CN107117295A - A kind of anti-new unmanned plane that crashes - Google Patents
A kind of anti-new unmanned plane that crashes Download PDFInfo
- Publication number
- CN107117295A CN107117295A CN201710214932.XA CN201710214932A CN107117295A CN 107117295 A CN107117295 A CN 107117295A CN 201710214932 A CN201710214932 A CN 201710214932A CN 107117295 A CN107117295 A CN 107117295A
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- air bag
- crashes
- controller
- storage warehouse
- 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.)
- Pending
Links
- 230000004224 protection Effects 0.000 claims abstract description 17
- 210000002414 leg Anatomy 0.000 claims description 13
- 210000003127 knee Anatomy 0.000 claims description 6
- 230000008602 contraction Effects 0.000 claims 1
- 238000005516 engineering process Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 210000001940 cystoblast Anatomy 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 230000003287 optical effect Effects 0.000 description 1
- 230000001953 sensory effect Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
- B64C25/62—Spring shock-absorbers; Springs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
- B64D45/04—Landing aids; Safety measures to prevent collision with earth's surface
-
- 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
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
- B64D45/04—Landing aids; Safety measures to prevent collision with earth's surface
- B64D45/06—Landing aids; Safety measures to prevent collision with earth's surface mechanical
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Warehouses Or Storage Devices (AREA)
Abstract
The invention discloses the anti-new unmanned plane that crashes of one kind, including unmanned plane body, it is connected on the outer wall of the unmanned plane body by connection support bar with pivoting controller, it is connected on the pivoting controller by rotary shaft and fan blade, air bag storage warehouse is welded with the top of the unmanned plane body, it is provided with expansion controller, the expansion controller and is connected by expansion link with air bag layer on the power supply electrical storage device.In the present invention; air bag storage warehouse is provided with unmanned plane body, when unmanned plane falls, expansion controller timely releases air bag layer by expansion link; so that unmanned plane is in drop event; supporting leg can be down, it is to avoid other positions of unmanned plane towards ground, and due to air bag layer protection; on the one hand the speed of falling of unmanned plane can be caused to slow down; on the other hand it can timely be protected for unmanned plane when unmanned plane contacts ground, prevent that unmanned plane from falling damage.
Description
Technical field
The present invention relates to unmanned air vehicle technique field, more particularly to a kind of anti-new unmanned plane that crashes.
Background technology
Unmanned plane is the not manned vehicle manipulated by radio robot or airborne computer stored program controlled.
Unmanned plane is simple in construction, use cost is low, can not only complete the task of manned aircraft execution, be more suitable for someone's aircraft not
Preferably performing for task.Burst thing is emergent, early warning play the role of it is very big.
Unmanned plane photography is using UAV as aerial platform, with airborne sensory equipment, such as high-resolution
CCD digital cameras, light optical camera, infrared scanner, laser scanner, magnetic determining device etc. obtain information, with computer to figure
As information is handled, and image is fabricated to according to certain required precision.Total system has in terms of design and optimal combination
Prominent the characteristics of, be integrated with high-altitude shooting, remote control, telemetry, video image microwave transmission and computer image information
The new application technology of reason
But existing unmanned plane has some shortcomings part in use, in face of emergency situations, unmanned plane is falling
During there is no enough safeguard measures so that unmanned plane is easily damaged.
The content of the invention
The invention aims to solve shortcoming present in prior art, and a kind of anti-crash for proposing it is new nobody
Machine.
To achieve these goals, present invention employs following technical scheme：A kind of anti-new unmanned plane that crashes, including nothing
It is connected on man-machine body, the outer wall of the unmanned plane body by connection support bar with pivoting controller, the pivoting controller
It is upper to be connected by rotary shaft with fan blade, air bag storage warehouse is welded with the top of the unmanned plane body, and air bag is stored up
Being internally provided with power supply electrical storage device, the power supply electrical storage device for storage is provided with expansion controller, the expansion controller
It is connected by expansion link with air bag layer, and connecting rope is connected between air bag layer and air bag storage warehouse, the unmanned plane body
Bottom middle position is provided with camera, and the outside of camera is filled with buffer protection layer, the bottom of the unmanned plane body
Corner of four, portion is connected by spring knee with supporting leg.
It is used as further describing for above-mentioned technical proposal：
Rotated and be connected with protection cap by hinge on the air bag storage warehouse.
It is used as further describing for above-mentioned technical proposal：
The bottom of the supporting leg is provided with buffer spring.
It is used as further describing for above-mentioned technical proposal：
The middle position of the protection cap offers opening mouth.
It is used as further describing for above-mentioned technical proposal：
The pivoting controller is provided with four altogether, and four pivoting controllers are in same level.
