CN208963312U - A kind of folding three rotors mixed layout unmanned plane - Google Patents
A kind of folding three rotors mixed layout unmanned plane Download PDFInfo
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- CN208963312U CN208963312U CN201821296691.4U CN201821296691U CN208963312U CN 208963312 U CN208963312 U CN 208963312U CN 201821296691 U CN201821296691 U CN 201821296691U CN 208963312 U CN208963312 U CN 208963312U
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- fuselage
- wing
- unmanned plane
- mounting base
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Abstract
The utility model discloses a kind of folding three rotors mixed layout unmanned planes, towards the rotor assemblies of front fuselage there are two being arranged on the wing, the tail portion of the fuselage is provided with the fin assembly towards back body, the rotor assemblies include the connecting rod connecting with wing, the fin assembly includes and fuselage and folding foot piece, the end of the foot piece and connecting rod is provided with steering mechanism, is fixed with helical blade in the steering mechanism；Complete machine lightweight, miniaturization, and the steering mechanism of rotor assemblies and fin assembly enables helical blade to change direction, it is horizontally and vertically rotated, so that unmanned plane can carry out high speed, long-time and operation of cruising at a distance with VTOL as fixed wing aircraft；And rotor assemblies, fin assembly and wing are foldable, and parking space becomes smaller, and carries more convenient.
Description
Technical field
The utility model relates to unmanned plane during flying device field, more particularly to a kind of folding three rotors mixed layout nobody
Machine.
Background technique
Traditional rotor wing unmanned aerial vehicle aircraft uses the rotor structure of fixed-direction, is able to achieve VTOL, and can compared with
Fly in small space, flexibility is higher than fixed-wing class unmanned plane, but its that there are payload is smaller, cruising speed compared with
Slowly, shorter disadvantage in cruise duration.But this method mechanism complexity, function limitation, efficiency are lower, it is difficult to adapt to wider range and fly
Row environment converts the requirement of (such as speed, weather, height), limits its using flexible and efficiency.
Utility model content
In order to overcome the above-mentioned deficiencies of the prior art, the utility model provide it is a kind of setting three can turn to rotor, can
It realizes VTOL and high-performance cruise, meets the folding three rotors mixed layout unmanned plane of different flight demands.
To achieve the goals above, the technical solution adopted in the utility model is:
A kind of folding three rotors mixed layout unmanned plane, including fuselage, fuselage two sides are provided with folding wing,
It is arranged on the wing there are two the rotor assemblies towards front fuselage, the tail portion of the fuselage is provided with one towards after fuselage
The fin assembly at end, the rotor assemblies include the connecting rod connecting with wing, and the fin assembly includes and fuselage and can roll over
The end of folded foot piece, the foot piece and connecting rod is provided with steering mechanism, is fixed with helical blade in the steering mechanism.
As a further improvement of the foregoing solution, the steering mechanism includes mounting base, and the two sides of mounting base are provided with
Rolling bearing, is provided with rotary drive motor in the mounting base, the rotary shaft of the rotary drive motor pass through mounting base with
Rolling bearing is connected and is rotate in same direction, and connecting plate is arranged on the rolling bearing, and connecting plate is fixedly arranged at the front end with mounting plate,
Rotary electric machine is fixed on the mounting plate, the helical blade is driven by rotary electric machine.
As a further improvement of the foregoing solution, the outside of the mounting base passes through connector and is fixed with fixed plate, institute
Fixed plate is stated to press against rolling bearing in mounting base.
As a further improvement of the foregoing solution, the two sides of the rotary drive motor are provided with locating plate, the positioning
On piece is provided with location hole, and positioning hole is equipped with locating shaft, and locating shaft is fixed in mounting base.
As a further improvement of the foregoing solution, the surrounding of the rotary drive motor is provided with gag lever post, the limit
The both ends of bar are fixed in mounting base.
As a further improvement of the foregoing solution, the wing includes the inner wing connecting with fuselage, is hinged on the outside of inner wing
The outer wing of turnover folding.
As a further improvement of the foregoing solution, the connecting rod and foot piece are rotatably connected by linkwork with wing
It connects.
As a further improvement of the foregoing solution, the front end of the fuselage is provided with the camera cradle head for placing photographic device.
As a further improvement of the foregoing solution, control system is provided in the fuselage, including in control system can nothing
Line transmits the communication module of data, and the GPS sensing device of guiding is provided on fuselage, and GPS sensing device and control system are electrical
Connection.
