CN106767186A - It is used to realize aircraft, system, method and the supporting fireworks of firework display function - Google Patents
It is used to realize aircraft, system, method and the supporting fireworks of firework display function Download PDFInfo
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- CN106767186A CN106767186A CN201710001256.8A CN201710001256A CN106767186A CN 106767186 A CN106767186 A CN 106767186A CN 201710001256 A CN201710001256 A CN 201710001256A CN 106767186 A CN106767186 A CN 106767186A
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- firework display
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- 238000000034 method Methods 0.000 title claims abstract description 19
- 230000000694 effects Effects 0.000 claims abstract description 16
- 238000005422 blasting Methods 0.000 claims description 63
- 238000006073 displacement reaction Methods 0.000 claims description 4
- 239000007921 spray Substances 0.000 claims description 4
- 238000004891 communication Methods 0.000 claims description 3
- 230000000007 visual effect Effects 0.000 abstract description 3
- 238000010586 diagram Methods 0.000 description 5
- 235000019504 cigarettes Nutrition 0.000 description 4
- 238000010276 construction Methods 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 3
- 238000012986 modification Methods 0.000 description 3
- 230000004048 modification Effects 0.000 description 3
- 238000003032 molecular docking Methods 0.000 description 2
- 238000004458 analytical method Methods 0.000 description 1
- 238000010009 beating Methods 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 239000013536 elastomeric material Substances 0.000 description 1
- 230000004438 eyesight Effects 0.000 description 1
- 238000010030 laminating 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
- 239000000575 pesticide Substances 0.000 description 1
- 239000000779 smoke Substances 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
- 239000000725 suspension Substances 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B4/00—Fireworks, i.e. pyrotechnic devices for amusement, display, illumination or signal purposes
-
- 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
- B64D1/04—Dropping, ejecting, or releasing articles the articles being explosive, e.g. bombs
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Illuminated Signs And Luminous Advertising (AREA)
Abstract
It is used to realize the aircraft of firework display function, system, method and supporting fireworks the invention provides a kind of, belongs to aircraft field.It is provided with putting the receiving chamber of fireworks on the aircraft for being used to realize firework display function that the present invention is provided, and is provided with the unit of lighting set off fireworks, and the outlet of setting off of correspondence fireworks at least includes upwardly direction.The scheme that the present invention is provided, its good effect is：Fireworks are put using unmanned vehicle, it will bring more convenient and distinguished visual experiences.
Description
Technical field
The invention belongs to unmanned vehicle field.
Background technology
Unmanned vehicle abbreviation unmanned plane, is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned vehicle.Because it has the advantages that small volume, low cost, easy to use, the favor of countries in the world is enjoyed, it is wide
It is general to apply in military field.At the same time, unmanned vehicle is also non-in the technique effect and economic effect of civilian aspect
Often it is expected, the range of application of civilian unmanned vehicle is all actively being expanded in current countries in the world, is mainly reflected in map
The side such as mapping, geological exploration, disaster monitoring, meteorological detection, air traffic control, border control, communication relay, pesticide spraying
Face.Additionally, unmanned vehicle is in film and television play shooting, logistics express delivery, food and drink food delivery, insurance survey, police execution etc.
Use in work and life is also shown in without cease repeatly.Be referred to as " air-robot " unmanned vehicle gradually entering into it is general
The logical lives of the people, are applied to the various aspects of production and living.
When happiness, such as National Day, wedding celebration, New Year, opening ceremony etc. occasion often puts fireworks to people, if
Fireworks can be put using unmanned vehicle, it is believed that will bring more convenient and distinguished visions
Experience.
The content of the invention
It is an object of the invention to：A kind of aircraft for being used to realize firework display function of offer, and corresponding system,
Method and supporting fireworks, are used to discharge fireworks by aircraft.
To realize above-mentioned target, the invention provides following technical scheme：
The invention provides a kind of aircraft for being used to realize firework display function, it is provided with putting on board the aircraft
The receiving chamber of fireworks, and be provided with to set off fireworks light unit, the spout of the fireworks being positioned in receiving chamber is upward
Set.
