CN207374668U - Remove the snow unmanned plane - Google Patents
Remove the snow unmanned plane Download PDFInfo
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- CN207374668U CN207374668U CN201721491218.7U CN201721491218U CN207374668U CN 207374668 U CN207374668 U CN 207374668U CN 201721491218 U CN201721491218 U CN 201721491218U CN 207374668 U CN207374668 U CN 207374668U
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- unmanned plane
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Abstract
The utility model discloses a kind of snow removing unmanned plane, including：Head；Fuselage, inside along material transferring direction successively be equipped with storing hopper, guide auger and discharge unit；A pair of of flank, free end are equipped with the second motor；A pair of of balance wing, free end are equipped with the 3rd motor；Tailstock is balanced, extends frame, a pair of of empennage and connecting plate including a pair；Wherein, the line of the second motor positioned at one side and the 3rd motor positioned at opposite side is that the line of the first line, the 3rd motor positioned at one side and the second motor positioned at opposite side is the second line, and the crosspoint of the first line and the second line falls in the floor projection of the fuselage.The utility model can keep good stability and balance quality in the case where loading and unloading deicing salt, have the advantages that spreading scope is wide, reliability is high.
Description
Technical field
The utility model is related to vehicle technology fields.More specifically, the utility model is related to a kind of snow removing unmanned planes.
Background technology
Winter China it is many area all can occurrence of large-area snowfall, especially in recent years, heavy snow is to caused by road traffic
It is inconvenient increasingly severe.If cleared up road surface not in time, road snow can cause the friction on road surface after being seriously compacted by vehicular traffic
Power greatly reduces, and snow melting can form layers of ice in ground surface, and very big puzzlement is brought to pedestrian and traffic.If using sweeping
Sled carries out spreading deicing salt to urban road, highway, and work efficiency is low, also results in road congestion.Therefore, using nothing
It is man-machine carry out dispense deicing salt idea should by and give birth to.
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned unmanned plane, have the characteristics that portability is high, easy to operate, using flexible.Traditional unmanned plane is flown using six axis,
The various flare maneuvers of unmanned plane are realized by the rotating speed difference of each propeller, take photo by plane, the unmanned fields such as scout obtain
Extensive use.But this unmanned plane requires load-carrying relatively low, is not suitable for loading cargo, larger change can occur for center of gravity during unloading
It is low when changing, personnel and building are caused with very big danger, and dispensing high during deicing salt requirement unmanned plane during flying, maintaining balance
Under the premise of dispense and become a problem, therefore be dfficult to apply to snow removing field.
Utility model content
One purpose of the utility model is to solve at least the above, and provides the advantages of at least will be described later.
The utility model is to provide a kind of snow removing unmanned plane there are one purpose, can be in the case where loading and unloading deicing salt
Good stability and balance quality are kept, has the advantages that spreading scope is wide, reliability is high.
In order to realize these purposes and further advantage according to the present utility model, a kind of snow removing unmanned plane is provided, including：
Head；
Fuselage, inside along material transferring direction successively be equipped with storing hopper, guide auger and discharge unit, the storing
Hopper is equipped with the space of storage deicing salt, and the guide auger axis is horizontally disposed with, is distributed along the length direction of the fuselage, institute
The arrival end for stating guide auger accepts the outlet of the storing hopper, the discharge unit include baffle, air blower, turntable and
First motor, the baffle is installed on the fuselage, the globoidal structure in the half cycle for wrapping up the turntable, the baffle center
Place offers the notch connected with the port of export of the guide auger, and the air blower is installed in above the baffle and outlet air
Mouthful towards the turntable, the shaft of the turntable is vertically arranged, bearing is connected on the fuselage, the periphery of the turntable and institute
It states baffle and forms gap, first motor drives the shaft to rotate, and rotates horizontally the turntable；
A pair of of flank, is symmetricly set on the both sides of the fuselage, and the free end of the flank is equipped with the second motor；
A pair of of balance wing is symmetrically distributed in the both sides of the fuselage, and a pair of of balance wing is with a pair of of flank in same plane
On, and the fixing end of the balance wing is connected on the flank at the fuselage, the free end of the balance wing is equipped with
3rd motor；
Balance tailstock, include it is a pair of extend frame, a pair of of empennage and connecting plate, a pair of of extension frame is horizontally disposed with, along described
The length direction distribution of fuselage, and a pair of one end for extending frame is separately fixed on a pair of of flank, the other end passes through the connection
Plate is fixedly connected, and a pair of of empennage is symmetrically fixed on the connecting plate and set straight up；
Wherein, the line of the second motor positioned at one side and the 3rd motor positioned at opposite side is the first line, positioned at one
The line of 3rd motor of side and the second motor positioned at opposite side is the crosspoint of the second line, the first line and the second line
Fall in the floor projection of the fuselage.
