CN108031048A - The fire-fighting equipment of crash resistance enhancing based on unmanned plane - Google Patents
The fire-fighting equipment of crash resistance enhancing based on unmanned plane Download PDFInfo
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- CN108031048A CN108031048A CN201711274330.XA CN201711274330A CN108031048A CN 108031048 A CN108031048 A CN 108031048A CN 201711274330 A CN201711274330 A CN 201711274330A CN 108031048 A CN108031048 A CN 108031048A
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- vehicle body
- aerial vehicle
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- 229920000049 Carbon (fiber) Polymers 0.000 claims abstract description 8
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- 229920001971 elastomer Polymers 0.000 claims abstract description 8
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- 239000003973 paint Substances 0.000 claims description 15
- 229920002635 polyurethane Polymers 0.000 claims description 14
- 239000004814 polyurethane Substances 0.000 claims description 14
- PRPAGESBURMWTI-UHFFFAOYSA-N [C].[F] Chemical compound [C].[F] PRPAGESBURMWTI-UHFFFAOYSA-N 0.000 claims description 13
- 239000000126 substance Substances 0.000 claims description 6
- 239000007788 liquid Substances 0.000 claims description 5
- 238000004891 communication Methods 0.000 claims description 4
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- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims 1
- YCKRFDGAMUMZLT-UHFFFAOYSA-N Fluorine atom Chemical compound [F] YCKRFDGAMUMZLT-UHFFFAOYSA-N 0.000 claims 1
- 229910052799 carbon Inorganic materials 0.000 claims 1
- 229910052731 fluorine Inorganic materials 0.000 claims 1
- 239000011737 fluorine Substances 0.000 claims 1
- 238000012549 training Methods 0.000 abstract description 41
- 238000005516 engineering process Methods 0.000 description 6
- 230000006378 damage Effects 0.000 description 5
- 238000012544 monitoring process Methods 0.000 description 4
- 230000009931 harmful effect Effects 0.000 description 3
- 238000013507 mapping Methods 0.000 description 3
- 230000002265 prevention Effects 0.000 description 3
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- 238000010586 diagram Methods 0.000 description 2
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- 230000005484 gravity Effects 0.000 description 2
- 230000000415 inactivating effect Effects 0.000 description 2
- 230000002779 inactivation Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
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Classifications
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- A—HUMAN NECESSITIES
- A62—LIFE-SAVING; FIRE-FIGHTING
- A62C—FIRE-FIGHTING
- A62C37/00—Control of fire-fighting equipment
- A62C37/50—Testing or indicating devices for determining the state of readiness of the equipment
-
- A—HUMAN NECESSITIES
- A62—LIFE-SAVING; FIRE-FIGHTING
- A62C—FIRE-FIGHTING
- A62C99/00—Subject matter not provided for in other groups of this subclass
- A62C99/0081—Training methods or equipment for fire-fighting
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D—PROCESSES FOR APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D7/00—Processes, other than flocking, specially adapted for applying liquids or other fluent materials to particular surfaces or for applying particular liquids or other fluent materials
- B05D7/50—Multilayers
- B05D7/56—Three layers or more
- B05D7/58—No clear coat specified
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
-
- 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
-
- 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
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
-
- G—PHYSICS
- G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
- G09B—EDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
- G09B9/00—Simulators for teaching or training purposes
- G09B9/02—Simulators for teaching or training purposes for teaching control of vehicles or other craft
- G09B9/08—Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer
- G09B9/085—Special purpose teaching, e.g. alighting on water, aerial photography
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D—PROCESSES FOR APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D2503/00—Polyurethanes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D—PROCESSES FOR APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D2506/00—Halogenated polymers
- B05D2506/10—Fluorinated polymers
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Business, Economics & Management (AREA)
- Health & Medical Sciences (AREA)
- Theoretical Computer Science (AREA)
- Emergency Management (AREA)
- Public Health (AREA)
- Educational Technology (AREA)
- Mechanical Engineering (AREA)
- Life Sciences & Earth Sciences (AREA)
- Wood Science & Technology (AREA)
- General Physics & Mathematics (AREA)
- Educational Administration (AREA)
- Physics & Mathematics (AREA)
- Manipulator (AREA)
Abstract
The invention discloses a kind of fire-fighting equipment of the crash resistance enhancing based on unmanned plane, including：Unmanned aerial vehicle body, has been internally formed accommodating space；First pair of wing, is arranged on unmanned aerial vehicle body；Second pair of wing, positioned at the rear portion of first pair of wing；Fluid passage, including extended to the first and second pipelines, one end and the accommodating space fluid connection of the first pipeline, the other end outside fuselage, one end of second pipe is connected with the other end of the first pipeline；Pump, water inlet are connected with accommodating space, and water outlet is connected with fluid passage, is arranged in the upper inside walls of unmanned aerial vehicle body；Cushion is arranged at the outside of protective coating, is coated on unmanned aerial vehicle body, be disposed with from outside to inside the elastic rubber layer of 5~15mm of thickness, 5~15mm of thickness 5~15mm of spongy layer and thickness carbon fiber layer.The present invention can improve training effectiveness, and unmanned aerial vehicle body can receive protection, and crash resistance improves, and has fire-fighting function.