Preferably, the aircraft is fixed-wing formula, rotary wind type, flapping wings type, umbrella wing formula, jet-propelled or airship type.
Preferably, the receiving chamber is located at the aircraft upper back, and with upward opening.
Preferably, the receiving chamber is constituted by for clamping the clamp structure of fireworks.
Preferably, the clamp structure includes two activity jig arm of mutual cooperation；Cut with scissors by middle part between two jig arm
Connect, and be fixed on the aircraft by the middle part being hinged.
Preferably, the unit of lighting includes rotor, sparking generating mechanism and ignitor switch；The ignitor switch is used for
The control sparking generating mechanism is lighted a fire at the rotor.
Preferably, it is described to be arranged on lighting unit activity on the aircraft；The unit of lighting is by displacement
Make the rotor closer or far from the blasting fuse of fireworks.
Further, it is additionally provided with image identification unit on the aircraft；Described image recognition unit lights list with described
Unit's communication connection, the blasting fuse for recognizing fireworks.
Preferably, it is provided with relaying blasting fuse on the rotor；The relaying blasting fuse is used for the blasting fuse with fireworks
Connection.
Preferably, the clamping element for clamping fireworks blasting fuse is provided with the rotor.
Preferably, the sparking interface for being docked with fireworks is provided with the rotor.
It is used to be arranged on carry-on supporting fireworks present invention also offers one kind, is provided with supporting fireworks and cigarette
What flower blasting fuse was connected lights interface；The interface of lighting is docked to the unit of lighting with setting in aircraft.
Preferably, it is described to light bottom or sidepiece that interface is arranged on the supporting fireworks.
Present invention also offers a kind of aerocraft system for being used to realize firework display function, including at least one set is to real
The aircraft and control device of existing firework display function；The control device is used to control at least one set to be used to realize fireworks
The aircraft for setting off function is set off fireworks according to default fit system.
The invention provides a kind of method for being used to and realizing firework display function, comprise the following steps：
Aircraft carries fireworks and flies in the air；
Aircraft is set off fireworks in the air, and the fireworks seted off spray upwards.
Present invention also offers a kind of method for being used to and realizing fireworks release function, comprise the following steps：
Pre-set flight path；
Aircraft carries the fireworks lighted and is flown according to foregoing path.
The present invention is allowed to compared with prior art, have the following advantages that and actively imitate due to using above technical scheme
Really：Fireworks are put using unmanned vehicle, it will bring more convenient and distinguished visual experiences.
Brief description of the drawings
Fig. 1 is the structured flowchart of the aircraft for being used to and realizing firework display function provided in an embodiment of the present invention；
Fig. 2 is the structural representation of the aircraft for being used to and realizing firework display function provided in an embodiment of the present invention；
Fig. 3 is the structural representation of the aircraft for being used to and realizing firework display function provided in an embodiment of the present invention；
Fig. 4 is the structural representation of the aircraft for being used to and realizing firework display function provided in an embodiment of the present invention；
Fig. 5 a, 5b are the aircraft for being used to realize firework display function using supporting fireworks provided in an embodiment of the present invention
Structural representation；
Fig. 5 c are the structural representation of supporting fireworks provided in an embodiment of the present invention；
Fig. 5 d are the mplifying structure schematic diagram for lighting interface of supporting fireworks provided in an embodiment of the present invention；
Fig. 6 is the method flow diagram for being used to realize firework display function provided in an embodiment of the present invention；
Fig. 7 is the flow chart of another method for being used to realize firework display function provided in an embodiment of the present invention.
Label is as follows in figure：
It is used to realize the aircraft 100 of firework display function, fixed-wing formula 100a, rotary wind type 100b, flapping wings type 100c, umbrella
The wing formula 100d, jet-propelled 100e, airship type 100f；
Receiving chamber 110, clamp structure 111, activity jig arm 111a；
Unit 120 is lighted, rotor 121, image identification unit 121a relays blasting fuse 121b, and strike sparks interface 121c, folder
Element 121d is held, strike sparks recurring structure 122, ignitor switch 123；
Fireworks 200, fireworks blasting fuse 210；
Supporting fireworks 200a, supporting fireworks blasting fuse 210a, light interface 220a, conduit 221a.
