CN106240811A - Unmanned plane safety device and unmanned plane safety protecting method - Google Patents
Unmanned plane safety device and unmanned plane safety protecting method Download PDFInfo
- Publication number
- CN106240811A CN106240811A CN201610692921.8A CN201610692921A CN106240811A CN 106240811 A CN106240811 A CN 106240811A CN 201610692921 A CN201610692921 A CN 201610692921A CN 106240811 A CN106240811 A CN 106240811A
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- sensing
- air bag
- sensor
- predetermined
- 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.)
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Classifications
-
- 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
- B64U30/29—Constructional aspects of rotors or rotor supports; Arrangements thereof
- B64U30/299—Rotor guards
-
- 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
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U70/00—Launching, take-off or landing arrangements
- B64U70/80—Vertical take-off or landing, e.g. using rockets
- B64U70/83—Vertical take-off or landing, e.g. using rockets using parachutes, balloons or the like
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
- B64U10/13—Flying platforms
- B64U10/14—Flying platforms with four distinct rotor axes, e.g. quadcopters
Abstract
The invention discloses a kind of unmanned plane safety device and unmanned plane safety protecting method.Unmanned plane safety device according to the present invention includes: one or more motors that aircraft controller device is connected with aircraft controller device and paddle device, the one or more air bags being arranged corresponding to each motor and paddle device and sensor；Wherein, sensor is for sensing the speed of unmanned plane, and when the falling speed sensing unmanned plane is more than predetermined falling speed threshold value or when the whereabouts acceleration sensing unmanned plane is more than predetermined whereabouts acceleration rate threshold, the one or more air bag is ejected.
Description
Technical field
The present invention relates to unmanned plane field, particularly relate to a kind of unmanned plane safety device and corresponding unmanned plane peace
Full protection method.
Background technology
Conventional multi-rotor aerocraft, generation air crash the most out of control or misoperation bump against anyone/thing, on aircraft
Device is easy to damage, and including blade, motor, flies control, fuselage etc..
The protection device of unmanned many gyroplanes is fairly simple in the market, substantially protects aircraft with oar protective cover
Air crash or misoperation cause the loss that emergency is brought, this device can only slightly protect individual parts on aircraft,
Blade, motor, do not have the effect of all kinds of important device on protection aircraft, can not prevent the peace thus brought during real air crash
Full hidden danger.
Therefore, those skilled in the art is devoted to develop one and can solve unmanned many gyroplanes air crash out of control well
Or the technical scheme of the badly damaged and potential safety hazard that misoperation is brought.
Summary of the invention
Because the drawbacks described above of prior art, the technical problem to be solved is to provide one can be well
The unmanned plane safety of the badly damaged and potential safety hazard that the unmanned many gyroplanes air crash out of control of solution or misoperation are brought is anti-
Protection unit.
For achieving the above object, the invention provides a kind of unmanned plane safety device, including: aircraft controller fills
Put the one or more motors being connected with aircraft controller device and paddle device, be arranged on the one or more of fuselage interior
Air bag and sensor；Wherein, sensor is used for sensing the speed of unmanned plane, and in the whereabouts sensing unmanned plane
It is more than predetermined whereabouts acceleration threshold when speed is more than predetermined falling speed threshold value or at the whereabouts acceleration sensing unmanned plane
The one or more air bag is made to eject during value.
Preferably, sensor is when the falling speed sensing unmanned plane is more than predetermined falling speed threshold value or at sensing
Whereabouts acceleration to unmanned plane sends cue, aircraft to aircraft controller device when being more than predetermined whereabouts acceleration rate threshold
Control device sends pop instruction when receiving cue to the one or more air bag, so that described one
Individual or multiple air bags eject.
Preferably, wherein it is arranged the one or more air bag corresponding to each motor and paddle device.
Preferably, described unmanned plane safety device also includes: one or more blade protection networks, one of them oar
Leaf protection network corresponds to a motor and paddle device and at least partly surrounds one motor and paddle device layout.
Preferably, the one or more air bag is arranged in below the one or more blade protection network.
For achieving the above object, present invention also offers a kind of unmanned plane safety protecting method, described unmanned plane safety is anti-
Maintaining method uses above-mentioned unmanned plane safety device, it is characterised in that including:
First step: by the speed of sensor sensing unmanned plane；
Second step: when sensor senses the falling speed of unmanned plane more than predetermined falling speed threshold value or in sense
When measuring the whereabouts acceleration of unmanned plane more than predetermined whereabouts acceleration rate threshold so that the one or more air bag bullet
Go out.
