CN208975034U - Fire extinguishing system - Google Patents
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- CN208975034U CN208975034U CN201820743450.3U CN201820743450U CN208975034U CN 208975034 U CN208975034 U CN 208975034U CN 201820743450 U CN201820743450 U CN 201820743450U CN 208975034 U CN208975034 U CN 208975034U
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Abstract
A kind of fire extinguishing system is related to fire-extinguishing apparatus technical field, comprising: aircraft, traction device and toter；Traction device is used for traction carrying device, and one end is fixed on board the aircraft, and the other end connects toter；The weight and load capacity of traction device are less than the weight and load capacity of toter.The load capacity of unmanned plane can be improved in above-mentioned fire extinguishing system, so that unmanned plane plays bigger effect in fire extinguishing procedure.
Description
Technical field
The utility model relates to fire-extinguishing apparatus technical field more particularly to a kind of fire extinguishing systems.
Background technique
With the development of vehicle technology, this small aircraft of unmanned plane is increasingly being applied to the aspect of life
Aspect, such as high-altitude fire extinguishing.However, the load capacity of unmanned plane is limited, it can only be used for fire behavior monitoring at present, can not put out a fire
Bigger effect is played in the process.
Utility model content
In view of this, the utility model embodiment provides a kind of fire extinguishing system, it can be used for improving the load capacity of unmanned plane,
So that unmanned plane plays bigger effect in fire extinguishing procedure.
The utility model embodiment provides a kind of fire extinguishing system, comprising: aircraft, traction device and toter；
The traction device, for drawing the toter, one end is fixed on the aircraft, and the other end connects the delivery dress
It sets；The weight and load capacity of the traction device are less than the weight and load capacity of the toter.
Above-mentioned fire extinguishing system combines building self structure and unmanned plane, by pullling lighter in weight using aircraft
Traction device, drive weight and the biggish toter of load capacity to reach ignition point, on the one hand, due to traction device
Lighter in weight, thus it is lower to unmanned plane requirement, on the other hand, the load capacity of unmanned plane can be improved simultaneously by toter
So that in addition, toter can be with multipurpose, such as formation, personnel flee from channel, so that nothing with equipment diversification is carried
It is man-machine that bigger effect is played in fire extinguishing procedure.
Detailed description of the invention
Fig. 1 is the structural schematic diagram for the fire extinguishing system that an embodiment of the present invention provides；
Fig. 2 is the structural schematic diagram for the fire extinguishing system that another embodiment of the utility model provides；
Fig. 3 is the implementation process schematic diagram for the flying vehicles control method that an embodiment of the present invention provides；
Fig. 4 is the implementation process schematic diagram for the flying vehicles control method that another embodiment of the utility model provides；
Fig. 5 to Figure 10 is drilling for a practical application example of the flying vehicles control method that another embodiment of the utility model provides
Diagram；
Figure 11 is the hardware structural diagram for the electronic flight device that an embodiment of the present invention provides.
Specific embodiment
To enable the goal of the invention, feature, advantage of the utility model more obvious and understandable, below in conjunction with this
Attached drawing in utility model embodiment, the technical scheme in the utility model embodiment is clearly and completely described, shows
So, the described embodiments are only a part of the embodiments of the utility model, and not all embodiments.Based in the utility model
Embodiment, those skilled in the art's every other embodiment obtained without making creative work all belongs to
In the range of the utility model protection.
Referring to Fig. 1, the structural schematic diagram of the fire extinguishing system provided for an embodiment of the present invention.As shown in Fig. 1,
Fire extinguishing system 100 includes: aircraft 101, traction device 102 and toter 103.
Wherein, traction device 102 are used for traction carrying device 103.One end of traction device 102 is fixed on aircraft 101
On, the other end connects toter 103.The weight and load capacity of traction device 102 are less than the weight and band of toter 103
Loading capability.That is, the weight of traction device 102 is within the scope of the load-bearing of aircraft 101, the weight of toter 103
It can be except the load-bearing range of aircraft 101.In general, the weight of object is bigger when the constancy of volume of object, the band of object
Loading capability is bigger, that is to say, that the weight of its other object that can be carried or carry is bigger.Therefore, it is filled by traction
102 and toter 103 are set, may make that the load capacity of aircraft 101 is extended.
