes unmanned plane during flying.
Preferably, the chassis interior is provided with Zhong Kong mechanisms, the Zhong Kong mechanisms include central control module and center
Control module connection power module, motor control module, communication control module, distance controlling module, display control module and
Rotational speed control module, first motor, the second motor, the 3rd motor and the 4th motor are electrically connected with motor control module,
The central control module is single-chip microcomputer.
Wherein, central control module, for controlling modules, improves intelligence degree；Power module, for equipment
The power supply of stabilization is provided, the stability of equipment is improve；Motor control module, works for controlled motor, improves intelligence
Energyization is controlled；Communication control module, realization carries out remote control to equipment, improves the intelligent of equipment；Distance controlling module,
For testing equipment flying height, the accuracy of equipment is improved；Display control module, is used to refer to the running status of equipment, carries
The reliability of equipment high；Rotational speed control module, for controlling the rotating speed of aviation mechanism blade, improves the security of equipment.
Preferably, the operation in order to enable a device to stabilization, the inside of the base is additionally provided with battery, the electric power storage
Pond electrically connects with power module.
Preferably, in order to realize the remote control to equipment, the chassis interior is provided with bluetooth, the bluetooth and communication
Control module is electrically connected.
Preferably, in order to the flying height of real-time watch device, the bottom of the base is provided with infrared sensor,
The infrared sensor is electrically connected with distance controlling module.
Preferably, the running status in order to judge equipment, the bottom of the base is provided with some LED lights,
The LED light is electrically connected with display control module.
Preferably, the rotating speed in order to monitor blade, the fixed support is provided with tachogenerator, described to test the speed
Sensor is electrically connected with rotational speed control module.
Preferably, in order to allow the bottom of equipment safety land, the base to be provided with some support frames.
Preferably, in order that the more stable land of equipment, the bottom of support frame as described above is provided with buffering cotton.
The beneficial effects of the invention are as follows, this is easy in the Intelligent unattended machine of safe flight, when unmanned plane during flying to the woods or
Person is run into when descending slowly and lightly thing in the air, and blade is protected by protection mechanism, prevents blade from being influenceed normal flight by external world's thing that descends slowly and lightly, and is carried
The high security of unmanned plane, effectively protection unmanned plane normal work；In order to allow unmanned plane in failure forced landing without receiving
Damage, unmanned plane is made by the opening of the pack that lands by forced landing mechanism, unmanned plane can slowly be force-landed prevents nothing
It is man-machine to be damaged when failure is landed, make unmanned plane more safe and reliable, while reducing loss.
Brief description of the drawings
The present invention is further described with reference to the accompanying drawings and examples.
Fig. 1 is the structural representation of the Intelligent unattended machine for being easy to safe flight of the invention；
Fig. 2 is the structural representation of the Intelligent unattended machine for being easy to safe flight of the invention；
Fig. 3 is the structural representation of the protection mechanism of the Intelligent unattended machine for being easy to safe flight of the invention；
Fig. 4 is the structural representation of the forced landing mechanism of the Intelligent unattended machine for being easy to safe flight of the invention；
Fig. 5 is the system diagram of the Intelligent unattended machine for being easy to safe flight of the invention；
In figure：1. blade, 2. fixed support, 3. protection mechanism, 4. forced landing mechanism, 5. drive disk, 6. fix bar, 7.
First motor, 8. the first drive shaft, 9. the second drive shaft, 10. the second motor, 11. buffering cottons, 12. bases, 13. support frames,
14. guide rails, 15. fixed blocks, 16. the 3rd motors, 17. the 3rd drive shafts, 18. protection networks, 19. the 4th motors, 20. connecting rods, 21.
Hinged block, 22. cover plates, 23. landing packs, 24. guide posts, 25. springs, 26. batteries, 27. power modules, 28. motor controls
Molding block, 29. central control modules, the distance controlling module of 30. communication control module 31., 32. display control modules, 33. rotating speeds
Control module, 34. bluetooths, 35. infrared sensors, 36.LED indicator lamps, 37. tachogenerators.
