CN106218901A - A kind of airbag structure of unmanned plane water surface forced landing device - Google Patents
A kind of airbag structure of unmanned plane water surface forced landing device Download PDFInfo
- Publication number
- CN106218901A CN106218901A CN201610871864.XA CN201610871864A CN106218901A CN 106218901 A CN106218901 A CN 106218901A CN 201610871864 A CN201610871864 A CN 201610871864A CN 106218901 A CN106218901 A CN 106218901A
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- CN
- China
- Prior art keywords
- forced landing
- water surface
- air bag
- unmanned aerial
- aerial vehicles
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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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- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 title claims abstract description 28
- 238000000034 method Methods 0.000 claims abstract description 6
- 239000000779 smoke Substances 0.000 claims description 3
- 239000002775 capsule Substances 0.000 claims 2
- 230000005540 biological transmission Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 238000010276 construction Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000001771 impaired effect Effects 0.000 description 1
- 238000002372 labelling Methods 0.000 description 1
Classifications
-
- 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
- B64D25/00—Emergency apparatus or devices, not otherwise provided for
- B64D25/08—Ejecting or escaping means
- B64D25/18—Flotation gear
-
- 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
- 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
- B64D47/02—Arrangements or adaptations of signal or lighting devices
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Business, Economics & Management (AREA)
- Emergency Management (AREA)
- Emergency Lowering Means (AREA)
Abstract
The invention discloses the airbag structure of a kind of unmanned plane water surface forced landing device, be the lower surface of main body at many rotor wing unmanned aerial vehicles, be provided with on aerating gasbag, and the lower surface of the main body being arranged on many rotor wing unmanned aerial vehicles by air bag ejecting mechanism；Air bag ejecting mechanism is connected with the main body of many rotor wing unmanned aerial vehicles by the seat that supports that can horizontally rotate；Air bag ejecting mechanism is provided with air bag accommodating container；During many rotor wing unmanned aerial vehicles normal flight, the gas emptying in aerating gasbag, it is accommodated in air bag accommodating container.Using technique scheme, when needs work in the water surface overhead when, can carry out repeatedly, long unsettled observation, collection image data, saves energy, the working time is unrestricted；Break down on the water surface at unmanned aerial vehicle, when needing forced landing, unmanned vehicle can force-land safely on the water surface, the safety of protection unmanned plane, and can normally work.
Description
Technical field
The invention belongs to the technical field of unmanned vehicle, relate to various field construction, exploration, transportation, travel, rescue
Help, many rotary wind types unmanned vehicle of the occasion such as particularly work on rivers and lakes.More particularly it relates to an it is unmanned
The airbag structure of machine water surface forced landing device.
Background technology
At present, many rotor unmanned aircrafts are constructed the most in the wild, are explored, transportation, travel, rescue, particularly rivers
Working on lake etc. and to be used widely in field, its Main Function is the observation of field condition, the collection of information, a small amount of goods and materials
Transmission etc..It has the advantage of uniqueness, can be with vertical lift；Do not limited by landform, road, can arrive rapidly and need work
The scene of the position make, rescued, the most unfrequented place, carry out in-plant observation；By photography, picture pick-up device,
To the transmission video of relevant department, image document, be provided with pass department technology personnel and be analyzed scene judging, or rapidly to
The on-the-spot goods and materials that transport, acquirement very good effect.
But current unmanned vehicle there is problems:
One is, when needs work in the water surface overhead when, due to needs repeatedly, long unsettled observation, gather shadow
As data, energy expenditure is very big, and the working time is restricted；Two are, unmanned vehicle breaks down on the water surface, needs forced landing
Time, unmanned vehicle meeting submerged, cause unmanned aerial vehicle impaired and scrap.
Summary of the invention
The present invention provides a kind of unmanned plane water surface forced landing device, its objective is that the safety realized on the water surface is force-landed and carries out
Normal work.
To achieve these goals, the technical scheme that the present invention takes is:
The unmanned plane water surface forced landing device of the present invention, is arranged in the main body of many rotor wing unmanned aerial vehicles；Described water surface forced landing
The structure of device is the lower surface of the main body at described many rotor wing unmanned aerial vehicles, is provided with aerating gasbag, and ejects machine by air bag
On the lower surface of the main body that structure is arranged on described many rotor wing unmanned aerial vehicles.
Described air bag ejecting mechanism is connected by the main body supporting seat and described many rotor wing unmanned aerial vehicles that can horizontally rotate
Connect.
Described air bag ejecting mechanism is provided with air bag accommodating container；Process at described many rotor wing unmanned aerial vehicles normal flight
In, the gas emptying in described aerating gasbag, it is accommodated in described air bag accommodating container.
Described many rotor wing unmanned aerial vehicles are provided with forced landing signal alarm, and described forced landing signal alarm is colored smoke report
Alert device.
Described many rotor wing unmanned aerial vehicles are provided with forced landing signal alarm, and described forced landing signal alarm is light flash report
Alert device.
Described many rotor wing unmanned aerial vehicles are provided with forced landing signal alarm, and described forced landing signal alarm is audible alarm
Device.
