CN108392759A - A kind of unmanned plane fire extinguishing equipped system that can mend bullet filling automatically - Google Patents
A kind of unmanned plane fire extinguishing equipped system that can mend bullet filling automatically Download PDFInfo
- Publication number
- CN108392759A CN108392759A CN201810108286.3A CN201810108286A CN108392759A CN 108392759 A CN108392759 A CN 108392759A CN 201810108286 A CN201810108286 A CN 201810108286A CN 108392759 A CN108392759 A CN 108392759A
- Authority
- CN
- China
- Prior art keywords
- bomb
- steering engine
- fire extinguisher
- unmanned plane
- bottom outer
- 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
Classifications
-
- A—HUMAN NECESSITIES
- A62—LIFE-SAVING; FIRE-FIGHTING
- A62C—FIRE-FIGHTING
- A62C3/00—Fire prevention, containment or extinguishing specially adapted for particular objects or places
- A62C3/02—Fire prevention, containment or extinguishing specially adapted for particular objects or places for area conflagrations, e.g. forest fires, subterranean fires
- A62C3/0228—Fire prevention, containment or extinguishing specially adapted for particular objects or places for area conflagrations, e.g. forest fires, subterranean fires with delivery of fire extinguishing material by air or aircraft
- A62C3/025—Fire extinguishing bombs; Projectiles and launchers therefor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS 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
- B64D1/04—Dropping, ejecting, or releasing articles the articles being explosive, e.g. bombs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS 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
- B64D1/04—Dropping, ejecting, or releasing articles the articles being explosive, e.g. bombs
- B64D1/06—Bomb releasing; Bombs doors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D9/00—Equipment for handling freight; Equipment for facilitating passenger embarkation or the like
Abstract
The invention discloses a kind of unmanned plane fire extinguishing equipped systems that can mend bullet filling automatically, including unmanned aerial vehicle body, and the bottom outer surface of the unmanned aerial vehicle body is installed with apical ring, and the bottom outer surface of apical ring is equipped with connecting rod.A kind of unmanned plane fire extinguishing equipped system that can mend bullet filling automatically of the present invention, disk is launched equipped with No.1 fire extinguisher bomb, No. two fire extinguisher bombs launch disk, steering engine and steering engine extension shaft, it can be controlled by the steering engine extension shaft of unified steering engine by the way that two layers of turntable that drops a bomb is arranged, two layers of disk notch that drops a bomb differs the position of a fire extinguisher bomb when steering engine rotates, upper layer fire extinguisher bomb can fall to lower layer's fire extinguisher bomb by the slot that drops a bomb on upper layer automatically and place in cabin after lower layer's fire extinguisher bomb is launched down, it drops a bomb, increasing unmanned plane primary quantity of dropping a bomb of rising and falling promptly can put out or control bigger fire behavior, and it controls simple, a steering engine rotation need to only be controlled, bring better prospect of the application.
Description
Technical field
The present invention relates to fire extinguishing equipped system field, more particularly to a kind of unmanned plane fire extinguishing that can mend bullet filling automatically is carried
System.
Background technology
Unmanned plane has been widely used in various fields as a kind of infant industry technology, has at home many
Fire department successfully carried out the trials such as scene of a fire investigation monitoring, relief goods of jettisoninging using unmanned plane, and effect is clearly.In day
In the explosion accident rescue of Tianjin, each department also once carried out high-altitude investigation using unmanned plane to the scene of the accident, was provided for rescue decision
Partial reference frame；There is certain disadvantage when in use in the existing unmanned plane fire extinguishing equipped system that can mend bullet filling automatically
End can not achieve primary load and promptly be put out or controlled bigger fire behavior, brings certain influence to fire extinguishing, be likely to result in
Fire spreading timely cannot disposably put out a fire, and need repeatedly to put out a fire, and be brought to the control of the intensity of a fire with putting out
Certain influence, for this purpose, it is proposed that a kind of unmanned plane fire extinguishing equipped system that can mend bullet filling automatically.
Invention content
The technical problem to be solved by the present invention is to overcome the defects of the prior art, provide a kind of nothing that can mend bullet filling automatically
Man-machine fire extinguishing equipped system.