Specifically, one end of traction device 102 can for example be set by latching the fuselage for being fixed on aircraft 101 or bottom
In the cyclic structure set.Alternatively, in another example, one end of traction device 102 can wind fuselage or its bottom in aircraft 101
In the line wheel of portion's setting.
Optionally, the other end of traction device 102 can be fixed on toter 103 by dismountable mode, such as: benefit
It is fixed with lock or the mode to knot.Alternatively, the other end of traction device 102 can also be fixed by non-dismountable mode
On toter 103, such as: being fixed by way of welding or weaving.
Optionally, aircraft 101 is small-sized or miniature unpiloted aircraft, preferably four axis unmanned planes.
Optionally, traction device 102 is the load-carrying of band-like or linear structure, weight and load capacity in aircraft 101
Within the scope of.
Toter 103 can be used for delivering people, fire extinguishing or survival equipment.103 part of toter includes band-like or linear
Structure.Optionally, other than band-like or linear structure part, the main body of toter 103 be can be, but not limited to further include: basket
Body structure, band-like or linear structure (such as: foldable or telescopic fire-fighting rack) or people, fire extinguishing or survival equipment can be adhered to
Other structures.Fire-extinguishing apparatus for example can be, but not limited to include: water pipe, hydraulic giant, all types of fire extinguishers and fire extinguishing ball etc.
Deng.Survival equipment for example can be, but not limited to include: fire mask, slip rope etc..
Preferably, traction device 102 and toter 103 are rope, and the diameter of the rope as traction device 102 is small
In the diameter of the rope as toter 103.The rope for example can be, but not limited to be high-temperature resistant aramid fiber rope, Kev drawstring
Etc..
Optionally, traction device 102 and toter 103 are high temperature resistant material, alternatively, traction device 102 and delivery
The outer surface of device 103 is coated with heat-resisting material.
In a practical application example, it is assumed that aircraft 101 is unmanned plane, and traction device 102 is that thin Kev drawstring is (following
Abbreviation thin cord), toter 103 is thick Kev drawstring (hereinafter referred to as hawser rope), then in scene of fire, using unmanned plane
The one end for pullling thin cord is gone up to the air by fire fighting truck roof, when rising to the top of building where ignition point, unmanned plane after
The continuous railing or others door opening structure pullled thin cord and penetrate top of building, then around the railing or door opening structure
Peripheral flight half cycle after fall, thus by thin cord bypass the railing or door opening structure.It lands when unmanned plane carries thin cord
Afterwards, one end of hawser rope is linked together with the other end for being tethered in the thin cord on fire fighting truck, then by pullling fixation
One end of thin cord on unmanned plane, by hawser Suo Shangti, until hawser rope passes through the railing or others of top of building
After door opening structure, ground is reached, is tethered on fire fighting truck.Later, fire fighter can carry hydraulic giant, be reached by climbing hawser rope
Ignition point on building is put out a fire.Alternatively, hawser rope can also be penetrated with fire-fighting jigger, is risen using hawser rope, will be gone out
Fiery equipment or fire main are brought nearby to be implemented to put out a fire to ignition point.Or the personnel near ignition point, climbing can also be passed through
Hawser rope is escaped.
Fire extinguishing system provided by the embodiment of the utility model combines building self structure and unmanned plane, passes through utilization
Aircraft pulls the traction device of lighter in weight, and weight and the biggish toter of load capacity is driven to reach ignition point, and one
Aspect, it is lower to unmanned plane requirement due to the lighter in weight of traction device, on the other hand, it can be mentioned by toter
The load capacity of high unmanned plane simultaneously makes band carry equipment diversification, in addition, toter can such as form personnel with multipurpose
Channel is fled from, so that unmanned plane plays bigger effect in fire extinguishing procedure.