Description
Technical field
The present invention relates to a kind of fire-fighting domain.It is more particularly related to a kind of crash resistance based on unmanned plane increases
Strong fire-fighting equipment.
Background technology
Fire refers in the time or spatially out of control disastrous combustion phenomena.In various disasters, fire is most
Often, one of major casualty of public security and social development is most generally threatened.With the development of society, building is increasingly
Height, fire also happen occasionally.Many buildings catch fire in high level, to bring extreme difficulties for the rescue of fire fighter, being easy to
Cause casualties and financial losses.
Various UAVs are to utilize radio robot and the presetting apparatus provided for oneself referred to as " unmanned plane "
The not manned aircraft manipulated, or fully or intermittently independently operated by car-mounted computer.At present take photo by plane, agricultural, plant
Guarantor, miniature self-timer, express transportation, disaster relief, observation wild animal, monitoring infectious disease, mapping, news report, electric inspection process,
The disaster relief, movies-making, manufacture romance etc. technical field, have greatly expanded the purposes of unmanned plane in itself.Therefore, how to provide
A kind of unmanned plane that can sow extinguishing chemical is particularly important, meanwhile, the unmanned plane of various functions needs before coming into operation
The fire-fighting equipment for having a crash resistance enhancing based on unmanned plane is trained it, and the unmanned plane for making to be trained to has required
The function of wanting, therefore, requirement of the fire-fighting equipment that the crash resistance based on unmanned plane strengthens for crash resistance, stability are very high, and
The fire-fighting equipment for being currently based on the crash resistance enhancing of unmanned plane can only instruct same unmanned plane to be trained in the same time
Practice, the training of the unmanned plane of multiple unmanned planes even multiple functions can not be realized by a unmanned plane.
The content of the invention
It is excellent it is an object of the invention to solve at least the above and/or defect, and provide at least to will be described later
Point.
A further object of the invention is the fire-fighting equipment of the crash resistance enhancing based on unmanned plane, it can be used in fire-fighting,
Fire-fighting efficiency and training effectiveness are improved, and unmanned aerial vehicle body can receive protection, crash resistance improves.
