CN107380445A - A kind of unmanned plane for launching lifebuoy - Google Patents
A kind of unmanned plane for launching lifebuoy Download PDFInfo
- Publication number
- CN107380445A CN107380445A CN201710698668.1A CN201710698668A CN107380445A CN 107380445 A CN107380445 A CN 107380445A CN 201710698668 A CN201710698668 A CN 201710698668A CN 107380445 A CN107380445 A CN 107380445A
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- China
- Prior art keywords
- guard shield
- lifebuoy
- unmanned plane
- mechanical
- paw
- 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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- 239000000523 sample Substances 0.000 claims description 10
- 206010013647 Drowning Diseases 0.000 abstract description 12
- 238000000034 method Methods 0.000 abstract description 6
- 230000008569 process Effects 0.000 abstract description 4
- 230000009286 beneficial effect Effects 0.000 abstract description 2
- NMFHJNAPXOMSRX-PUPDPRJKSA-N [(1r)-3-(3,4-dimethoxyphenyl)-1-[3-(2-morpholin-4-ylethoxy)phenyl]propyl] (2s)-1-[(2s)-2-(3,4,5-trimethoxyphenyl)butanoyl]piperidine-2-carboxylate Chemical compound C([C@@H](OC(=O)[C@@H]1CCCCN1C(=O)[C@@H](CC)C=1C=C(OC)C(OC)=C(OC)C=1)C=1C=C(OCCN2CCOCC2)C=CC=1)CC1=CC=C(OC)C(OC)=C1 NMFHJNAPXOMSRX-PUPDPRJKSA-N 0.000 description 6
- 101150117895 LAMP2 gene Proteins 0.000 description 4
- 230000007246 mechanism Effects 0.000 description 4
- 239000002699 waste material Substances 0.000 description 4
- 230000009471 action Effects 0.000 description 2
- 230000037396 body weight Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 208000035473 Communicable disease Diseases 0.000 description 1
- 230000003321 amplification Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 238000003199 nucleic acid amplification method Methods 0.000 description 1
- 238000002360 preparation method 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
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63C—LAUNCHING, HAULING-OUT, OR DRY-DOCKING OF VESSELS; LIFE-SAVING IN WATER; EQUIPMENT FOR DWELLING OR WORKING UNDER WATER; MEANS FOR SALVAGING OR SEARCHING FOR UNDERWATER OBJECTS
- B63C9/00—Life-saving in water
- B63C9/01—Air-sea rescue devices, i.e. equipment carried by, and capable of being dropped from, an aircraft
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Ocean & Marine Engineering (AREA)
- Remote Sensing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
The invention discloses a kind of unmanned plane for launching lifebuoy, its structure includes upper end guard shield, aerial indicator lamp, fan blade, individual motor, lower end guard shield, support feet, mechanical paw, display, heat emission hole, camera, safe cushion, connect limited block, the lower end of upper end guard shield coordinates with the upper gap of lower end guard shield, individual motor is provided with four and is mounted on four ends of upper end guard shield, the lower end screw connection of fan blade is in the upper end of individual motor, support feet is welded with left and right sides of the guard shield of lower end, the upper mechanical of mechanical paw is connected to the lower end in the middle part of the guard shield of lower end, beneficial effects of the present invention：Mechanical paw is added by the lower end in unmanned plane, mechanical paw is carried lifebuoy in rescue heuristic process is carried out, when finding drowning person, dispensing lifebuoy can be carried out, so as to carry out rescue drowning person, greatly add rescue efficiency.
Description
Technical field
The present invention is a kind of unmanned plane for launching lifebuoy, belongs to unmanned plane emergency relief field.
