CN106927043A - A kind of octahedra aircraft - Google Patents
A kind of octahedra aircraft Download PDFInfo
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- CN106927043A CN106927043A CN201511020523.3A CN201511020523A CN106927043A CN 106927043 A CN106927043 A CN 106927043A CN 201511020523 A CN201511020523 A CN 201511020523A CN 106927043 A CN106927043 A CN 106927043A
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- ducted fan
- fan component
- middle housing
- upper shell
- aircraft
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- 230000005611 electricity Effects 0.000 claims description 4
- 239000007787 solid Substances 0.000 claims description 2
- 238000012544 monitoring process Methods 0.000 abstract description 4
- 230000033001 locomotion Effects 0.000 description 7
- 230000000694 effects Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 230000005484 gravity Effects 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 230000004888 barrier function Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 239000002360 explosive Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
- 230000007306 turnover Effects 0.000 description 1
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
-
- 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
- B64D29/00—Power-plant nacelles, fairings, or cowlings
-
- 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
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- Aviation & Aerospace Engineering (AREA)
- Cooling Or The Like Of Electrical Apparatus (AREA)
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Abstract
The present invention relates to aircraft, specifically a kind of octahedra aircraft, the upper of octahedral cavity is formed including being sequentially connected, in, lower house and the counterweight component being respectively contained in octahedral cavity, covered on circuit supporting frame, main circuit board, circuit supporting frame, ducted fan component and battery, on, at least one ducted fan component is respectively equipped with lower house, circuit supporting frame is arranged on middle housing, accommodated inside has the main circuit board on middle housing, circuit supporting top of the trellis is provided with circuit supporting frame and covers, on circuit supporting frame multiple counterweight components are evenly equipped with lid, the direction all around of circuit supporting frame periphery is equipped with the ducted fan component on middle housing；Battery is arranged on middle housing, and is connected with main circuit board；Each ducted fan component is connected with main circuit board respectively, and the switch being connected with main circuit board is provided with upper shell.Structure of the present invention is novel, and control is flexible, it is adaptable to flight monitoring service in station module.
Description
Technical field
The present invention relates to aircraft, specifically a kind of octahedra aircraft.
Background technology
In recent decades, in order to meet various civil, military and scientific experiments, miniature self-service flies
Row device is increasingly becoming the focus of every country research with its simple structure, easy to control.Such
Aircraft typically energy straighforward operation or automatic flight, and some sensing elements can be carried, can complete
The special duties such as detecting, monitoring, communication transfer, and with low latitude, low-speed performance, can realize
Position tracking, Attitude Tracking and hovering.Along with the progress of science and technology, miniature self-service
Direction of the aircraft just towards multi-functional, high security, high stability is developed.
Existing small-sized unmanned aircraft includes that fixed-wing formula, rotary wind type and flapping wings type are all kinds of miniature winged
Row device.These existing aircraft propellers are most of to be all exposed to engine body exterior, easily with outward
Boundary collides, and causes propeller to damage so that aircraft crashes.
The content of the invention
Regarding to the issue above, it is an object of the invention to provide a kind of octahedra aircraft.This eight
Face body Flight Vehicle Structure is novel, and control is flexible, it is adaptable to flight monitoring in station module.
The purpose of the present invention is achieved through the following technical solutions：
The present invention include being sequentially connected to be formed the upper shell of octahedral cavity, middle housing, lower house with
And it is respectively contained in the counterweight component in the octahedral cavity, lid, main electricity on circuit supporting frame
Divide on road plate, circuit supporting frame, ducted fan component and battery, wherein upper shell and lower house
At least one ducted fan component is not provided with, and the circuit supporting frame is arranged on middle housing, interior
Portion is equipped with the main circuit board on the middle housing, and the circuit supporting top of the trellis is provided with
Covered on circuit supporting frame, multiple counterweight components, institute are evenly equipped with lid on the circuit supporting frame
State the duct wind that the direction all around of circuit supporting frame periphery is equipped with middle housing
Fan component；The battery is arranged on middle housing, and is connected with the main circuit board；It is each described
Ducted fan component is connected with main circuit board respectively, is provided with the upper shell and main circuit board
The switch of connection.