In order to realize these purposes and further advantage according to the present invention, there is provided a kind of crash resistance based on unmanned plane increases
Strong fire-fighting equipment, including：
Unmanned aerial vehicle body, it includes fuselage cover and coated in the protective coating outside the fuselage cover, the protection
Coating include successively from outside to inside thick 50~70 μm fluorine carbon finishing paint, zinc yellow acrylic polyurethane primer layer 10~20 μm thick,
Fluorine carbon finishing paint layer 40~50 μm thick and zinc yellow acrylic polyurethane primer layer 5~12 μm thick, the fuselage cover is using illiteracy
Scytoblastema material, the unmanned aerial vehicle body are internally formed the accommodating space for accommodating extinguishing chemical；
Fluid passage, it is included with the first pipeline of the accommodating space fluid connection and perpendicular to first pipeline
Second pipe, one end of first pipeline and the accommodating space fluid connection, and the other end extends to the unmanned plane machine
Outside body, the other end of one end of the second pipe vertically with first pipeline is connected, the second pipe it is another
At one end is provided with check valve, and the check valve defines the side that liquid is flowed out from the accommodating space to outside the fluid passage
To；
Pump, its water inlet is connected with the accommodating space, and water outlet is connected with the fluid passage, and the pump is arranged at
In the upper inside walls of the unmanned aerial vehicle body；
First pair of wing, it is symmetrically disposed on the unmanned aerial vehicle body；
Second pair of wing, it is symmetrically disposed on the unmanned aerial vehicle body, and second pair of wing is located at first pair of wing
Rear portion, and second pair of wing is higher than first pair of wing in the height of vertical direction；
First pair and second pair of motor cabinet, described first pair and second pair of motor cabinet are each fixed on described respectively symmetrically
On unmanned aerial vehicle body, and respectively positioned at the front side of first pair of wing and second pair of wing；
First pair and second pair of motor, described first pair and second pair of motor are each respectively correspondingly arranged at described first
Pair and second pair of motor cabinet on；
First and second connecting rods, the both ends of first and second connecting rod are each individually fixed in the same side
On one of wing of first pair of wing and one of wing of second pair of wing；
First pair and second pair of propeller, first pair of propeller are rotationally arranged at first and second connecting rod
At one end, and second pair of propeller is rotationally arranged at the second end of first and second connecting rod, described
A pair of and second pair of propeller is each electrically connected with described first Dui and second pair of motor respectively；
Wherein, be additionally provided with cushion, the cushion is arranged at the outside of the protective coating, be coated on it is described nobody
On machine fuselage, the cushion is disposed with the elastic rubber layer of 5~15mm of thickness, the sea of 5~15mm of thickness from outside to inside
The carbon fiber layer of 5~15mm of continuous layer and thickness.
Preferably, the fire-fighting equipment of the crash resistance enhancing based on unmanned plane, further includes：
Multiple slots, it is opened in the top of the unmanned aerial vehicle body, and the multiple slot is along the unmanned aerial vehicle body
Y direction is set, and the interface of at least one chip is provided with each slot, the slot from its closed section to its
The internal diameter of openend is less and less；
Multiple closure bodies, it corresponds with the slot and sets, and described closure body one end is connected with the slot,
And the other end can be opened and closed to close the opening of the slot.
Preferably, in the fire-fighting equipment of the crash resistance enhancing based on unmanned plane, second pair of wing is in vertical
The height in direction is higher than first pair of wing.
Preferably, in the fire-fighting equipment of the crash resistance enhancing based on unmanned plane, the cushion is from outside to inside
It is disposed with the carbon fiber layer of the elastic rubber layer of thickness 10mm, the spongy layer of thickness 10mm and thickness 10mm.
Preferably, the fire-fighting equipment of the crash resistance enhancing based on unmanned plane, further includes：
Wireless communication module, it is arranged at the inside of the unmanned plane.
Preferably, the fire-fighting equipment of the crash resistance enhancing based on unmanned plane, further includes：
Fixed part, its one end are movably arranged on the first or second connecting rod, and the other end is connected with rotation axis,
The rotation axis is connected with the propeller.
Preferably, in the fire-fighting equipment of the crash resistance enhancing based on unmanned plane, the protective coating is from extroversion
Inside include fluorine carbon finishing paint 60 μm thick, zinc yellow acrylic polyurethane primer layer 15 μm thick, fluorine carbon finishing paint layer 45 μm thick successively
With zinc yellow acrylic polyurethane primer layer 8 μm thick.
The present invention includes at least following beneficial effect：
The present invention is provided with fluid passage and pump, and under the drive of pump, the extinguishing chemical in accommodating space is led to by liquid
Road ejects, and for inactivating, substantially increases time when inactivation starts, it is existing to avoid casualties and financial losses etc.