Background technology
UAV referred to as " unmanned plane, is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft, or fully or intermittently independently operated by car-mounted computer.Unmanned plane presses application field, can be divided into
It is military with civilian, military aspect, unmanned plane is divided into reconnaissance plane and target drone.Civilian aspect, unmanned plane+sector application, it is unmanned plane
Really just need；At present take photo by plane, agricultural, plant protection, miniature self-timer, express transportation, disaster relief, observation wild animal, monitoring
The application in infectious disease, mapping, news report, electric inspection process, the disaster relief, movies-making, manufacture romance etc. field, is greatly expanded
The purposes of unmanned plane in itself, developed country is also in actively extension sector application and development unmanned air vehicle technique.
Prior art discloses Application No.：201520466183.6 a kind of unmanned plane for launching lifebuoy, belong to
Unmanned plane emergency relief field.Including lifebuoy throwing mechanism, the lifebuoy throwing mechanism includes retainer plate, the retainer plate
Lower section is provided with positioned at equally distributed three horns on same circumference, and the horn bottom is provided with one by the first of servos control
Mechanical snap and the second mechanical snap, a lifebuoy can be placed between first mechanical snap and the second mechanical snap,
First mechanical snap blocks a bottom lifebuoy, and second mechanical snap blocks lifebuoy above.The present invention
Dispensing lifebuoy unmanned plane, there is unique mechanism of jettisoninging, simple in construction, weight is light, saves loading capacity, reduces
Motor load, power saving, extend the hang time.And can realize and repeatedly independently jettisoning, greatly reduce back and forth it is round it is time-consuming with
And the waste thrown more.Mechanism arm has retractility, versatile.In the prior art, it is wild when finding when unmanned plane is rescued in the wild
It is outer when having drowning person, it can not carry out taking rescue measure in time, it is necessary to artificial rescue, not only waste rescue time and increasing
Add rescue difficulty, it is more inconvenient.
The content of the invention
In view of the deficienciess of the prior art, it is an object of the present invention to provide a kind of unmanned plane for launching lifebuoy, with solution
Certainly in the prior art, when unmanned plane is rescued in the wild, when finding that there is drowning person in field, can not carry out taking rescue to arrange in time
Apply, it is necessary to artificial rescue, not only waste rescue time and add rescue difficulty, it is more inconvenient the problem of.
To achieve these goals, the present invention is to realize by the following technical solutions：A kind of lifebuoy launched
Unmanned plane, its structure include upper end guard shield, aerial indicator lamp, fan blade, individual motor, lower end guard shield, support feet, machine
Tool paw, display, heat emission hole, camera, safe cushion, connection limited block, the lower end and lower end of the upper end guard shield
The upper gap of guard shield coordinates, and the individual motor is provided with four and is mounted on four ends of upper end guard shield, described
The lower end screw connection of fan blade is welded with support feet at left and right sides of the upper end of individual motor, the lower end guard shield, institute
The upper mechanical for stating mechanical paw is connected to lower end in the middle part of the guard shield of lower end, and the lower end of the individual motor is provided with radiating
Hole, the upper end of the camera are welded by connecting limited block with lower end guard shield, and the mechanical paw includes connection and inputted
End, rotate element, motor housing, Mechanical course block, miniature probe, lifebuoy, paw, protection shell, fixed thread block, the company
It is outer that the lower end for connecing input is threadedly coupled by fixed thread block with rotate element, the lower end of the rotate element is welded in protection
The upper end of shell, the lower end of the motor housing are welded in the upper end of Mechanical course block and are integrated, the Mechanical course block
Lower end in the middle part of be provided with miniature probe, the paw is connected to the left and right sides of Mechanical course block provided with two and upper mechanical,
The lower end interval of the paw is matched with the left and right ends of lifebuoy, and the upper gap of the motor housing is matched with protection shell
Lower end.
Further, the upper center of the upper end guard shield installs aerial indicator lamp.
Further, the front end robot of the lower end guard shield is connected to the rear end of display.
Further, safe cushion is glued in the lower end of the support feet.
Further, the safe cushion is provided with four and is parallel to each other two-by-two.
Further, the safe cushion is plasticized rubber material, has the characteristic that resiliency is high, body weight is light.
Further, the motor housing is parallel to each other with Mechanical course block.