Wherein：Each described ducted fan modular construction is identical, including ducted fan fixture
And two ducted fans, two ducted fans are opposite to each other installed in the ducted fan fixture
On, i.e., the air-out direction of described two ducted fans is opposite；Each described counterweight component knot
Structure is identical, and including screw thread guide post and mass, the screw thread guide post is arranged on the circuit
On support frame on lid, the mass is threadedly connected on the screw thread guide post；The main electricity
Road plate include gesture module, control module and power module, the gesture module, control module and
Power module is connected by support column between many plates, the lower end screw thread of support column between each plate
It is connected on the bottom surface of the middle housing；
The upper shell and lower casing shape are identical, the upper shell include top surface and be sequentially connected,
And eight sides being connected with the top surface respectively, the lower house include bottom surface and be sequentially connected,
And eight sides being connected with the bottom surface respectively, the ducted fan component set on the upper shell
In the locating slot opened up on the top surface lower surface, the duct set on the lower house
Fan component is arranged in the locating slot opened up on the bottom surface upper surface；The upper shell and under
Air inlet/outlet is provided with intervals in eight sides on housing, and two are taken up an official post in the upper shell
The switch being connected with the main circuit board is installed on side between the individual air inlet/outlet；Institute
Eight sides for stating upper shell and lower house include four gores and four square faces, respectively
The gore and each square face interval setting, wherein four square faces are provided with
Air inlet/outlet, the switch is arranged on upper shell on any one gore；The upper shell
Top surface on the camera module being connected with main circuit board is installed；
The middle housing includes bottom surface and eight being sequentially connected and being connected with the bottom surface respectively
Side, is provided with air inlet/outlet at intervals in eight sides, the middle housing is gone forward rear left
The ducted fan component of right setting is separately mounted on the side between air inlet/outlet described in two；Institute
State eight equal face square faces in side, eight square faces it is upper following respectively with the upper shell and under
Housing is connected；The bottom surface of the middle housing is along the circumferential direction provided with inside and outside two groups of screw threads positioning
Hole, respectively outer periphery Positioning hole and inner circumferential location hole, the bottom of the circuit supporting frame pass through spiral shell
Nail is fixed to the outer periphery Positioning hole of middle housing bottom surface, in the main circuit board and middle housing bottom surface
All location holes are connected；The battery is arranged on the lower surface of middle housing bottom surface；
The ducted fan that the ducted fan component count that the upper shell is set is set with lower house
Component count is identical, and the ducted fan group on ducted fan component on upper shell and lower house
The longitudinal center line of part is each parallel to horizontal plane；The middle housing is set on left and right directions after going forward
Ducted fan component in, fore-and-aft direction set ducted fan component longitudinal center line it is vertical
The longitudinal center line of the ducted fan component set in left and right directions, and the culvert that fore-and-aft direction is set
In the axial direction of the ducted fan component that the longitudinal center line or left and right directions of road fan component are set
What the ducted fan component or fore-and-aft direction that heart line is set parallel to horizontal plane, left and right directions were set
Ducted fan of the longitudinal center line of ducted fan component on horizontal plane, the upper shell
On the longitudinal center line and middle housing of the ducted fan component on component and lower house parallel to
The projection in the horizontal plane of the longitudinal center line of the ducted fan component of horizontal plane is mutually perpendicular to.
Advantages of the present invention is with good effect：
1. whole electronic components of the invention and structure are protected in upper, middle and lower housing shape
Into inside cavity, protected well, circuit inner lead and moving link be not sudden and violent outside
Dew, is difficult to be tangled by barrier or hangs up wire, allows the robot to adapt to many precision environment.
2. the present invention is using the propulsion of ducted fan component, the isolated propeller of more same diameter, meeting
Produce bigger thrust；Ducted fan component is arranged in the cavity that upper, middle and lower housing is formed
Portion, is distributed in upper and lower, left and right and front and rear totally six groups, the six-freedom degree of control aircraft, both
Can ensure that aircraft space rectilinear flight can control aircraft space attitude again, simultaneously because
The ring of duct includes effect, and its compact conformation, aerodynamic noise are low, safety in utilization is good.