Specific embodiment
Below in conjunction with the flight for being used to realize firework display function that specific embodiment and its accompanying drawing are provided the present invention
The technical scheme of device, system, method and supporting fireworks makes further clear and complete instructions.It should be noted that of the invention
Embodiment has preferably implementation, and any type of limitation, any one skilled in the art are not made to the present invention
Changed possibly also with the technology contents of the disclosure above or be modified to equivalent effective embodiment, as long as without departing from the technology of the present invention side
The content of case, any modification or equivalent variations and modification made to above example according to technical spirit of the invention, belongs to
In the scope of technical solution of the present invention protection.With reference to following explanation and claims, advantages and features of the invention will be more clear
Chu.It should be noted that, accompanying drawing in the form of simplifying very much and uses non-accurately ratio, is only used to conveniently, lucidly
Aid in illustrating the purpose of the embodiment of the present invention.
Fig. 1 is the structured flowchart of the aircraft for being used to and realizing firework display function provided in an embodiment of the present invention.The present invention
There is provided a kind of aircraft 100 for being used to realize firework display function, it is provided with putting fireworks 200 on aircraft 100
Receiving chamber 110, and be used to set off fireworks and 200 light unit 120, the spout of the fireworks 200 being positioned in receiving chamber 110
Set up.
Unrestricted as an example, Flight Vehicle Structure could be arranged to fixed-wing formula 100a, rotary wind type 100b, flapping wings type
100c, umbrella wing formula 100d, jet-propelled 100e or airship type 100f.
Receiving chamber 110 is located at the upper back of aircraft 100, and with upward opening.It is unrestricted as an example, receiving
Chamber 110 can be constituted by for clamping the clamp structure 111 of fireworks 200.For example, clamp structure 111 includes two phase interworkings
The activity jig arm 111a of conjunction, is hinged, and be fixed on aircraft 100 by the middle part being hinged between two jig arm 111a by middle part
On.Equally unrestricted as an example, receiving chamber 110 may be arranged as the hollow structure of upper shed, and the hollow structure has
With the shape for matching of fireworks 200, fireworks 200 can from receiving chamber upper shed at enter receiving chamber in, be put into receiving chamber
In fireworks with receiving chamber hollow structure be brought into close contact.The receiving chamber is fixed on the back of aircraft by its bottom.Make
For for example and not limitation, the receiving chamber can be made of elastomeric material.
Lighting unit 120 includes rotor 121, sparking generating mechanism 122 and ignitor switch 123.Ignitor switch 123 is used for
Control sparking generating mechanism 122 is in the igniting of the top of rotor 121.Unrestricted as an example, lighting unit 120 can be actively
It is arranged on aircraft 100, lighting unit 120 can make the leading closer or far from fireworks 200 of rotor 121 by displacement
Live wire 210.Further, be additionally provided with image identification unit 121a on aircraft 100, image identification unit 121a with light list
Unit 120 communicates to connect, the blasting fuse 210 for recognizing fireworks 200.It is unrestricted as an example, can also be set on rotor 121
Relaying blasting fuse 121b is put, relaying blasting fuse 121b is used for and the blasting fuse 210 of fireworks 200 is connected.As an example rather than limit
System, may be provided for the sparking interface 121c docked with fireworks on rotor 121.It is unrestricted as an example, rotor
May be provided for clamping the clamping element 121d of fireworks blasting fuse 210 on 121.
It is unrestricted as an example, single receiving chamber can be set on board the aircraft and unit is lighted, for setting off one
Individual fireworks.It is equally unrestricted as an example, multiple receiving chambers can be set on board the aircraft and unit is lighted, it is many for setting off
Individual fireworks, concrete condition can be arranged as required to.
Present invention also offers a kind of aerocraft system for being used to realize firework display function, including at least one set is to real
The aircraft and control device of existing firework display function.Wherein, control device realizes that fireworks fire for controlling at least one set to be used to
The aircraft of playing function is set off fireworks according to default fit system.
