CN108128469A - A kind of amphibious unmanned plane for preventing from crashing - Google Patents
A kind of amphibious unmanned plane for preventing from crashing Download PDFInfo
- Publication number
- CN108128469A CN108128469A CN201711422560.6A CN201711422560A CN108128469A CN 108128469 A CN108128469 A CN 108128469A CN 201711422560 A CN201711422560 A CN 201711422560A CN 108128469 A CN108128469 A CN 108128469A
- Authority
- CN
- China
- Prior art keywords
- shaft
- trigger
- processing unit
- parachute
- unmanned plane
- 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
- 238000012545 processing Methods 0.000 claims abstract description 26
- 230000005540 biological transmission Effects 0.000 claims abstract description 7
- 239000003814 drug Substances 0.000 claims abstract description 4
- 230000001133 acceleration Effects 0.000 claims description 18
- 230000006698 induction Effects 0.000 claims description 12
- 238000005192 partition Methods 0.000 claims description 5
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 abstract description 6
- 238000010586 diagram Methods 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- 238000005273 aeration Methods 0.000 description 2
- 238000004458 analytical method Methods 0.000 description 2
- 238000005422 blasting Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 239000002917 insecticide Substances 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 239000000575 pesticide Substances 0.000 description 2
- 238000013459 approach Methods 0.000 description 1
- 230000008602 contraction Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000004880 explosion Methods 0.000 description 1
- 238000011031 large-scale manufacturing process Methods 0.000 description 1
- 238000010338 mechanical breakdown Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60F—VEHICLES FOR USE BOTH ON RAIL AND ON ROAD; AMPHIBIOUS OR LIKE VEHICLES; CONVERTIBLE VEHICLES
- B60F5/00—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media
- B60F5/003—Off the road or amphibian vehicles adaptable for air or space transport
-
- 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
- B64D17/00—Parachutes
- B64D17/62—Deployment
- B64D17/72—Deployment by explosive or inflatable means
-
- 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
- B64D17/00—Parachutes
- B64D17/62—Deployment
- B64D17/72—Deployment by explosive or inflatable means
- B64D17/725—Deployment by explosive or inflatable means by explosive means
-
- 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
- B64D2201/00—Airbags mounted in aircraft for any use
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transportation (AREA)
- Mechanical Engineering (AREA)
- Toys (AREA)
Abstract
The present invention provides a kind of amphibious unmanned plane for preventing from crashing, including body, processing unit and engine are equipped in body, processing unit is electrically connected with engine, body is equipped with rotor, shaft is equipped in body, shaft is equipped with groove close to one end of rotor, rotor is equipped with connecting portion, connecting portion is inserted into shaft groove, connecting portion is interference fitted with shaft, the shaft other end is connect with engine transmission, upper pack and lower pack are equipped in the groove of shaft, upper pack is equipped with parachute with prescribe medicine parlor, parachute has bottom trigger, the second trigger is equipped with by upper pack, second trigger is electrically connected with processing unit；Organism bottom is equipped with undercarriage, and undercarriage includes air bag and frame body, and air bag covering shelf body surface face, body is interior air charging system, and the gas outlet of air charging system is connected with air bag, and protection unmanned plane prevents from crashing, even if air crash will not also sink under water.
Description
Technical field
The present invention relates to unmanned plane field, particularly a kind of amphibious unmanned plane for preventing from crashing.
Background technology
Agricultural development trend is necessarily intensive large-scale production pattern, is substituted in such a mode using mechanized tool
Manual work is one of necessary condition, and the approach that one of which is sprayed insecticide is to carry pesticide using unmanned plane to spray in the air.
In the operation process that existing unmanned plane is sprayed insecticide, due to some fortuitous events may be wounded by exotic or itself
Mechanical breakdown is generated, air crash accident may occur for unmanned plane under this state, and unmanned plane once crashes, and economic loss is very
Greatly, and oil plant, pesticide solution of unmanned plane carrying etc. may pollute the environment.
Invention content
Institute of the invention purpose to be achieved is to provide a kind of amphibious unmanned plane for preventing crash, can prevent in the event of an accident
Only unmanned plane air crash is damaged, while provides unmanned plane amphibious function.
