CN105947210B - A kind of four axis folding unmanned planes - Google Patents
A kind of four axis folding unmanned planes Download PDFInfo
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- CN105947210B CN105947210B CN201610315248.6A CN201610315248A CN105947210B CN 105947210 B CN105947210 B CN 105947210B CN 201610315248 A CN201610315248 A CN 201610315248A CN 105947210 B CN105947210 B CN 105947210B
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- control cabin
- circular hole
- wing
- side plate
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Classifications
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- 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
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- 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
- B64C1/30—Parts of fuselage relatively movable to reduce overall dimensions of aircraft
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
Abstract
The invention discloses a kind of four axis folding unmanned planes, are made of first/second mobile jib, first/second wing component, winged control cabin component, cloud control cabin component, head assembly, four propeller components, several connectors, it is characterised in that：First/second mobile jib is parallel；Fly the both sides of control cabin/cloud control cabin component, by connector, on first, second mobile jib；First/second wing component is set on first/second mobile jib；First/second propeller component is on the second wing component, and the three/the quadruple screw propeller component is on the first wing component；Head assembly is connected with cloud control cabin component.The present invention, compared with prior art, have the characteristics that simple in structure, easily manufactured, maintenance is convenient, foldable, have that flight low noise, Oscillation Amplitude are small, the flying quality well such as stability of rising and falling height concurrently, also there is higher antijamming capability and heat conduction and heat radiation ability, it is low in energy consumption, realize handling good, high-time purpose.
Description
Technical field
The present invention relates to a kind of unmanned plane, more particularly to a kind of four axis folding unmanned planes.
Background technology
Existing battery-type unmanned plane, generally an only control cabinet, the various automatically controlled components of unmanned plane, e.g., fly
The controller of row motor, fly control GPRS, the controller of horizontal stage electric machine, cloud control GPRS, cloud control cabin component, battery component and other are each
Class sensor, is each provided in control cabinet.This structure, can both cause the mutual electromagnetic between control element to disturb, flight control
Effect is poor.Meanwhile the adjustment of each element is difficult, when flight, is not easy to ensure balance, and flight stability is poor.Control cabinet generally by
Carbon fiber etc. does not allow the material of easy heat radiation to be made, and heat dissipation effect is poor.Therefore, existing battery-type unmanned plane, effective power
Universal relatively low, the flight time is generally shorter.In addition, when realizing folder function, foldable structure is usually all complex, cost into
This height, is also unfavorable for adjustment maintenance.
The content of the invention
The embodiment of the present invention purpose is that providing one kind has simple in structure, easily manufactured, maintenance is convenient, foldable etc.
The four axis folding unmanned plane of one kind of feature, while have that flight low noise, Oscillation Amplitude are small, stability of rising and falling height etc. is good concurrently
Ground flying quality, also has higher antijamming capability and heat conduction and heat radiation ability, low in energy consumption, during realizing handling good, flight
Between long purpose.