Preferably, the snow removing unmanned plane, the afterbody of the fuselage are equipped with hatch door, the width of the hatch door with it is described
The diameter of turntable is equal, and the junction of the hatch door and the afterbody of the fuselage is matched inclined surface, forms deicing salt
Glide slope.
Preferably, the snow removing unmanned plane, the extended line of the air outlet of the air blower intersect with the turntable
Point is located on semi circular surface of the turntable away from the baffle.
Preferably, the snow removing unmanned plane, the distance of free end to the fuselage of the balance wing, which is more than, fixes
It holds to the distance of the fuselage.
Preferably, the snow removing unmanned plane, the length for extending frame are more than the length of the balance wing.
Preferably, the snow removing unmanned plane, the gap are not more than 1mm.
The utility model includes at least following advantageous effect：
Firstth, the utility model will be set gradually before and after head and fuselage, both sides set flank, middle part set balance wing,
Afterbody sets balance tailstock, using lightweight material, increases the balance of unmanned plane in own physical structure and aerodynamics angle
Property, optimizing flight structure and traction power, flank, balance wing is symmetrical arranged, make unmanned plane during flying it is more steady, can hovering,
Side flies and rotates etc. to switch rapidly between state of flights, and balance tailstock increases the structural strength of unmanned plane, scattered stress, is formed strong
Power supports, and greatly improves reliability of structure and load-bearing capacity；
Secondth, deicing salt is delivered to downwards by storing hopper on guide auger, then helical feed to turntable, turntable rotation cloth
Expect that scope is wide and cloth is uniform, baffle avoids deicing salt from sucking fuselage interior, air blower by deicing salt be sent into disk edge and
Hatch door is thrown away under centrifugal force effect, each component is arranged in order in the small space of fuselage, simple and practical, reliability is high；
Three, the second motors, the 3rd motor offer power make the steady flight forward of unmanned plane, and control is equipped with inside head
Module, detection module and auxiliary device etc., positioned at the head of unmanned plane, the action point made a concerted effort becomes in the lift of unmanned plane
The heart, the arrangement of the balance that is conducive to unmanned plane and the handling parts that loads deicing salt to the rear positioned at the middle part of unmanned plane, more preferably
Control unmanned plane makes it, and center of gravity is maintained near centre of lift on gravity direction, puts down unmanned plane during deicing salt reduction
Steady flight；
4th, hatch door is equal with disk diameter, and the deicing salt that turntable is turned at hatch door is made to be thrown out of completely, avoids snow melt
Agent returns back to fuselage interior, and inclined surface reduces the resistance that deicing salt is thrown out of；The setting of the air outlet of air blower provides certain side
To wind-force, cooperateed with centrifugal force, promote deicing salt thrown away completely, avoid falling into fuselage interior by the gap of shaft；Balance
The angle of the wing sets the stress of scattered unmanned plane, makes unmanned plane structure arrangement more reasonable；Extend the relatively long of frame and balance wing
Degree sets the anti-twisting property for improving unmanned plane, reduces the resistance of balance wing；The size setting in gap makes melting for certain specification size
Snow agent can not be slid by the gap to fuselage interior.