In the present invention, it is connected first in the bottom of unmanned plane by spring knee with supporting leg, and at the bottom of supporting leg
Portion is provided with adjustable spring, when being fallen for unmanned plane, can timely carry out a certain degree of stretch at support contact ground
Contracting, is protected hence for unmanned plane body, and air bag storage warehouse is secondly provided with unmanned plane body, is fallen in unmanned plane
When, expansion controller timely releases air bag layer by expansion link, so that unmanned plane is in drop event, supporting leg can court
Under, it is to avoid on the one hand other positions of unmanned plane can cause the pendant of unmanned plane towards ground, and due to the protection of air bag layer
Terminal-velocity degree slows down, and on the other hand can timely be protected for unmanned plane when unmanned plane contacts ground, prevent unmanned plane
Fall damage.
Brief description of the drawings
Fig. 1 is a kind of structural representation of the anti-new unmanned plane that crashes proposed by the present invention；
Fig. 2 is the structural representation of supporting leg of the present invention；
Fig. 3 is the internal structure schematic diagram of air bag storage warehouse of the present invention.
Marginal data：
1- fan blade, 2- pivoting controllers, 3- connection support bars, 4- unmanned planes body, 5- air bags storage warehouse, 6- power supply storing up electricities
Device, 7- buffer protections layer, 8- cameras, 9- supporting legs, 91- buffer springs, 10- springs knee, 11- hinges, 12- protection caps,
13- air bags layer, 14- connecting ropes, 15- expansion controllers, 16- expansion links.
Embodiment
Below in conjunction with the accompanying drawing in the embodiment of the present invention, the technical scheme in the embodiment of the present invention is carried out clear, complete
Site preparation is described, it is clear that described embodiment is only a part of embodiment of the invention, rather than whole embodiments.
Lead on reference picture 1-3, a kind of anti-new unmanned plane that crashes, including unmanned plane body 4, the outer wall of unmanned plane body 4
Cross connection support bar 3 to be connected with pivoting controller 2, be connected on pivoting controller 2 by rotary shaft with fan blade 1, nothing
The top of man-machine body 4 is welded with air bag storage warehouse 5, and air bag storage warehouse 5 is internally provided with power supply electrical storage device 6, power supply storage
It is provided with expansion controller 15, expansion controller 15 and is connected by expansion link 16 with air bag layer 13 on electrical equipment 6, and air bag layer 13
Connecting rope 14 is connected between air bag storage warehouse 5, the bottom middle position of unmanned plane body 4 is provided with camera 8, and takes the photograph
The outside of picture first 8 passes through spring knee 10 and branch filled with buffer protection layer 7, the corner of bottom four of unmanned plane body 4
Support leg 9 is connected.
Rotated and be connected with protection cap 12 by hinge 11 on air bag storage warehouse 5, the bottom of supporting leg 9 is provided with buffer spring
91, the middle position of protection cap 12 offers opening mouth, and pivoting controller 2 is provided with four, and four pivoting controllers 2 altogether
It is in same level.
Pivoting controller 2 is used to drive fan blade 1 to be rotated by rotary shaft, and air bag storage warehouse 5 is used to deposit gas
Cystoblast 13, buffer protection layer 7 is used to protect camera 8, prevents it from damaging, and camera 8 is used to shoot photo, and buffer spring 9 is used
In playing buffer protection, protection cap 12 is used to protect the air bag layer 13 in air bag storage warehouse 5.
Operation principle：In use, power supply electrical storage device 6 is powered for all parts in unmanned plane body 4 so that nothing
Man-machine body 4 is normally carried out flight, when emergency situations occur for unmanned plane body 4, and the control expansion link 16 of expansion controller 15 enters
Row stretches out, so that the support air bag of expansion link 16 layer 13 is broken out from air bag storage warehouse 5, and air bag layer 13 timely deploys, and one
Aspect causes the supporting leg 9 in unmanned plane body 4 to reduce the speed that unmanned plane body 4 falls downwards, on the other hand, works as unmanned plane
When body 4 touches ground, the adjustable spring 91 in supporting leg 9 plays cushioning effect, and certain angle occurs in spring knee 10
The expansion of degree so that unmanned plane body 4 is timely protected.
The foregoing is only a preferred embodiment of the present invention, but protection scope of the present invention be not limited thereto,
Any one skilled in the art the invention discloses technical scope in, technique according to the invention scheme and its
Inventive concept is subject to equivalent substitution or change, should all be included within the scope of the present invention.
Claims (5)
1. a kind of anti-new unmanned plane that crashes, including unmanned plane body（4）, it is characterised in that the unmanned plane body（4）It is outer
Pass through connection support bar on wall（3）With pivoting controller（2）Connection, the pivoting controller（2）It is upper to pass through rotary shaft and fan
Blade（1）Drive connection, the unmanned plane body（4）Top be welded with air bag storage warehouse（5）, and air bag storage warehouse（5）'s
It is internally provided with power supply electrical storage device（6）, the power supply electrical storage device（6）On be provided with expansion controller（15）, the extension and contraction control
Device（15）It is upper to pass through expansion link（16）With air bag layer（13）Connection, and air bag layer（13）With air bag storage warehouse（5）Between be connected with
Connecting rope（14）, the unmanned plane body（4）Bottom middle position be provided with camera（8）, and camera（8）Outside
Filled with buffer protection layer（7）, the unmanned plane body（4）The corner of bottom four pass through spring knee（10）With support
Leg（9）Connection.
