CN106152123B - Flame device applied to unmanned plane - Google Patents
Flame device applied to unmanned plane Download PDFInfo
- Publication number
- CN106152123B CN106152123B CN201610727329.7A CN201610727329A CN106152123B CN 106152123 B CN106152123 B CN 106152123B CN 201610727329 A CN201610727329 A CN 201610727329A CN 106152123 B CN106152123 B CN 106152123B
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- China
- Prior art keywords
- fixed
- ontology
- unmanned plane
- positioning
- injection
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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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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
- F23D11/36—Details, e.g. burner cooling means, noise reduction means
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
- F23D14/46—Details, e.g. noise reduction means
-
- 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
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Feeding And Controlling Fuel (AREA)
Abstract
The present invention provides a kind of flame devices applied to unmanned plane, belong to air vehicle technique field, comprising: ontology is fixed on the fuselage of unmanned plane；Firing device is fixed on ontology；Injection equipment is fixed on ontology, and is connect with firing device；Wherein, a memory space is provided in injection equipment, for storing inflammable substance；And what is be connected in injection equipment with memory space is additionally provided with a combustion zone, and spark directive combustion zone is burst out when acting firing device, to light the inflammable substance for flowing into combustion zone by memory space.The present invention, so that flame device is transported to the position for needing flame to remove foreign matter in the air by the flight of unmanned plane carries out flame operation, has the characteristics that convenient and efficient and security performance is high by the way that flame device to be fixed on the fuselage of unmanned plane.
Description
Technical field
The invention belongs to air vehicle technique field, in particular to a kind of flame device applied to unmanned plane.
Background technique
In recent years, the hanging wire foreign matter on transmission line wire has become the great threat of electric power netting safe running, currently, operation
Department passes through frequently with being purged processing under power failure, but this method is by foreign matter position, route surrounding geographical environmental restrictions
It is larger, and power failure processing also will affect transmission reliability.Electric field equipotential live line work is such as entered using operating personnel and is faced with peace again
The unfavorable situation that full blast danger is big, operating efficiency is low.
From live hanging wire foreign matter statistical number it has been found that most foreign matters are that plastic film, kite, ad banner etc. are flammable
Property foreign matter, therefore a kind of convenient, practical method is become by burning removal foreign matter.However, often height is higher for power transmission line,
When removing foreign matter using combustion method, flame projector also farther out, is made troubles apart from operator to foreign matter removing.
Summary of the invention
The technical problem to be solved in the present invention is that how faster, effective removing high-altitude foreign matter.
In order to solve the above technical problems, the present invention provides a kind of flame device applied to unmanned plane, the flame dress
Setting includes: ontology, and the ontology is fixed on the fuselage of the unmanned plane；Firing device, the firing device are fixed on described
On ontology；Injection equipment, the injection equipment are fixed on the ontology, and are connect with the firing device；Wherein, the spray
It penetrates in mechanism and is provided with a memory space, for storing inflammable substance；And in the injection equipment with the memory space phase
Connection is additionally provided with a combustion zone, so that the firing device is burst out combustion zone described in spark directive when acting, to light by institute
State the inflammable substance that memory space flows into the combustion zone.
Optionally, the firing device includes: ignition system, and the ignition system is fixed on the ontology, is used for point
Fire movement injection spark；First tank body, first tank body is fixed on the ontology, for storing combustion gas；Combustion gas bar, it is described
Combustion gas bar is fixed on the ontology, and is communicated with first tank body, and the combustion gas is used for transmission；Wherein, the combustion gas bar
The spark injection end position of fuel gas injection end and the ignition system it is corresponding, with by the spark ejection end in the combustion
Gas jet end carries out spark injection.
Optionally, the ignition system includes: ignition switch, and the inside of the ontology is arranged in the ignition switch；Electricity
Sub-conductor, the electronic wire include electric connecting terminal and the spark ejection end, and the electric connecting terminal and the ignition switch
Connection.
Optionally, the injection equipment includes: injection system, and the injection system is fixed in the ontology；Second tank
Body, second tank body is fixed on the ontology, for storing oil；Spray bar, the spray bar include fixing end and oil spout
End, and the spray bar is fixed on the ontology by the fixing end；The spray bar passes through the injection system and institute
The connection of the second tank body is stated, transmits the oil into the spray bar to control second tank body by the injection system.
Optionally, the oil spout end is corresponding with the position at the fuel gas injection end.
Optionally, the spray bar, the electronic wire and the combustion gas bar three and column distribution, and the spark sprays
The corresponding linking of end, the fuel gas injection end and the oil spout end three.
Optionally, the injection system includes: power supply source, and the power supply source is fixed in the ontology；Controller, it is described
Controller is fixed in the ontology；Voltage-stablizer, the voltage-stablizer are fixed in the ontology, and the power supply source is described in
Voltage-stablizer is connect with the controller and the firing device respectively, to the controller and firing device power supply；Pipe
Way switch, the pipeline switch are fixed in the ontology, and the pipeline switch is connect with the controller, and respectively with institute
The fixing end pipeline for stating the second tank body and the spray bar communicates.
Optionally, the fuel gas injection end is provided with several air inlets.
Optionally, further includes: locating piece, the locating piece is fixed on the spark ejection end, and passes through the locating piece
The electronic wire is flexibly connected with the spray bar.
Optionally, the ontology is the cabinet of square structure；And the cabinet includes: first side, second side, third
Side and the 4th side；The first side and the second side are two opposites of the cabinet, the third side
With the 4th side be the cabinet two opposites, the first side respectively with the third side and the described 4th
Side adjacent distributions；Wherein, the power supply source, the controller, the voltage-stablizer, the pipeline switch and the ignition switch
It is placed in the cabinet；The fuselage is fixed in the first side, and first tank body is fixed on the second side
On, second tank body is fixed on the third side, and the spray bar is fixed on the 4th side by the fixing end
On.
The utility model has the advantages that
A kind of flame device applied to unmanned plane provided by the invention, the fuselage of unmanned plane is fixed on by an ontology
On, so that the flame device is transported to the position for needing flame to remove foreign matter in the air by the flight of unmanned plane carries out flame work
Industry has the characteristics that convenient and efficient and security performance is high, solves and is hung in the prior art when on the high empty body such as power transmission line
When foreign matter, since suspension height is higher, using combustion method removal foreign matter when flame projector apart from operator farther out, give foreign matter
Removing brings unhandy technological deficiency.