As protecting fire fighter's safety and people life property safety.
Second pair of wing of the present invention is higher than first pair of wing in the height of vertical direction；To reduce the air-flow of first pair of wing
Harmful effect to second pair of wing, lifts the arrangement lift of aircraft.
The present invention cushion can the fire-fighting equipment is out of control fall when, protect its fuselage and other important components, with
Exempt to crash, to reduce loss to the greatest extent.
Multiple slots of the present invention are used to receiving and protecting chip, unmanned plane training can be set to include in chip interior
Hold, such as：Professional unmanned plane airmanship training, the training of unmanned plane camera work, fixed-wing unmanned plane drive skill
Art and manipulation technology training, what the training comprising single-rotor helicopter, unmanned plane hanging strip width operated uses training, unmanned plane long distance
From monitoring system training, unmanned plane mapping training, unmanned electro-mechanical force cruise training, unmanned plane come reconnoitre the condition of a disaster or fire prevention training and
Traffic police the functions such as police training such as is directed traffic with unmanned plane, and multiple inserting for chip can be replaced at any time since the unmanned plane is provided with
Groove, therefore the chip containing related training content can be inserted into as needed, to train unmanned plane, simultaneously as being provided with multiple
Slot, therefore, can receive multiple chips, complete the training to other unmanned planes or to itself.Meanwhile the aperture of the slot is got over
It is next smaller, it is easy to the protection to chip, and prevent destruction when falling to its internals.
The equipment of the present invention has fire-fighting function, substantially increases fire-fighting efficiency and fire-fighting efficiency, with strong points, accuracy
It is high.
Further advantage, target and the feature of the present invention embodies part by following explanation, and part will also be by this
The research and practice of invention and be understood by the person skilled in the art.
Brief description of the drawings
Fig. 1 is the structural representation of the fire-fighting equipment of the crash resistance enhancing based on unmanned plane in one embodiment of the present of invention
Figure；
Fig. 2 is the structure diagram of protective coating in one embodiment of the present of invention；
Fig. 3 is the structure diagram of cushion in one embodiment of the invention.
Embodiment
The present invention is described in further detail below in conjunction with the accompanying drawings, to make those skilled in the art with reference to specification text
Word can be implemented according to this.
It should be appreciated that such as " having ", "comprising" and " comprising " term used herein do not allot one or more
The presence or addition of a other elements or its combination.
Fig. 1,2,3 show a kind of way of realization according to the present invention, and the fire-fighting of the crash resistance enhancing based on unmanned plane is set
It is standby, including：
Unmanned aerial vehicle body 1；Unmanned aerial vehicle body pattern, it includes fuselage cover and coated in the guarantor outside the fuselage cover
Coating is protected, the protective coating includes fluorine carbon finishing paint 50~70 μm thick, zinc yellow propylene 10~20 μm thick successively from outside to inside
Sour polyurethane primer layer, fluorine carbon finishing paint layer 40~50 μm thick and zinc yellow acrylic polyurethane primer layer 5~12 μm thick, it is described
Fuselage cover uses skin substrate.The unmanned aerial vehicle body is internally formed the accommodating space for accommodating extinguishing chemical.
Fluid passage, it is included with the first pipeline 20 of the accommodating space fluid connection and perpendicular to first pipeline
20 second pipe 21, one end of first pipeline 20 and the accommodating space fluid connection, and the other end extend to it is described
Outside unmanned aerial vehicle body, the other end of one end of the second pipe 21 vertically with first pipeline 20 is connected, described
It is provided with check valve at the other end of second pipe 21, the check valve defines liquid from the accommodating space to the liquid
The direction flowed out outside passage；Second pipe 21 may be configured as hose, in this way, when the fire-fighting equipment of the present invention flies above sky
When, second pipe 21 vertically downward, can spray water against the place to catch fire naturally.
Pump, its water inlet is connected with the accommodating space, and water outlet is connected with the fluid passage, and the pump is arranged at
In the upper inside walls of the unmanned aerial vehicle body.Under the drive of pump, the extinguishing chemical in accommodating space is sprayed by fluid passage
Out, for inactivating, substantially increasing time when inactivation starts, avoid casualties and financial losses phenomena such as, protection
Fire fighter's safety and people life property safety.