Specific embodiment
In conjunction with the accompanying drawings, the present invention is further explained in detail.These accompanying drawings are simplified schematic diagram, only with
Illustration illustrates basic structure of the invention, therefore it only shows the composition relevant with the present invention.
As Figure 1-Figure 5, a kind of Intelligent unattended machine for being easy to safe flight, including base 12, aviation mechanism, protection machine
Structure 3 and forced landing mechanism 4, the aviation mechanism and protection mechanism 3 are arranged at the top of base 12, the forced landing mechanism
4 tops for being arranged on protection mechanism 3；
The protection mechanism 3 include vertically arranged fix bar 6, fixed block 15, guide rail 14, the first drive component, four
Second drive component and four guard assemblies, one end of the fix bar 6 are arranged on base 12, the other end of the fix bar 6 with
Fixed block 15 is fixedly connected, and the fixed block 15 is connected with guide rail 14, and first drive component is arranged in base 12
Portion, first drive component includes the first motor 7, the first drive shaft 8 and drive disk 5, and first motor 7 drives by first
Moving axis 8 is connected with drive disk 5, and the guide rail 14 is arranged on inside drive disk 5, and the guide rail 14 is circle, the guide rail
14 center of circle is located on the vertical central axis of drive disk 5, and four second drive components are uniformly arranged the outer of drive disk 5
Week, second drive component includes the 3rd motor 16 and the 3rd drive shaft 17, and the 3rd motor 16 is arranged on drive disk 5
Inside, the 3rd motor 16 is connected with the 3rd drive shaft 17；
The guard assembly includes protection network 18, and the protection network 18 is corresponded with the 3rd drive shaft 17, the described 3rd
Motor 16 is connected by the 3rd drive shaft 17 with corresponding protection network 18；
Wherein, in order to realize protecting aviation mechanism, the 3rd motor 16, the 3rd are controlled by motor control module 28
Motor 16 drives protection network 18 by the 3rd drive shaft 17, and the 3rd drive shaft 17 of control makes protection network 18 be rotated by 90 ° in level
State, then control the first motor 7, the first motor 7 to drive drive disk 5 by the first drive shaft 8, drive by motor control module 28
Moving plate 5 is rotated on fixed block 15 along guide rail 14, the first motor 7 is stopped when protection network 18 turns to 1 surface of blade and is acted.
The forced landing mechanism 4 includes urgent case, the 3rd drive component, landing pack 23, guide post 24 and spring 25,
3rd drive component is arranged on the side of urgent case, and the 3rd drive component includes the 4th motor 19, connecting rod 20, is hinged
Block 21 and cover plate 22, the 4th motor 19 are connected by the drive shaft of the 4th motor 19 with connecting rod 20, the connecting rod 20
One end be hinged with the drive shaft of the 4th motor 19, the other end of the connecting rod 20 is hinged with the one end of cover plate 22, the cover plate 22 lead to
Cross hinged block 21 to be hinged with urgent case, the cover plate 22 is arranged on the top of urgent case, the landing pack 23 is arranged on promptly
Inside case, the guide post 24 is arranged on the lower section of landing pack 23, and the spring 25 is set in the periphery of guide post 24, described to lead
Urgent bottom portion is fixed on to the lower end of bar 24, the lower end of the spring 25 is fixed on urgent bottom portion, the upper end of the spring 25 and drop
The pack 23 that falls is connected.
Wherein, the 4th motor 19, the control drive shaft turns of the 4th motor 19, drive shaft are controlled by motor control module 28
Drive link 20 is rotated, and connecting rod 20 is with hinged block 21 for the center of circle causes that cover plate 22 does arc operation so that cover plate 22 is opened, due to
The reaction force of urgent case inner spring 25 so that landing pack 23 is extruded by spring 25, and spring 25 is outwards dynamic along guide post 24
Make so that the landing pack 23 being fixed on spring 25 is gone out by ejection, landing pack 23 causes unmanned plane safe after opening
Fall.