In the present invention, use at unmanned many gyroplanes fuselage interior (such as, horn, center flying disc) installation air bag
Device, and sensor is installed on this air bag device, sensor detects that aircraft hurtles down and aviator's misoperation
Causing aircraft meeting out of control to immediately enter safeguard protection pattern, fuselage can eject air bag at once, the unmanned many gyroplanes of protection
Air crash or with anyone/the collide device that brings of thing calculates bad and unnecessary potential safety hazard.
Below with reference to accompanying drawing, the technique effect of design, concrete structure and the generation of the present invention is described further, with
It is fully understood from the purpose of the present invention, feature and effect.
Accompanying drawing explanation
Fig. 1 is the structural representation of unmanned plane safety device according to the preferred embodiment of the invention.
Fig. 2 is the flow chart of unmanned plane safety protecting method according to the preferred embodiment of the invention.
It should be noted that accompanying drawing is used for illustrating the present invention, and the unrestricted present invention.Note, represent that the accompanying drawing of structure can
Can be not necessarily drawn to scale.Further, in accompanying drawing, same or like element indicates same or like label.
Detailed description of the invention
Fig. 1 is the structural representation of unmanned plane safety device according to the preferred embodiment of the invention.
Specifically, as it is shown in figure 1, according to the preferred embodiment of the invention unmanned plane safety device include: aircraft
Control device 10 (such as, generally comprising battery in aircraft controller device 10) be connected with aircraft controller device 10 one
Individual or multiple motor and paddle device 20, be arranged on fuselage interior one or more air bags 30 (such as, as it is shown in figure 1,
The one or more air bags 30 being arranged corresponding to each motor and paddle device 20) and sensor (it is not shown,
Sensor may be mounted at any appropriate location).
Wherein, sensor is for sensing the speed of unmanned plane, and is sensing the falling speed of unmanned plane more than predetermined
Described in making during falling speed threshold value or when the whereabouts acceleration sensing unmanned plane is more than predetermined whereabouts acceleration rate threshold
One or more air bags 30 eject.
Such as, sensor when the falling speed sensing unmanned plane is more than predetermined falling speed threshold value or is sensing
Cue, aircraft is sent to aircraft controller device 10 when the whereabouts acceleration of unmanned plane is more than predetermined whereabouts acceleration rate threshold
Control device 10 sends pop instruction when receiving cue to the one or more air bag 30, so that institute
State one or more air bag 30 to eject.
Preferably, unmanned plane safety device also includes according to the preferred embodiment of the invention: one or more blades
Protection network 40, one of them blade protection network corresponds to a motor and paddle device 20 and at least partly surrounds described one
Individual motor and paddle device 20 are arranged.
Preferably, the one or more air bag 30 is arranged in the one or more blade protection network 40 times
Side.
In the present invention, use at unmanned many gyroplanes fuselage interior (such as, horn, center flying disc) installation air bag
Device, and sensor is installed, sensor detects that aircraft hurtles down and aviator's misoperation causes aircraft meeting out of control at once
Entering into safeguard protection pattern, fuselage can eject air bag at once, the unmanned many gyroplanes air crash of protection or with anyone/thing
Bad and unnecessary potential safety hazard calculated by the device brought that collides.
Fig. 2 is the flow chart of unmanned plane safety protecting method according to the preferred embodiment of the invention.The process employs Fig. 1
Shown unmanned plane safety device according to the preferred embodiment of the invention.
Specifically, as in figure 2 it is shown, according to the preferred embodiment of the invention unmanned plane safety protecting method include:
First step S1: by the speed of sensor sensing unmanned plane；
Second step S2: when sensor senses the falling speed of unmanned plane more than predetermined falling speed threshold value or
When sensing the whereabouts acceleration of unmanned plane more than predetermined whereabouts acceleration rate threshold so that the one or more air bag 30
Eject.
It is tight that the present invention can well reduce unmanned many gyroplanes air crash out of control or misoperation bumps against that people/thing brings
Heavily loss, device failure and unnecessary potential safety hazard.The benefit of present invention maximum is exactly that unmanned gyroplane is the most out of control,
Ejecting air bag, at utmost each position on protection unmanned gyroplane, is possible to prevent unnecessary heavy losses, it is also possible to
Greatly increasing the safety of aircraft, there is the emergency that air crash out of control or misoperation cause in the most gyroplanes,
Aircraft will eject air bag at once, is greatly reduced speed that aircraft declines and pressure to any object when landing,
Farthest reduce aircraft self damage and the injury to all other men/thing.