Detailed description of the invention
It in order to more clearly explain the embodiment of the invention or the technical proposal in the existing technology, below will be to institute in embodiment
Attached drawing to be used is needed to be briefly described, it should be apparent that, the accompanying drawings in the following description is only some implementations of the invention
Example, for those of ordinary skill in the art, without creative efforts, can also obtain according to these attached drawings
Obtain other attached drawings.
Fig. 1 is the unmanned plane overall structure diagram provided in an embodiment of the present invention for being equipped with flame device；
Fig. 2 is the overall structure diagram of flame device provided in an embodiment of the present invention；
Fig. 3 is the overall structure side view of flame device shown in Fig. 2；
Fig. 4 is injection system in flame device shown in Fig. 2 and ignition system in intrinsic connection block diagram；
Fig. 5 is the structural schematic diagram of rotary part in support component provided in an embodiment of the present invention；
Fig. 6 is the structural schematic diagram of positioning element in support component provided in an embodiment of the present invention；
Fig. 7 is the overall structure diagram of fast removable member shown in FIG. 1；
Fig. 8 is the overall structure main view of fast removable member in Fig. 7；
Fig. 9 is that first positioning plunger is in the cross-sectional view under contraction state in fast removable member shown in FIG. 1；
Figure 10 is that first positioning plunger is in the overall structure diagram under contraction state in fast removable member shown in FIG. 1；
Figure 11 is that first positioning plunger is in the cross-sectional view under raised position in fast removable member shown in FIG. 1；
Figure 12 is that first positioning plunger is in the overall structure diagram under raised position in fast removable member shown in FIG. 1.
Specific embodiment
The embodiment of the invention provides a kind of flame devices applied to unmanned plane, are fixed on unmanned plane by an ontology
On fuselage, sprayed so that the flame device is transported to the position for needing flame to remove foreign matter in the air by the flight of unmanned plane
Fiery operation has the characteristics that convenient and efficient and security performance is high, solves in the prior art when outstanding on the high empty body such as power transmission line
When hanging with foreign matter, since suspension height is higher, using combustion method removal foreign matter when flame projector apart from operator farther out, give
Foreign matter removing brings unhandy technological deficiency.
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, those of ordinary skill in the art's every other embodiment obtained belong to what the present invention protected
Range；Wherein "and/or" keyword involved in this implementation, indicate and or two kinds of situations, in other words, the present invention implement
A and/or B mentioned by example, illustrate two kinds of A and B, A or B situations, describe three kinds of states present in A and B, such as A and/or
B, indicate: only including A does not include B；Only including B does not include A；Including A and B.
Meanwhile in the embodiment of the present invention, when component is referred to as " being fixed on " another component, it can be directly at another
On component or there may also be components placed in the middle.When a component is considered as " connection " another component, it be can be directly
It is connected to another component or may be simultaneously present component placed in the middle.When a component is considered as " being set to " another group
Part, it, which can be, is set up directly on another component or may be simultaneously present component placed in the middle.Made in the embodiment of the present invention
Term "vertical", "horizontal", "left" and "right" and similar statement are merely for purposes of illustration, and are not intended to
The limitation present invention.
In order to which the flame device provided invention elaborates, to support the technical problems to be solved by the invention, under
Face in embodiment provided by the invention, first elaborates to the overall structure for the unmanned plane for being equipped with flame device, then
During describing unmanned plane, flame device provided by the invention is further targetedly drawn, to reach complete, clear
Chu, clear purpose.
Referring to Fig. 1, unmanned plane provided in an embodiment of the present invention, includes at least: fuselage 1, fast removable member 5 and institute of the present invention
The flame device 2 stated.
Wherein, the flame device 2 be used for flame, and by the fast removable member 5 it is detachable be fixed on the machine
On body 1, as shown in Figure 1, flame device 2 is securable to the bottom of the fuselage 1, and it is located at the underface position of the fuselage 1
Place, with this make flame device 2 and unmanned plane undercarriage or support frame fuselage 1 bottom reasonable layout, with maximize
The reasonable bottom space using fuselage 1.Certainly, as shown in Figure 1, unmanned flight's equipment choosing in the embodiment of the present invention
It is eight rotor wing unmanned aerial vehicles, but not indicates that flame device 2 provided by the embodiment of the present invention is only used for eight rotor wing unmanned aerial vehicles.Change sentence
Talk about, flame device 2 provided by the embodiment of the present invention, it can also be used to quadrotor drone, six rotor wing unmanned aerial vehicles, fixed-wing without
It is man-machine, unmanned helicopter etc., as long as can by fly by flame device 2 be transported in the air need flame remove foreign matter position into
The flight equipment of row flame operation is suitable for the present invention.
For flame device 2,
Fig. 2-4 is please referred to, the flame device 2 includes at least: ontology 21, firing device and injection equipment.Wherein, described
Ontology 21 is fixed on the fuselage 1 by the Quick-dismantle component 5.The firing device is fixed on the ontology 21.It is described
Injection equipment is fixed on the ontology 21, and connect with the firing device.And a storage is provided in the injection equipment
Space, for storing inflammable substance.What is be connected in the injection equipment with the memory space is additionally provided with a combustion zone,
So that the firing device is burst out combustion zone described in spark directive when acting, the combustion zone is flowed by the memory space to light
The inflammable substance；The inflammable substance includes one of following substances: imflammable gas (such as hydrogen, helium
Deng), flammable liquid (such as gasoline) or flammable gas-liquid mixture (such as liquefied gas).
Specifically, the ontology 21 can be the cabinet of the structure that is square, it is mainly in embodiments of the present invention
The installation of fast removable member 5, firing device and injection equipment provides fixing base, and the inside of the cabinet is in hollow structure.It is described
Cabinet includes the side of top to bottom, left and right, front and rear 6, surface therein are as follows: first side, second side, third side and
Four sides.First side described in this four sides and the second side are two opposites up and down of the cabinet, described
Third side and the 4th side are the opposite of left and right two of the cabinet, and the first side respectively with the third
Side and the 4th side adjacent distributions.Wherein, the fast removable member 5 is fixed in the first side.The ignitor
Structure and the injection equipment are fixed on other three sides of the cabinet.
Further, the firing device includes: ignition system 221, the first tank body 222 and combustion gas bar 223.Wherein, institute
It states ignition system 221 to be fixed on the ontology 21, sprays spark for firing action.First tank body 222 is fixed on institute
In the second side for stating ontology 21, for storing combustion gas.The 4th side on the ontology 21 is fixed in one end of the combustion gas bar
Face, and communicated with first tank body, it is used for transmission the combustion gas.And the other end of the combustion gas bar 223 is as fuel gas injection
End 2231 is corresponding with the spark position ejection end 2212a of the ignition system 221, i.e., so that fuel gas injection end 2231 is sprayed
Combustion gas out reaches exactly at the spark ejection end 2212a of the ignition system 221, to pass through the spark ejection end
2212 sparks sprayed light the combustion gas that the fuel gas injection end 2231 is ejected.