Fig. 2 is the structural representation of the aircraft for being used to and realizing firework display function provided in an embodiment of the present invention.In Fig. 2
In, Flight Vehicle Structure uses rotary wind type structure as an example.
In the embodiment shown in Figure 2, it is provided with putting the receiving chamber of fireworks 200 on the back of aircraft 100, should
Receiving chamber is constituted by for clamping the clamp structure of fireworks 200.As an example, the clamp structure includes two mutual cooperations
Activity jig arm 111a, be hinged by middle part between two jig arm 111a, and aircraft 100 is fixed on by the middle part being hinged
On.Two the two of jig arm 111a ends respectively constitute the holding end and bare terminal end of clamp structure.On bare terminal end is adjacent thereto
Lower space collectively forms the receiving chamber for accommodating fireworks 200.Further, in grip end, tensioning unit is provided between two jig arm
Part, can use spring as the tension element of holding end as an example.Apply certain grip compression spring by holding end
Can open the bare terminal end of clamp structure, be easy to place fireworks 200.After fireworks 200 are placed, unclamp or release is applied to
The grip of holding end, spring stretches, and bare terminal end is by the held tight of fireworks 200.
In order that bare terminal end can more closely clamp fireworks, two jig arm 111a can be according to the shape of fireworks 200, thick
It is thin to set.As in fig. 2, fireworks 200 are cylindrical shape, and two bare terminal ends of jig arm are corresponding in order to adapt to the shape of fireworks
Be set to arc-shaped, and the smallest circumference that surrounds of bare terminal end of two jig arm is less than the lateral circumferential of fireworks 200, so
Two jig arm just can closely, be held fixedly fireworks.
As shown in Fig. 2 be additionally provided with to set off fireworks on aircraft 100 200 lighting unit 120.Light unit
120 are fixedly installed on the back of aircraft 100, and are shifted to install with receiving chamber 110.Light unit 120 including rotor 121,
Sparking generating mechanism 122 and ignitor switch 123.Ignitor switch 123 is used to control sparking generating mechanism 122 to be pushed up in rotor 121
Light a fire in portion.It is unrestricted as an example, light unit 120 and be movably arranged as on aircraft 100, lighting unit 120 can lead to
Cross the blasting fuse 210 that displacement makes rotor 121 closer or far from fireworks 200.Further, rotor 121 could be arranged to
Activity, rotor 121 can move up and down relative to sparking generating mechanism 122 and ignitor switch 123, in order to be close to
Or away from the blasting fuse 210 of fireworks.
In order to accurately light fireworks, image identification unit 121a is additionally provided with aircraft 100, the image recognition list
First 121a is communicated to connect with unit 120 is lighted, the blasting fuse 210 for recognizing fireworks 200.Accordingly, also set on board the aircraft
It is equipped with and image identification unit 121a and lights the control unit that unit 120 is connected, further control unit and the He of rotor 121
Ignitor switch 123 is connected respectively.Under in working order, the image of fireworks blasting fuse is gathered first with image identification unit 121a
Data message, and the blasting fuse image data information that will be collected compares with default standard blasting fuse image data information
Analysis, when the blasting fuse image data information of collection is mismatched with default standard blasting fuse image data information, image is known
Other unit 121a continues to gather the image data information of fireworks blasting fuse, when collection blasting fuse image data information with it is default
When standard blasting fuse image data information matches, the positional information of fireworks blasting fuse is sent to control unit.Control unit
After receiving the positional information of fireworks blasting fuse 210, control rotor 121 moves up and down, near fireworks blasting fuse 210.
When rotor 121 is near fireworks blasting fuse 210, control unit opens ignitor switch 123.The control sparking hair of ignitor switch 123
Life structure 122 is struck sparks at rotor 121, and lights fireworks blasting fuse.