3. the inside cavity that the present invention is formed in upper, middle and lower housing, front, rear, left and right,
It is upper and lower to be mounted on ducted fan component, it is capable of achieving the motion of space six-freedom degree.
4. the present invention is internal is provided with counterweight component, can adjust the position of centre of gravity of aircraft.
5. main circuit board of the invention uses modularized design, including gesture module, controls mould
Block and power module, replaceability are strong, are easy to firmware to update upgrading.
6. motion control of the invention, video acquisition transmission are by controlled in wireless, operation control
System is convenient.Returned data can be processed on computers.
Brief description of the drawings
Fig. 1 is the outside schematic diagram that the present invention installs state；
Fig. 2 is the structure sectional view that the present invention installs state；
Fig. 3 is the explosive view that the present invention installs state；
Fig. 4 is the structural representation of ducted fan component of the present invention；
Fig. 5 is the structural representation of lid and counterweight component on circuit supporting frame of the present invention；
Fig. 6 is the structural representation of main circuit board of the present invention；
Fig. 7 is the structural representation of upper shell of the present invention and ducted fan component；
Fig. 8 is the structural representation of housing and ducted fan component in the present invention；
Fig. 9 is the structural representation of housing and ducted fan component in the present invention；
Wherein：1 is upper shell, and 2 is camera module, and 3 is switch, and 4 is counterweight group
Part, 5 is to be covered on circuit supporting frame, and 6 is gesture module, and 7 is control module, and 8 is power supply mould
Block, 9 is support column between main circuit board, 10 plates, 11 circuit supporting framves, and 12 is ducted fan
Component, 12a is ducted fan component A, and 12b is ducted fan component B, and 12c is duct wind
Fan component C, 12d are ducted fan component D, and 13 is ducted fan, and 14 is solid for ducted fan
Determine part, 15 is middle housing, and 16 is battery, and 17 is lower house, and 18 is air inlet/outlet, 19
It is locating slot, 20 is screw thread guide post, and 21 is mass.
Specific embodiment
The invention will be further described below in conjunction with the accompanying drawings.
As shown in Figures 1 to 3, the present invention include upper shell 1, camera module 2, switch 3,
Lid 5 on counterweight component 4, circuit supporting frame, main circuit board 9, circuit supporting frame 11,
Ducted fan modular assembly 12, middle housing 15, battery 16 and lower house 17, wherein upper casing
Body 1, middle housing 15 and lower house 17 are sequentially connected to form octahedral cavity, and upper shell 1 is with
Junction between housing 15 and the junction between middle housing 15 and lower house 17 use
Groove and the cooperation of boss, steel is provided with the hole that the upper and lower ends of middle housing 15 are formed around
Silk swivel nut, with screw by upper shell 1, middle housing 15 and lower house 17 at each steel-wire screw-socket
Link together.Lid 5, main circuit board 9, electricity on counterweight component 4, circuit supporting frame
Road support frame 11, ducted fan component 12 and battery 16 are respectively contained in upper, middle and lower shell
In the octahedral cavity that body 1,15,17 is formed.
At least one ducted fan component 12 is respectively equipped with upper shell 1 and lower house 17, on
The ducted fan component that the quantity of ducted fan component 12 that housing 1 is set is set with lower house 17
12 quantity are identical, and the present embodiment is respectively provided with a culvert on upper shell 1 and lower house 17
Road fan component 12, respectively ducted fan component A12a and ducted fan component B12b.
As shown in Fig. 1~3 and Fig. 7, upper shell 1 includes top surface and is sequentially connected and difference
Eight sides being connected with the top surface, the ducted fan component A12a peaces set on upper shell 1
In the locating slot 19 opened up on top surface lower surface.Eight sides of upper shell 1 include four
Individual gore and four square faces, each gore and each square face interval setting, wherein four
Individual square face is provided with air inlet/outlet 18, i.e. air inlet/outlet 18 for four；Switch 3 is arranged on
On upper shell 1 on any one gore, it is connected with main circuit board 9；On the top of upper shell 1
Face upper surface is provided with the camera module 2 being connected with main circuit board 9.