Referring to Fig. 2, the structural schematic diagram of the fire extinguishing system provided for another embodiment of the utility model.With shown in Fig. 1
Fire extinguishing system 100 unlike, as shown in Fig. 2, in fire extinguishing system 200 provided in this embodiment::
Further, fire extinguishing system 200 further include: band carries equipment 201.Band carries equipment 201 and is mounted on toter 103
On, comprising: fire-extinguishing apparatus and/or lowering rope device.
Optionally, fire-extinguishing apparatus can be fixed on the bottom of toter 103.Such as: it can will be put out a fire by lock or rope
Equipment is fixed on the bottom of toter 103.
Optionally, it is provided with driving device on fire-extinguishing apparatus or lowering rope device, for driving fire-extinguishing apparatus or lowering rope device
It is soaring along toter 103.
Wherein, fire-extinguishing apparatus is for putting out a fire.Lowering rope device is used to help fire fighter and reaches near ignition point, alternatively, with
In escape, alternatively, lowering rope device can be used for being fixed together with fire-extinguishing apparatus, make fire-extinguishing apparatus edge using lowering rope device
Toter 103 it is soaring.
Further, fire extinguishing system 200 further include: guide structure 202.
Guide structure 202, is fixed on the top or exterior wall of building, and guide structure 202 is open with frame-type.It is real one
In the application examples of border, guide structure 202 can be gate mount structure.
Aircraft 101, for pullling traction device 102, by a part of traction device 102 via guide structure 202
Return to ground.Specifically, the frame-type opening that a part of traction device 102 passes through guide structure 202 returns to ground.
Since the exterior wall of not every building and top all have railing or similar structures, by building
Guide structure 202 is installed on the top of object or exterior wall, aircraft 101 can be saved and searched on building for limiting traction dress
The time for setting 102 facility avoids delaying fire extinguishing because can not find facilities available.
Further, in other embodiments, fire extinguishing system 200 further include: towing device 203, fixed device 204, around
At least one of line apparatus 205 and sender unit 206.
Wherein, towing device 203 includes coiling apparatus or trailer.Coiling apparatus and bobbin winder device 205 for example can with but not
It is limited to include: that line wheel, winder, winding roll, reel etc. can be used for winding or discharging band-like or thread-shaped body device,
Specific control mode can be electronic be also possible to manually.
Optionally, towing device 203 and fixed device 204 may be provided on fire fighting truck or ground, and toter 103 is not
The one end connecting with traction device 102 is fixed on fixed device 204.Fixed device 204 can be the biggish object of weight, example
It such as can be the stone pier, metal block.
Towing device 203 draws high toter 103 to aerial direction for pulling traction device 102.Pass through benefit
Manpower can be saved when pulling traction device 102 with towing device, accelerate the speed for drawing high toter 103.Optionally,
Towing device 203 includes fixed structure.One end of traction device 102 is fixed on the fixed structure under the traction of aircraft 101
On, that is, aircraft 101 is also used to draw one end of traction device 102 and be fixed on the fixed structure.Work as towing device
203 be coiling apparatus when, fixed structure be coiling apparatus spool.When towing device 203 is trailer, fixed structure is to set
It sets and drags thick stick in trailer tail portion.Aircraft 101 draws fixed structure of the one end round towing device 203 of traction device 102
It detours, by the one ends wound of traction device 102 on the fixed structure.
Optionally, bobbin winder device 205 is arranged on aircraft 101, is wound with traction device 102 thereon.By that will draw
Device 102 is wrapped on bobbin winder device 205, it can be achieved that its one end is fixed on aircraft 101.Bobbin winder device 205 is used for
Traction device 102 is discharged during aircraft 101 flies, and controls the length of the traction device 102 of release.Pass through benefit
Traction device 102 can be preferably controlled with bobbin winder device.
Optionally, sender unit 206 is mounted on guide structure 202, for sending the positioning of guide structure 202
Signal.Sender unit 206 can be, but not limited to include: signal lamp, RF signal transmitter and loudspeaker etc..Wherein
RF signal transmitter can be wired or wireless network RF signal transmitter.Nobody can be helped by sender unit
Machine faster orients the position of guide structure 202.