Fig. 3 is another structural representation of the aircraft for being used to realize firework display function provided in an embodiment of the present invention
Figure.In the present embodiment, be provided with the back of aircraft 100 putting the receiving chamber of fireworks 200, the receiving chamber be by with
Constituted in the clamp structure of clamping fireworks 200.As an example, the clamp structure includes two activity jig arm of mutual cooperation
111a, is hinged, and be fixed on aircraft 100 by the middle part being hinged between two jig arm 111a by middle part.Two jig arm
Two ends of 111a respectively constitute the holding end and bare terminal end of clamp structure.The bare terminal end upper and lower common structure in space adjacent thereto
Into the receiving chamber for accommodating fireworks 200.Further, in grip end, it is provided with as the spring of tension element between two jig arm.
In Fig. 3, it is additionally provided with to set off fireworks on aircraft 100 and 200 lights unit 120.Unit 120 is lighted to consolidate
Surely set on the back of aircraft 100, and shifted to install with receiving chamber 110.Lighting unit 120 includes rotor 121, sparking hair
Life structure 122 and ignitor switch 123.Ignitor switch 123 is used to control sparking generating mechanism 122 in the igniting of the top of rotor 121.
In order to accurately light fireworks, relaying blasting fuse 121b is additionally provided with rotor 121.One end of relaying blasting fuse 121b
The top of rotor 121 is fixed on, the other end is connected with the blasting fuse of the fireworks placed on aircraft.As an example rather than limit
System, can be fixedly installed a small circle ring in the top outer of rotor 121, and one end of relaying blasting fuse 121b passes through and ties up
On small circle ring.It is worth noting that to avoid the terminal for relaying blasting fuse 121b directly to tie up on small circle ring as far as possible, it is preferably square
Formula is that the lead that there be a segment length its end extends from binding after relaying blasting fuse 121b binds on small circle ring
Come, and in the top of rotor 121.Certainly, the small circle ring of the top outer of rotor 121 is not by relaying blasting fuse 121b
The sole mode at the top of rotor 121 is connected to, other all appropriate connection means are applicable.For relaying blasting fuse 121b
It is as an example that directly both are knotted by end compared with quick way with the connection between fireworks blasting fuse 210.For reality
Existing aircraft lights fireworks in the air, and the control unit being connected with ignitor switch 123 is there is provision of on board the aircraft.Needing a little
When burning smoke is spent, control unit starts ignitor switch 123, and control sparking generating mechanism 122 is struck sparks at rotor 121, will
Light one end of relaying blasting fuse 121b.With the burning of relaying blasting fuse 121b, the other end of relaying blasting fuse 121b is by cigarette
Flower blasting fuse 210 is lighted.
Fig. 4 is the third structural representation of the aircraft for being used to and realizing firework display function provided in an embodiment of the present invention
Figure.In the present embodiment, be provided with the back of aircraft 100 putting the receiving chamber of fireworks 200, the receiving chamber be by with
Constituted in the clamp structure of clamping fireworks 200.As an example, the clamp structure includes two activity jig arm of mutual cooperation
111a, is hinged, and be fixed on aircraft 100 by the middle part being hinged between two jig arm 111a by middle part.Two jig arm
Two ends of 111a respectively constitute the holding end and bare terminal end of clamp structure.The bare terminal end upper and lower common structure in space adjacent thereto
Into the receiving chamber for accommodating fireworks 200.Further, in grip end, it is provided with as the spring of tension element between two jig arm.
In Fig. 4, it is additionally provided with to set off fireworks on aircraft 100 and 200 lights unit 120.Unit 120 is lighted to consolidate
Surely set on the back of aircraft 100, and shifted to install with receiving chamber 110.Lighting unit 120 includes rotor 121, sparking hair
Life structure 122 and ignitor switch 123.Ignitor switch 123 is used to control sparking generating mechanism 122 in the igniting of the top of rotor 121.
In order to accurately light fireworks, the clamping element 121d for clamping fireworks blasting fuse 210 is additionally provided with rotor 121.