To reach above-mentioned purpose, the embodiment of the present invention adopts the following technical scheme that：
A kind of four axis folding unmanned planes, by the first mobile jib, the second mobile jib, fly control cabin component, the first wing component, cloud control
Cabin component, head assembly, the second wing component, the first propeller component, the second propeller component, the 3rd propeller component, the 4th
Propeller component, connector composition, it is characterised in that：First mobile jib, the second mobile jib are identical, and are parallel to each other；
The winged control cabin component is by flying to control cabin, battery component, flying control hatchcover, the first winged control cabin stent, winged control GPRS groups
Part forms, and it is that aircraft aluminum is made that winged control cabin, first, which fly to control cabin stent, and the front end of battery component is fixed at first and flies to control
On the stent of cabin, the rear end of battery component, which is arranged on, to fly in control cabin, flies control hatchcover and be fastened on fly control cabin, first fly on control cabin stent
Side, on control hatchcover is flown, equipped with winged control GPRS components；
The connector is the flat structure with middle part circular hole, its bottom is equipped with the first connecting hole, is connected by first
Hole is connect, can be packed in and fly control cabin, the sidepiece of the first winged control cabin stent；
It is packed in and flies control cabin, several connectors in the first winged arranged on left and right sides portion for controlling cabin stent, passes through its middle part circle
Hole, is respectively sleeved on the first mobile jib, on the second mobile jib；
First wing component, the second wing modular construction are identical, are symmetricly set on the arranged on left and right sides for flying control cabin；
First wing component is made of the first side plate, the second side plate, the 3rd side plate, the 4th side plate, lower plate, upper cover plate, institute
The first side plate, the second side plate, the 3rd side plate, the 4th side plate stated, are vertically set between lower plate, upper cover plate successively, and outside
Side is concordant with the outer edge of lower plate, upper cover plate；First side plate, the structure of the 3rd side plate is identical and is arranged in parallel；
The side both ends of first side plate are respectively equipped with the first circular hole, the first open pore, and the first vibration damping is equipped with the first circular hole
Ring；
The side both ends of 3rd side plate are respectively equipped with the second circular hole, the second open pore, and the second vibration damping is equipped with the second circular hole
Ring；
First circular hole, second circular hole etc. are coaxial, are sleeved on the first mobile jib；
On lower plate, equipped with the 3rd propeller bracket bar buckle, quadruple screw propeller cradling piece buckle, respectively with the first side
The second open pore on the first open pore, the 3rd side plate on plate is arranged in parallel, and respectively with the 3rd propeller component, the 4th spiral shell
Revolve the connection of paddle component；
In upper cover plate upper surface, equipped with wing pintle hook lock, when wing pintle hook lock is vertical with the second round hole axial, the 3rd side plate can be prevented
Rotated around the second circular hole, when wing pintle hook lock is parallel with the second round hole axial, the 3rd side plate can be rotated around the second circular hole；
Second wing assembly set is connected with the first propeller component, the second propeller component respectively on the second mobile jib；
The cloud control cabin component, is made of cloud control cabin, cloud control hatchcover, cloud control GPRS components, and cloud control cabin is hollow length
Cube structure, and there is aircraft aluminum to be made, cloud control GPRS components are equipped with equipped with cloud control hatchcover, cloud control hatchcover top above it,
In the left and right side in cloud control cabin, the 5th lug, the 6th lug are arranged with；5th lug, the middle part of the 6th lug, respectively band
There are the 5th circular hole, the 6th circular hole, the 5th damping ring, the 6th damping ring, cloud control cabin point are respectively equipped with the 5th circular hole, the 6th circular hole
Not by the 5th circular hole, the 6th circular hole, the first mobile jib is sleeved on, on the second mobile jib；Cloud is equipped with the middle part of the leading flank in cloud control cabin
Platform component mounting hole, and be connected with head assembly.
As an optimization, the head assembly, is two-degree-of-freedom cradle head component, is pacified by the first motor, first support, camera
Loading board, the second motor, shaft, the first connecting plate, the second connecting plate composition, the first support is by first support bar, second
Cradling piece is formed, and one end of first support bar is equipped with the side company of the second motor mounting part, the other end and the first motor coupling portion
Connect, the opposite side of the first motor coupling portion is connected with second support bar one end, and the first hinge is equipped with the other end of second support bar
Chain hole；Second motor mounting part of the first support is fixed with the second motor, the second electric machine main shaft and the first connecting plate
Lower part connects；The top of first connecting plate is connected with camera installing plate one end；The camera installing plate other end and the second connecting plate
Top is connected, and the first connecting plate is parallel with the second connecting plate；The lower part of second connecting plate is equipped with the second through hole, and passes through shaft
Hinges are formed with the first axle hole in first support, and the axis of rotation of hinges is conllinear with the second electrical axis；
The first limited block is equipped with the end face outside of the second through hole；First electric machine main shaft and the first motor coupling portion of first support connect
Connect.
As an optimization, in winged control cabin, cloud control cabin, the first wing component, the second wing component, it is equipped with water proof nonwoven cloth
Layer, to prevent the rainwater of outside, dust to enter by strip grooves in engine space, protects each control element in engine space.