Wherein, the ignition system 221 may include: ignition switch 2211 and electronic wire 2212.The ignition switch
2211 are arranged in the inside of the ontology 21.The electronic wire 2212 includes electric connecting terminal and above-mentioned spark ejection end 2212a,
Namely the both ends of electric connecting terminal and spark ejection end 2212a as electronic wire 2212, and electricity described in the electronic wire 2212
Connecting pin is connect with the ignition switch 2211.Herein ignition switch 2211, electronic wire 2212 spark ejection end 2212a and
Ignition principle between the fuel gas injection end 2231 of combustion gas bar 223, it can be understood as the igniting of lighter or household gas cooker
Principle, working principle is with for the prior art, details are not described herein again.But it is applied in the embodiment of the present invention, it is logical to realize
Crossing unmanned flight's equipment is in the sky innovation place of the invention to needing flame to remove the position progress flame operation of foreign matter, herein
First offer some clarification.
It at least may include: injection system 231, the second tank for the injection equipment provided by the embodiment of the present invention
Body 232 and spray bar 233.Wherein, the injection system 231 is fixed in the ontology 21.Second tank body 231 can be managed
Solution is fixed on the third side of the ontology 21, to be memory space described in above-mentioned flame device 2 for storing oil.Institute
Stating spray bar 233 includes fixing end 2331 and oil spout end 2332, and the spray bar 233 is fixed on by the fixing end 2331
On the ontology 21；The spray bar 233 is connect by the injection system 231 with second tank body 232, by described
Injection system 231 controls second tank body 232 and transmits the oil into the spray bar 233.And the spray of the spray bar 233
Oily end 2332 is corresponding with the position at fuel gas injection end 2231 of the combustion gas bar 223.That is, spraying oil spout end 2332
Oil out reaches exactly at the fuel gas injection end 2231 lighted through the spark ejection end 2212a, to pass through the combustion lighted
Further light the oil that the oil spout end 2332 is ejected in gas jet end 2231.It should be noted that institute in the process
Spray bar 233, the electronic wire 2212 and 223 three of combustion gas bar and column distribution are stated, to reach the spark ejection end
The technical effect of the corresponding linking of 2212a, the fuel gas injection end 2231 and 2332 three of oil spout end.
Certainly, during actual job, in order to enable the imflammable gas that fuel gas injection end 2231 is ejected is (such as
Hydrogen, helium etc.) it can effectively in conjunction with air and then burn, preferably, the embodiment of the present invention is in the fuel gas injection
It holds and is additionally provided with several air inlets 2231a at 2231.Make in this way when the imflammable gas in the fuel gas injection end 2231
After ejection, due to the temporary reduction of its air pressure inside, then the air (having carrier of oxygen) around fuel gas injection end 2231 is outside
Entered in fuel gas injection end 2231 under the action of boundary's atmospheric pressure by air inlet 2231a, is sufficiently mixed quilt in turn with imflammable gas
Ejection is lighted.
In order to it is effective, easily the second tank body 232 controlled into the spray bar 233 by injection system 231
The oil is inputted, and then realizes the gas injection that the oil for reaching the oil spout end 2332 by spray bar 233 can be ignited
End 2231 is penetrated to be ignited.Preferably, the injection system 231 includes at least: power supply source 2311, controller 2312, voltage-stablizer
2313, pipeline switch 2314.Wherein, the power supply source 2311 is fixed in the cabinet of the ontology 21.The controller 2313
It is fixed in the cabinet of the ontology 21.The voltage-stablizer 2313 is fixed in the cabinet of the ontology 21, and the power supply source
2311 are connect with the controller 2312 and the firing device (ignition switch 2211) respectively by the voltage-stablizer 2313, with
It is powered in real time to each component in the controller 2312 and the firing device.Meanwhile the pipeline switch 2314 is solid
Due in the cabinet of the ontology 21, and the pipeline switch 2314 is connect with the controller 2312, and respectively with described
2332 pipeline of the fixing end of two tank bodies 232 and the spray bar 233 communicates.It can thus to work as and need by second
When tank body 232 transmits oil into spray bar 233, controlling the pipeline switch 2314 by controller 2312 at this time is opening state
State, and then the channel status between second tank body 232 and the spray bar 233 is formed, realize the transmission of oil.And working as needs
It when stopping oil spout, only needs controller 2312 to control the pipeline switch 2314 at this time and is in off state, cut off described with this
Channel status between two tank bodies 232 and the spray bar 233.
Certainly, it for controller 2312 described in the embodiment of the present invention, can also be controlled with the flight inside unmanned plane
System connection, and by the information communication between flight control system and earth station, realize ground handling operator to controller
2312 long-range control has been existing for the flight control system inside unmanned plane and the transmission control of the instruction between earth station
Technology is not described in more detail here.It is emphasized that the embodiment of the present invention can also be in ignition system 221, with injection system 231
It is identical, can also add one group for can only intelligent control ignition switch igniting device, may include a control single chip computer and
One valve, the control single chip computer are connect with the ignition switch 2211 and the controller 2312 respectively, the valve setting
It is connect between the combustion gas bar 223 and first tank body 222, and with the control single chip computer.Likewise, the behaviour of earth station
Make personnel by carrying out instruction transmission with the flight control system inside unmanned plane, and then remotely control the controller 2312,
And control instruction is sent to the control single chip computer by the controller, to control the igniting of ignition switch 2211 operation,
And the valve is switched on or off state.It is finally reached the technical effect of long-distance intelligent control.Specifically, work as needs
When transmitting combustion gas into combustion gas bar 223 by the first tank body 222, controlling the valve by control single chip computer at this time is opening state
State, and then the channel status between first tank body 222 and the combustion gas bar 223 is formed, realize the transmission of combustion gas.And when combustion
After the oil drop combustion that the flame that gas jet end 2231 sprays is sprayed the spray bar 233, the controller can be passed through at this time
2312 send the instruction for closing valve to the control single chip computer, and then control the valve by the control single chip computer and close
It closes, to cut off the transmission line between first tank body 222 and the combustion gas bar 223, stops fuel gas injection.