Clamping element 121d is preferably provided at the end of rotor 121.As an example, the clamping element 121d can use common
Clip structure.After fireworks 200 are positioned over receiving chamber 110, the blasting fuse 210 of fireworks is clamped with clamping element 121d.In order to
Realize that aircraft lights fireworks in the air, the control unit being connected with ignitor switch 123 is there is provision of on board the aircraft.Needing
When lighting fireworks, control unit starts ignitor switch 123, and control sparking generating mechanism 122 is struck sparks at rotor 121,
Clamped fireworks blasting fuse 210 is lighted.
Fig. 5 a, 5b are the aircraft for being used to realize firework display function using supporting fireworks provided in an embodiment of the present invention
Structural representation, Fig. 5 c are the structural representation of supporting fireworks provided in an embodiment of the present invention, and Fig. 5 d are the embodiment of the present invention
The mplifying structure schematic diagram for lighting interface of the supporting fireworks for providing.The present embodiment provides a kind of aircraft using supporting fireworks
Structure and supporting fireworks.
In Fig. 5 a, 5b, be provided with the back of aircraft 100 put fireworks 200 receiving chamber, the receiving chamber be by
What the clamp structure for clamping fireworks 200 was constituted.As an example, the clamp structure includes two activity jig arm of mutual cooperation
111a, is hinged, and be fixed on aircraft 100 by the middle part being hinged between two jig arm 111a by middle part.Two jig arm
Two ends of 111a respectively constitute the holding end and bare terminal end of clamp structure.The bare terminal end upper and lower common structure in space adjacent thereto
Into the receiving chamber for accommodating fireworks 200.Further, in grip end, it is provided with as the spring of tension element between two jig arm.
In Fig. 5 a, 5b, it is again provided with setting off fireworks in aircraft 100 and 200 lights unit 120.Light unit
120 include rotor 121, sparking generating mechanism 122 and ignitor switch 123, and ignitor switch 123 is used to control sparking generating mechanism
122 in the igniting of the top of rotor 121.From unlike two foregoing embodiments, light unit 120 set aircraft 100 in,
And it is in upper bottom with receiving chamber 110；And be also provided with rotor 121 for beating that supporting fireworks 200a is docked
Fiery interface 121c.Unrestricted as an example, sparking interface 121c could be arranged to outlet structure or plug construction.
Fig. 5 c are the structural representation of supporting fireworks provided in an embodiment of the present invention, be provided with supporting fireworks 200a with
Fireworks blasting fuse 210a connection light interface 220a, light interface 220a to and aircraft 100 in set light unit
120 docking.Unrestricted as an example, this is lighted interface 220a and can be arranged on bottom or the sidepiece of supporting fireworks 200a.
In embodiment, the bottom that interface 220a is arranged on supporting fireworks 200a is lighted.Further, light interface 220a can with light list
The sparking interface 121c docking set on rotor 121 in unit 120.For the ease of lighting interface 220a and sparking interface 121c
Between dock, the structure for lighting interface 220a should be corresponding with the structure of foregoing sparking structure 121c, unrestricted as an example,
It can be plug construction or outlet structure that this lights interface 220a.
In the present embodiment, sparking interface 121c is set to outlet structure, and the hollow structure with upper and lower opening, such as schemes
Shown in 5a；Light interface 220a and be set to plug construction, and with downwardly open hollow structure, as shown in Figure 5 c；Light and connect
Mouth 220a can be plugged in sparking interface 121c, as shown in Figure 5 b.
Fig. 5 d are the mplifying structure schematic diagram for lighting interface of supporting fireworks provided in an embodiment of the present invention, can from figure
Know, the inside top for lighting interface 220a of supporting fireworks 200a is additionally provided with for leading through supporting fireworks blasting fuse 210a
Pipe 221a, as an example, conduit 221a is horizontally set on the top for lighting interface 220a, and one end of conduit 221a is run through
The side wall of interface 220 is lighted, the other end is located at the centre of the inside top for lighting interface 220a.In the present embodiment, supporting cigarette
Blasting fuse 210a is more longer than general fireworks blasting fuse for flower.Supporting fireworks blasting fuse 210a can be vertical along supporting fireworks 220a
To extending to down, it is possible to penetrated near the one end for lighting interface 220a sides wall from the conduit 221a for lighting interface 220a, run through
After conduit 221a, passed from the other end of conduit 221a, the rear suspension of supporting fireworks blasting fuse 210a is lighting interface 220a
In.