In order to solve the above technical problem, the present invention provides the following technical solutions：
A kind of unmanned plane fire extinguishing equipped system that can mend bullet filling automatically of the present invention, including unmanned aerial vehicle body, it is described nobody
The bottom outer surface of machine fuselage is installed with apical ring, and the bottom outer surface of apical ring is equipped with connecting rod, the bottom of the connecting rod
End outer surface is installed with No.1 fixed plate, and is movably installed with steering engine at the top outer surface center of No.1 fixed plate, institute
The bottom outer surface for stating steering engine is installed with steering engine extension shaft, and the top outer surface of the No.1 fixed plate is close to a side position
Cabin is placed equipped with fire extinguisher bomb, the bottom outer surface of the No.1 fixed plate is installed with connecting pole close to a side position, described
One side external surface of steering engine extension shaft is equipped with upper junction plate close to apical position, and the bottom outer surface of upper junction plate is fixedly mounted
There is No.1 fire extinguisher bomb to launch disk, the bottom outer surface of the steering engine extension shaft is installed with lower connecting plate, and lower connecting plate
Bottom outer surface is equipped with No. two fire extinguisher bombs and launches disk, and the side external surface that No. two fire extinguisher bombs launch disk is equipped with the slot that drops a bomb, and
The drop a bomb top outer surface of slot is equipped with No. two fixed plates, and the output end of the steering engine and the input terminal telecommunications of steering engine extension shaft connect
It connects.
Preferably, the bottom outer surface of the lower connecting plate is equipped with fixing bolt, and the quantity of fixing bolt is eight groups, and under
Connecting plate is launched disk with No. two fire extinguisher bombs by fixing bolt and is fixedly connected.
Preferably, the shape of the connecting rod be cylinder, and the quantity of connecting rod be four groups, the No.1 fixed plate with
The shape of No. two fixed plates is circle.
Preferably, the shape that the fire extinguisher bomb places cabin is cylinder, and fire extinguisher bomb places 16 groups of the quantity in cabin.
Preferably, the top outer surface of the connecting pole is equipped with weld seam, and connecting pole is solid by weld seam and No. two fixed plates
Fixed connection.
Preferably, the diameter of the slot that drops a bomb is identical as the fire extinguisher bomb placement diameter in cabin, the shape of the steering engine extension shaft
For cylinder.
The advantageous effect that is reached of the present invention is：This can mend the unmanned plane fire extinguishing equipped system of bullet filling automatically, by setting
The No.1 fire extinguisher bomb set launches disk, No. two fire extinguisher bombs launch disks, steering engine and steering engine extension shaft, can be dropped a bomb by being arranged two layers and be turned
Disk is controlled by the steering engine extension shaft of unified steering engine, and two layers of disk notch that drops a bomb differs the position of a fire extinguisher bomb when steering engine rotates,
Upper layer fire extinguisher bomb can fall to lower layer's fire extinguisher bomb by the slot that drops a bomb on upper layer automatically and place cabin after lower layer's fire extinguisher bomb is launched down
In, it drops a bomb, increases unmanned plane and rise and fall primary quantity of dropping a bomb, promptly can put out or control bigger fire behavior, Ke Yigeng
Add and timely and effectively controls the intensity of a fire；And present invention control is simple, need to only control a steering engine rotation, can entirely mend automatically
The unmanned plane fire extinguishing equipped system of bullet filling is simple in structure, and easy to operate, the effect used has relative to traditional approach significantly to be carried
It is high.
Description of the drawings
Attached drawing is used to provide further understanding of the present invention, and a part for constitution instruction, the reality with the present invention
It applies example to be used to explain the present invention together, not be construed as limiting the invention.In the accompanying drawings：
Fig. 1 is a kind of overall structure upward view for the unmanned plane fire extinguishing equipped system that can mend bullet filling automatically of the present invention；
Fig. 2 is a kind of partial structurtes vertical view for the unmanned plane fire extinguishing equipped system that can mend bullet filling automatically of the present invention；
Fig. 3 is a kind of overall structure figure for the unmanned plane fire extinguishing equipped system steering engine that can mend bullet filling automatically of the present invention.
In figure：1, unmanned aerial vehicle body；2, apical ring；3, connecting rod；4, No.1 fixed plate；5, steering engine；6, steering engine extension shaft；7、
Fire extinguisher bomb places cabin；8, connecting pole；9, upper junction plate；10, No.1 fire extinguisher bomb launches disk；11, lower connecting plate；12, No. two fire extinguishings
Bullet launches disk；13, drop a bomb slot；14, No. two fixed plates.
Specific implementation mode
Hereinafter, preferred embodiments of the present invention will be described with reference to the accompanying drawings, it should be understood that preferred reality described herein
Apply example only for the purpose of illustrating and explaining the present invention and is not intended to limit the present invention.