Described above illustrate and describes the preferred embodiments of the present invention, as previously mentioned, it should be understood that the present invention not office
Be limited to form disclosed herein, be not to be taken as the eliminating to other embodiments, and can be used for other combinations various, amendment and
Environment, and can be changed by above-mentioned teaching or the technology of association area or knowledge in invention contemplated scope described herein
Dynamic.And the change that those skilled in the art are carried out and change are without departing from the spirit and scope of the present invention, the most all should be appended by the present invention
In scope of the claims.
Claims (6)
1. a unmanned plane safety device, it is characterised in that including: aircraft controller device and aircraft controller device are even
The one or more motors connect and paddle device, the one or more air bags being arranged on fuselage interior and sensor；Its
In, sensor is for sensing the speed of unmanned plane, and is sensing the falling speed of unmanned plane more than predetermined falling speed threshold
The one or more is made during value or when the whereabouts acceleration sensing unmanned plane is more than predetermined whereabouts acceleration rate threshold
Air bag ejects.
2. unmanned plane safety device as claimed in claim 1, it is characterised in that sensor is under sensing unmanned plane
It is more than predetermined whereabouts acceleration when terminal-velocity degree is more than predetermined falling speed threshold value or at the whereabouts acceleration sensing unmanned plane
Send cue to aircraft controller device during threshold value, aircraft controller device when receiving cue to one
Or multiple air bag sends pop instruction, so that the one or more air bag ejects.
3. unmanned plane safety device as claimed in claim 1 or 2, it is characterised in that wherein corresponding to each motor and
Paddle device is arranged the one or more air bag.
4. unmanned plane safety device as claimed in claim 1 or 2, it is characterised in that also include: one or more blades
Protection network, one of them blade protection network corresponds to a motor and paddle device and at least partly surrounds one electricity
Machine and paddle device are arranged.
5. unmanned plane safety device as claimed in claim 1 or 2, it is characterised in that the one or more air bag
It is arranged in below the one or more blade protection network.
6. a unmanned plane safety protecting method, described unmanned plane safety protecting method uses as described in one of claim 1 to 5
Unmanned plane safety device, it is characterised in that including:
First step: by the speed of sensor sensing unmanned plane；
Second step: when sensor senses the falling speed of unmanned plane more than predetermined falling speed threshold value or sensing
When the whereabouts acceleration of unmanned plane is more than predetermined whereabouts acceleration rate threshold so that the one or more air bag ejects.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610692921.8A CN106240811A (en) | 2016-08-18 | 2016-08-18 | Unmanned plane safety device and unmanned plane safety protecting method |
| PCT/CN2017/093216 WO2018032924A1 (en) | 2016-08-18 | 2017-07-17 | Safety guard device for unmanned aerial vehicle and safety guard method for unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610692921.8A CN106240811A (en) | 2016-08-18 | 2016-08-18 | Unmanned plane safety device and unmanned plane safety protecting method |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106240811A true CN106240811A (en) | 2016-12-21 |
Family
ID=57593249
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610692921.8A Pending CN106240811A (en) | 2016-08-18 | 2016-08-18 | Unmanned plane safety device and unmanned plane safety protecting method |
Country Status (2)
| Country | Link |
|---|---|
| CN (1) | CN106240811A (en) |
| WO (1) | WO2018032924A1 (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018032924A1 (en) * | 2016-08-18 | 2018-02-22 | 上海未来伙伴机器人有限公司 | Safety guard device for unmanned aerial vehicle and safety guard method for unmanned aerial vehicle |
| WO2018209708A1 (en) * | 2017-05-19 | 2018-11-22 | 深圳市大疆创新科技有限公司 | Blade protection cover of unmanned aerial vehicle, and unmanned aerial vehicle system |
| WO2019061387A1 (en) * | 2017-09-30 | 2019-04-04 | 林燕凤 | Unmanned aerial vehicle safe landing apparatus |
| CN110948525A (en) * | 2019-12-25 | 2020-04-03 | 西南石油大学 | Wall climbing robot safety protection combined protection device |