It is noted that for controller, control single chip computer, ignition switch, pipeline switch, valve and flight control system
Signal transmission, instruction control between system have been the prior art, i.e., send a control to the flight control system by earth station
System instruction, and control instruction is transmitted to by the controller by the flight control system, to pass through the controller to institute
Received control instruction makes corresponding response, then makes operation to control single chip computer, pipeline switch, ignition switch, valve etc.
Its control principle with for the prior art, but is applied to flame device 2 described in the embodiment of the present invention by control, further will spray
Fiery device be applied to unmanned flight's equipment, with realize by unmanned flight's equipment in the sky to need flame remove foreign matter position into
Row flame operation is innovation place of the invention, is first offered some clarification herein.
Further, for electronic wire 2212 involved in the ignition system 221 in the embodiment of the present invention, due to
Itself light weight is easy to be blown and swung by extraneous wind-force in the flight course of unmanned plane, then causes electronic wire
2212 spark ejection end 2212a corresponding can not be connected with the spatial position at the fuel gas injection end 2231 of combustion gas bar 223, Jin Erying
Ring ignition results.In this regard, the embodiment of the present invention also has additional positioning piece 3, the locating piece 3 is fixed on the spark ejection end
2212a, and be flexibly connected the electronic wire 2212 with the combustion gas bar 223 by the locating piece 3.Activity herein is even
It connects and can be understood as detachable connection between the two.Locating piece 3 can be it is diversified, such as can be with screw or spiral shell
The collocation of bolt and nut uses, and is also possible to pin shaft, fixed pin is applied in combination to the spark ejection end 2212a in the combustion
It is positioned, directly spark ejection end 2212a can also be wound on combustion gas bar 223 with thin wire on gas bar 223.It changes
Sentence is talked about, as long as can be fixed on the spark ejection end 2212a of the electronic wire of lighter weight is stable on combustion gas bar 223,
And make the locating piece 3 at the fuel gas injection end 2231 of combustion gas bar 223 and the corresponding linking in position of spark ejection end 2212a, then
It is within the scope of the present invention.
You need to add is that for spray bar 233, in order to avoid spray bar 233 is made since quality is relatively light
At applied defect same as above-mentioned electronic wire 2212, i.e., it is easy to be blown by extraneous wind-force in the flight course of unmanned plane
And swing, the oil spout end 2332 at the fuel gas injection end 2231 and spray bar 233 that then lead to combustion gas bar 223 on spatial position not
Linking can accurately be corresponded to.Therefore, at the oil spout end 2332 of spray bar 233, it can also be fixed on an above-mentioned locating piece, i.e.,
The electronic wire 2212 is flexibly connected with the spray bar 233 by the locating piece 3.Flexible connection herein can be managed
It solves to be detachable connection between the two.Locating piece 3 equally can be it is diversified, such as can with screw or bolt with
The collocation of nut uses, and is also possible to pin shaft, fixed pin is applied in combination to the oil spout end 2332 on the combustion gas bar 223
It is positioned, directly oil spout end 2332 can also be wound on combustion gas bar 223 with thin wire.In other words, as long as energy
Enough oil spout ends 2332 by the spray bar 233 of lighter weight are stable to be fixed on combustion gas bar 223, and makes combustion gas bar 223
The locating piece 3 of the corresponding linking in the position at fuel gas injection end 2231 and oil spout end 2332, then protection scope of the present invention it
It is interior.
And then, since combustion gas bar 223 is as above-mentioned electronic wire 2212 and/or the load-carrying support rod of spray bar 233,
In order to avoid combustion gas bar 223 occurs bending or even falls off because load-carrying is excessive.Preferably, also being had additional in the embodiment of the present invention
One support component 4, the support component 4 may include a movable end and a support end, and the support component 4 passes through the work
Moved end and the 4th side of the ontology 21 are rotatablely connected, and the support component 4 passes through the support end and the combustion gas bar 223
Intermediate position be fixedly connected close to the one end at fuel gas injection end 2231.
Specifically, Fig. 5 and Fig. 6 are please referred to, the support component 4 includes at least: support rod 41, rotary part 42 and fixed
Position component 43.Wherein, one end of the support rod 41 is rotated by the 4th side of the rotary part 42 and the ontology 21
Connection.The other end of the support rod is fixedly connected by the positioning element 43 with the combustion gas bar 223.It is to be understood that
What one end of the rotary part 42 and the support rod 41 was constituted is the movable end of above-mentioned support component 4, the positioning region
What the other end of part 43 and the support rod 41 was constituted is the support end of above-mentioned support component 4.
Wherein, the rotary part 42 at least may include: T-type sleeve 421 and support base 422.The T-type sleeve
421 include T-type end 4211 and transverse end 4212.The support base 422 is fixed on the 4th side of the ontology 21, and institute
It states T-type sleeve 421 to be rotationally fixed in the support base 422 by the transverse end 4212, so that the T-type sleeve
421 is rotatable relative to the support base 422.One end of the support rod 41 is set on the T-type end 4211, by institute
Support rod 41 is stated to be fixedly connected with the T-type sleeve 421.
The support base 422 may include: the first pedestal 4221 and the second pedestal 4222.Wherein, first pedestal
4221 are fixed on the 4th side of the ontology 21, and offer the first circular groove on first pedestal 4221.Described second
Pedestal 4222 is fixed on the 4th side of the ontology 21, and offers the second circular groove on second pedestal 4222.Wherein,
The transverse end 4212 of the T-type sleeve 421 can be understood as a hollow cylindrical structure, and the external world of the hollow cylinder with
The internal diameter of first circular groove and second circular groove is adapted, and the both ends for allowing for the transverse end 4212 in this way respectively correspond
Pass through first circular groove and second circular groove, the transverse end 4212 is rotationally fixed to first pedestal
Between 4221 and second pedestal 4222.
It in embodiments of the present invention can be exactly that two independent circular grooves are whole for the first circular groove and the second circular groove
That is, during the installation process body directly penetrates one end of transverse end 4212 in first circular groove, by transverse end 4212 after penetrating
The other end penetrate in second circular groove, realize that transverse end 4212 is rotationally fixed to the first pedestal 4221 and second with this
On body 4222.Certainly, in order to enable the rotation connection between transverse end 4212 and the first pedestal 4221 and the second pedestal 4222 is clever
It is living, detachable.If for the first pedestal 4221 and the second pedestal 4222 moreover, it is also possible to be the assembling of dismountable dry part and
At.