Preferably, the aviation mechanism includes fixed support 2, the quantity of the fixed support 2 is four, described in four
Fixed support 2 is uniformly arranged on the periphery of base 12, and the one end of the fixed support 2 is provided with the 4th drive component, the 4 wheel driven
Dynamic component includes the second motor 10, the second drive shaft 9 and blade 1, and second motor 10 is by the second drive shaft 9 and blade 1
Drive connection, second motor 10 is arranged on fixed support 2.
Wherein, the second motor 10 is controlled by motor control module 28, second drive shaft 9 of the control of the second motor 10 makes blade
1 rotates, and blade 1 produces air-flow after rotating, and makes unmanned plane during flying.
Preferably, be provided with Zhong Kong mechanisms inside the base 12, the Zhong Kong mechanisms include central control module 29 and
Central control module 29 connection power module 27, motor control module 28, communication control module 30, distance controlling module 31,
Display control module 32 and rotational speed control module 33, first motor 7, the second motor 10, the 3rd motor 16 and the 4th motor
19 electrically connect with motor control module 28, and the central control module 29 is single-chip microcomputer.
Wherein, central control module 29, for controlling modules, improve intelligence degree；Power module 27, for giving
Equipment provides the power supply of stabilization, improves the stability of equipment；Motor control module 28, works for controlled motor, carries
Intelligentized control method high；Communication control module 30, realization carries out remote control to equipment, improves the intelligent of equipment；Distance
Control module 31, for testing equipment flying height, improves the accuracy of equipment；Display control module 32, is used to refer to equipment
Running status, improve equipment reliability；Rotational speed control module 33, for controlling the rotating speed of aviation mechanism blade 1, improves
The security of equipment.
Preferably, the operation in order to enable a device to stabilization, the inside of the base 12 is additionally provided with battery 26, described
Battery 26 is electrically connected with power module 27.
Preferably, in order to realize the remote control to equipment, bluetooth 34, the bluetooth 34 are provided with inside the base 12
Electrically connected with communication control module 30.
Preferably, in order to the flying height of real-time watch device, the bottom of the base 12 is provided with infrared sensing
Device 35, the infrared sensor 35 is electrically connected with distance controlling module 31.
Preferably, the running status in order to judge equipment, the bottom of the base 12 is provided with some LED lights
36, the LED light 36 is electrically connected with display control module 32.
Preferably, the rotating speed in order to monitor blade 1, the fixed support 2 is provided with tachogenerator 37, described
Tachogenerator 37 is electrically connected with rotational speed control module 33.
Preferably, in order to allow the bottom of equipment safety land, the base 12 to be provided with some support frames 13.
Preferably, in order that the more stable land of equipment, the bottom of support frame as described above 13 is provided with buffering cotton 11.
Compared with prior art, this is easy in the Intelligent unattended machine of safe flight, when unmanned plane during flying to the woods or sky
In run into when descending slowly and lightly thing, blade 1 is protected by protection mechanism 3, prevent blade 1 from being influenceed normal flight by external world's thing that descends slowly and lightly, carry
The high security of unmanned plane, effectively protection unmanned plane normal work；In order to allow unmanned plane in failure forced landing without receiving
Damage, make unmanned plane by the opening of the pack 23 that lands by forced landing mechanism 4, unmanned plane can slowly be force-landed to be prevented
Unmanned plane is damaged when failure is landed, and makes unmanned plane more safe and reliable, while reducing loss.
With above-mentioned according to desirable embodiment of the invention as enlightenment, by above-mentioned description, relevant staff is complete
Various changes and amendments can be carried out without departing from the scope of the technological thought of the present invention' entirely.The technology of this invention
Property scope is not limited to the content on specification, it is necessary to its technical scope is determined according to right.