As shown in Fig. 1~3 and Fig. 9, lower house 17 is identical with the shape of upper shell 1, including
Bottom surface and eight sides for being sequentially connected and being connected with the bottom surface respectively, set on lower house 17
The ducted fan component F12f for putting is arranged in the locating slot 19 opened up on the upper surface of bottom surface.Under
Eight sides of housing 17 include four gores and four square faces, each gore with
Each square face interval setting, wherein four square faces are provided with air inlet/outlet 18, that is, enters outlet
Mouth 18 is four.
As shown in Fig. 1~3 and Fig. 8, middle housing 15 includes bottom surface and is sequentially connected and difference
Eight sides being connected with the bottom surface, eight equal face square faces in side, eight square faces it is upper
Following eight sides top phase following with eight sides of upper shell 1 and lower house 17 respectively
Connection.The bottom surface of middle housing 15 be along the circumferential direction provided with diameter not wait inside and outside two groups of screw threads determine
Position hole, every group of threaded locating hole be four, along the circumferential direction uniformly, respectively outer periphery Positioning
Hole and inner circumferential location hole.The bottom of circuit supporting frame 11 is provided with four threaded locating holes, and leads to
Cross the outer periphery Positioning hole that screw is fixed to the bottom surface of middle housing 15；The inside of circuit supporting frame 11 holds
The main circuit board 9 on the bottom surface of middle housing 15 is equipped with, the top of circuit supporting frame 11 sets
There is lid 5 on circuit supporting frame, be evenly equipped with multiple counterweight groups on the circuit supporting frame on lid 5
Part 4.The four direction all around of the periphery of circuit supporting frame 11 is equipped with installed in middle housing
Ducted fan component 12 on 15, turnover is provided with eight sides of middle housing 15 at intervals
Gas port 18, i.e. air inlet/outlet 18 are four, and four ducted fan components 12 are separately mounted to
On side between 15 liang of air inlet/outlets 18 of middle housing, respectively ducted fan component B12b,
Ducted fan component C12c, ducted fan component D12d, ducted fan component E12e, install
Locating slot 19 is provided with four the four of ducted fan component 12 sides, for installing duct
Fan component 12.Battery 16 (battery 16 of the present embodiment is two) is arranged on middle housing
The lower surface of 15 bottom surfaces, is connected with main circuit board 9.
As shown in fig. 6, main circuit board 9 includes gesture module 6, control module 7 and power supply mould
Block 8, the gesture module 6, control module 7 and power module 8 pass through many (the present embodiment
It is four) support column 10 is connected between plate, and support column 10 is copper post, lower end between four plates
It is threaded, the inner circumferential location hole of the bottom surface of middle housing 15 is threadedly connected to respectively.
As shown in figure 5, be provided with four groups of balances on the circuit supporting frame of the present embodiment on lid 5 matching somebody with somebody
Restructuring part 4, every group of counterweight component is comprising a screw thread guide post 20 and with interior spiral shell
The mass 21 of line, screw thread guide post 20 is arranged on the circuit supporting frame on lid 5, matter
Gauge block 21 is threadedly connected on screw thread guide post 20, is led in screw thread by adjusting mass 21
The position of centre of gravity of aircraft can be adjusted to the position on bar 20.