Specifically, first pedestal 4221 at least may include: first semifixed piece of 4221a, and second semifixed piece
4221b and several first fixing screws 4221c.Wherein, first semifixed piece of 4221a is fixed on the ontology 21
On 4th side, and the first half slot is offered on first semifixed piece of 4221a.On second semifixed piece of 4221b
Offer the second half slot.And first semifixed piece of 4221a and second semifixed piece of 4221b are interlocked, and are made with this
First half slot and second half slot linking are obtained to constitute first circular groove；Several described first fixing screws
4221c passes through second semifixed piece of 4221b, is threadedly coupled with first semifixed piece of 4221a.
Likewise, second pedestal 4222 at least may include: semifixed piece of 4222a of third, the 4th semifixed piece
4222b and several second fixing screws 4222c.Wherein, semifixed piece of 4222a of the third is fixed on the ontology 21
On 4th side, and third half slot is offered on semifixed piece of 4222a of the third.On the four semifixed pieces 4222b
Offer the 4th half slot.And described semifixed piece of 4222a of third and the four semifixed pieces 4222b is interlocked, and is made with this
The third half slot and the 4th half slot linking are obtained to constitute second circular groove；Several described second fixing screws
4222c passes through the four semifixed pieces 4222b, is threadedly coupled with semifixed piece of 4222a of the third.
It can thus make, when installing T-type sleeve 421, first put at the both ends of transverse end 4212 with being corresponding in turn to
Set the first half slot of first semifixed piece of 4221a, semifixed piece of 4222a of third third half slot on, after the completion of placement,
Second semifixed piece of 4221b and the four semifixed pieces 4222b are accordingly directly fastened on first semifixed piece of 4221a and third
On semifixed piece of 4222a, make that the first semicircle is wiped and the second half slot forms first circular groove with this, third half slot and the
Four half slots form second circular groove.It is finally directly that the first fixing screws 4221c and the second fixing screws 4222c is corresponding slotting
Enter locking.The detachable installation between T-type sleeve 421 and support base 422 is thereby realized, so that working as T-type set
When 421 appearance abrasion of cylinder need to substitute, directly dismantling the first fixing screws 4221c and the second fixing screws 4222c be can be completed more
For disassembly.Preferably, the quantity of the second fixing screws 4221c and the second fixing screws 4222c can respectively be 2.
It needs exist for, it is emphasized why passing through T-type sleeve 421 in embodiments of the present invention makes the T-type sleeve
It is rotatable between 421 and support base 422, it is to realize the angle between support rod 41 and the 4th side of the ontology 21
Angle adjustable.Because during actual job, the sagging angle according to job requirements and combustion gas bar 223 is needed, to adjust
Angle of the support rod 41 relative to the 4th side of ontology 21, to complete its suspension strut to combustion gas bar 223, to reach flexible behaviour
The purpose of work has the characteristics that structure is simple, applicable performance is wide.
Further, the positioning element 43 at least may include: a positioning snap ring, one end setting of the positioning snap ring
There is the first positioning ring, the other end of the positioning snap ring is provided with the second positioning ring；And the other end of the support rod 41 passes through
First positioning ring is fixedly connected with the positioning snap ring, the combustion gas bar 223 pass through second positioning ring with it is described fixed
Position snap ring is fixedly connected.Support rod 41 and the combustion gas bar 223 are realized by the first positioning ring and the second positioning ring with this
Between suspension be located by connecting.
It in embodiments of the present invention can be exactly two independent ring-types for the first positioning ring and the second positioning ring
That is, during the installation process structure directly penetrates one end of support rod 41 in first positioning ring, combustion gas bar 223 is directly worn
Enter in the second positioning ring, and due to being fixedly connected with relationship there are one between the first positioning ring and the second positioning ring, then allow for
There is also a suspension fixed relationship between the support rod 41 and the combustion gas bar 223, the final suspension for realizing combustion gas bar 223 is fixed
Position.Certainly, in order to enable being fixedly connected with connection between support rod 41 and the first positioning ring, combustion gas bar 223 and the second positioning ring
Flexibly, detachably.For positioning snap ring, if can also be, dismountable dry part assembles.
Specifically, the positioning snap ring at least may include: the first half positioning snap rings 431, the second half positioning snap rings 432
With third fixing screws 433.Wherein, one end of the first half positioning snap ring 431 is provided with the first half circle groove, and described the first half
The other end of positioning snap ring 431 is provided with the second half circle groove.One end of the second half positioning snap ring 432 is provided with third semi-ring
The other end of slot, the described second fixed half positioning snap ring 432 is provided with the 4th half circle groove.Wherein, first half circle groove and described
The corresponding linking of third half circle groove constitutes first positioning ring, second half circle groove and the corresponding linking structure of the 4th half circle groove
At second positioning ring；And the third fixing screws pass through the first half positioning snap ring 431 (or second semidefinite
Position snap ring 432), it is threadedly coupled with the second half positioning snap ring 432 (or described the first half positioning snap ring 431).
Here it is worth noting that constituting described first by first half circle groove and the corresponding linking of the third half circle groove
The internal diameter of positioning ring is less than the outer diameter of the support rod 41；Second half circle groove and the corresponding linking of the 4th half circle groove are constituted
The internal diameter of second positioning ring is less than the outer diameter of the combustion gas bar 223.This is because in actual installation process, the first semidefinite
Position snap ring 431 and the second half positioning snap rings 432 are disassembly status in advance, at this time that support rod 41 and/or combustion gas bar 223 is corresponding
It is placed at the first half circle groove and the second semi-ring groove location of the first half positioning snap rings 431, then fastens the second half positioning snap rings
432, make first half circle groove and the third half circle groove be constituted first positioning ring with this, second half circle groove and
4th half circle groove constitutes second positioning ring.Just because of first half circle groove and the corresponding rank of the third half circle groove
It connects and constitutes outer diameter of the internal diameter of first positioning ring less than the support rod 41；Second half circle groove and the 4th semi-ring
The internal diameter that the corresponding linking of slot constitutes second positioning ring is less than the outer diameter of the combustion gas bar 223, thus makes by tightening the
Three fixing screws 433 can constantly reduce the vertical range between the first half positioning snap rings 431 and the second half positioning snap rings 432,
The two is fixed with this.Support rod 41 and combustion gas bar 223 are carried out the fixed purpose of suspension by final realize.
For fast removable member 5,
Please refer to Fig. 7-12, wherein the fast removable member 5 includes at least: fixed plate 51 and positioning element 52.