As shown in Figs. 1-3, a kind of unmanned plane fire extinguishing equipped system that can mend bullet filling automatically, including unmanned aerial vehicle body 1, nothing
The bottom outer surface of man-machine fuselage 1 is installed with apical ring 2, and the bottom outer surface of apical ring 2 is equipped with connecting rod 3, connecting rod 3
Bottom outer surface is installed with No.1 fixed plate 4, and is movably installed with steering engine at the top outer surface center of No.1 fixed plate 4
5, the bottom outer surface of steering engine 5 is installed with steering engine extension shaft 6, and the top outer surface of No.1 fixed plate 4 is close to a side position
Cabin 7 is placed equipped with fire extinguisher bomb, the bottom outer surface of No.1 fixed plate 4 is installed with connecting pole 8 close to a side position, and steering engine adds
One side external surface of long axis 6 is equipped with upper junction plate 9 close to apical position, and the bottom outer surface of upper junction plate 9 is installed with
No.1 fire extinguisher bomb launches disk 10, and the bottom outer surface of steering engine extension shaft 6 is installed with lower connecting plate 11, and lower connecting plate 11
Bottom outer surface is equipped with No. two fire extinguisher bombs and launches disk 12, and the side external surface that No. two fire extinguisher bombs launch disk 12 is equipped with the slot 13 that drops a bomb,
And the top outer surface for the slot 13 that drops a bomb is equipped with No. two fixed plates 14, the output end of steering engine 5 and the input terminal telecommunications of steering engine extension shaft 6
Connection.
The bottom outer surface of lower connecting plate 11 is equipped with fixing bolt, and the quantity of fixing bolt is eight groups, and lower connecting plate 11
Disk 12 is launched by fixing bolt with No. two fire extinguisher bombs to be fixedly connected；The shape of connecting rod 3 is cylinder, and the number of connecting rod 3
Amount is four groups, and the shape of No.1 fixed plate 4 and No. two fixed plates 14 is circle；The shape that fire extinguisher bomb places cabin 7 is cylinder,
And fire extinguisher bomb places 16 groups of the quantity in cabin 7；The top outer surface of connecting pole 8 is equipped with weld seam, and connecting pole 8 passes through weld seam and two
Number fixed plate 14 is fixedly connected；Drop a bomb slot 13 diameter and fire extinguisher bomb place the diameter in cabin 7 it is identical, the shape of steering engine extension shaft 6
For cylinder.
It should be noted that the present invention is a kind of unmanned plane fire extinguishing equipped system that can mend bullet filling automatically, in use, first
First, fire extinguisher bomb is put into the fire extinguisher bomb being respectively put into No.1 fixed plate 4 and No. two fixed plates 14 to place in cabin 7, by right
Unmanned plane is controlled the place for being transported to fire extinguisher bomb and putting out a fire, by controlling the steering engine 5 on unmanned plane, steering engine
5 rotations drive steering engine extension shafts 6 to be rotated, and steering engine extension shaft 6 is by being fixed on the upper junction plate 9 and lower connecting plate of side
11, driving No.1 fire extinguisher bomb to launch disk 10 by upper junction plate 9, lower connecting plate 11 drives No. two fire extinguisher bombs to launch disk 12, leads to
It crosses two layers of turntable that drops a bomb of setting to be controlled by the steering engine extension shaft 6 of unified steering engine 5, two layers of disk notch difference of dropping a bomb when steering engine 5 rotates
The position of one fire extinguisher bomb, after lower layer's fire extinguisher bomb is launched down, upper layer fire extinguisher bomb can be automatically by the slot 13 that drops a bomb on upper layer
It falls, drops a bomb in cabin 7 until lower layer fire extinguisher bomb is placed, increase unmanned plane and rise and fall primary quantity of dropping a bomb, can promptly flutter
It goes out or controls bigger fire behavior, can effectively control the intensity of a fire much sooner, and control simply, need to only control a steering engine rotation
, more practical.
Finally it should be noted that：The foregoing is only a preferred embodiment of the present invention, is not intended to restrict the invention,
Although the present invention is described in detail referring to the foregoing embodiments, for those skilled in the art, still may be used
With technical scheme described in the above embodiments is modified or equivalent replacement of some of the technical features.
All within the spirits and principles of the present invention, any modification, equivalent replacement, improvement and so on should be included in the present invention's
Within protection domain.
Claims (6)
1. a kind of unmanned plane fire extinguishing equipped system that can mend bullet filling automatically, including unmanned aerial vehicle body (1), it is characterised in that：Institute
The bottom outer surface for stating unmanned aerial vehicle body (1) is installed with apical ring (2), and the bottom outer surface of apical ring (2) is equipped with connecting rod
(3), the bottom outer surface of the connecting rod (3) is installed with No.1 fixed plate (4), and outside the top of No.1 fixed plate (4)
Steering engine (5) is movably installed at centre of surface, the bottom outer surface of the steering engine (5) is installed with steering engine extension shaft (6), institute
The top outer surface for stating No.1 fixed plate (4) is equipped with fire extinguisher bomb placement cabin (7), the No.1 fixed plate (4) close to a side position
Bottom outer surface be installed with connecting pole (8) close to a side position, a side external surface of the steering engine extension shaft (6) is close
Apical position is equipped with upper junction plate (9), and the bottom outer surface of upper junction plate (9) is installed with No.1 fire extinguisher bomb and launches disk
(10), the bottom outer surface of the steering engine extension shaft (6) is installed with lower connecting plate (11), and the bottom end of lower connecting plate (11)
Outer surface is equipped with No. two fire extinguisher bombs and launches disk (12), and the side external surface that No. two fire extinguisher bombs launch disk (12) is equipped with the slot that drops a bomb
(13), and the top outer surface of the slot that drops a bomb (13) is equipped with No. two fixed plates (14), and output end and the steering engine of the steering engine (5) lengthen
The input terminal telecommunications of axis (6) connects.