In order to achieve the above object, the present invention adopts the following technical scheme that：A kind of amphibious unmanned plane for preventing from crashing, packet
Body is included, processing unit and engine are equipped in body, processing unit is electrically connected with engine, and body is equipped with rotor, is set in body
There is shaft, shaft is equipped with groove close to one end of rotor, and rotor is equipped with connecting portion, and connecting portion is inserted into shaft groove, connecting portion
It is interference fitted with shaft, the shaft other end is connect with engine transmission, and upper pack and lower pack, upper pack are equipped in the groove of shaft
The parachute being equipped with prescribe medicine parlor after collapsible, parachute are connect by line with groove inner wall, and parachute has bottom
The first sharp trigger, the first trigger are equipped with partition board with prescribe medicine parlor, the second trigger are equipped with by upper pack, and second ignites
Device is electrically connected with processing unit；Acceleration induction device is additionally provided in body, acceleration induction device is electrically connected with processing unit；Body
Bottom is equipped with undercarriage, and undercarriage includes air bag and frame body, and air bag covering shelf body surface face, body is interior air charging system, inflation
Device is connect with engine transmission, and air charging system is electrically connected with processing unit, and the gas outlet of air charging system is connected with air bag.
Acceleration induction device monitors the acceleration of unmanned plane in real time, when unmanned plane receives installation damage, will necessarily occur
The acceleration not being inconsistent with regular flight condition, processing unit by acceleration induction device obtain the information and with the data of normal flight
It is compared, once analysis show that unmanned plane is in air crash state, processing unit controls the second trigger to ignite upper pack, medicine-feeding
Rotor is released out of shaft groove after packet explosion, so as to abandon rotor, while by the compressed parachute of groove interior folding
It pushes downwards, the first trigger under parachute is made to puncture partition board, ignite lower pack, lower pack releases parachute after igniting recessed
Outside slot, so as to release a parachute, parachute is connect by line with groove inner wall, and landing is suspended on so as to the unmanned plane of air crash state
Under umbrella, it is ensured that safety, this is successively ignited in the process due to upper pack and lower pack, and lower pack releases the process of parachute not
It is influenced by upper pack.In addition, when engine or rotor break down, the processing unit being electrically connected with engine can obtain information,
So as to it also can trigger parachute in the state of not detecting disorderly acceleration in acceleration induction device.Upper pack, lower pack
Triggering pattern can avoid parachute from being blocked by rotor.Processing unit can also control engine to drive air charging system, while control inflation
Device is airbag aeration, after the air bag for covering undercarriage surface fills gas, even if unmanned plane falls within the water surface and may also be nobody
Machine is bubbled through the water column.
Further, first trigger is striker.The cost of striker is relatively low, and blasting effect is good.
After adopting the above technical scheme, the invention has the advantages that：
Parachute system is installed additional on unmanned plane, so as to which unmanned plane be protected to prevent from crashing, even if air crash will not also sink to water
Bottom.
Description of the drawings
The invention will be further described below in conjunction with the accompanying drawings：
Fig. 1 is the schematic diagram of an embodiment of the present invention；
Fig. 2 is the schematic diagram that the parachute of Fig. 1 embodiments is opened；
Fig. 3 is the schematic diagram of the parachute contraction state of Fig. 1 embodiments；
Fig. 4 is the schematic diagram of the airbag aeration of Fig. 1 embodiments.
Specific embodiment
Fig. 1-4 show a kind of embodiment of the present invention.
A kind of amphibious unmanned plane for preventing from crashing including body 1, is equipped with processing unit and engine in body 1, processing is single
Member is electrically connected with engine, and body 1 is equipped with rotor 2, and shaft 3 is equipped in body 1, and shaft 3 is equipped with groove close to one end of rotor 2
4, rotor 2 is equipped with connecting portion 5, and connecting portion 5 is inserted into 3 groove 4 of shaft, and connecting portion 5 is interference fitted with shaft 3,3 other end of shaft
It is connect with engine transmission, upper pack 6 and lower pack 7 is equipped in the groove 4 of shaft 3, be equipped with and fold between upper pack 6 and lower pack 7
Compressed parachute 8, parachute 8 are connect by line 9 with 4 inner wall of groove, and parachute 8 has the first sharp ignition of bottom
Device 10, the first trigger 10 are striker, and the cost of striker is relatively low, and blasting effect is good, is set between the first trigger 10 and lower pack 7
There is partition board 11, upper 6 side of pack is equipped with the second trigger 12, and the second trigger 12 is electrically connected with processing unit；It is additionally provided in body 1
Acceleration induction device, acceleration induction device are electrically connected with processing unit.1 bottom of body is equipped with undercarriage 15, and undercarriage 15 includes
Air bag 13 and frame body 14, air bag 13 cover 14 surface of frame body, also have air charging system in body 1, and air charging system connects with engine transmission
It connects, air charging system is electrically connected with processing unit, and the gas outlet of air charging system is connected with air bag 13.