Fire extinguishing system provided by the embodiment of the utility model combines building self structure and unmanned plane, passes through utilization
Aircraft pulls the traction device of lighter in weight, and weight and the biggish toter of load capacity is driven to reach ignition point, and one
Aspect, it is lower to unmanned plane requirement due to the lighter in weight of traction device, on the other hand, it can be mentioned by toter
The load capacity of high unmanned plane simultaneously makes band carry equipment diversification, in addition, toter can such as form personnel with multipurpose
Channel is fled from, so that unmanned plane plays bigger effect in fire extinguishing procedure.
Referring to Fig. 3, the implementation process schematic diagram of the flying vehicles control method provided for an embodiment of the present invention, it can
Applied to the aircraft 101 in fire extinguishing system shown in Fig. 1 or Fig. 2.For purposes of illustration only, following by taking unmanned plane as an example.Such as Fig. 3 institute
Show, this method mainly comprises the steps that
301, the position of ignition point or the guide structure on ignition point nearby buildings is obtained；
Specifically, unmanned plane can be by other electronic equipments for having matched (such as: mobile phone, server, plate electricity before lift-off
Brain, smartwatch etc.), obtain the position of the guide structure on the building of user's input.
The instruction alternatively, unmanned plane is put out a fire based on the received goes up to the air in fire-extinguishing location, then shoots the photo of ignition point, point
Analysis photo obtains the position of guide structure.It include the coordinate of fire-extinguishing location in fire extinguishing instruction.
The instruction alternatively, unmanned plane is put out a fire based on the received is gone up to the air in fire-extinguishing location, is then installed on acquisition guide structure
The positioning signal of sender unit transmitting obtains the position of guide structure according to positioning signal.
Wherein, the top or the railing on exterior wall of building or Adjacent Buildings where guide structure can be fire extinguishing point,
Alternatively, other similar settings with gate mount structure.Guide structure can be the self facility of building, be also possible to individually
The gate mount structure dedicated for guidance unmanned plane during flying being reserved on building.
The positioning signal of sender unit transmitting can be, but not limited to specific sound and optic signal or radiofrequency signal.?
That is unmanned plane can spiral near ignition point, the pilot light or instruction sound issued to sender unit, or
Person, the radio-frequency information comprising coordinate information scan for, and according to the positioning signal searched, determine the position of guide structure.
302, control aircraft reaches the position, and returns to ground after detouring along the direction of guide structure guidance, will
The traction device carried on aircraft returns to ground after bypassing guide structure, and is drawn toter by pullling traction device
To predeterminated position.
Traction device can be band-like or linear structure, thin Kev drawstring preferably resistant to high temperature.
Optionally, control aircraft reaches the position of guide structure, and the frame-type across guide structure is open, and around guidance
Ground is returned to after structure flight half cycle.
Specifically, passing through gate frame, and fly upwards after unmanned plane reaches the position where the reserved gate frame of roof
Row after winding half cycle, falls, so that the thin Kev drawstring of traction is around gate frame and returns to ground.
It should be understood that in practical applications, according to opening direction and its specific structure that the frame-type of guide structure is open,
Unmanned plane pass through gate frame after be not limited to fly upwards, can also it is downward, left and right or along other angles and direction around door
The flight of type frame.
Unmanned machine travel after thin Kev drawstring returns to ground, by pullling traction device, traction device can be drawn
Toter is drawn to predeterminated position.Wherein, predeterminated position, for example, one end that toter is connect with traction device passes through door
Ground is reached after type frame, alternatively, the other end that toter is not connect with traction device reaches near ignition point.
Flying vehicles control method provided by the embodiment of the utility model, building self structure and unmanned plane are combined, and are led to
The traction device for pullling lighter in weight using aircraft is crossed, weight and the biggish toter of load capacity is driven to reach kindling
Point, on the one hand, due to the lighter in weight of traction device, lower, another aspect is required unmanned plane, it can by toter
To improve the load capacity of unmanned plane and band is made to carry equipment diversification, in addition, toter can such as be formed with multipurpose
Personnel flee from channel, so that unmanned plane plays bigger effect in fire extinguishing procedure.