Part is illustrated to embody by the further advantage, target and feature of the utility model by following, and part will also pass through
Research and practice to the utility model and be understood by the person skilled in the art.
Description of the drawings
Fig. 1 is the structure diagram of the utility model；
Fig. 2 is the top view of the utility model；
The structure diagram of the fuselage interior of Fig. 3 positions the utility model.
Specific embodiment
The utility model is described in further detail below in conjunction with the accompanying drawings, to make those skilled in the art with reference to explanation
Book 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.
It should be noted that experimental method described in following embodiments, is conventional method unless otherwise specified, institute
Reagent and material are stated, unless otherwise specified, is commercially obtained；In the description of the utility model, it is necessary to explanation
It is that unless otherwise clearly defined and limited, term " installation ", " connected ", " setting " should be interpreted broadly, for example, it may be
It is fixedly linked, sets or be detachably connected, set or be integrally connected, set.For the ordinary skill of this field
For personnel, concrete meaning of the above-mentioned term in the utility model can be understood with concrete condition.Term " transverse direction ", " longitudinal direction ",
The orientation of instructions such as " on ", " under ", "front", "rear", "left", "right", " vertical ", " level ", " top ", " bottom ", " interior ", " outer " or
Position relationship is based on orientation shown in the drawings or position relationship, is for only for ease of description the utility model and simplifies description,
It is not instruction or implies signified device or element there must be specific orientation, with specific azimuth configuration and operation, because
This is it is not intended that limitation to the utility model.
As shown in Figures 1 to 3, the utility model provides a kind of snow removing unmanned plane, including：
Head 1；
Fuselage 2, inside along material transferring direction successively be equipped with storing hopper 21, guide auger 22 and discharge unit, institute
State the space that storing hopper 21 is equipped with storage deicing salt, 22 axis horizontal of guide auger sets, along the length of the fuselage 2
Directional spreding, the arrival end of the guide auger 22 accept the outlet of the storing hopper 21, and the discharge unit includes baffle
23rd, air blower 24,25 and first motor of turntable, the baffle 23 are installed on the fuselage 2, in the package turntable 25
The globoidal structure of half cycle offers the notch connected with the port of export of the guide auger 22 at 23 center of baffle, described
Air blower 24 is installed in 23 top of the baffle and air outlet is towards the turntable 25, the shaft of the turntable 25 is vertically arranged,
Bearing is connected on the fuselage 2, and the periphery of the turntable 25 forms gap with the baffle 23, and first motor drives institute
Shaft rotation is stated, rotates horizontally the turntable 25；
A pair of of flank 3, is symmetricly set on the both sides of the fuselage 2, and the free end of the flank 3 is equipped with the second motor
31；
A pair of of balance wing 4 is symmetrically distributed in the both sides of the fuselage 2, and a pair of of balance wing 4 is with a pair of of flank 3 same
In plane, and the fixing end of the balance wing 4 is connected on the flank 3 at the fuselage 2, the balance wing 4 from
3rd motor 41 is equipped with by end；
Tailstock is balanced, extends frame 51, a pair of of empennage 52 and connecting plate 53 including a pair, a pair extends 51 level of frame and sets
It puts, be distributed along the length direction of the fuselage 2, and a pair of one end for extending frame 51 is separately fixed on a pair of of flank 3, the other end
It is fixedly connected by the connecting plate 53, a pair of of empennage 52 is symmetrically fixed on the connecting plate 53 and set straight up；
Wherein, it is the first line, position positioned at the second motor 31 of one side and the line of the 3rd motor 41 positioned at opposite side
In the 3rd motor 41 of one side and the line of the second motor 31 positioned at opposite side be the second line, the first line and the second line
Crosspoint fall in the floor projection of the fuselage 2.