2. a kind of unmanned plane fire extinguishing equipped system that can mend bullet filling automatically according to claim 1, it is characterised in that：Institute
The bottom outer surface for stating lower connecting plate (11) is equipped with fixing bolt, and the quantity of fixing bolt is eight groups, and lower connecting plate (11) is logical
Fixing bolt is crossed to be fixedly connected with No. two fire extinguisher bombs dispensing disks (12).
3. a kind of unmanned plane fire extinguishing equipped system that can mend bullet filling automatically according to claim 1, it is characterised in that：Institute
The shape for stating connecting rod (3) is cylinder, and the quantity of connecting rod (3) is four groups, the No.1 fixed plate (4) and No. two fixations
The shape of plate (14) is circle.
4. a kind of unmanned plane fire extinguishing equipped system that can mend bullet filling automatically according to claim 1, it is characterised in that：Institute
It is cylinder to state fire extinguisher bomb and place the shape of cabin (7), and fire extinguisher bomb places 16 groups of the quantity of cabin (7).
5. a kind of unmanned plane fire extinguishing equipped system that can mend bullet filling automatically according to claim 1, it is characterised in that：Institute
The top outer surface for stating connecting pole (8) is equipped with weld seam, and connecting pole (8) is fixedly connected by weld seam with No. two fixed plates (14).
6. a kind of unmanned plane fire extinguishing equipped system that can mend bullet filling automatically according to claim 1, it is characterised in that：Institute
It states the diameter of the slot that drops a bomb (13) and fire extinguisher bomb places that the diameter of cabin (7) is identical, and the shape of the steering engine extension shaft (6) is cylinder
Body.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810108286.3A CN108392759A (en) | 2018-02-02 | 2018-02-02 | A kind of unmanned plane fire extinguishing equipped system that can mend bullet filling automatically |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810108286.3A CN108392759A (en) | 2018-02-02 | 2018-02-02 | A kind of unmanned plane fire extinguishing equipped system that can mend bullet filling automatically |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108392759A true CN108392759A (en) | 2018-08-14 |
Family
ID=63095934
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810108286.3A Pending CN108392759A (en) | 2018-02-02 | 2018-02-02 | A kind of unmanned plane fire extinguishing equipped system that can mend bullet filling automatically |
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| Country | Link |
|---|---|
| CN (1) | CN108392759A (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20060011355A1 (en) * | 2004-06-30 | 2006-01-19 | Cleary William W | Firefighting bomblets and a precision aerial firefighting method utilizing the same |
| CN103212170A (en) * | 2013-04-03 | 2013-07-24 | 哈尔滨工程大学 | Forest fire fighting bomb launching device |
| CN206797738U (en) * | 2017-06-21 | 2017-12-26 | 东海县腾翔航空科技有限公司 | A kind of fire-fighting unmanned plane |
| CN206813325U (en) * | 2016-06-08 | 2017-12-29 | 青海山水生态科技有限公司 | A kind of unmanned plane hanging fire extinguisher bomb launches cabin |
| CN206822983U (en) * | 2017-06-01 | 2018-01-02 | 国家电网公司 | Unmanned plane fire extinguisher bomb launches cabin |
-
2018
- 2018-02-02 CN CN201810108286.3A patent/CN108392759A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20060011355A1 (en) * | 2004-06-30 | 2006-01-19 | Cleary William W | Firefighting bomblets and a precision aerial firefighting method utilizing the same |
| CN103212170A (en) * | 2013-04-03 | 2013-07-24 | 哈尔滨工程大学 | Forest fire fighting bomb launching device |
| CN206813325U (en) * | 2016-06-08 | 2017-12-29 | 青海山水生态科技有限公司 | A kind of unmanned plane hanging fire extinguisher bomb launches cabin |
| CN206822983U (en) * | 2017-06-01 | 2018-01-02 | 国家电网公司 | Unmanned plane fire extinguisher bomb launches cabin |
| CN206797738U (en) * | 2017-06-21 | 2017-12-26 | 东海县腾翔航空科技有限公司 | A kind of fire-fighting unmanned plane |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
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| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20180814 |
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| RJ01 | Rejection of invention patent application after publication |