As an optimization, on winged control cabin, cloud control cabin, the first wing component, the second wing component, heat dissipation hole slot is equipped with, to carry
High heat-sinking capability.
The advantageous effects of the present invention：A kind of four axis folding unmanned planes, by the first mobile jib, the second mobile jib, fly control
Cabin component, the first wing component, cloud control cabin component, head assembly, the second wing component, the first propeller component, the second propeller group
Part, the 3rd propeller component, quadruple screw propeller component, connector composition, the first mobile jib, the second mobile jib are arranged in parallel, and fly control cabin
The both sides of component, cloud control cabin component, by connector, are sleeved on the first mobile jib, on the second mobile jib；First wing component is set with
In the first mobile jib, the second wing assembly set is mounted in the second mobile jib；First propeller component, the second propeller component are installed on second wing
On component, the 3rd propeller component, quadruple screw propeller component are installed on the first wing component；Head assembly is installed on cloud control cabin group
On part.It is this by an existing control cabinet, be arranged to the two winged control cabin being separated from each other components, cloud control cabin modular construction, energy
Enough to realize that winged control GPRS, cloud control GPRS are separated from each other, reduction interferes with each other between the two.Meanwhile main heater element, set respectively
Put in two different control cabinets, realize the separately positioned of pyrotoxin, reduce heat dissipation difficulty.Adjust and fly control cabin component, cloud control
Distance is easy between the component of cabin, and the state of flight for adjusting unmanned plane is relatively easy to.
Fly control cabin, first to fly control cabin stent, cloud control cabin be that aircraft aluminum is made, antijamming capability and heat-sinking capability all compared with
By force, the antijamming capability and heat-sinking capability of complete machine are further increased.By upper in first wing of turn component, the second wing component
The wing pintle hook lock of cover board upper surface, it is easy to realize the rotary type folding action of the first wing component, the second wing component, folding mode letter
It is single.In the shock ring that cloud control cabin component and the first mobile jib, the second mobile jib junction are equipped with, the first wing component, the second wing component, glue
Gusset plate, the bottom plate of water proof nonwoven cloth are had, the rainwater of outside, dust can be prevented to enter by strip grooves in engine space, protected
Each control element in engine space is protected.
The present invention, compared with prior art, has the characteristics that simple in structure, easily manufactured, maintenance convenient, foldable one
Four axis folding unmanned planes of kind, while have the flights well such as flight low noise, Oscillation Amplitude are small, stability of rising and falling height concurrently
Can, also there is higher antijamming capability and heat conduction and heat radiation ability, it is low in energy consumption, realize handling good, high-time mesh
, it can effectively strengthen unmanned plane fan's customer experience.
Brief description of the drawings
In order to illustrate more clearly about the embodiment of the present invention or technical scheme of the prior art, below will be to embodiment or existing
There is attached drawing needed in technology description to be briefly described, it should be apparent that, drawings in the following description are only this
Some embodiments of invention, for those of ordinary skill in the art, without creative efforts, can be with
Other attached drawings are obtained according to these attached drawings.