In figure 5b, after supporting fireworks 200a is placed, the interface 220a that lights of supporting fireworks 200a is plugged on sparking
In first 121 sparking interface 121c, the afterbody of supporting fireworks blasting fuse 210a is towards rotor 121.In order to realize that aircraft exists
Fireworks are lighted in the air, the control unit being connected with ignitor switch 123 is there is provision of on board the aircraft.Need to light fireworks when
Wait, control unit starts ignitor switch 123, control sparking generating mechanism 122 is struck sparks at rotor 121, and flame is located at sparking
In first 121 sparking interface 121c, the tail that supporting fireworks light the supporting fireworks blasting fuse 210a in interface 220a will be suspended on
Light in portion.With the burning of supporting fireworks blasting fuse 210a, supporting fireworks 200a is ignited.
The present invention has also put forward a kind of method for being used to and realizing firework display function, and Fig. 6 is use provided in an embodiment of the present invention
To realize the method flow diagram of firework display function.
The method comprises the following steps：
S110：Aircraft carries fireworks and flies in the air；
S120：Aircraft is set off fireworks in the air, and the fireworks seted off spray upwards.
In the technical scheme that the present invention is provided, it is provided with putting the receiving chamber of fireworks on aircraft, and be used to
That sets off fireworks lights unit.Lighting unit includes rotor, sparking generating mechanism and ignitor switch, and ignitor switch is used to control
Sparking generating mechanism point at rotor is fought and lights fireworks.As an example, receiving chamber can be by the clamping for clamping fireworks
Structure is constituted.Preferably, clamp structure is set to two activity jig arm of mutual cooperation, is cut with scissors by middle part between two jig arm
Connect, and fixed on board the aircraft by the middle part being hinged, and two jig arm are parallel with aircraft back.Equally as an example rather than
Limitation, receiving chamber may be arranged as the hollow structure of upper shed, and the hollow structure has the shape for matching with fireworks, cigarette
Spend to enter in receiving chamber from the upper shed in receiving chamber, and the fireworks being put into receiving chamber are tight with the hollow structure in receiving chamber
Laminating, the receiving chamber is fixed on the back of aircraft by its bottom.By aforementioned embodiments, receiving chamber is positioned over
In fireworks be ignited after, the fireworks seted off spray upwards.
The present invention has also carried another kind and has been used to the method for realizing firework display function, and Fig. 7 is provided in an embodiment of the present invention
It is used to realize the flow chart of another method of firework display function.
The method comprises the following steps：
S210：Pre-set flight path；
S220：Aircraft carries the fireworks lighted and is flown according to foregoing path.
At pre-set flight path, can be set according to the desired effects of firework display.For example, it is desirable to aircraft is carried
Fireworks on high in set off and show heart pattern, then during pre-set flight path, can be set as heart-shaped track.Thus,
What the present invention was provided is used to realize the method for firework display function by pre-set flight path, aircraft is carried the fireworks lighted
Flown according to preset path, allow for setting off for fireworks more abundant, more dazzling colorful.
Technical scheme has the following advantages that, puts fireworks using unmanned vehicle, it will give people band
Carry out more convenient and distinguished visual experiences.
Foregoing description is only the description to present pre-ferred embodiments, any not to any restriction of the scope of the invention
Any change, modification that those skilled in the art does according to the disclosure above content, belong to claims
Protection domain.
Claims (16)
1. a kind of aircraft for being used to realize firework display function, it is characterised in that：
Be provided with putting the receiving chamber of fireworks on board the aircraft, and be provided with to set off fireworks light unit, put
The spout of the fireworks being placed in receiving chamber sets up.
2. the aircraft for being used to realize firework display function according to claim 1, it is characterised in that：
The aircraft is fixed-wing formula, rotary wind type, flapping wings type, umbrella wing formula, jet-propelled or airship type.