Beneficial effects of the present invention：Mechanical paw is added by the lower end in unmanned plane, is being rescued mechanical paw
Help in heuristic process, lifebuoy can be carried, when finding drowning person, dispensing lifebuoy can be carried out, so as to carry out rescue drowning person, greatly
Big adds rescue efficiency.
Brief description of the drawings
The detailed description made by reading with reference to the following drawings to non-limiting example, further feature of the invention,
Objects and advantages will become more apparent upon：
Fig. 1 is a kind of structural representation for the unmanned plane for launching lifebuoy of the present invention.
Fig. 2 is a kind of structural representation of the lower end for the unmanned plane for launching lifebuoy of the present invention.
Fig. 3 is a kind of structural representation of the mechanical paw for the unmanned plane for launching lifebuoy of the present invention.
In figure：Upper end guard shield -1, aerial indicator lamp -2, fan blade -3, individual motor -4, lower end guard shield -5, branch
Spike -6, mechanical paw -7, display -8, heat emission hole -9, camera -10, safe cushion -11, connection limited block -12, connection
Input -701, rotate element -702, motor housing -703, Mechanical course block -704, miniature probe -705, lifebuoy -706, hand
Pawl -707, protection shell -708, fixed thread block -709.
Embodiment
To be easy to understand the technical means, the inventive features, the objects and the advantages of the present invention, with reference to
Embodiment, the present invention is expanded on further.
Fig. 1, Fig. 2 and Fig. 3 are referred to, the present invention provides a kind of unmanned plane for launching lifebuoy：Its structure includes upper end
Guard shield 1, aerial indicator lamp 2, fan blade 3, individual motor 4, lower end guard shield 5, support feet 6, mechanical paw 7, display
8th, heat emission hole 9, camera 10, safe cushion 11, connection limited block 12, lower end and the lower end of the upper end guard shield 1 are protected
The upper gap of shell 5 coordinates, and the individual motor 4 is provided with four and is mounted on four ends of upper end guard shield 1, the wind
The lower end screw connection of leaf 3 is welded with support feet 6 in the upper end of individual motor 4, the left and right sides of the lower end guard shield 5,
The upper mechanical of the mechanical paw 7 is connected to the lower end at the middle part of lower end guard shield 5, and the lower end of the individual motor 4 is provided with
Heat emission hole 9, the upper end of the camera 10 are welded by connecting limited block 12 with lower end guard shield 5, and the mechanical paw 7 wraps
Include connection input 701, rotate element 702, motor housing 703, Mechanical course block 704, miniature probe 705, lifebuoy 706, hand
Pawl 707, protection shell 708, fixed thread block 709, the lower end of the connection input 701 pass through fixed thread block 709 and rotation
Turn element 702 be threadedly coupled, the lower end of the rotate element 702 be welded in protection shell 708 upper end, the motor housing 703
Lower end be welded in the upper end of Mechanical course block 704 and be integrated, be provided with the middle part of the lower end of the Mechanical course block 704
Miniature probe 705, the paw 707 is provided with two and upper mechanical is connected to the left and right sides of Mechanical course block 704, the hand
The lower end interval of pawl 707 is matched with the left and right ends of lifebuoy 706, and the upper gap of the motor housing 703 is matched with outside protection
The lower end of shell 708, the upper center of the upper end guard shield 1 install aerial indicator lamp 2, before the lower end guard shield 5
End is mechanically connected to the rear end of display 8, and safe cushion 11 is glued in the lower end of the support feet 6, and the safe cushion 11 is provided with
Four and it is parallel to each other two-by-two, the safe cushion 11 is plasticized rubber material, has the characteristic that resiliency is high, body weight is light, institute
Motor housing 703 is stated to be parallel to each other with Mechanical course block 704.