Claims (10)
1. a kind of Intelligent unattended machine for being easy to safe flight, it is characterised in that including base (12), aviation mechanism, protection mechanism
(3) and forced landing mechanism (4), the aviation mechanism and protection mechanism (3) are arranged at base (12) top, the urgent drop
The mechanism (4) that falls is arranged on the top of protection mechanism (3)；
The protection mechanism (3) including vertically arranged fix bar (6), fixed block (15), guide rail (14), the first drive component,
Four the second drive components and four guard assemblies, described fix bar (6) one end are arranged on base (12), the fix bar
(6) other end is fixedly connected with fixed block (15), and the fixed block (15) is connected with guide rail (14), first driving group
Part is arranged on base (12) middle part, and first drive component includes the first motor (7), the first drive shaft (8) and drive disk
(5), first motor (7) is connected by the first drive shaft (8) and drive disk (5), and the guide rail (14) is arranged on drive
Moving plate (5) is internal, and the guide rail (14) is circle, and the center of circle of the guide rail (14) is located at the vertical central axis of drive disk (5)
On, four second drive components are uniformly arranged the periphery of drive disk (5), and second drive component includes the 3rd motor
(16) and the 3rd drive shaft (17), the 3rd motor (16) is arranged on the inside of drive disk (5), the 3rd motor (16) with
3rd drive shaft (17) is connected；
The guard assembly includes protection network (18), and the protection network (18) and the 3rd drive shaft (17) are corresponded, described the
Three motors (16) are connected by the 3rd drive shaft (17) with corresponding protection network (18)；
The forced landing mechanism (4) includes urgent case, the 3rd drive component, landing pack (23), guide post (24) and spring
(25), the 3rd drive component is arranged on the side of urgent case, and the 3rd drive component includes the 4th motor (19), connecting rod
(20), hinged block (21) and cover plate (22), drive shaft and connecting rod (20) that the 4th motor (19) passes through the 4th motor (19)
Drive connection, one end and the drive shaft of the 4th motor (19) of the connecting rod (20) be hinged, connecting rod (20) other end with cover
Plate (22) one end is hinged, and the cover plate (22) is hinged by hinged block (21) and urgent case, and the cover plate (22) is arranged on promptly
The top of case, the landing pack (23) is arranged on inside urgent case, and the guide post (24) is arranged under landing pack (23)
Side, the spring (25) is set in the periphery of guide post (24), and guide post (24) lower end is fixed on urgent bottom portion, described
Spring (25) lower end is fixed on urgent bottom portion, and spring (25) upper end is connected with landing pack (23).
2. the Intelligent unattended machine of safe flight is easy to as claimed in claim 1, it is characterised in that the aviation mechanism includes solid
Fixed rack (2), the quantity of the fixed support (2) is four, and four fixed supports (2) are uniformly arranged on base (12) outward
Week, described fixed support (2) one end is provided with the 4th drive component, and the 4th drive component includes the second motor (10), the
Two drive shafts (9) and blade (1), second motor (10) are connected by the second drive shaft (9) and blade (1), described
Second motor (10) is arranged on fixed support (2).
3. the Intelligent unattended machine of safe flight is easy to as claimed in claim 2, it is characterised in that is set inside the base (12)
You Zhongkong mechanisms, the Zhong Kong mechanisms include the power module that central control module (29) and central control module (29) are connected
(27), motor control module (28), communication control module (30), distance controlling module (31), display control module (32) and turn
Fast control module (33), first motor (7), the second motor (10), the 3rd motor (16) and the 4th motor (19) with electricity
Machine control module (28) is electrically connected, and the central control module (29) is single-chip microcomputer.
4. the Intelligent unattended machine of safe flight is easy to as claimed in claim 3, it is characterised in that the inside of the base (12)
Battery (26) is additionally provided with, the battery (26) electrically connects with power module (27).
5. the Intelligent unattended machine of safe flight is easy to as claimed in claim 3, it is characterised in that is set inside the base (12)
There is bluetooth (34), the bluetooth (34) electrically connects with communication control module (30).
6. the Intelligent unattended machine of safe flight is easy to as claimed in claim 3, it is characterised in that the bottom of the base (12)
Infrared sensor (35) is provided with, the infrared sensor (35) electrically connects with distance controlling module (31).
7. the Intelligent unattended machine of safe flight is easy to as claimed in claim 3, it is characterised in that the bottom of the base (12)
Some LED lights (36) are provided with, the LED light (36) electrically connects with display control module (32).