First pair of wing 2,3, it is symmetrically disposed on the both sides of the unmanned aerial vehicle body；
Second pair of wing 4,5, it is symmetrically disposed on the both sides of the unmanned aerial vehicle body, and second pair of wing is positioned at described the
The rear portion of a pair of of wing, and second pair of wing is higher than first pair of wing in the height of vertical direction；With first pair of wing of reduction
Harmful effect of the air-flow to second pair of wing, lifts the arrangement lift of aircraft.
First pair and second pair of motor cabinet, described first pair and second pair of motor cabinet are each fixed on described respectively symmetrically
On unmanned aerial vehicle body, and respectively positioned at the front side of first pair of wing and second pair of wing；
First pair and second pair of motor 7,8,9,10, described first pair and second pair of motor are each respectively correspondingly arranged at
On described first pair and second pair of motor cabinet；
First and second connecting rods 11,12, the both ends of first and second connecting rod are each individually fixed in together
On one of wing of first pair of wing of side and one of wing of second pair of wing；
First pair and second pair of propeller 13,14,15,16, first pair of propeller are rotationally arranged at first He
The at one end of second connecting rod, and second pair of propeller is rotationally arranged at the second of first and second connecting rod
At end, described first pair and second pair of propeller are each electrically connected with described first Dui and second pair of motor respectively.Using this
Scheme, which has, enables to unmanned plane voluntarily to take off.Also, this mode is a kind of explanation of preferred embodiments, but is not limited to
In this.When implementing the present invention, suitable motor cabinet can be set according to the pattern of user's demand motor, and needed for setting
The propeller of shape；
Wherein, be additionally provided with cushion, the cushion is arranged at the outside of the protective coating, be coated on it is described nobody
On machine fuselage, the cushion is disposed with the elastic rubber layer 17 of 5~15mm of thickness, 5~15mm of thickness from outside to inside
The carbon fiber layer 19 of 5~15mm of spongy layer 18 and thickness.The present invention cushion can the fire-fighting equipment is out of control fall when, protect
Its fuselage and other important components are protected, in order to avoid crash, to reduce loss to the greatest extent.
In the present invention in one embodiment, preferably, further including：
Multiple slots 6, it is opened in the top of the unmanned aerial vehicle body, prevents from causing damage to it when unmanned plane from falling.
The multiple slot is set along the y direction of the unmanned aerial vehicle body, and is provided with least one chip in each slot
Interface, internal diameter of the slot from its closed section to its openend be less and less；The plurality of slot is used to receiving and protecting core
Piece, the content that unmanned plane training can be set in chip to include, such as：Professional unmanned plane airmanship training, unmanned plane
Camera work of taking photo by plane training, fixed-wing unmanned plane driving technology and manipulation technology training, training, nothing comprising single-rotor helicopter
Man-machine hanging strip width operation is patrolled with training, the training of unmanned plane remote monitoring system, unmanned plane mapping training, unmanned electro-mechanical force
Boat training, unmanned plane the functions such as police training such as are directed traffic to reconnoitre the condition of a disaster or fire prevention training and traffic police with unmanned plane, due to
The unmanned plane is provided with multiple slots that can replace chip at any time, therefore can be inserted into the core containing related training content as needed
Piece, to train unmanned plane, simultaneously as being provided with multiple slots, therefore, can receive multiple chips, complete to other unmanned planes
Or the training to itself.Meanwhile the aperture of the slot is less and less, it is easy to the protection to chip, and prevents when falling pair
The destruction of its internals.
Multiple closure bodies, it corresponds with the slot and sets, and described closure body one end is connected with the slot,
And the other end can be opened and closed to close the opening of the slot.Preferably to protect slot and its inner member.In the present invention wherein
In one embodiment, preferably, the motor cabinet uses aeronautical material.So as to mitigate the quality of unmanned plane, easy to take off.