Fig. 1 is the complete machine floor map in the embodiment of the present invention；
Fig. 2 is the engine space component structure diagram in the embodiment of the present invention；
Fig. 3 is the connecting-piece structure schematic diagram in the embodiment of the present invention；
Fig. 4 is the engine space component partial assembled schematic diagram in the embodiment of the present invention；
Fig. 5 is the first wing component internal assembling schematic diagram in the embodiment of the present invention；
Fig. 6 is the first wing component entirety assembling schematic diagram in the embodiment of the present invention；
Fig. 7 is the cloud control cabin component entirety assembling schematic diagram in the embodiment of the present invention；
Fig. 8 is the head assembly entirety assembling schematic diagram in the embodiment of the present invention；
Fig. 9 is the first support structure diagram in the embodiment of the present invention；
Figure 10 is the second connecting board structure schematic diagram in the embodiment of the present invention；
Figure 11 is the main structure schematic diagram in the embodiment of the present invention；
In figure：1-the first mobile jib；2-the second mobile jib；3-fly control cabin component；4-the first wing component；5-cloud control cabin group
Part；6-head assembly；7-the second wing component；8-the first propeller component；9-the second propeller component；10-the three is spiral
Paddle component；11-the quadruple screw propeller component；12-connector；31-fly control cabin；32-battery component；33-fly control hatchcover；
34-the first flies control cabin stent；35-fly control GPRS components；51-cloud control hatchcover；52-cloud control GPRS components；The control of 53-cloud
Cabin；54-the five lug；55-the six lug；61-the first motor；62-first support；63-video camera mounting plate；64—
Second motor；65-shaft；66-the first connecting plate；67-the second connecting plate；80-lower plate；81-the first side plate；82—
Second side plate；83-the three side plate；84-the four side plate；85-the three propeller bracket bar is buckled；86-the quadruple screw propeller branch
Hack lever is buckled；87-the first damping ring；88-upper cover plate；89-wing pintle hook lock；121-the first connecting hole；122-middle part circular hole；
531-head assembly mounting hole；541-the five circular hole；542-the five damping ring；551-the six circular hole；552-the six subtracts
Shake ring；621-the second motor mounting part；The 623-the first motor coupling portion of 622-first support bar；；624-second support
Bar；625-first axle hole；671-the second through hole；672-the first limited block；811-the first circular hole；812-the first
Open pore；831-the second open pore；832-the second circular hole；833-the second damping ring.
Embodiment
Below in conjunction with the attached drawing in the embodiment of the present invention, the technical solution in the embodiment of the present invention is carried out clear, complete
Site preparation describes, it is clear that described embodiment is only part of the embodiment of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, those of ordinary skill in the art are obtained every other without creative efforts
Embodiment, belongs to the scope of protection of the invention.
As the embodiment of the present invention, as shown in Figure 1, a kind of four axis folding unmanned planes, by the first mobile jib 1, second
Mobile jib 2, fly control cabin component 3, the first wing component 4, cloud control cabin component 5, head assembly 6, the second wing component 7, the first propeller group
Part 8, the second propeller component 9, the 3rd propeller component 10, quadruple screw propeller component 11, connector 12 form, its feature exists
In：First mobile jib 1, the second mobile jib 2 are identical, and are parallel to each other；
As shown in Fig. 2, fly control cabin component 3 flies control cabin stent by flying control cabin 31, battery component 32, flying control hatchcover 33, first
34th, fly control GPRS components 35 to form, the front end of battery component 32 is fixed at first and flies on control cabin stent 34, battery component 32
Rear end be arranged on and fly in control cabin 31, fly control hatchcover 33 and be fastened on to fly control cabin 31, first and fly control cabin stent 34 top, flying control cabin
On lid 33, equipped with winged control GPRS components 35；
As shown in figure 3, connector 12 is the flat annulus structure of the middle part circular hole 122 with openend, its bottom is equipped with
First connecting hole 121, by the first connecting hole 121, can be packed in and fly the sidepiece that control cabin 31, first flies control cabin stent 34；
Fly the left side that control cabin 31, first flies control cabin stent 34, to be fixed with several connectors 12, each connector 12 respectively
By middle part circular hole 122 thereon, it is set on the first mobile jib 1；
As shown in figure 4, flying the right side that control cabin 31, first flies control cabin stent 34, several connectors 12 are also fixed with respectively,
Each connector 12 is set on the second mobile jib 2 by middle part circular hole 122 thereon；