Referring to Fig. 4, the implementation process schematic diagram of the flying vehicles control method provided for another embodiment of the utility model,
It can be applied to the aircraft 101 in fire extinguishing system shown in Fig. 1 or Fig. 2.As shown in figure 4, unlike embodiment illustrated in fig. 3,
In this present embodiment, the position of guide structure is reached in control aircraft, and is returned after detouring along the direction of guide structure guidance
It returns after ground, further comprising the steps of:
401, traction device is drawn and is fixed on towing device by control aircraft；
Due to the power limited of unmanned plane, traction device can not be drawn and pull too heavy toter, it is therefore desirable to be dragged
Device is dragged to assist to pull traction device.Towing device can be remote-controlled powerful electric coil winder or trailer.It pulls
Fixed structure is provided on device.When towing device is coiling apparatus, fixed structure is the spool of coiling apparatus.Work as dragging
When device is trailer, fixed structure be trailer tail portion is set drag thick stick.After unmanned plane returns to ground, continue to draw traction dress
The one end set is detoured round the fixed structure of towing device, by the one ends wound of traction device on the fixed structure, thus
It realizes and fixes.
402, it is sent to towing device and pulls instruction, dragging instruction is used to indicate towing device and pulls traction device, will
It pulls to the first predeterminated position one end of the toter of traction device traction；
If towing device is coiling apparatus, pulls instruction and be used to indicate coiling apparatus and start wrap traction arrangement.If dragging
Dragging device is trailer, then pulls instruction and be used to indicate trailer and move forward.
One end of toter is pullled to the first predeterminated position, can be, but not limited to include: by toter and traction
One end of device connection is pullled after passing through guide structure to ground, alternatively, toter is not connect with traction device another
End is pulled up to the position of the preset height near ignition point.
403, when one end of toter reaches the first predeterminated position, equipment is carried to band and sends driving instruction；
Specifically, unmanned plane after transmission pulls instruction, discharges traction device, simultaneously captured in real-time toter is then tracked
Whether dragged image reaches the first predeterminated position according to one end of the image detection toter of shooting.Work as toter
One end reach the first predeterminated position when, to band carry equipment send driving instruction, driving instruction be used to indicate band load equipment in
Driving device, driving band carry equipment and rise to the second predeterminated position along toter.Second predeterminated position is near ignition point.
Band carries equipment and can be, but not limited to include fire-extinguishing apparatus and/or lowering rope device.Fire-extinguishing apparatus such as water pipe, all types of goes out at hydraulic giant
Firearm and fire extinguishing ball etc..Lowering rope device can be used for escaping, or fireman is sent to ignition point.
404, defeated according to preset advice method when band, which carries equipment, rises to the second predeterminated position along toter
It puts up a notice message.
Specifically, unmanned plane after sending driving instruction, is tracked and captured in real-time band carries the image of equipment, according to shooting
Image detection band carries whether equipment reaches the second predeterminated position.The second predeterminated position is risen to along toter when band carries equipment
When, according to preset advice method, notification message is exported, notification message is for notifying that user is in place with equipment is carried.It is preset logical
Knowing mode can be, but not limited to include: output notice prompt tone, and notice prompt light, the smart phone of Xiang Zhiding, intelligent wearing are set
Standby equal intelligent mobile terminals send a notification message in any one or several combination.Notification message is for notifying user with load equipment
In place, it puts out a fire or escapes so that user carries equipment using band in time.
It should be noted that in practical applications, step 401 to step 404 selectively can be executed partially, for example,
Only carry out step 401 and 402, step 403 and 404 is replaced executing by fireman, alternatively, only carry out step 403, remaining step by
Fireman replaces executing, alternatively, only carrying out step 401 to step 403, step 404 is replaced executing by fireman.