Wherein, the fixed plate 51 is fixed on the fuselage 1, and is slidably connected with the ontology 21, so that described
Body 21 is slided relative to the fixed plate 51, and since fixed plate 51 is fixed relative to fuselage 1, and then realize 21 phase of ontology
Fuselage 1 is slided.Certainly, between fixed plate 51 and the fuselage 1 be fixedly connected mode can be it is diversified,
It such as can be and be bolted, can be screw connection, can be welding, be also possible to be integrally formed, in this embodiment of the present invention
With no restrictions, as long as can be realized fixed plate 51 is fixed on the fuselage 1.The positioning element 52 is fixed on the fixation
It on plate 51, is positioned with the position to the ontology 21 relative to the fixed plate 51, and then realizes that the ontology 21 is opposite
It installs or dismantles in the fuselage.
Herein, positioning element 52 is equivalent to a detent component, when needing for ontology 21 to be installed on fuselage 1, this
A certain position is slid into relative to fixed plate 51 between Shi Benti 21 and fixed plate 51, then by positioning element 52 to the position
Ontology 21 positioned, with prevent ontology 21 relative to fixed plate 51 slide.And when needing to remove ontology 21, it only needs at this time
Manual toggle positioning element 52, allow ontology 21 skidded off relative to fixed plate 51, can be realized ontology 21 it is quick, flexibly tear open
It unloads.During this, the installation and removal of ontology 21 are easy to operate without any extraneous utensil such as spanner etc., have quickly,
Convenient feature.
In embodiments of the present invention, preferably, please continue to refer to Fig. 7-8, it is U-shaped that the fixed plate 42 can be section
Shape, the fixed plate 42 under the shape at least may include: the first side plate 511；Second side plate 512 and transverse slat 513.
Wherein, first side plate 511 and second side plate 512 are parallel；And first side plate 511 and described
Two side plates 512 and the transverse slat 513 are perpendicular, and the transverse slat 513 respectively with first side plate 511 and second side plate
512 are slidably connected, and the ontology 21 is fixedly connected with the transverse slat 513, and then make the ontology 21 by the transverse slat 513
It is slided relative to first side plate 511 and second side plate 512.Meanwhile the positioning element 41 is individually fixed in
On first side plate 511 and second side plate 512, with to the transverse slat 513 relative to first side plate 511 and described
The position of second side plate 512 is positioned.Certainly, between first side plate 511, second side plate 512 and the fuselage 1
Be fixedly connected mode can be it is diversified, such as can be bolted, can be screw connection, can be welding,
Can be integrated molding, this embodiment of the present invention with no restrictions, as long as can be realized first side plate 511, described second
Side plate 512 is fixed on the fuselage 1.
Same principle, between the ontology 21 and the transverse slat 513 be fixedly connected mode be also possible to it is varied
, it such as can be and be bolted, can be screw connection, can be welding, be also possible to be integrally formed, the present invention is implemented herein
Example with no restrictions, as long as can be realized the ontology 21 and the transverse slat 513 is relatively fixed, protection scope of the present invention it
It is interior.
It further, is the transverse slat 513 convenient for being fixed with ontology 21, it can be with the first side plate 511,512 spirit of the second side plate
Living, quickly sliding, in order to which ontology 21 is flexible, quickly installation or disassembly.A kind of implementation as the embodiment of the present invention
It is respectively arranged with a sliding slot on mode, first side plate 511 and second side plate 512, the transverse slat 513 setting is existed
In the sliding slot, so that the transverse slat 513 is by the sliding slot relative to first side plate 511 and second side plate 512
It is slided.
Meanwhile one end of the positioning element 52 is corresponding across first side plate 511, second side plate 512, and
In the sliding slot internal projection or contraction, so that one end of the positioning element 52 is relative to the sliding slot in the sliding slot convex
When rising, one end of the positioning element 52 stops the transverse slat 513 to be slided in the sliding slot, the positioning element 52
Relative to the sliding slot in the sliding slot contract, one end of the positioning element 52 is separated with 513 phase of transverse slat for one end,
So that the transverse slat 513 is slided in the sliding slot.
What needs to be explained here is that in embodiments of the present invention, it is described " protrusion ", it can be understood as to be a component
It slides into some component, " contraction " can be understood as a component and skid off some component.For example, described above is described
One end of positioning element 52 in the sliding slot internal projection, that is, refers to that one end of the positioning element 52 slides into relative to the sliding slot
In the sliding slot, one end of positioning element 52 described above relative to the sliding slot in the sliding slot contract, that is, refer to described in
One end of positioning element 52 skids off the sliding slot.Disassembly of the ontology 21 relative to fuselage 1 is realized by positioning element 52 with this
Or installation.
For the positioning element 52, in embodiments of the present invention, as a kind of implementation of the present embodiment, institute
Stating positioning element 52 can include at least: the first positioning plunger and the second positioning plunger.And the first positioning plunger packet
Include the first positioning end；The second positioning plunger includes the second positioning end.
Wherein, first positioning end is corresponding passes through first side plate, and the sliding slot in first side plate 511
Internal projection or contraction, so that first positioning end is when relative to sliding slot internal projection in first side plate 511, it is described
First positioning end stops the transverse slat 513 to be slided in sliding slot, and first positioning end is relative to first side plate
When sliding slot contract in 511, first positioning end is separated with 513 phase of transverse slat, so that the transverse slat 513 is in sliding slot
It is slided.Wherein, second positioning end is corresponding passes through second side plate 512, and in second side plate 512
Sliding slot internal projection or contraction, so that second positioning end is when relative to sliding slot internal projection in second side plate 512,
Second positioning end stops the transverse slat 513 to be slided in sliding slot, and second positioning end is relative to described second
When sliding slot contract in side plate 512, second positioning end is mutually separated with the transverse slat, so that the transverse slat 513 is in sliding slot
Inside slided.
It herein, can be as shown in Fig. 7 or Fig. 8, it can be understood as the first side plate 511 and the second side plate 512 are symmetrical
The two sides of the transverse slat 513 are distributed in, allow for being inserted into first side plate while two sides of the transverse slat 513 correspond in this way
511 and second side plate 512 sliding slot that is opened up in, realize the transverse slat 513 for being fixed with ontology 21 relative to first with this
Side plate 511 and the second side plate 512 are slided.Meanwhile in order to preferably be positioned to the transverse slat 513 in sliding process.This
Inventive embodiments by first positioning plunger and second positioning plunger, be symmetrically arranged in the two sides of transverse slat 513 namely first
It is corresponding with the first side plate 511 to position plunger, the second positioning plunger is corresponding with the second side plate 512.It should be noted that at this
In inventive embodiments, the first side plate 511 identical can also be different with the structure of the second side plate 512, the first positioning column
Plug identical can also be different with the second positioning plunger.And in embodiments of the present invention, it is for convenience of description, selected
First side plate 511 is identical with 512 structure of the second side plate, the complete phase of structure of the first positioning plunger and the second positioning plunger
Together.