Carrying out in use, staff should first confirm whether unmanned plane damages, and whether mechanical paw 7 can normally make
With, after no problem is confirmed, can with this equipment of normal use, in use, first unmanned plane should be carried out it is fully charged, and be machinery
The clamping jaw of paw 707 on paw 7 lives lifebuoy 706, and rear equipment of opening carries out rescue action, in unmanned plane during flying, camera
10 will be opened, and video is sent in computer end, and in rescue operations, in case of found drowning person, user of service will should set
Make preparation for dropping low, and by miniature probe 705 detect the particular location of drowning person, after lifebuoy is thrown to drowning person, so as to
Reach rescue.
Individual motor 4 described in this patent is that volume, capacity are smaller, motor of the power output typically below hundreds of watts and
Purposes, performance and environmental condition require special motor.The miniature specific type of electric machine of full name, abbreviation micro machine.It is usually used in control system
In, the functions such as detection, resolving, amplification, execution or the conversion of dynamoelectric signal or energy are realized, or loaded for gearing,
Can be as the AC and DC power supply of equipment.
Component upper ends guard shield 1 of the present invention, aerial indicator lamp 2, fan blade 3, individual motor 4, lower end guard shield 5, branch
Spike 6, mechanical paw 7, display 8, heat emission hole 9, camera 10, safe cushion 11, connection limited block 12, connection input
701st, rotate element 702, motor housing 703, Mechanical course block 704, miniature probe 705, lifebuoy 706, paw 707, protection are outer
The part that shell 708, fixed thread block 709 are universal standard part or those skilled in the art know, its structure and principle are all
This technology personnel can learn or know by normal experiment method that the present invention solves the problems, such as prior art by technical manual
In, when unmanned plane is rescued in the wild, when finding that there is drowning person in field, it can not carry out taking rescue measure in time, it is necessary to artificial
Carry out rescue, not only waste and rescue time and add rescue difficulty, more inconvenient, the present invention passes through the mutual of above-mentioned part
Combination, adds mechanical paw by the lower end in unmanned plane, mechanical paw is carried and is rescued in rescue heuristic process is carried out
Raw circle, when finding drowning person, dispensing lifebuoy can be carried out, so as to carry out rescue drowning person, greatly adds rescue efficiency, had
Body is as described below:
The lower end of the connection input 701 is threadedly coupled by fixed thread block 709 with rotate element 702, the rotation
The lower end for turning element 702 is welded in the upper end of protection shell 708, and the lower end of the motor housing 703 is welded in Mechanical course block 704
Upper end and be integrated, be provided with miniature probe 705 in the middle part of the lower end of the Mechanical course block 704, the paw 707 is set
There are two and upper mechanical is connected to the left and right sides of Mechanical course block 704, the lower end interval of the paw 707 is matched with lifesaving
The left and right ends of circle 706, the upper gap of the motor housing 703 are matched with the lower end of protection shell 708.
The general principle and principal character and advantages of the present invention of the present invention has been shown and described above, for this area skill
For art personnel, it is clear that the invention is not restricted to the details of above-mentioned one exemplary embodiment, and without departing substantially from the present invention spirit or
In the case of essential characteristic, the present invention can be realized in other specific forms.Which point therefore, no matter from the point of view of, all should incite somebody to action
Embodiment regards exemplary as, and be it is nonrestrictive, the scope of the present invention by appended claims rather than on state
Bright restriction, it is intended that all changes fallen in the implication and scope of the equivalency of claim are included in the present invention
It is interior.Any reference in claim should not be considered as to the involved claim of limitation.
Moreover, it will be appreciated that although the present specification is described in terms of embodiments, not each embodiment is only wrapped
Containing an independent technical scheme, this narrating mode of specification is only that those skilled in the art should for clarity
Using specification as an entirety, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art
It is appreciated that other embodiment.