In conjunction with Fig. 5 to Figure 10, to further illustrate flying vehicles control method provided in this embodiment, with using four axis nobody
For machine 1108 puts out a fire to the high building of a kindling, first with four axis unmanned planes 1108 and the airborne line of four axis unmanned plane 1108
Wheel draws one end of thin cord 1104, is gone up to the air by 1105 roof of fire fighting truck.The other end of thin cord 1104 connects hawser rope
1103 one end, the other end of hawser rope 1103 are tethered on fire fighting truck 1105.After the lift-off of four axis unmanned planes 1108, when climbing
Discharge thin cord 1104.When rising to 1109 roof position of building, after reaching reserved 1101 position of gate frame, four axis unmanned planes
1108, which draw thin cord 1104, penetrates gate frame 1101, and flies upwards, wind half cycle after fall, by thin cord 1104 around
Cross gate frame 1101.Then, one end that four axis unmanned planes 1108 carry thin cord 1104 is landed, and by one end of thin cord 1104
It is wound on the electric coil winder in fire fighting truck 1105.Later, four axis unmanned planes 1108 instruction electric coil winder winds thin cord
1104, to the hawser rope 1103 for being connected to thin cord 1104 above be mentioned, until hawser rope 1103 passes through roof gate frame 1101
Afterwards, ground is reached.Then, the driving of four axis unmanned planes, 1108 order-driven device penetrates the fire-fighting jigger 1106 of hawser rope 1103
It is soaring along hawser rope 1103,1107 band of fire extinguisher on fire-fighting jigger 1106 to ignition point 1102 is nearby implemented to go out
Fire.
Flying vehicles control method provided by the embodiment of the utility model, building self structure and unmanned plane are combined, and are led to
The traction device for pullling lighter in weight using aircraft is crossed, weight and the biggish toter of load capacity is driven to reach kindling
Point, on the one hand, due to the lighter in weight of traction device, lower, another aspect is required unmanned plane, it can by toter
To improve the load capacity of unmanned plane and band is made to carry equipment diversification, in addition, toter can such as be formed with multipurpose
Personnel flee from channel, so that unmanned plane plays bigger effect in fire extinguishing procedure.
Figure 11 is please referred to, Figure 11 is the hardware configuration signal for the electronic flight device that an embodiment of the present invention provides
Figure.
Electronic flight device as described in this embodiment, comprising:
Memory 601, processor 602 and it is stored in the computer journey that can be run on memory 601 and on processor 602
Sequence when processor 602 executes the computer program, realizes flying vehicles control side described in earlier figures 3 and embodiment illustrated in fig. 4
Method.
Further, electronic device further include: at least one input equipment 603 and at least one output equipment 604.
Above-mentioned memory 601, processor 602, input equipment 603 and output equipment 604, are connected by bus 605.
Wherein, input equipment 603 concretely camera, microphone etc..Output equipment 604 concretely indicator light,
Radiofrequency signal R-T unit etc..
Memory 601 can be high random access memory body (RAM, Random Access Memory) memory,
It can be non-labile memory (non-volatile memory), such as magnetic disk storage.Memory 601 is for storing one
Group executable program code, processor 602 are coupled with memory 601.
Further, the utility model embodiment additionally provides a kind of computer readable storage medium, this is computer-readable
Storage medium can be in the electronic device being set in the various embodiments described above, which can be aforementioned
Memory in embodiment illustrated in fig. 11.It is stored with computer program on the computer readable storage medium, the program is processed
Flying vehicles control method described in earlier figures 3 and embodiment illustrated in fig. 4 is realized when device executes.Further, which can
Storage medium can also be USB flash disk, mobile hard disk, read-only memory (ROM, Read-Only Memory), RAM, magnetic disk or light
The various media that can store program code such as disk.
In the above-described embodiments, it all emphasizes particularly on different fields to the description of each embodiment, there is no the portion being described in detail in some embodiment
Point, it may refer to the associated description of other embodiments.
The above are the descriptions to fire extinguishing system provided by the utility model, for those skilled in the art, according to this
The thought of utility model embodiment, there will be changes in the specific implementation manner and application range, to sum up, in this specification
Appearance should not be construed as a limitation of the present invention.