The inside division of described aerating gasbag is multiple mutual disconnected ballonets.
The present invention uses technique scheme, when needs work in the water surface overhead when, can carry out repeatedly, for a long time
Unsettled observation, gather image data, saves energy, the working time is unrestricted；Break down on the water surface at unmanned aerial vehicle,
When needing forced landing, unmanned vehicle can force-land safely on the water surface, the safety of protection unmanned plane, and can normally work.
Accompanying drawing explanation
Labelling in attached diagramatic content and figure is briefly described as follows:
Fig. 1 is the structural representation of the present invention.
Figure is labeled as:
1, many rotor wing unmanned aerial vehicles, 2, aerating gasbag, 3, air bag ejecting mechanism, 4, support seat, 5, air bag accommodating container, 6, compel
Fall signal alarm, 7, ballonet.
Detailed description of the invention
Below against accompanying drawing, by the description to embodiment, the detailed description of the invention of the present invention is made further details of
Illustrate, to help those skilled in the art that inventive concept, the technical scheme of the present invention are had more complete, accurate and deep reason
Solve.
The structure of the present invention as expressed by Fig. 1, for a kind of unmanned plane water surface forced landing device, is arranged on many rotor wing unmanned aerial vehicles
In the main body of 1.
In order to solve the problem of prior art existence and overcome its defect, it is achieved the safety on the water surface is force-landed and just carries out
The often goal of the invention of work, the technical scheme that the present invention takes is:
As it is shown in figure 1, the unmanned plane water surface forced landing device of the present invention is under the main body of described many rotor wing unmanned aerial vehicles 1
Surface, is provided with aerating gasbag 2, and is arranged on the lower surface of the main body of described many rotor wing unmanned aerial vehicles 1 by air bag ejecting mechanism 3
On.
Use technique scheme, when needs work in the water surface overhead when, can carry out repeatedly, the most unsettled
Observing, gather image data, saves energy, the working time is unrestricted；Break down on the water surface at unmanned aerial vehicle, need to compel
During fall, unmanned vehicle can force-land safely on the water surface, the safety of protection unmanned plane, and can normally work.
Described air bag ejecting mechanism 3 is by the main body supporting seat 4 and described many rotor wing unmanned aerial vehicles 1 that can horizontally rotate
Connect.
After forced landing, many rotor wing unmanned aerial vehicles can carry out multi-faceted, the work in every of multi-angle.
Described air bag ejecting mechanism 3 is provided with air bag accommodating container 5；At described many rotor wing unmanned aerial vehicles 1 normal flight
During, the gas emptying in described aerating gasbag 2, it is accommodated in described air bag accommodating container 5.
Described many rotor wing unmanned aerial vehicles 1 are provided with forced landing signal alarm 6, and described forced landing signal alarm is colored smoke
Alarm.
Described many rotor wing unmanned aerial vehicles 1 are provided with forced landing signal alarm 6, and described forced landing signal alarm is light flash
Alarm.
Described many rotor wing unmanned aerial vehicles 1 are provided with forced landing signal alarm 6, and described forced landing signal alarm is audible alarm
Device.
Use above-mentioned multiple alarm device, after forced landing, send alarm signal, facilitate the search of rescue personnel.
The inside division of described aerating gasbag 2 is multiple mutual disconnected ballonets 7.
When wherein one or more ballonets 7, other ballonet 7 can ensure aerating gasbag 2 to continue normally to work.
Above in conjunction with accompanying drawing, the present invention is exemplarily described, it is clear that the present invention implements not by aforesaid way
Restriction, as long as have employed the method design of the present invention and the improvement of various unsubstantialities that technical scheme is carried out, or without changing
Enter and design and the technical scheme of the present invention are directly applied to other occasion, all within protection scope of the present invention.
Claims (5)
1. an airbag structure for unmanned plane water surface forced landing device, is arranged in the main body of many rotor wing unmanned aerial vehicles (1), and its feature exists
In: the structure of described water surface forced landing device is the lower surface of the main body at described many rotor wing unmanned aerial vehicles (1), is provided with inflating air
Capsule (2), and pass through on the lower surface of the main body that air bag ejecting mechanism (3) is arranged on described many rotor wing unmanned aerial vehicles (1)；Described
Air bag ejecting mechanism (3) is connected with the main body of described many rotor wing unmanned aerial vehicles (1) by the support seat (4) that can horizontally rotate；Institute
The air bag ejecting mechanism (3) stated is provided with air bag accommodating container (5)；Process at described many rotor wing unmanned aerial vehicles (1) normal flight
In, the gas emptying in described aerating gasbag (2), it is accommodated in described air bag accommodating container (5).
2. according to the airbag structure of the unmanned plane water surface forced landing device described in claim 1, it is characterised in that: described many rotors
Unmanned plane (1) is provided with forced landing signal alarm (6), and described forced landing signal alarm is colored smoke alarm.