Each ducted fan component 12 on upper shell 1, middle housing 15 and lower house 17 is distinguished
It is connected with main circuit board 9, as shown in figure 4, each structure of ducted fan component 12 is identical,
Include ducted fan fixture 14 and two ducted fans 13, two ducted fans 13
It is arranged on ducted fan fixture 14 opposite to each other, i.e., the two air-out direction phases of ducted fan 13
Instead.The ducted fan component on ducted fan component A12a and lower house 17 on upper shell 1
The longitudinal center line of F12f is coplanar, and each parallel to horizontal plane；On middle housing 15 all around
Ducted fan component B12b, ducted fan component C12c, the duct wind set on four direction
In fan component D12d, ducted fan component E12e, the ducted fan component that fore-and-aft direction is set
The duct that the longitudinal center line of B12B and ducted fan component D12d is set perpendicular to left and right directions
The longitudinal center line of fan component C12c and ducted fan component E12E, and fore-and-aft direction setting
Ducted fan component B12b and ducted fan component D12d axial centerline parallel in level
Face, the axial direction of the ducted fan component C12c that left and right directions is set and ducted fan component E12e
Central axis are in the ducted fan component A12a on horizontal plane, upper shell 1 and lower house 17
On ducted fan component F12f longitudinal center line and fore-and-aft direction set ducted fan
The projection in the horizontal plane of the longitudinal center line of component B12b and ducted fan component D12d is mutual
Vertically.Or, the ducted fan component C12c that left and right directions is set and ducted fan component E12e
Axial centerline parallel in horizontal plane, the ducted fan component B12B that fore-and-aft direction is set with
Duct of the longitudinal center line of ducted fan component D12d on horizontal plane, upper shell 1
The longitudinal center line of the ducted fan component F12f on fan component A12a and lower house 17 with
And in the axial direction of the ducted fan component C12c and ducted fan component E12e of left and right directions setting
The projection in the horizontal plane of heart line is mutually perpendicular to.
Battery 16 is connected with gesture module 6, control module 7 and power module 8 respectively, opens
Close each duct on 3, camera module 2 and upper shell 1, middle housing 15 and lower house 17
Fan component 12 was both connected with control module 7 respectively, and was connected with power module 8 respectively.
Operation principle of the invention is：
Battery 16 is powered to main circuit board 9, and the power module 8 on main circuit board 9 is according to each
The operating voltage of individual device is powered to each device；Gesture module 6 passes through sensor real-time monitoring
Current flight device attitude information, control module 7 is sent to by attitude of flight vehicle information, controls mould
Block 7 is used for and the external world is communicated, and is simultaneously emitted by control signal to each ducted fan component 12
Speed governing is carried out, the control to aircraft is realized.Camera module 2 collection image information via
Control module 7 on main circuit board 9, is subsequently sent to host computer, and host computer is by wirelessly connecing
Receive image information and show in real time and process.
The present invention sets six ducted fan components 12 altogether, octahedra aircraft it is forward and backward, left,
It is right, upper and lower to be mounted on ducted fan component 12, two, each direction ducted fan 13.
Ducted fan 13 and lower house 1 at ducted fan component A12a in upper shell 1 later
Ducted fan 13 at middle ducted fan component F12f later is rotated simultaneously when, aircraft is whole
Body straight forward movement；When ducted fan component A12a is in duct above in upper shell 1
Fan 13 is same in ducted fan 13 above with ducted fan component F12f in lower house 1
When rotating, aircraft integrally moves along a straight line backward.Ducted fan component in central housing 15
B12b is in ducted fan 13 above and is in duct above with ducted fan component D12d
Fan 13 is rotated simultaneously when, the overall linear motion downwards of aircraft；Duct in central housing 15
Fan component B12b is in following ducted fan 13 and is in down with ducted fan component D12d
The ducted fan 13 in face is rotated simultaneously when, the overall linear motion upwards of aircraft.Central housing
Ducted fan 13 and ducted fan component in 15 at ducted fan component C12c later
Ducted fan 13 at E12e later is rotated simultaneously when, aircraft integrally moves along a straight line to the left；
Ducted fan component C12c is in ducted fan 13 and duct wind above in central housing 15
The ducted fan 13 that fan component E12e is in above is rotated simultaneously when, aircraft is overall straight to the right
Line is moved.When being in the ducted fan component B12b being oppositely arranged and ducted fan component D12d
(i.e. ducted fan component B12b is in culvert above to two ducted fans 13 of diagonal
Road fan 13 is in following ducted fan 13 or ducted fan with ducted fan component D12d
It is above with ducted fan component D12d that component B12b is in following ducted fan 13
Ducted fan 13) while when rotating, you can realize aircraft unitary rotation；Similarly, phase is worked as
To being in diagonal in the ducted fan component C12c and ducted fan component E12e of setting
Two ducted fans 13 (i.e. ducted fan component C12c be in ducted fan 13 above with
At ducted fan 13 or ducted fan component C12c at ducted fan component E12e later
Ducted fan 13 later is in ducted fan 13 above with ducted fan component E12e)
When rotating simultaneously, you can realize aircraft unitary rotation；Again similarly, when duct in upper shell 1
Ducted fan 13 at fan component A12a later and ducted fan component in lower house 1
The ducted fan 13 that F12f is in above is rotated simultaneously when, you can realize aircraft unitary rotation；
When ducted fan component A12a is in ducted fan 13 above and lower house 1 in upper shell 1
Ducted fan 13 at middle ducted fan component F12f later is rotated simultaneously when, you can realize
Aircraft unitary rotation.Therefore, by the cooperation of each ducted fan component 12, it is capable of achieving to fly
Linear motion and three rotary motions in direction of the row device in three directions of three dimensions.