Claims (9)
1. a kind of fire extinguishing system characterized by comprising aircraft, traction device and toter；
The traction device, for drawing the toter, one end is fixed on the aircraft, and the other end connects the fortune
It carries and sets；
The weight and load capacity of the traction device are less than the weight and load capacity of the toter；
Wherein, the traction device and the toter are rope, and the diameter of the rope as the traction device is less than
The diameter of rope as the toter.
2. fire extinguishing system as described in claim 1, which is characterized in that the traction device and the toter are resistance to height
Warm material, alternatively, the outer surface of the traction device and the toter is coated with heat-resisting material.
3. fire extinguishing system as described in claim 1, which is characterized in that the system also includes:
Band carries equipment, is mounted on the toter, including fire-extinguishing apparatus and/or lowering rope device.
4. fire extinguishing system as claimed in claim 3, which is characterized in that
The fire-extinguishing apparatus is fixed on the bottom of the toter；Alternatively,
It is provided with driving device on the fire-extinguishing apparatus or the lowering rope device, for driving the fire-extinguishing apparatus or the slip rope
Device is soaring along the toter.
5. fire extinguishing system according to any one of claims 1 to 4, which is characterized in that the system also includes:
Guide structure is fixed on the top or exterior wall of building, has frame-type opening；
A part of the traction device returns to ground via the guide structure under the traction of the aircraft.
6. fire extinguishing system as claimed in claim 5, which is characterized in that the system also includes:
Towing device, including fixed structure；
One end of the traction device is fixed on the fixed structure under the traction of the aircraft.
7. system as claimed in claim 5, which is characterized in that the system also includes: fixed device；
One end that the toter is not connect with the traction device is fixed on the fixed device.
8. system as claimed in claim 5, which is characterized in that the system also includes:
Bobbin winder device is arranged on the aircraft；
The traction device realizes that described one end is fixed on the aircraft by being wrapped on the bobbin winder device.
9. system as claimed in claim 5, which is characterized in that the system also includes:
Sender unit is mounted on the guide structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820743450.3U CN208975034U (en) | 2018-05-18 | 2018-05-18 | Fire extinguishing system |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820743450.3U CN208975034U (en) | 2018-05-18 | 2018-05-18 | Fire extinguishing system |
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| CN208975034U true CN208975034U (en) | 2019-06-14 |
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| CN201820743450.3U Active CN208975034U (en) | 2018-05-18 | 2018-05-18 | Fire extinguishing system |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108853839A (en) * | 2018-05-18 | 2018-11-23 | 深圳市易飞方达科技有限公司 | Fire extinguishing system, flying vehicles control method and computer readable storage medium |
| CN110435890A (en) * | 2019-07-02 | 2019-11-12 | 上海鲲哥无人机科技有限公司 | A kind of fire-fighting fire extinguishing platform based on aircraft |
| CN110465011A (en) * | 2019-07-02 | 2019-11-19 | 上海鲲哥无人机科技有限公司 | A kind of deployment device of fire-fighting rope |
| CN110502029A (en) * | 2019-07-02 | 2019-11-26 | 上海鲲哥无人机科技有限公司 | Rope lift control method based on aircraft |
-
2018
- 2018-05-18 CN CN201820743450.3U patent/CN208975034U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108853839A (en) * | 2018-05-18 | 2018-11-23 | 深圳市易飞方达科技有限公司 | Fire extinguishing system, flying vehicles control method and computer readable storage medium |
| CN110435890A (en) * | 2019-07-02 | 2019-11-12 | 上海鲲哥无人机科技有限公司 | A kind of fire-fighting fire extinguishing platform based on aircraft |
| CN110465011A (en) * | 2019-07-02 | 2019-11-19 | 上海鲲哥无人机科技有限公司 | A kind of deployment device of fire-fighting rope |
| CN110502029A (en) * | 2019-07-02 | 2019-11-26 | 上海鲲哥无人机科技有限公司 | Rope lift control method based on aircraft |
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