First wing component 4,7 structure of the second wing component are identical, as shown in figure 11, are symmetrically arranged at and fly control cabin 31
Arranged on left and right sides；
As shown in Figure 5 and Figure 6, the first wing component 4 is by the first side plate 81, the second side plate 82, the 3rd side plate 83, the 4th side plate
84th, lower plate 80, upper cover plate 88 form, first side plate 81, the second side plate 82, the 3rd side plate 83, the 4th side plate 84, according to
It is secondary to be vertically set between lower plate 80, upper cover plate 88, and lateral surface is concordant with the outer edge of lower plate 80, upper cover plate 88；The
Side plate 81, the structure of the 3rd side plate 83 is identical and is arranged in parallel；
The side both ends of first side plate 81 are respectively equipped with the first circular hole 811, the first open pore 812, are set in the first circular hole 811
There is the first damping ring 87；The side both ends of 3rd side plate 83 are respectively equipped with the second circular hole 832, the second open pore 831, the second circular hole
The second damping ring 833 is equipped with 832；
First circular hole 811, the second circular hole 832 are coaxial, are sleeved on the first mobile jib 1；
On lower plate 80, equipped with the 3rd propeller bracket bar buckle 85, quadruple screw propeller cradling piece buckle 86, respectively with
The second open pore 831 on the first open pore 812, the 3rd side plate 83 on first side plate 81 is arranged in parallel, and with it is the 3rd spiral
Paddle component 10, be connected with quadruple screw propeller component 11；
In 88 upper surface of upper cover plate, equipped with wing pintle hook lock 89, when wing pintle hook lock 89 is vertical with 832 axis of the second circular hole, can hinder
Only the 3rd side plate 83 is rotated around the second circular hole 832, when wing pintle hook lock 89 is parallel with 832 axis of the second circular hole, the 3rd side plate 83
It can be rotated around the second circular hole 832；Second wing component 7 is sleeved on the second mobile jib 2, and respectively with the first propeller component 8, with
Second propeller component 9 connects；
Cloud control cabin component 5, as shown in fig. 7, being made of cloud control hatchcover 51, cloud control GPRS components 52, cloud control cabin 53, cloud control cabin
53 be hollow cuboid, and above it equipped with cloud control hatchcover 51, the top of cloud control hatchcover 51 is equipped with cloud control GPRS components 52, in cloud
53 left and right side of cabin is controlled, is arranged with the 5th lug 54, the 6th lug 55, the 5th lug 54, the middle part difference of the 6th lug 55
With the 5th circular hole 541, the 6th circular hole 551, the 5th damping ring 542, are respectively equipped with the 5th circular hole 541, the 6th circular hole 551
Six damping rings 552, cloud control cabin 53 by the 5th circular hole 541, the 6th circular hole 551, are sleeved on the first mobile jib 1, the second mobile jib 2 respectively
On；Head assembly mounting hole 531 is equipped with the middle part of the leading flank in cloud control cabin 53, and is connected with head assembly 6；
Head assembly 6, can be the multiple degrees of freedom holder of diversified forms, as the embodiment of the present invention, there is provided one kind two is certainly
By degree holder, have the characteristics that simple in structure, mounting and adjusting is convenient, of low cost, as shown in Fig. 8, Fig. 9, Figure 10, head assembly
6, connected by the first motor 61, first support 62, camera installing plate 63, the second motor 64, shaft 65, the first connecting plate 66, second
Fishplate bar 67 forms, and the first support 62 is made of first support bar 622, second support bar 624, first support bar 622
One end is equipped with the second motor mounting part 621, and the other end is connected with the side of the first motor coupling portion 623, the first motor coupling portion
623 opposite side is connected with 624 one end of second support bar, and first axle hole 625 is equipped with the other end of second support bar 624；
Second motor mounting part 621 of the first support 62 is fixed with the second motor 64, and the main shaft of the second motor 64 and first connect
The lower part connection of fishplate bar 66；The top of first connecting plate 66 is connected with 63 one end of camera installing plate；63 other end of camera installing plate
It is connected with the top of the second connecting plate 67, and the first connecting plate 66 is parallel with the second connecting plate 67；The lower part of second connecting plate 67
Hinges, and activity are formed equipped with the second through hole 671, and by the first axle hole 625 in shaft 65 and first support 62
The axis of rotation of hinge is conllinear with the main-shaft axis of the second motor 64；It is spacing that first is equipped with the end face outside of the second through hole 671
Block 672；The main shaft of first motor 61 is connected with the first motor coupling portion 623 of first support 62.