Certainly, it will be understood by those skilled in the art that the first side plate 511 and the second side plate 512, first positioning plunger and the
Two positioning plungers are also possible to mutually different various structures, and such as the first side plate 511 can be square structure, the second side plate
512 can be rectangle structure perhaps the first side plate 511 can be the second side plate of trapezium structure 512 can be square or
The polygonized structures such as rectangle or diamond shape.In other words, if be that by the first side plate 511 and the second side plate 512 with
Fuselage 1 is relatively fixed, and transverse slat 513 can with the first side plate 511 of the first side plate 511 and the opposite sliding of the second side plate 512 and
Second side plate, 512 structure, it is within the scope of the present invention.Likewise, the first positioning plunger and the second positioning plunger
It can be a variety of different structures, as long as can satisfy the first positioning plunger corresponding can pass through the first side plate 511, second is fixed
Position plunger corresponding can pass through the second side plate 512, and carry out protrusion or flexible in its each comfortable corresponding sliding slot, to cross
Plate 513, which is limited, to the greatest extent may be used.Whether the planform for being placed in the first positioning plunger and the second positioning plunger is identical, the present invention
Embodiment does not further limit.
Please continue to refer to Fig. 9-12, as stated above, a kind of embodiment as the embodiment of the present invention, it is assumed that at this
The first selected positioning plunger and the second positioning plunger are completely identical in structure in inventive embodiments, shown in Fig. 9-12
For first positioning plunger 521, to be described in further detail to the internal structure of positioning plunger.
Such as Fig. 9-12, the first positioning plunger 521 includes: the first positioning bolt 5211, the first positioning thread insert 5212, the
One retaining spring 5213.
Wherein, first positioning bolt 5211 is provided with the first positioning end 5211a；First positioning thread insert
5212 are set on first positioning bolt 5211, and first positioning thread insert 5212 and first positioning bolt 5211
Between be provided with one first compression space 5214.It can be understood as first positioning thread insert 5212 in embodiments of the present invention
Internal diameter is greater than the outer diameter of first positioning bolt 5211, and allowing for the first positioning thread insert 5212 in this way, to be set in described first fixed
When on the bolt 5211 of position, there is neutral gear region therebetween, this neutral gear region is above-mentioned first compression space 5214.It is described
First retaining spring is set in first compression space 5214；Wherein, the first positioning end 5211a sequentially passes through described
First retaining spring 5213, first compression space 5214 and first side plate 511, in first side plate 511
Sliding slot internal projection or contraction.
It is noted that being the first positioning end 5211a shown in Fig. 9-10 in the sliding slot in first side plate 511
Schematic diagram when contraction state.It is the first positioning end 5211a shown in Figure 11-12 in the sliding slot in first side plate 511
Schematic diagram when raised position.And in order to preferably by the first retaining spring 5213 completely now in the first compression space
In 5214, on the first positioning end 5211a of the first positioning bolt 5211 described in the embodiment of the present invention, it is provided with one first
First retaining spring 5213 is fully defined in first compression space 5214 by card convex 5215, and is made described
First positioning end 5211a passes through first card convex 5215 and presses when relative to sliding slot contract in first side plate 511
Contract first retaining spring 5213.
Specifically, for the embodiment of the present invention during actual job, the first retaining spring 5213 is in the first compression space
In 5214, whole process allows in its natural state in this way in compression or pre-compressed state, and the first retaining spring 5213 is the
The first positioning end 5211a is pushed to enter institute by the first side plate 511 by the elasticity tension of itself in one compression space 5214
In the sliding slot for stating the first side plate 511, and then the transverse slat 513 in sliding slot is positioned.And works as and need transverse slat 513 from cunning
When skidding off in slot, namely when needing to dismantle ontology 21 from fuselage 1, the first positioning bolt of manual toggle is only needed at this time
5211, so that the first positioning end 5211a compresses the first retaining spring 5213 by the first card convex 5215, then make the first positioning
End 5211a is skidded off out of the first side plate 511 sliding slot, and then realizes skidding off relative to the first side plate 511 for transverse slat 513.And work as
Without external force after the first positioning bolt 5211, under the elasticity tension effect of the first retaining spring 5213, the is continued to press on
One positioning end 5211a carries out the working condition of the first positioning plunger 521 shown in return namely Figure 11 or Figure 11.Effectively
The installation and removal of ontology 21 are realized without any extraneous utensil such as spanner etc., it is easy to operate, have quickly, easily
Feature.
In embodiments of the present invention, the second positioning plunger includes: the second positioning bolt, and second positioning bolt is set
It is equipped with second positioning end；Second positioning thread insert, second positioning thread insert is set on second positioning bolt, and institute
It states and is provided with one second compression space between the second positioning thread insert and second positioning bolt；Second retaining spring, described
Two retaining springs are set in second compression space；Wherein, second positioning end sequentially passes through the second positioning bullet
Spring, second compression space and second side plate, with the sliding slot internal projection or contraction in second side plate.It is described
On second positioning end of second positioning bolt, it is provided with one second card convex, second retaining spring is limited to institute
It states in the second compression space, and makes second positioning end when relative to sliding slot contract in second side plate, lead to
It crosses second card convex and compresses second retaining spring.
As described above, the second positioning plunger in the embodiment of the present invention and the first positioning plunger 521 shown in Fig. 9-12
Structure is identical, no longer repeats herein the internal structure of the second positioning plunger, for the inside of the second positioning plunger
The non-detailed portion of structure sees the detailed portion of the first positioning plunger 521 in the embodiment of the present invention.
In conclusion a kind of flame device applied to unmanned plane provided by the invention, winged at nobody by fast removable member
On the fuselage of row equipment such as unmanned plane, detachable fixes a flame device, so that passing through unmanned plane during actual job
Flight by flame device be transported in the air need flame remove foreign matter position carry out flame operation, have it is convenient and efficient and pacify
The high feature of full performance, solves in the prior art when being hung with foreign matter on the high empty body such as power transmission line, due to suspension height
It is higher, using combustion method removal foreign matter when flame projector apart from operator farther out, to foreign matter removing bring it is unhandy
Technological deficiency.
Although preferred embodiments of the present invention have been described, it is created once a person skilled in the art knows basic
Property concept, then additional changes and modifications may be made to these embodiments.So it includes excellent that the following claims are intended to be interpreted as
It selects embodiment and falls into all change and modification of the scope of the invention.
Obviously, various changes and modifications can be made to the invention without departing from essence of the invention by those skilled in the art
Mind and range.In this way, if these modifications and changes of the present invention belongs to the range of the claims in the present invention and its equivalent technologies
Within, then the present invention is also intended to include these modifications and variations.