3. according to the airbag structure of the unmanned plane water surface forced landing device described in claim 1, it is characterised in that: described many rotors
Unmanned plane (1) is provided with forced landing signal alarm (6), and described forced landing signal alarm is light flash alarm.
4. according to the airbag structure of the unmanned plane water surface forced landing device described in claim 1, it is characterised in that: described many rotors
Unmanned plane (1) is provided with forced landing signal alarm (6), and described forced landing signal alarm is acoustic alarm.
5. according to the airbag structure of the unmanned plane water surface forced landing device described in claim 1, it is characterised in that: described inflating air
The inside division of capsule (2) is multiple mutual disconnected ballonets (7).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610871864.XA CN106218901A (en) | 2016-09-30 | 2016-09-30 | A kind of airbag structure of unmanned plane water surface forced landing device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610871864.XA CN106218901A (en) | 2016-09-30 | 2016-09-30 | A kind of airbag structure of unmanned plane water surface forced landing device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106218901A true CN106218901A (en) | 2016-12-14 |
Family
ID=58076828
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610871864.XA Pending CN106218901A (en) | 2016-09-30 | 2016-09-30 | A kind of airbag structure of unmanned plane water surface forced landing device |
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| CN (1) | CN106218901A (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107907889A (en) * | 2017-12-25 | 2018-04-13 | 成都壹橙科技有限公司 | A kind of deliverance apparatus based on unmanned plane |
| CN108058837A (en) * | 2017-12-21 | 2018-05-22 | 江西绿卫士智能科技有限公司 | A kind of detecting fish school unmanned plane |
| CN108116687A (en) * | 2017-12-20 | 2018-06-05 | 郑州康晓科技有限公司 | Unmanned plane accidental falling deceleration damping device |
| CN109436305A (en) * | 2018-11-20 | 2019-03-08 | 南京信息工程大学 | Can water surface landing unmanned plane |
| CN111147718A (en) * | 2019-12-24 | 2020-05-12 | 深圳市安思科电子科技有限公司 | Monitoring device convenient to accomodate based on block chain technique |
| CN111717405A (en) * | 2020-06-23 | 2020-09-29 | 长沙航华电子科技有限公司 | Buoyancy auxiliary lifting device for unmanned aerial vehicle |
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| EP2733066A1 (en) * | 2012-11-14 | 2014-05-21 | Airbus Helicopters | Method for automatically triggering an emergency buoyancy system for a hybrid helicopter |
| US20140252166A1 (en) * | 2013-03-06 | 2014-09-11 | Bell Helicopter Textron Inc. | Crash Load Attenuator for Water Ditching and Floatation |
| CN104627370A (en) * | 2013-11-13 | 2015-05-20 | 银川上河图新技术研发有限公司 | Safe landing device used when helicopter breaks down and shuts down in sky above land and sea |
| 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 |
| CN205203376U (en) * | 2015-08-24 | 2016-05-04 | 深圳市诺亚星辰科技开发有限公司 | Rotorcraft unmanned aerial vehicle that can flexiblely descend |
-
2016
- 2016-09-30 CN CN201610871864.XA patent/CN106218901A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2733066A1 (en) * | 2012-11-14 | 2014-05-21 | Airbus Helicopters | Method for automatically triggering an emergency buoyancy system for a hybrid helicopter |
| US20140252166A1 (en) * | 2013-03-06 | 2014-09-11 | Bell Helicopter Textron Inc. | Crash Load Attenuator for Water Ditching and Floatation |
| CN104627370A (en) * | 2013-11-13 | 2015-05-20 | 银川上河图新技术研发有限公司 | Safe landing device used when helicopter breaks down and shuts down in sky above land and sea |
| CN205203376U (en) * | 2015-08-24 | 2016-05-04 | 深圳市诺亚星辰科技开发有限公司 | Rotorcraft unmanned aerial vehicle that can flexiblely descend |
| 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 |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108116687A (en) * | 2017-12-20 | 2018-06-05 | 郑州康晓科技有限公司 | Unmanned plane accidental falling deceleration damping device |
| CN108116687B (en) * | 2017-12-20 | 2021-07-27 | 郑州康晓科技有限公司 | Unexpected speed reduction damping device that falls of unmanned aerial vehicle |
| CN108058837A (en) * | 2017-12-21 | 2018-05-22 | 江西绿卫士智能科技有限公司 | A kind of detecting fish school unmanned plane |
| CN107907889A (en) * | 2017-12-25 | 2018-04-13 | 成都壹橙科技有限公司 | A kind of deliverance apparatus based on unmanned plane |
| CN109436305A (en) * | 2018-11-20 | 2019-03-08 | 南京信息工程大学 | Can water surface landing unmanned plane |
| CN111147718A (en) * | 2019-12-24 | 2020-05-12 | 深圳市安思科电子科技有限公司 | Monitoring device convenient to accomodate based on block chain technique |
| CN111717405A (en) * | 2020-06-23 | 2020-09-29 | 长沙航华电子科技有限公司 | Buoyancy auxiliary lifting device for unmanned aerial vehicle |
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| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20161214 |
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| RJ01 | Rejection of invention patent application after publication |