The utility model has the beneficial effects that
A kind of folding three rotors mixed layout unmanned plane of the utility model, two sides rotor assemblies and fin assembly layout
Realize complete machine lightweight, miniaturization, and the steering mechanism of rotor assemblies and fin assembly enables helical blade to change direction,
It is horizontally and vertically rotated, so that unmanned plane can be carried out with VTOL as fixed wing aircraft
At a high speed, long-time and operation of cruising at a distance；And rotor assemblies, fin assembly and wing are foldable, and parking space becomes smaller,
It carries more convenient.
Detailed description of the invention
It, below will be to required in embodiment description in order to illustrate more clearly of the technical scheme in the embodiment of the utility model
Attached drawing to be used is briefly described.Obviously, described attached drawing is a part of the embodiment of the utility model, rather than complete
Portion's embodiment, those skilled in the art without creative efforts, can also be obtained according to these attached drawings
Other design schemes and attached drawing:
Fig. 1 is structural schematic diagram when the best embodiment of the utility model is unfolded；
Fig. 2 is the structural schematic diagram of the utility model steering mechanism；
Fig. 3 is the decomposition diagram of the utility model steering mechanism；
Fig. 4 is the folded structural schematic diagram of the best embodiment of the utility model.
Specific embodiment
It is carried out below with reference to technical effect of the embodiment and attached drawing to the design of the utility model, specific structure and generation
It clearly and completely describes, to be completely understood by the purpose of this utility model, feature and effect.Obviously, described embodiment
It is a part of the embodiment of the utility model, rather than whole embodiments, it is based on the embodiments of the present invention, the skill of this field
Art personnel other embodiments obtained without creative efforts belong to the model of the utility model protection
It encloses.
Referring to figs. 1 to Fig. 4, a kind of folding three rotors mixed layout unmanned plane, including fuselage 1, the setting of 1 two sides of fuselage
There is folding wing, there are two the rotor assemblies towards front fuselage, the tail portion settings of the fuselage 1 for setting on the wing
There is the fin assembly towards back body, the rotor assemblies include the connecting rod 2 connecting with wing, the fin assembly
Including being provided with steering mechanism with the end of fuselage 1 and folding foot piece 16, the foot piece 16 and connecting rod 2, described turn
Helical blade 3 is fixed in mechanism.
The steering mechanism includes mounting base 4, and the two sides of mounting base 4 are provided with rolling bearing 5, in the mounting base 4
It is provided with rotary drive motor 11, the rotary shaft of the rotary drive motor 11 passes through mounting base 4 and connect simultaneously with rolling bearing 5
It rotates in same direction, the outside of the mounting base 4 passes through connector and is fixed with fixed plate 6, and the fixed plate 6 pushes up rolling bearing 5
It is pressed in mounting base 4, falls off to prevent rolling bearing 5.
Connecting plate 7 is arranged on the rolling bearing 5, connecting plate 7 is fixedly arranged at the front end with mounting plate 8, the mounting plate 8
On be fixed with rotary electric machine 9, the driving axis connection of the helical blade 3 and rotary electric machine 9, rotary electric machine 9 drives helical blade 3
Rotation.
After rotary drive motor 11 starts, rotary shaft drives the connecting plate 7 being arranged outside rolling bearing 5 to rotate, so that even
The mounting plate 8 of 7 front end of fishplate bar realizes the swing around drive shaft, and helical blade 3 is driven to move to different angle, rotor assemblies and tail
Wing component is to realize rotation both horizontally and vertically.When taking off, helical blade 3 horizontally rotates, and realization subtracts VTOL,
When horizontal flight, the axis of helical blade 3 goes to course direction, carries out high speed, long-time and operation of cruising at a distance.
The surrounding of the rotary drive motor 11 is provided with gag lever post 13, and the both ends of the gag lever post 13 are fixed on installation
On seat 4.The two sides of the rotary drive motor 11 are provided with locating plate 10, are provided with location hole on the locating plate 10, positioning
Locating shaft 12 is equipped in hole, locating shaft 12 is fixed in mounting base 4.Gag lever post 13 and locating shaft 12 all play preferably solid
It is set for using, rotary drive motor 11 is easier for installation.
The wing includes the inner wing 14 connecting with fuselage 1, and the outer wing 15 of turnover folding, institute are hinged on the outside of inner wing 14
It states connecting rod 2 and foot piece 16 is rotatably connected by linkwork and wing.According to Fig. 1 to Fig. 4, the hinged machine of connecting rod 2
Structure selects the linkwork of ship and resell on another market 20 and 21 coordination hinge of rotation seat, inner wing 14 and outer wing 15 and foot piece 16 to match using hinge page 19
Close it is hinged, it is described ship and resell on another market 20 can with the rotation axis connection for folding driving motor, realize ship and resell on another market 20 automatic control.Or outer wing
15, it being connected with push rod, the telescopic component connection of push rod and pneumatic mechanism on connecting rod 2 or foot piece 16, driving push rod moves forward and backward,
Realize turning folding for outer wing 15, connecting rod 2 or foot piece 16.