Acceleration induction device monitors the acceleration of unmanned plane in real time, when unmanned plane receives installation damage, will necessarily occur
The acceleration not being inconsistent with regular flight condition, processing unit by acceleration induction device obtain the information and with the data of normal flight
It is compared, once analysis show that unmanned plane is in air crash state, processing unit controls the second trigger 12 to ignite upper pack 6,
Upper pack 6 releases rotor 2 after exploding out of shaft 3 groove 4, so as to abandon rotor 2, while 4 interior folding of groove is compressed
Parachute 8 afterwards is pushed downwards, and the first trigger 10 under parachute 8 is made to puncture partition board 11, ignites lower pack 7, and lower pack 7 draws
Parachute 8 is released outside groove 4 after quick-fried, so as to release a parachute 8, parachute 8 is connect by line 9 with 4 inner wall of groove, so as to fall
The unmanned plane of machine state is suspended under parachute 8, it is ensured that safety, since upper pack 6 and lower pack 7 are successively ignited during this,
Therefore the process that lower pack 7 releases parachute 8 is not influenced by upper pack 6.In addition, when engine or rotor 2 break down, with drawing
Information can be obtained by holding up the processing unit of electrical connection, in the state of the acceleration so as to not detect disorder in acceleration induction device
Also it can trigger parachute 8.Upper pack 6, lower pack 7 triggering pattern parachute 8 can be avoided to be blocked by rotor 2.Processing unit is also
Engine can be controlled to drive air charging system, while air charging system is controlled to be inflated for air bag 13, when the air bag on 15 surface of covering undercarriage
After full gas, it may also be unmanned plane even if unmanned plane falls within the water surface and bubble through the water column.
In addition to above preferred embodiment, the present invention also has other embodiments, and those skilled in the art can be according to this
Invention makes various changes and modifications, and without departing from the spirit of the present invention, should all belong to appended claims of the present invention and determine
The range of justice.
Claims (2)
1. a kind of amphibious unmanned plane for preventing from crashing, it is characterised in that：Be equipped with including body (1), in body processing unit and
Engine, processing unit are electrically connected with engine, and body is equipped with rotor (2), is equipped with shaft (3) in body, shaft is close to rotor
One end is equipped with groove (4), and rotor is equipped with connecting portion (5), and connecting portion is inserted into shaft groove, and connecting portion is interference fitted with shaft,
The shaft other end is connect with engine transmission, and upper pack (6) and lower pack (7), upper pack and lower pack are equipped in the groove of shaft
Between be equipped with the parachute (8) after collapsible, parachute connect by line (9) with groove inner wall, and it is sharp that parachute has bottom
Sharp the first trigger (10), the first trigger are equipped with partition board (11) with prescribe medicine parlor, the second trigger are equipped with by upper pack
(12), the second trigger is electrically connected with processing unit；Acceleration induction device is additionally provided in body, acceleration induction device is single with processing
Member electrical connection；Organism bottom is equipped with undercarriage (15), and undercarriage includes air bag (13) and frame body (14), air bag covering shelf body surface
Face, body is interior air charging system, and air charging system is connect with engine transmission, and air charging system is electrically connected with processing unit, inflation dress
The gas outlet put is connected with air bag.
2. a kind of amphibious unmanned plane for preventing from crashing according to claim 1, it is characterised in that：First trigger
For striker.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711422560.6A CN108128469A (en) | 2017-12-25 | 2017-12-25 | A kind of amphibious unmanned plane for preventing from crashing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711422560.6A CN108128469A (en) | 2017-12-25 | 2017-12-25 | A kind of amphibious unmanned plane for preventing from crashing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108128469A true CN108128469A (en) | 2018-06-08 |
Family
ID=62392470
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711422560.6A Pending CN108128469A (en) | 2017-12-25 | 2017-12-25 | A kind of amphibious unmanned plane for preventing from crashing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108128469A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111452980A (en) * | 2020-05-09 | 2020-07-28 | 天峋创新（北京）科技有限公司 | Unmanned aerial vehicle safety guarantee system |
| CN112638773A (en) * | 2018-09-28 | 2021-04-09 | 日本化药株式会社 | Aircraft with deployed body |
-
2017
- 2017-12-25 CN CN201711422560.6A patent/CN108128469A/en active Pending
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112638773A (en) * | 2018-09-28 | 2021-04-09 | 日本化药株式会社 | Aircraft with deployed body |
| CN112638773B (en) * | 2018-09-28 | 2024-04-16 | 日本化药株式会社 | Aircraft with body to be deployed |
| CN111452980A (en) * | 2020-05-09 | 2020-07-28 | 天峋创新（北京）科技有限公司 | Unmanned aerial vehicle safety guarantee system |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20180608 |
|
| WD01 | Invention patent application deemed withdrawn after publication |