| CN113859525A (en) * | 2021-11-16 | 2021-12-31 | 山东省国土测绘院 | High remote sensing survey and drawing unmanned aerial vehicle of security |
| CN114136294A (en) * | 2021-11-26 | 2022-03-04 | 山东省物化探勘查院 | Intelligent three-dimensional topographic surveying and mapping device |
| CN114261514A (en) * | 2021-12-27 | 2022-04-01 | 广东电网有限责任公司广州供电局 | Unmanned aerial vehicle safety hook device |
| TWI817961B (en) * | 2018-01-03 | 2023-10-11 | 美商高通公司 | Aerial robotic vehicle with adjustable object avoidance proximity threshold and method and processing device for the same |
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| US10720070B2 (en) | 2018-01-03 | 2020-07-21 | Qualcomm Incorporated | Adjustable object avoidance proximity threshold of a robotic vehicle based on presence of detected payload(s) |
| US10636314B2 (en) | 2018-01-03 | 2020-04-28 | Qualcomm Incorporated | Adjusting flight parameters of an aerial robotic vehicle based on presence of propeller guard(s) |
| US10719705B2 (en) | 2018-01-03 | 2020-07-21 | Qualcomm Incorporated | Adjustable object avoidance proximity threshold based on predictability of the environment |
| US10717435B2 (en) | 2018-01-03 | 2020-07-21 | Qualcomm Incorporated | Adjustable object avoidance proximity threshold based on classification of detected objects |
| CN113905946A (en) * | 2020-06-29 | 2022-01-07 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle and be applicable to unmanned aerial vehicle's protector |
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| KR101373038B1 (en) * | 2012-12-27 | 2014-03-11 | 김영진 | For water rescue levitation flying robot equipped with airbags and airbag dropping device |
| CN104163241B (en) * | 2014-08-12 | 2016-03-02 | 中国航空工业经济技术研究院 | A kind of logistics depopulated helicopter |
| JP6425969B2 (en) * | 2014-10-29 | 2018-11-21 | ヤンマー株式会社 | helicopter |
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| CN104890891B (en) * | 2015-06-10 | 2017-12-22 | 山东领信信息科技股份有限公司 | A kind of amphibious unmanned plane of recordable accident |
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| CN205098464U (en) * | 2015-10-31 | 2016-03-23 | 汕头市杰泰电子科技有限公司 | Rotor unmanned aerial vehicle of flexible function that lands of utensil |
| CN106240811A (en) * | 2016-08-18 | 2016-12-21 | 上海未来伙伴机器人有限公司 | Unmanned plane safety device and unmanned plane safety protecting method |
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- 2016-08-18 CN CN201610692921.8A patent/CN106240811A/en active Pending
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- 2017-07-17 WO PCT/CN2017/093216 patent/WO2018032924A1/en active Application Filing
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| WO2018032924A1 (en) * | 2016-08-18 | 2018-02-22 | 上海未来伙伴机器人有限公司 | Safety guard device for unmanned aerial vehicle and safety guard method for unmanned aerial vehicle |
| WO2018209708A1 (en) * | 2017-05-19 | 2018-11-22 | 深圳市大疆创新科技有限公司 | Blade protection cover of unmanned aerial vehicle, and unmanned aerial vehicle system |
| CN109890700A (en) * | 2017-05-19 | 2019-06-14 | 深圳市大疆创新科技有限公司 | The blade protective cover and UAV system of unmanned vehicle |
| CN109890700B (en) * | 2017-05-19 | 2021-06-22 | 深圳市大疆创新科技有限公司 | Unmanned vehicles's paddle safety cover and unmanned aerial vehicle system |
| CN113232845A (en) * | 2017-05-19 | 2021-08-10 | 深圳市大疆创新科技有限公司 | Unmanned vehicles's paddle safety cover and unmanned aerial vehicle system |
| WO2019061387A1 (en) * | 2017-09-30 | 2019-04-04 | 林燕凤 | Unmanned aerial vehicle safe landing apparatus |
| TWI817961B (en) * | 2018-01-03 | 2023-10-11 | 美商高通公司 | Aerial robotic vehicle with adjustable object avoidance proximity threshold and method and processing device for the same |
| CN110948525A (en) * | 2019-12-25 | 2020-04-03 | 西南石油大学 | Wall climbing robot safety protection combined protection device |
| CN110948525B (en) * | 2019-12-25 | 2021-11-30 | 西南石油大学 | Wall climbing robot safety protection combined protection device |
| CN113859525A (en) * | 2021-11-16 | 2021-12-31 | 山东省国土测绘院 | High remote sensing survey and drawing unmanned aerial vehicle of security |
| CN114136294A (en) * | 2021-11-26 | 2022-03-04 | 山东省物化探勘查院 | Intelligent three-dimensional topographic surveying and mapping device |
| CN114261514A (en) * | 2021-12-27 | 2022-04-01 | 广东电网有限责任公司广州供电局 | Unmanned aerial vehicle safety hook device |
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| Publication number | Publication date |
|---|---|
| WO2018032924A1 (en) | 2018-02-22 |
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Legal Events
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| C06 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20161221 |