In the above-mentioned technical solutions, by head 1 with being set gradually before and after fuselage 2, it is flat that both sides set flank 3, middle part to set
Weigh the wing 4, afterbody setting balance tailstock, using lightweight material, increases unmanned plane in own physical structure and aerodynamics angle
Balance, optimize flight structure and traction power, flank 3, balance wing 4 are symmetrical arranged, and make that unmanned plane during flying is more steady, energy
Fly and rotate etc. in hovering, side to switch rapidly between state of flights, balance tailstock increase the structural strength of unmanned plane, disperse by
Power forms strength and supports, greatly improves reliability of structure and load-bearing capacity；
Deicing salt is delivered to downwards by storing hopper 21 on guide auger 22, then helical feed to turntable 25, and turntable 25 revolves
Turn that cloth scope is wide and cloth is uniform, baffle 23 is avoided inside deicing salt sucking fuselage 2, and deicing salt is sent into turntable by air blower 24
25 edges simultaneously throw away hatch door under the action of the centrifugal force, each component in the small space of fuselage 2 in order arrangement, it is simple and practical, can
By property height；
Second motor 31, the 3rd motor 41 offer power make the steady flight forward of unmanned plane, and control is equipped with inside head 1
Module, detection module and auxiliary device etc., positioned at the head of unmanned plane, the action point made a concerted effort becomes in the lift of unmanned plane
The heart, the arrangement of the balance that is conducive to unmanned plane and the handling parts that loads deicing salt to the rear positioned at the middle part of unmanned plane, more preferably
Control unmanned plane makes it, and center of gravity is maintained near centre of lift on gravity direction, puts down unmanned plane during deicing salt reduction
Steady flight
In another technical solution, the snow removing unmanned plane, the afterbody of the fuselage 2 is equipped with hatch door, the hatch door
Width it is equal with the diameter of the turntable 25, and the junction of the hatch door and the afterbody of the fuselage 2 is inclined to be matched
Inclined-plane forms the glide slope of deicing salt.Hatch door is equal with 25 diameter of turntable, makes the deicing salt that turntable 25 is turned at hatch door complete
It is thrown out of, deicing salt is avoided to return back to inside fuselage 2, inclined surface reduces the resistance that deicing salt is thrown out of.
In another technical solution, the snow removing unmanned plane, the extended line of the air outlet of the air blower 24 and institute
The crosspoint for stating turntable 25 is located on semi circular surface of the turntable 25 away from the baffle 23.The setting of the air outlet of air blower 24
The wind-force of certain orientation is provided, is cooperateed with centrifugal force, deicing salt is promoted to be thrown away completely, avoids falling into fuselage by the gap of shaft
Inside 2.
In another technical solution, the snow removing unmanned plane, the free end of the balance wing 4 to the fuselage 2
Distance is more than fixing end to the distance of the fuselage 2.The angle of balance wing 4 sets the stress of scattered unmanned plane, makes unmanned plane knot
Structure arrangement is more reasonable.
In another technical solution, the snow removing unmanned plane, the length for extending frame 51 is more than the balance wing 4
Length.The relative length for extending frame 51 and balance wing 4 sets the anti-twisting property for improving unmanned plane, reduces the resistance of balance wing 4.
In another technical solution, the snow removing unmanned plane, the gap is not more than 1mm.The size in gap is set
Make the deicing salt of certain specification size can not be slid by the gap to fuselage 2.
Number of devices and treatment scale described herein are the explanations for simplifying the utility model.To the utility model
Application, modifications and variations will be readily apparent to persons skilled in the art.
Although the embodiment of the utility model is disclosed as above, it is not restricted in specification and embodiment
Listed utilization, it can be applied to the field of various suitable the utility model completely, for those skilled in the art,
Other modification is easily achieved, therefore without departing from the general concept defined in the claims and the equivalent scope, this reality
Specific details is not limited to new and shown here as the legend with description.