The above description is merely a specific embodiment, but protection scope of the present invention is not limited thereto, any
Those familiar with the art the invention discloses technical scope in, change or replacement can be readily occurred in, should all be contained
Cover within protection scope of the present invention.Therefore, protection scope of the present invention should be based on the protection scope of the described claims.
Claims (4)
- A kind of 1. four axis folding unmanned planes, by the first mobile jib（1）, the second mobile jib（2）, fly control cabin component（3）, the first wing group Part（4）, cloud control cabin component（5）, head assembly（6）, the second wing component（7）, the first propeller component（8）, the second propeller group Part（9）, the 3rd propeller component（10）, quadruple screw propeller component（11）, several connectors（12）Composition, it is characterised in that：First mobile jib（1）, the second mobile jib（2）It is arranged in parallel；The winged control cabin component（3）By flying control cabin（31）, battery component（32）, fly control hatchcover（33）, first fly control cabin stent （34）, fly control GPRS components（35）Composition, flies control cabin（31）, first fly control cabin stent（34）It is made by aircraft aluminum, battery Component（32）Front end be fixed at first fly control cabin stent（34）On, battery component（32）Rear end be arranged on fly control cabin （31）It is interior, fly control hatchcover（33）It is fastened on and flies control cabin（31）Fly control cabin stent with first（34）Top, is flying control hatchcover（33）On, Equipped with winged control GPRS components（35）；The connector（12）For with middle part circular hole（122）Flat structure, its bottom is equipped with the first connecting hole（121）, Pass through the first connecting hole（121）, can be packed in and fly control cabin（31）, first fly control cabin stent（34）Sidepiece；Flying control cabin（31）Fly control cabin stent with first（34）The left and right sides, be fixed with several connectors（12）, left and right The connector of both sides（12）Pass through middle part circular hole thereon respectively（122）, it is corresponding to be sleeved on the first mobile jib（1）, the second mobile jib（2） On；First wing component（4）, the second wing component（7）Structure is identical, is symmetricly set on and flies control cabin（31）Left and right two Side；First wing component（4）By the first side plate（81）, the second side plate（82）, the 3rd side plate（83）, the 4th side plate（84）、 Lower plate（80）, upper cover plate（88）Composition, first side plate（81）, the second side plate（82）, the 3rd side plate（83）, the 4th side Plate（84）, lower plate is vertically set on successively（80）, upper cover plate（88）Between, and lateral surface and lower plate（80）, upper cover plate （88）Outer edge it is concordant；First side plate（81）, the 3rd side plate（83）Structure it is identical and be arranged in parallel；First side plate（81）Both ends be respectively equipped with the first circular hole（811）, the first open pore（812）, and the first circular hole（811）It is interior Equipped with the first damping ring（87）；3rd side plate（83）Both ends be respectively equipped with the second circular hole（832）, the second open pore（831）, and the second circular hole（832）It is interior Equipped with the second damping ring（833）；First circular hole（811）, the second circular hole（832）Coaxially, it is sleeved on the first mobile jib（1）On；In lower plate（80）On, it is buckled equipped with the 3rd propeller bracket bar（85）, quadruple screw propeller cradling piece buckle（86）, respectively With the first side plate（81）On the first open pore（812）, the 3rd side plate（83）On the second open pore（831）It is arranged in parallel, and Respectively with the 3rd propeller component（10）, quadruple screw propeller component（11）Connection；In upper cover plate（88）Upper surface, equipped with wing pintle hook lock（89）, when wing pintle hook lock（89）With the second circular hole（832）When axis is vertical, It can prevent the 3rd side plate（83）Around the second circular hole（832）Rotation, when wing pintle hook lock（89）With the second circular hole（832）Axis is parallel When, the 3rd side plate（83）Can be around the second circular hole（832）Rotation；Second wing component（7）It is sleeved on the second mobile jib（2）On, and respectively with the first propeller component（8）, the second propeller component （9）Connection；The cloud control cabin component（5）, by cloud control cabin（53）, cloud control hatchcover（51）, cloud control GPRS components（52）Composition, cloud control cabin （53）For hollow rectangular parallelepiped structure, and it is made of aircraft aluminum, above it equipped with cloud control hatchcover（51）, cloud control hatchcover（51） Top is equipped with cloud control GPRS components（52）, in cloud control cabin（53）Left and right side, be arranged with the 5th lug（54）, it is the 6th convex Ear（55）；5th lug（54）, the 6th lug（55）Middle part, be respectively provided with the 5th circular hole（541）, the 6th circular hole（551）, the Five circular holes（541）, the 6th circular hole（551）Inside it is respectively equipped with the 5th damping ring（542）, the 6th damping ring（552）, cloud control cabin（53） Pass through the 5th circular hole respectively（541）, the 6th circular hole（551）, it is sleeved on the first mobile jib（1）, the second mobile jib（2）On；In cloud control cabin （53）Leading flank in the middle part of be equipped with head assembly mounting hole（531）, and and head assembly（6）Connection.