Claims (9)
1. a kind of flame device applied to unmanned plane, which is characterized in that the flame device includes:
Ontology, the ontology are fixed on the fuselage of the unmanned plane；
Firing device, the firing device are fixed on the ontology；
Injection equipment, the injection equipment are fixed on the ontology, and are connect with the firing device；
Wherein, it is provided with a memory space in the injection equipment, for storing inflammable substance；And in the injection equipment with
What the memory space was connected is additionally provided with a combustion zone, and the firing device is made to burst out burning described in spark directive when acting
Area, to light the inflammable substance for flowing into the combustion zone by the memory space；
The firing device includes:
Ignition system, the ignition system are fixed on the ontology, spray spark for firing action；
First tank body, first tank body is fixed on the ontology, for storing combustion gas；
Combustion gas bar, the combustion gas bar are fixed on the ontology, and are communicated with first tank body, and the combustion gas is used for transmission；
Wherein, the fuel gas injection end of the combustion gas bar is corresponding with the spark of ignition system injection end position, to pass through
It states spark ejection end and carries out spark injection at the fuel gas injection end.
2. being applied to the flame device of unmanned plane as described in claim 1, which is characterized in that the ignition system includes:
The inside of the ontology is arranged in ignition switch, the ignition switch；
Electronic wire, the electronic wire include electric connecting terminal and the spark ejection end, and the electric connecting terminal and the point
Fire switch connection.
3. being applied to the flame device of unmanned plane as claimed in claim 2, which is characterized in that the injection equipment includes:
Injection system, the injection system are fixed in the ontology；
Second tank body, second tank body is fixed on the ontology, for storing oil；
Spray bar, the spray bar include fixing end and oil spout end, and the spray bar be fixed on by the fixing end it is described
On ontology；The spray bar is connect by the injection system with second tank body, to control institute by the injection system
It states the second tank body and transmits the oil into the spray bar.
4. being applied to the flame device of unmanned plane as claimed in claim 3, it is characterised in that:
The oil spout end is corresponding with the position at the fuel gas injection end.
5. the flame device applied to unmanned plane as described in claim 3 or 4, it is characterised in that:
The spray bar, the electronic wire and the combustion gas bar three and column distribution, and the spark ejection end, the combustion gas
Ejection end and the corresponding linking of the oil spout end three.
6. being applied to the flame device of unmanned plane as claimed in claim 3, which is characterized in that the injection system includes:
Power supply source, the power supply source are fixed in the ontology；
Controller, the controller are fixed in the ontology；
Voltage-stablizer, the voltage-stablizer are fixed in the ontology, and the power supply source by the voltage-stablizer respectively with the control
Device processed is connected with the firing device, to the controller and firing device power supply；
Pipeline switch, the pipeline switch are fixed in the ontology, and the pipeline switch is connect with the controller, and point
It is not communicated with the fixing end pipeline of second tank body and the spray bar.
7. being applied to the flame device of unmanned plane as described in claim 1, which is characterized in that
The fuel gas injection end is provided with several air inlets.
8. the flame device applied to unmanned plane as described in claim 3 or 4, which is characterized in that further include:
Locating piece, the locating piece are fixed on the spark ejection end, and pass through the locating piece for the electronic wire and institute
State spray bar flexible connection.
9. being applied to the flame device of unmanned plane as claimed in claim 6, which is characterized in that the ontology is square structure
Cabinet；And
The cabinet includes: first side, second side, third side and the 4th side；The first side and described second
Side is two opposites of the cabinet, and the third side and the 4th side are two opposites of the cabinet,
The first side respectively with the third side and the 4th side adjacent distributions；
Wherein, the power supply source, the controller, the voltage-stablizer, the pipeline switch and the ignition switch are placed in institute
It states in cabinet；The fuselage is fixed in the first side, and first tank body is fixed in the second side, and described
Two tank bodies are fixed on the third side, and the spray bar is fixed on the 4th side by the fixing end.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610727329.7A CN106152123B (en) | 2016-08-25 | 2016-08-25 | Flame device applied to unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610727329.7A CN106152123B (en) | 2016-08-25 | 2016-08-25 | Flame device applied to unmanned plane |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106152123A CN106152123A (en) | 2016-11-23 |
| CN106152123B true CN106152123B (en) | 2018-12-18 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610727329.7A Expired - Fee Related CN106152123B (en) | 2016-08-25 | 2016-08-25 | Flame device applied to unmanned plane |
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| Country | Link |
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| CN (1) | CN106152123B (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108488798A (en) * | 2018-04-25 | 2018-09-04 | 厦门南羽科技有限公司 | Flaming system and unmanned plane |
| CN115739848B (en) * | 2022-11-28 | 2024-01-12 | 国网黑龙江省电力有限公司超高压公司 | Unmanned aerial vehicle-mounted high-voltage transmission line obstacle remover and obstacle removing method |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105314111A (en) * | 2014-06-27 | 2016-02-10 | 周彦辉 | Large-size high-speed invisible flying saucer |
| CN205489261U (en) * | 2016-01-13 | 2016-08-17 | 昆山市工业技术研究院有限责任公司 | High altitude flame projecting robot that removes obstacles |
| CN206001457U (en) * | 2016-08-25 | 2017-03-08 | 易瓦特科技股份公司 | It is applied to the flame device of unmanned plane |
| CN206250675U (en) * | 2016-12-20 | 2017-06-13 | 北方天途无人机科技成都有限公司 | Flame is removed obstacles unmanned plane |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9334051B2 (en) * | 2014-02-28 | 2016-05-10 | Siemens Industry, Inc. | Apparatus for servicing a detector of a fire safety system |
-
2016
- 2016-08-25 CN CN201610727329.7A patent/CN106152123B/en not_active Expired - Fee Related
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105314111A (en) * | 2014-06-27 | 2016-02-10 | 周彦辉 | Large-size high-speed invisible flying saucer |
| CN205489261U (en) * | 2016-01-13 | 2016-08-17 | 昆山市工业技术研究院有限责任公司 | High altitude flame projecting robot that removes obstacles |
| CN206001457U (en) * | 2016-08-25 | 2017-03-08 | 易瓦特科技股份公司 | It is applied to the flame device of unmanned plane |
| CN206250675U (en) * | 2016-12-20 | 2017-06-13 | 北方天途无人机科技成都有限公司 | Flame is removed obstacles unmanned plane |
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|---|---|
| CN106152123A (en) | 2016-11-23 |
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