Claims (9)
1. a kind of octahedra aircraft, it is characterised in that：Octahedral chamber is formed including being sequentially connected
The upper shell (1) of body, middle housing (15), lower house (17) and be respectively contained in this eight
On counterweight component (4), circuit supporting frame in the cavity of face cover (5), main circuit board (9),
Circuit supporting frame (11), ducted fan component (12) and battery (16), wherein upper shell (1)
And at least one ducted fan component (12), the circuit are respectively equipped with lower house (17)
On middle housing (15), accommodated inside has installed in the middle housing support frame (11)
(15) main circuit board (9) on, circuit supporting frame (11) top is provided with circuit supporting
(5) are covered on frame, are covered on the circuit supporting frame on (5) and is evenly equipped with multiple counterweight components (4),
The direction all around of circuit supporting frame (11) periphery is equipped with installed in middle housing (15)
On ducted fan component (12)；The battery (16) on middle housing (15),
And be connected with the main circuit board (9)；Each ducted fan component (12) respectively with master
Circuit board (9) is connected, and is provided with the upper shell (1) and is connected with main circuit board (9)
Switch (3).
2. the octahedra aircraft as described in claim 1, it is characterised in that：Described in each
Ducted fan component (12) structure is identical, including ducted fan fixture (14) and two
Ducted fan (13), two ducted fans (13) are solid installed in the ducted fan opposite to each other
Determine on part (14), i.e., the air-out direction of described two ducted fans (13) is opposite.
3. the octahedra aircraft as described in claim 1, it is characterised in that：Described in each
Counterweight component (4) structure is identical, including screw thread guide post (20) and mass (21),
The screw thread guide post (20) is covered on (5) on the circuit supporting frame, the quality
Block (21) is threadedly connected on the screw thread guide post (20).
4. the octahedra aircraft as described in claim 1, it is characterised in that：The main electricity
Road plate (9) includes gesture module (6), control module (7) and power module (8), the appearance
Morphotype block (6), control module (7) and power module (8) are by support column (10) between many plates
It is connected, the lower end of support column (10) is threadedly connected to the middle housing (15) between each plate
Bottom surface on.
5. the octahedra aircraft as described in claim 1, it is characterised in that：The upper casing
Body (1) and lower house (17) shape are identical, and the upper shell (1) connects including top surface and successively
Eight sides for connecing and being connected with the top surface respectively, the lower house (17) including bottom surface and
Eight sides for being sequentially connected and being connected with the bottom surface respectively, set on the upper shell (1)
The locating slot (19) that the ducted fan component (12) put is opened up on the top surface lower surface
Interior, the ducted fan component (12) set on the lower house (17) is installed in the bottom surface
In the locating slot (19) opened up on upper surface；The upper shell (1) and lower house (17)
On eight sides in be provided with air inlet/outlet (18) at intervals, in the upper shell (1)
It is provided with and the main circuit board (9) on side between upper any two described air inlet/outlets (18)
Connected switch (3).