In the present invention in one embodiment, preferably, the cushion is disposed with thickness from outside to inside
The carbon fiber layer 19 of the elastic rubber layer 17 of 10mm, the spongy layer 18 of thickness 10mm and thickness 10mm.
In the present invention in one embodiment, preferably, the closure body is made of elastic material.To play
Flexibly protect internals and closing preferably effect.Second pair of wing is higher than described first pair in the height of vertical direction
The wing.
In the present invention in one embodiment, preferably, further including：
Wireless communication module, it is arranged at the inside of the unmanned plane.For being communicated with other unmanned planes.It can adopt
With modes such as WIFI, bluetooths.
In the present invention in one embodiment, preferably, further including：
Fixed part, its one end are movably arranged on the first or second connecting rod, and the other end is connected with rotation axis,
The rotation axis is connected with the propeller.To realize the rotation of propeller, and propeller can be adjusted in the position on unmanned plane
Put.The distance of first pair and the center of gravity of second pair of propeller and unmanned aerial vehicle body is equal.
In such scheme, preferably, the protective coating includes fluorine carbon finishing paint 60 μm thick successively from outside to inside
110th, zinc yellow acrylic polyurethane primer layer 120 15 μm thick, fluorine carbon finishing paint layer 130 45 μm thick and zinc yellow propylene 8 μm thick
Sour polyurethane primer layer 140.
To make those skilled in the art more fully understand technical scheme, examples below is now provided and is said
It is bright：
The fire-fighting equipment of crash resistance enhancing based on unmanned plane, including：
Unmanned aerial vehicle body 1；Unmanned plane unmanned aerial vehicle body pattern.Outside including fuselage cover and coated in the fuselage cover
Protective coating, the protective coating includes thick 60 μm of fluorine carbon finishing paint 110, zinc yellow acrylic acid 15 μm thick successively from outside to inside
Polyurethane primer layer 120, fluorine carbon finishing paint layer 130 45 μm thick and zinc yellow acrylic polyurethane primer layer 140 8 μm thick, it is described
Fuselage cover uses skin substrate.First pair of wing 2,3, it is symmetrically disposed on the both sides of the unmanned aerial vehicle body；Second pair of wing
4,5, it is symmetrically disposed on the both sides of the unmanned aerial vehicle body, and second pair of wing is located at the rear portion of first pair of wing, and
Second pair of wing is higher than first pair of wing in the height of vertical direction；To reduce the air-flow of first pair of wing to second pair of wing
Harmful effect, lifts the arrangement lift of aircraft.Multiple slots 6, it is opened in the top of the unmanned aerial vehicle body, prevents unmanned plane
Cause damage when falling to it.The multiple slot is set along the y direction of the unmanned aerial vehicle body, and each slot
The interface of at least one chip is inside provided with, internal diameter of the slot from its closed section to its openend is less and less；It is the plurality of
Slot is used to receiving and protecting chip, the content that unmanned plane training can be set to include in chip, such as：Professional unmanned plane
Airmanship training, the training of unmanned plane camera work, fixed-wing unmanned plane driving technology and manipulation technology training, include list
What the training of heligyro, unmanned plane hanging strip width operated surveys with training, the training of unmanned plane remote monitoring system, unmanned plane
Paint training, the cruise of unmanned electro-mechanical force is trained, unmanned plane is directed traffic to reconnoitre the condition of a disaster or fire prevention training and traffic police with unmanned plane
The functions such as police training, since the unmanned plane is provided with multiple slots that can replace chip at any time, can be inserted into as needed
Chip containing related training content, to train unmanned plane, simultaneously as being provided with multiple slots, therefore, can receive multiple cores
Piece, completes the training to other unmanned planes or to itself.Meanwhile the aperture of the slot is less and less, it is easy to the guarantor to chip
Shield, and prevent destruction when falling to its internals.Multiple closure bodies, it corresponds with the slot and sets, institute
Closure body one end is stated to be connected with the slot, and the other end can be opened and closed to close the opening of the slot.Preferably to protect
Slot and its inner member.First pair and second pair of motor cabinet, described first pair and second pair of motor cabinet it is each respectively symmetrically solid
Due on the unmanned aerial vehicle body, and respectively positioned at the front side of first pair of wing and second pair of wing；First pair and second pair of electricity
Machine 7,8,9,10, described first pair and second pair of motor are each respectively correspondingly arranged at described first pair and second pair of motor cabinet
On；First and second connecting rods 11,12, the both ends of first and second connecting rod are each individually fixed in the same side
On one of wing of first pair of wing and one of wing of second pair of wing；First pair and second pair of propeller 13,14,15,16,
First pair of propeller is rotationally arranged at the at one end of first and second connecting rod, and second pair of propeller is rotatable
Ground is arranged at the second end of first and second connecting rod, described first pair and second pair of propeller each respectively with institute
State first pair and second pair of motor is electrically connected.Being had using this scheme enables to unmanned plane voluntarily to take off.Also, this side
Formula is a kind of explanation of preferred embodiments, but is not limited thereto.