8. the Intelligent unattended machine of safe flight is easy to as claimed in claim 3, it is characterised in that on the fixed support (2)
Tachogenerator (37) is provided with, the tachogenerator (37) electrically connects with rotational speed control module (33).
9. the Intelligent unattended machine of safe flight is easy to as claimed in claim 1, it is characterised in that the bottom of the base (12)
It is provided with some support frames (13).
10. the Intelligent unattended machine of safe flight is easy to as claimed in claim 9, it is characterised in that support frame as described above (13)
Bottom is provided with buffering cotton (11).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710134986.5A CN106892096B (en) | 2017-03-08 | 2017-03-08 | A kind of Intelligent unattended machine convenient for safe flight |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710134986.5A CN106892096B (en) | 2017-03-08 | 2017-03-08 | A kind of Intelligent unattended machine convenient for safe flight |
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| Publication Number | Publication Date |
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| CN106892096A true CN106892096A (en) | 2017-06-27 |
| CN106892096B CN106892096B (en) | 2019-02-01 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710134986.5A Active CN106892096B (en) | 2017-03-08 | 2017-03-08 | A kind of Intelligent unattended machine convenient for safe flight |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108583854A (en) * | 2018-04-10 | 2018-09-28 | 清远市巨劲科技有限公司 | A kind of contractile miniature portable unmanned plane of wing |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20110147511A1 (en) * | 2004-03-10 | 2011-06-23 | Poltorak Alexander I | Rotating wing aircraft with tip-driven rotor and rotor-guide ring |
| KR20120084433A (en) * | 2011-01-20 | 2012-07-30 | 건국대학교 산학협력단 | Composite protection structure for flying robot with rotary wings |
| CN202935581U (en) * | 2012-10-23 | 2013-05-15 | 宁波市鄞州发辉机械科技有限公司 | Rotor wing protection framework device |
| CN203094454U (en) * | 2012-10-31 | 2013-07-31 | 西安韦德沃德航空科技有限公司 | Safely recoverable non-coaxial multi-rotor vertical take-off and landing aircraft |
| CN204415740U (en) * | 2014-12-29 | 2015-06-24 | 马鞍山市赛迪智能科技有限公司 | Unmanned plane is left a blank Lighting System |
| CN204507264U (en) * | 2015-03-27 | 2015-07-29 | 滨州学院 | A kind of safe manned craft |
| CN204937514U (en) * | 2015-09-25 | 2016-01-06 | 佛山世寰智能科技有限公司 | A kind of unmanned plane with falling guard function |
-
2017
- 2017-03-08 CN CN201710134986.5A patent/CN106892096B/en active Active
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20110147511A1 (en) * | 2004-03-10 | 2011-06-23 | Poltorak Alexander I | Rotating wing aircraft with tip-driven rotor and rotor-guide ring |
| KR20120084433A (en) * | 2011-01-20 | 2012-07-30 | 건국대학교 산학협력단 | Composite protection structure for flying robot with rotary wings |
| CN202935581U (en) * | 2012-10-23 | 2013-05-15 | 宁波市鄞州发辉机械科技有限公司 | Rotor wing protection framework device |
| CN203094454U (en) * | 2012-10-31 | 2013-07-31 | 西安韦德沃德航空科技有限公司 | Safely recoverable non-coaxial multi-rotor vertical take-off and landing aircraft |
| CN204415740U (en) * | 2014-12-29 | 2015-06-24 | 马鞍山市赛迪智能科技有限公司 | Unmanned plane is left a blank Lighting System |
| CN204507264U (en) * | 2015-03-27 | 2015-07-29 | 滨州学院 | A kind of safe manned craft |
| CN204937514U (en) * | 2015-09-25 | 2016-01-06 | 佛山世寰智能科技有限公司 | A kind of unmanned plane with falling guard function |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108583854A (en) * | 2018-04-10 | 2018-09-28 | 清远市巨劲科技有限公司 | A kind of contractile miniature portable unmanned plane of wing |
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