2. the anti-new unmanned plane that crashes of one kind according to claim 1, it is characterised in that the air bag storage warehouse（5）On
Pass through hinge（11）With protection cap（12）Rotate connection.
3. the anti-new unmanned plane that crashes of one kind according to claim 1, it is characterised in that the supporting leg（9）Bottom
It is provided with buffer spring（91）.
4. the anti-new unmanned plane that crashes of one kind according to claim 2, it is characterised in that the protection cap（12）Centre
Opening mouth is offered at position.
5. the anti-new unmanned plane that crashes of one kind according to claim 1, it is characterised in that the pivoting controller（2）Altogether
It is provided with four, and four pivoting controllers（2）It is in same level.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710214932.XA CN107117295A (en) | 2017-04-02 | 2017-04-02 | A kind of anti-new unmanned plane that crashes |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710214932.XA CN107117295A (en) | 2017-04-02 | 2017-04-02 | A kind of anti-new unmanned plane that crashes |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107117295A true CN107117295A (en) | 2017-09-01 |
Family
ID=59725659
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710214932.XA Pending CN107117295A (en) | 2017-04-02 | 2017-04-02 | A kind of anti-new unmanned plane that crashes |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107117295A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108058835A (en) * | 2017-12-20 | 2018-05-22 | 郑州康晓科技有限公司 | Unmanned plane fortuitous event fall arrest damages device |
| CN108482690A (en) * | 2018-04-06 | 2018-09-04 | 丁奕森 | A kind of scalable comprehensive protective device of unmanned plane |
| CN109305351A (en) * | 2018-11-20 | 2019-02-05 | 南京森林警察学院 | A kind of autonomous extendible extension width rotor wing unmanned aerial vehicle |
| WO2022143764A1 (en) * | 2020-12-31 | 2022-07-07 | 江苏数字鹰科技股份有限公司 | Police unmanned aerial vehicle having crash protection function |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN205044945U (en) * | 2015-09-21 | 2016-02-24 | 温州乐享科技信息有限公司 | Unmanned aerial vehicle that can stably descend |
| CN106005434A (en) * | 2016-06-30 | 2016-10-12 | 张春生 | Shipborne unmanned aerial vehicle water traveling protection system based on Internet of Things |
| CN205819552U (en) * | 2016-07-04 | 2016-12-21 | 广东天米教育科技有限公司 | A kind of shockproof undercarriage of unmanned plane |
| CN205998118U (en) * | 2016-09-06 | 2017-03-08 | 中国电建集团成都勘测设计研究院有限公司 | Rotor wing unmanned aerial vehicle damping undercarriage |
-
2017
- 2017-04-02 CN CN201710214932.XA patent/CN107117295A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN205044945U (en) * | 2015-09-21 | 2016-02-24 | 温州乐享科技信息有限公司 | Unmanned aerial vehicle that can stably descend |
| CN106005434A (en) * | 2016-06-30 | 2016-10-12 | 张春生 | Shipborne unmanned aerial vehicle water traveling protection system based on Internet of Things |
| CN205819552U (en) * | 2016-07-04 | 2016-12-21 | 广东天米教育科技有限公司 | A kind of shockproof undercarriage of unmanned plane |
| CN205998118U (en) * | 2016-09-06 | 2017-03-08 | 中国电建集团成都勘测设计研究院有限公司 | Rotor wing unmanned aerial vehicle damping undercarriage |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108058835A (en) * | 2017-12-20 | 2018-05-22 | 郑州康晓科技有限公司 | Unmanned plane fortuitous event fall arrest damages device |
| CN108058835B (en) * | 2017-12-20 | 2021-07-27 | 郑州康晓科技有限公司 | Unmanned aerial vehicle accident condition falling prevention and damage device |
| CN108482690A (en) * | 2018-04-06 | 2018-09-04 | 丁奕森 | A kind of scalable comprehensive protective device of unmanned plane |
| CN109305351A (en) * | 2018-11-20 | 2019-02-05 | 南京森林警察学院 | A kind of autonomous extendible extension width rotor wing unmanned aerial vehicle |
| CN109305351B (en) * | 2018-11-20 | 2023-09-22 | 南京森林警察学院 | Independent retractable type hanging rotor unmanned aerial vehicle |
| WO2022143764A1 (en) * | 2020-12-31 | 2022-07-07 | 江苏数字鹰科技股份有限公司 | Police unmanned aerial vehicle having crash protection function |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| CB02 | Change of applicant information | ||
| CB02 | Change of applicant information |
Address after: No. 0109, unit 109, No. 62, Chengyi North Street, phase III, software park, Xiamen City, Fujian Province Applicant after: Xiamen Leading Tianxun Technology Co., Ltd. Address before: 361000 Fujian city of Xiamen Province torch torch high tech Zone Park torch torch Road Plaza South Building No. 56-58 203-75 (the residence only as legal instruments of commercial subject address for service) Applicant before: Xiamen Jiuxing Tianxiang Aviation Technology Co. Ltd. |
|
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20170901 |