Wherein, be additionally provided with cushion, the cushion is arranged at the outside of the protective coating, be coated on it is described nobody
On machine fuselage, cushion is disposed with 18 and of spongy layer of the elastic rubber layer 17 of thickness 10mm, thickness 10mm from outside to inside
The carbon fiber layer 19 of thickness 10mm.
When implementing the present invention, suitable motor cabinet can be set, and set institute according to the pattern of user's demand motor
Need the propeller of shape.The motor cabinet uses aeronautical material.So as to mitigate the quality of unmanned plane, easy to take off.The envelope
Lid is closed to be made of elastic material.To play the role of flexibly protecting internals and closing more preferable.Wireless communication module, its
It is arranged at the inside of the unmanned plane.For being communicated with other unmanned planes.The modes such as WIFI, bluetooth can be used.It is fixed
Portion, its one end are movably arranged on the first or second connecting rod, and other end connection is with rotation axis, the rotation axis with
The propeller connection.To realize the rotation of propeller, and propeller can be adjusted in the position on unmanned plane.First pair and
The distance of the center of gravity of two pairs of propellers and unmanned plane is equal.
The equipment of the present invention has fire-fighting function, substantially increases fire-fighting efficiency and fire-fighting efficiency, with strong points, accuracy
It is high.
Number of devices and treatment scale described herein are the explanations for simplifying the present invention.To the present invention based on nothing
The application of the fire-fighting equipment of man-machine crash resistance enhancing, modifications and variations are apparent to one skilled in the art
's.
Although embodiment of the present invention is disclosed as above, it is not restricted in specification and embodiment listed
With.It can be applied to various suitable the field of the invention completely., can be easily for those skilled in the art
Realize other modification.Therefore it is of the invention and unlimited under the universal limited without departing substantially from claim and equivalency range
In specific details and shown here as the legend with description.
Claims (7)
1. the fire-fighting equipment of the crash resistance enhancing based on unmanned plane, it is characterised in that including：
Unmanned aerial vehicle body, it includes fuselage cover and coated in the protective coating outside the fuselage cover, the protective coating
Include fluorine carbon finishing paint 50~70 μm thick, zinc yellow acrylic polyurethane primer layer 10~20 μm thick, thickness 40 successively from outside to inside
~50 μm of fluorine carbon finishing paint layer and zinc yellow acrylic polyurethane primer layer 5~12 μm thick, the fuselage cover use covering base
Material, the unmanned aerial vehicle body are internally formed the accommodating space for accommodating extinguishing chemical；
Fluid passage, it includes second with the first pipeline of the accommodating space fluid connection and perpendicular to first pipeline
Pipeline, one end of first pipeline and the accommodating space fluid connection, and the other end is extended to outside the unmanned aerial vehicle body,
The other end of the one end of the second pipe vertically with first pipeline is connected, at the other end of the second pipe
Check valve is provided with, the check valve defines the direction that liquid is flowed out from the accommodating space to outside the fluid passage；
Pump, its water inlet is connected with the accommodating space, and water outlet is connected with the fluid passage, and the pump is arranged at described
In the upper inside walls of unmanned aerial vehicle body；
First pair of wing, it is symmetrically disposed on the unmanned aerial vehicle body；
Second pair of wing, it is symmetrically disposed on the unmanned aerial vehicle body, after second pair of wing is located at first pair of wing
Portion；
First pair and second pair of motor cabinet, described first pair and second pair of motor cabinet be each fixed on respectively symmetrically it is described nobody
On machine fuselage, and respectively positioned at the front side of first pair of wing and second pair of wing；