Claims (6)
1. a kind of snow removing unmanned plane, which is characterized in that including：
Head；
Fuselage, inside along material transferring direction successively be equipped with storing hopper, guide auger and discharge unit, the storing hopper
Space equipped with storage deicing salt, the guide auger axis is horizontally disposed with, is distributed along the length direction of the fuselage, described to lead
Expect that the arrival end of auger accepts the outlet of the storing hopper, the discharge unit includes baffle, air blower, turntable and first
Motor, the baffle is installed on the fuselage, the globoidal structure in the half cycle for wrapping up the turntable, is opened at the baffle center
Equipped with the notch that the port of export with the guide auger connects, the air blower is installed in above the baffle and air outlet court
To the turntable, the shaft of the turntable is vertically arranged, bearing is connected on the fuselage, the periphery of the turntable and the gear
Plate forms gap, and first motor drives the shaft to rotate, and rotates horizontally the turntable；
A pair of of flank, is symmetricly set on the both sides of the fuselage, and the free end of the flank is equipped with the second motor；
A pair of of balance wing, is symmetrically distributed in the both sides of the fuselage, a pair of of balance wing with a pair of of flank at grade, and
The fixing end of the balance wing is connected on the flank at the fuselage, and the free end of the balance wing is equipped with the 3rd electricity
Machine；
Balance tailstock, include it is a pair of extend frame, a pair of of empennage and connecting plate, a pair of of extension frame is horizontally disposed with, along the fuselage
Length direction distribution, and a pair of one end for extending frame is separately fixed on a pair of of flank, the other end is consolidated by the connecting plate
Fixed connection, a pair of of empennage are symmetrically fixed on the connecting plate and set straight up；
Wherein, the line of the second motor positioned at one side and the 3rd motor positioned at opposite side is the first line, positioned at one side
For the second line, the crosspoint of the first line and the second line falls the line of 3rd motor and the second motor positioned at opposite side
In the floor projection of the fuselage.
2. snow removing unmanned plane as described in claim 1, which is characterized in that the afterbody of the fuselage is equipped with hatch door, the hatch door
Width it is equal with the diameter of the turntable, and the junction of the afterbody of the hatch door and the fuselage is matched inclination
Face forms the glide slope of deicing salt.
3. as described in claim 1 snow removing unmanned plane, which is characterized in that the extended line of the air outlet of the air blower with it is described
The crosspoint of turntable is located on semi circular surface of the turntable away from the baffle.
4. as described in claim 1 snow removing unmanned plane, which is characterized in that the free end of the balance wing to the fuselage away from
With a distance from more than fixing end to the fuselage.
5. snow removing unmanned plane as described in claim 1, which is characterized in that the length for extending frame is more than the balance wing
Length.
6. snow removing unmanned plane as described in claim 1, which is characterized in that the gap is not more than 1mm.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721491218.7U CN207374668U (en) | 2017-11-10 | 2017-11-10 | Remove the snow unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721491218.7U CN207374668U (en) | 2017-11-10 | 2017-11-10 | Remove the snow unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207374668U true CN207374668U (en) | 2018-05-18 |
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ID=62335597
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721491218.7U Active CN207374668U (en) | 2017-11-10 | 2017-11-10 | Remove the snow unmanned plane |
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| CN (1) | CN207374668U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112956469A (en) * | 2021-02-01 | 2021-06-15 | 农业农村部南京农业机械化研究所 | Uniform particle broadcasting operation method and system for unmanned aerial vehicle |
-
2017
- 2017-11-10 CN CN201721491218.7U patent/CN207374668U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112956469A (en) * | 2021-02-01 | 2021-06-15 | 农业农村部南京农业机械化研究所 | Uniform particle broadcasting operation method and system for unmanned aerial vehicle |
| CN112956469B (en) * | 2021-02-01 | 2022-01-18 | 农业农村部南京农业机械化研究所 | Uniform particle broadcasting operation method and system for unmanned aerial vehicle |
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