- A kind of 2. four axis folding unmanned plane according to claim 1, it is characterised in that：The head assembly （6）, it is two-degree-of-freedom cradle head component（6）, by the first motor（61）, first support（62）, camera installing plate, the second motor （64）, shaft（65）, the first connecting plate（66）, the second connecting plate（67）Composition, the first support（62）By first support Bar（622）, second support bar（624）Form, first support bar（622）One end be equipped with the second motor mounting part（621）, it is another End and the first motor coupling portion（623）Side connection, the first motor coupling portion（623）Opposite side and second support bar （624）One end connects, in second support bar（624）The other end be equipped with first axle hole（625）；The first support（62） The second motor mounting part（621）It is fixed with the second motor（64）, the second motor（64）Main shaft and the first connecting plate（66）Under Portion connects；First connecting plate（66）Top be connected with camera installing plate one end；The camera installing plate other end and the second connecting plate （67）Top be connected, and the first connecting plate（66）With the second connecting plate（67）It is parallel；Second connecting plate（67）Lower part be equipped with Second through hole（671）, and pass through shaft（65）With first support（62）On first axle hole（625）Hinges are formed, and The axis of rotation of hinges and the second motor（64）Axis collinear；In the second through hole（671）End face outside be equipped with first limit Position block（672）；First motor（61）Main shaft and first support（62）The first motor coupling portion（623）Connection.
- A kind of 3. four axis folding unmanned plane according to claim 1, it is characterised in that：Flying control cabin（31）, cloud control Cabin（53）, the first wing component（4）, the second wing component（7）Inside, is equipped with waterproof layer of non-woven fabric.
- A kind of 4. four axis folding unmanned plane according to claim 1, it is characterised in that：Flying control cabin（31）, cloud control Cabin（53）, the first wing component（4）, the second wing component（7）On, it is equipped with heat dissipation hole slot.
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| KR101805392B1 (en) | 2017-04-24 | 2017-12-06 | 주식회사 드론메이트 | Component of drone, and drone using the same |
| CN109804995A (en) * | 2019-01-31 | 2019-05-28 | 安徽梦之翼无人机科技有限公司 | A kind of novel agricultural plant protection drone |
| CN109823554A (en) * | 2019-04-02 | 2019-05-31 | 福建电力职业技术学院 | A kind of winged control cabin fast-detachable modular structure of unmanned plane |
| CN110329519B (en) * | 2019-07-05 | 2023-09-22 | 酷黑科技（北京）有限公司 | Cabin structure of aircraft, aircraft and aerocar |
| CN113942637A (en) * | 2020-07-15 | 2022-01-18 | 深圳市卓派自动化技术有限公司 | Unmanned plane |
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Effective date of registration: 20170418 Address after: 239000 Datong Road Anhui city Chuzhou province Nanqiao Industrial Development Zone Wu Yi Park No. 588 No. 7 Building Applicant after: Anhui dream wing UAV Technology Co., Ltd. Address before: 239000 Anhui City, Chuzhou Province Development Zone, No. 82, No. 1 Venture Center building, room, Room 305 Applicant before: Chuzhou navigation UAV Technology Co., Ltd. |
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