Claims (5)
1. a kind of unmanned plane for launching lifebuoy, its structure includes upper end guard shield (1), aerial indicator lamp (2), fan blade
(3), individual motor (4), lower end guard shield (5), support feet (6), mechanical paw (7), display (8), heat emission hole (9), take the photograph
As head (10), safe cushion (11), connection limited block (12), its characteristic is：
The lower end of the upper end guard shield (1) coordinates with the upper gap of lower end guard shield (5), the individual motor (4)
Provided with four and four ends of upper end guard shield (1) are mounted on, the lower end screw connection of the fan blade (3) is in individual motor
(4) upper end, support feet (6), the upper end of the mechanical paw (7) are welded with left and right sides of the lower end guard shield (5)
The lower end being mechanically connected in the middle part of lower end guard shield (5), the lower end of the individual motor (4) is provided with heat emission hole (9), described to take the photograph
As the upper end of head (10) is welded by connecting limited block (12) with lower end guard shield (5)；
The mechanical paw (7) includes connection input (701), rotate element (702), motor housing (703), Mechanical course block
(704), miniature probe (705), lifebuoy (706), paw (707), protection shell (708), fixed thread block (709), it is described
The lower end of connection input (701) is threadedly coupled by fixed thread block (709) with rotate element (702), the rotate element
(702) lower end is welded in the upper end of protection shell (708), and the lower end of the motor housing (703) is welded in Mechanical course block
(704) upper end and it is integrated, miniature probe (705) is provided with the middle part of the lower end of the Mechanical course block (704), it is described
Paw (707) is provided with the left and right sides that two and upper mechanical are connected to Mechanical course block (704), under the paw (707)
End interval is matched with the left and right ends of lifebuoy (706), and the upper gap of the motor housing (703) is matched with protection shell
(708) lower end.
A kind of 2. unmanned plane for launching lifebuoy according to claim 1, it is characterised in that：The upper end guard shield
(1) upper center installs aerial indicator lamp (2).
A kind of 3. unmanned plane for launching lifebuoy according to claim 1, it is characterised in that：The lower end guard shield
(5) front end robot is connected to the rear end of display (8).
A kind of 4. unmanned plane for launching lifebuoy according to claim 1, it is characterised in that：The support feet (6)
It is glued safe cushion (11) in lower end.
A kind of 5. unmanned plane for launching lifebuoy according to claim 1, it is characterised in that：The safe cushion (11)
It is parallel to each other provided with four and two-by-two.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710698668.1A CN107380445A (en) | 2017-08-15 | 2017-08-15 | A kind of unmanned plane for launching lifebuoy |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710698668.1A CN107380445A (en) | 2017-08-15 | 2017-08-15 | A kind of unmanned plane for launching lifebuoy |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107380445A true CN107380445A (en) | 2017-11-24 |
Family
ID=60355908
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710698668.1A Pending CN107380445A (en) | 2017-08-15 | 2017-08-15 | A kind of unmanned plane for launching lifebuoy |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107380445A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108082488A (en) * | 2017-12-19 | 2018-05-29 | 佛山市神风航空科技有限公司 | The disaster relief aircraft of adjustable point air-drop package |
| CN113060284A (en) * | 2021-04-14 | 2021-07-02 | 上海海事大学 | Unmanned aerial vehicle with life buoy throwing function |
| WO2022110240A1 (en) * | 2020-11-30 | 2022-06-02 | 南京溧水高新创业投资管理有限公司 | Unmanned aerial vehicle for water rescue |
-
2017
- 2017-08-15 CN CN201710698668.1A patent/CN107380445A/en active Pending
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108082488A (en) * | 2017-12-19 | 2018-05-29 | 佛山市神风航空科技有限公司 | The disaster relief aircraft of adjustable point air-drop package |
| CN108082488B (en) * | 2017-12-19 | 2021-06-15 | 金海森智能装备(佛山)有限公司 | Disaster relief aircraft capable of airdrop parcel at fixed point |
| WO2022110240A1 (en) * | 2020-11-30 | 2022-06-02 | 南京溧水高新创业投资管理有限公司 | Unmanned aerial vehicle for water rescue |
| CN113060284A (en) * | 2021-04-14 | 2021-07-02 | 上海海事大学 | Unmanned aerial vehicle with life buoy throwing function |
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Application publication date: 20171124 |