3. the aircraft for being used to realize firework display function according to claim 1, it is characterised in that：
The receiving chamber is located at the aircraft upper back, and with upward opening.
4. the aircraft for being used to realize firework display function according to claim 3, it is characterised in that：
The receiving chamber is constituted by for clamping the clamp structure of fireworks.
5. the aircraft for being used to realize firework display function according to claim 4, it is characterised in that：
The clamp structure includes two activity jig arm of mutual cooperation；
It is hinged by middle part between two jig arm, and is fixed on the aircraft by the middle part being hinged.
6. the aircraft for being used to realize firework display function according to claim 1, it is characterised in that：
The unit of lighting includes rotor, sparking generating mechanism and ignitor switch；
The ignitor switch is used to control the sparking generating mechanism to be lighted a fire at the rotor.
7. the aircraft for being used to realize firework display function according to claim 6, it is characterised in that：
It is described to be arranged on lighting unit activity on the aircraft；
The unit of lighting makes the rotor closer or far from the blasting fuse of fireworks by displacement.
8. the aircraft for being used to realize firework display function according to claim 7, it is characterised in that：
Image identification unit is additionally provided with the aircraft；
Described image recognition unit is connected with the unit communication of lighting, the blasting fuse for recognizing fireworks.
9. the aircraft for being used to realize firework display function according to claim 6, it is characterised in that：
Relaying blasting fuse is provided with the rotor；
The relaying blasting fuse is used for and the blasting fuse of fireworks is connected.
10. the aircraft for being used to realize firework display function according to claim 6, it is characterised in that：
The clamping element for clamping fireworks blasting fuse is provided with the rotor.
11. aircraft for being used to realize firework display function according to claim 6, it is characterised in that：
The sparking interface for being docked with fireworks is provided with the rotor.
12. one kind are used to be arranged on carry-on supporting fireworks, it is characterised in that：
It is provided with supporting fireworks and lights interface with fireworks blasting fuse is connected；
The interface of lighting is docked to the unit of lighting with setting in aircraft.
13. according to claim 12 are used to be arranged on carry-on supporting fireworks, it is characterised in that：
It is described to light bottom or sidepiece that interface is arranged on the supporting fireworks.
A kind of 14. aerocraft systems for being used to realize firework display function, it is characterised in that：
It is used to realize the aircraft and control device of firework display function including at least one set；
The control device realizes that the aircraft of firework display function is matched somebody with somebody according to default for controlling at least one set to be used to
Conjunction mode is set off fireworks.
A kind of 15. methods for being used to realize firework display function, it is characterised in that comprise the following steps：
Aircraft carries fireworks and flies in the air；
Aircraft is set off fireworks in the air, and the fireworks seted off spray upwards.
A kind of 16. methods for being used to realize fireworks release function, it is characterised in that comprise the following steps：
Pre-set flight path；
Aircraft carries the fireworks lighted and is flown according to foregoing path.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710001256.8A CN106767186A (en) | 2017-01-03 | 2017-01-03 | It is used to realize aircraft, system, method and the supporting fireworks of firework display function |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710001256.8A CN106767186A (en) | 2017-01-03 | 2017-01-03 | It is used to realize aircraft, system, method and the supporting fireworks of firework display function |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106767186A true CN106767186A (en) | 2017-05-31 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710001256.8A Pending CN106767186A (en) | 2017-01-03 | 2017-01-03 | It is used to realize aircraft, system, method and the supporting fireworks of firework display function |
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| CN (1) | CN106767186A (en) |
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| CN205919742U (en) * | 2016-07-26 | 2017-02-01 | 昆明理工大学 | Device is touched off to aerial firecracker of wireless remote control |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH11267369A (en) * | 1998-03-24 | 1999-10-05 | Naoki Harigai | Rocket firework propulsion type orbit flying doll |
| CN200947011Y (en) * | 2006-04-01 | 2007-09-12 | 肖方 | Fireworks and firecracker remote control setting off device |
| CN101949664A (en) * | 2010-02-22 | 2011-01-19 | 康子纯 | High-altitude platform fireworks |
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Application publication date: 20170531 |