First pair and second pair of motor, described first pair and second pair of motor be each respectively correspondingly arranged at described first pair and
On second pair of motor cabinet；
First and second connecting rods, the both ends of first and second connecting rod are each individually fixed in the first of the same side
To on one of wing of one of wing of the wing and second pair of wing；
First pair and second pair of propeller, first pair of propeller are rotationally arranged at the one of first and second connecting rod
At end, and second pair of propeller is rotationally arranged at the second end of first and second connecting rod, described first pair
Each it is electrically connected respectively with described first Dui and second pair of motor with second pair of propeller；
Wherein, cushion is additionally provided with, the cushion is arranged at the outside of the protective coating, is coated on the unmanned plane machine
With, the cushion is disposed with the elastic rubber layer of 5~15mm of thickness, the spongy layer of 5~15mm of thickness from outside to inside
With the carbon fiber layer of 5~15mm of thickness.
2. the fire-fighting equipment of the crash resistance enhancing based on unmanned plane as claimed in claim 1, it is characterised in that further include：
Multiple slots, it is opened in the top of the unmanned aerial vehicle body, the longitudinal axis of the multiple slot along the unmanned aerial vehicle body
Direction is set, and the interface of at least one chip is provided with each slot, and the slot is open from its closed section to it
The internal diameter at end is less and less；
Multiple closure bodies, it corresponds with the slot and sets, and described closure body one end is connected with the slot, and another
One end can be opened and closed to close the opening of the slot.
3. the fire-fighting equipment of the crash resistance enhancing based on unmanned plane as claimed in claim 1, it is characterised in that described second pair
The wing is higher than first pair of wing in the height of vertical direction.
4. the fire-fighting equipment of the crash resistance enhancing based on unmanned plane as claimed in claim 2, it is characterised in that the cushion
The carbon fiber layer of the elastic rubber layer of thickness 10mm, the spongy layer of thickness 10mm and thickness 10mm is disposed with from outside to inside.
5. the fire-fighting equipment of the crash resistance enhancing based on unmanned plane as claimed in claim 2, it is characterised in that further include：
Wireless communication module, it is arranged at the inside of the unmanned plane.
6. the fire-fighting equipment of the crash resistance enhancing based on unmanned plane as claimed in claim 2, it is characterised in that further include：
Fixed part, its one end are movably arranged on the first or second connecting rod, and other end connection is with rotation axis, described
Rotation axis is connected with the propeller.
7. the fire-fighting equipment of the crash resistance enhancing based on unmanned plane as claimed in claim 1, it is characterised in that the protection applies
Layer includes fluorine carbon finishing paint 60 μm thick, zinc yellow acrylic polyurethane primer layer 15 μm thick, fluorine 45 μm thick successively from outside to inside
Carbon finishing paint layer and zinc yellow acrylic polyurethane primer layer 8 μm thick.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711274330.XA CN108031048A (en) | 2017-12-06 | 2017-12-06 | The fire-fighting equipment of crash resistance enhancing based on unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711274330.XA CN108031048A (en) | 2017-12-06 | 2017-12-06 | The fire-fighting equipment of crash resistance enhancing based on unmanned plane |
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| Publication Number | Publication Date |
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| CN108031048A true CN108031048A (en) | 2018-05-15 |
Family
ID=62095612
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| Application Number | Title | Priority Date | Filing Date |
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| CN201711274330.XA Pending CN108031048A (en) | 2017-12-06 | 2017-12-06 | The fire-fighting equipment of crash resistance enhancing based on unmanned plane |
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Application publication date: 20180515 |