6. the octahedra aircraft as described in claim 5, it is characterised in that：The upper casing
Eight sides of body (1) and lower house (17) are square including four gores and four
Face, each gore and each square face interval setting, wherein four square faces
Be provided with air inlet/outlet (18), the switch (3) on upper shell (1) any one
On gore；It is provided with the top surface of the upper shell (1) and is connected with main circuit board (9)
The camera module (2) for connecing.
7. the octahedra aircraft as described in claim 1, it is characterised in that：The middle shell
Body (15) includes bottom surface and eight sides for being sequentially connected and being connected with the bottom surface respectively,
Air inlet/outlet (18) is provided with eight sides at intervals, on the middle housing (15)
The ducted fan component (12) for all around setting is separately mounted to air inlet/outlet described in two (18)
Between side on.
8. the octahedra aircraft as described in claim 7, it is characterised in that：Described eight
The equal face square face in side, eight square faces it is upper following respectively with the upper shell (1) and under
Housing (17) is connected；The bottom surface of the middle housing (15) is along the circumferential direction provided with inside and outside two
Group threaded locating hole, respectively outer periphery Positioning hole and inner circumferential location hole, the circuit supporting frame
(11) bottom is fixed to the outer periphery Positioning hole of middle housing (15) bottom surface by screw, described
Main circuit board (9) is connected with the inner circumferential location hole of middle housing (15) bottom surface；The battery (16)
Installed in the lower surface of middle housing (15) bottom surface.
9. the octahedra aircraft as described in claim 1, it is characterised in that：The upper casing
The duct that ducted fan component (12) quantity that body (1) is set is set with lower house (17)
Fan component (12) quantity is identical, and the ducted fan component (12) on upper shell (1)
With the longitudinal center line of the ducted fan component (12) on lower house (17) each parallel to level
Face；The ducted fan component (12) that the middle housing (15) is set on left and right directions after going forward
In, the longitudinal center line of the ducted fan component (12) that fore-and-aft direction is set is perpendicular to right and left
To the longitudinal center line of the ducted fan component (12) for setting, and the duct that fore-and-aft direction is set
The ducted fan component (12) that the longitudinal center line or left and right directions of fan component (12) are set
Axial centerline parallel in horizontal plane, ducted fan component (12) that left and right directions is set or
The longitudinal center line of the ducted fan component (12) that fore-and-aft direction is set is perpendicular to horizontal plane, institute
State the duct wind on the ducted fan component (12) and lower house (17) on upper shell (1)
Parallel to the duct of horizontal plane on the longitudinal center line and middle housing (15) of fan component (12)
The projection in the horizontal plane of the longitudinal center line of fan component (12) is mutually perpendicular to.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201511020523.3A CN106927043B (en) | 2015-12-31 | 2015-12-31 | Aircraft |
Applications Claiming Priority (1)
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN109819622A (en) * | 2019-03-18 | 2019-05-28 | 深圳市沃特沃德股份有限公司 | Mainboard mounting structure and electronic equipment |
| CN110127069A (en) * | 2019-04-17 | 2019-08-16 | 深圳市一刻创意电子有限公司 | A kind of plane-hop device with image processing function |
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| US20150360776A1 (en) * | 2014-06-11 | 2015-12-17 | Ecole Polytechnique Federale De Lausanne (Epfl) | Vertical take-off and landing aerial vehicle |
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| US20110226892A1 (en) * | 2008-08-08 | 2011-09-22 | William Crowther | Rotary wing vehicle |
| WO2013060693A2 (en) * | 2011-10-27 | 2013-05-02 | Desaulniers Jean-Marc Joseph | Active geometric exoskeleton with pseudo-rhombohedral annular fairing for gyropendular craft |
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| CN109819622A (en) * | 2019-03-18 | 2019-05-28 | 深圳市沃特沃德股份有限公司 | Mainboard mounting structure and electronic equipment |
| CN110127069A (en) * | 2019-04-17 | 2019-08-16 | 深圳市一刻创意电子有限公司 | A kind of plane-hop device with image processing function |
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| Publication number | Publication date |
|---|---|
| CN106927043B (en) | 2023-04-25 |
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