In actual design, the linkwork, which can be used, any can make wing and 1 phase of connecting rod 2, foot piece 16 and fuselage
To the structure of rotation.And inner wing 14 and 15 rotation direction of outer wing can also rotate down, it can be horizontal between connecting rod 2 and wing
Or vertical direction, or the rotation for using ball link to carry out each angle.Wing and connecting rod 2 are respectively articulated with, and can to fly
Device occupies smaller space in storage, and carrying is more convenient, and user's use is more convenient.
The front end of the fuselage 1 is provided with the camera cradle head 17 for placing photographic device, can facilitate and take photo by plane, and dismounts
Convenient, use is simpler.Be provided with control system in the fuselage 1, include in control system can wirelessly transmitting data it is logical
Module is interrogated, the GPS sensing device 18 of guiding is provided on fuselage, GPS sensing device 18 and control system are electrically connected.The rotation
Turn driving motor 11 and fold driving motor and control system electric connection, user can wirelessly manipulate rotor group in flight course
The direction of rotation and rotor assemblies of part and fin assembly and the auto-folder of fin assembly.
It is to be illustrated to the preferred embodiment of the utility model, but the utility model creation is not limited to above
The embodiment, those skilled in the art can also make various etc. without departing from the spirit of the present invention
Same variation or replacement, these equivalent variation or replacement are all included in the scope defined by the claims of the present application.
Claims (9)
1. a kind of folding three rotors mixed layout unmanned plane, it is characterised in that: including fuselage (1), the setting of fuselage (1) two sides
There is folding wing, there are two the rotor assemblies towards front fuselage, the tail portion of the fuselage (1) is set for setting on the wing
It is equipped with the fin assembly towards back body, the rotor assemblies include the connecting rod (2) connecting with wing, the empennage
Component includes being provided with steering with fuselage (1) and folding foot piece (16), the end of the foot piece (16) and connecting rod (2)
Mechanism is fixed with helical blade (3) in the steering mechanism.
2. folding three rotors mixed layout unmanned plane according to claim 1, it is characterised in that: the steering mechanism
Including mounting base (4), the two sides of mounting base (4) are provided with rolling bearing (5), and rotation is provided in the mounting base (4) and is driven
Dynamic motor (11), the rotary shaft of the rotary drive motor (11) pass through mounting base (4) and connect with rolling bearing (5) and turn in the same direction
It is dynamic, it is arranged with connecting plate (7) on the rolling bearing (5), connecting plate (7) is fixedly arranged at the front end with mounting plate (8), the installation
It is fixed on plate (8) rotary electric machine (9), the helical blade (3) is driven by rotary electric machine (9).
3. folding three rotors mixed layout unmanned plane according to claim 2, it is characterised in that: the mounting base
(4) outside passes through connector and is fixed with fixed plate (6), and rolling bearing (5) is pressed against mounting base by the fixed plate (6)
(4) on.
4. folding three rotors mixed layout unmanned plane according to claim 2, it is characterised in that: the rotation driving
The two sides of motor (11) are provided with locating plate (10), and location hole is provided on the locating plate (10), and positioning hole is equipped with fixed
Position axis (12), locating shaft (12) are fixed on mounting base (4).
5. folding three rotors mixed layout unmanned plane according to claim 2, it is characterised in that: the rotation driving
The surrounding of motor (11) is provided with gag lever post (13), and the both ends of the gag lever post (13) are fixed on mounting base (4).
6. folding three rotors mixed layout unmanned plane according to claim 1, it is characterised in that: the wing includes
The inner wing (14) connecting with fuselage (1), inner wing (14) outside are hinged with the outer wing (15) of turnover folding.
7. folding three rotors mixed layout unmanned plane according to claim 1, it is characterised in that: the connecting rod
(2) it is rotatably connected with foot piece (16) by linkwork and wing.
8. folding three rotors mixed layout unmanned plane according to claim 1, it is characterised in that: the fuselage (1)
Front end be provided with place photographic device camera cradle head (17).
9. folding three rotors mixed layout unmanned plane according to claim 1, it is characterised in that: the fuselage (1)
Inside be provided with control system, include in control system can wirelessly transmitting data communication module, the GPS of guiding is provided on fuselage
Sensing device (18), GPS sensing device (18) and control system are electrically connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821296691.4U CN208963312U (en) | 2018-08-13 | 2018-08-13 | A kind of folding three rotors mixed layout unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821296691.4U CN208963312U (en) | 2018-08-13 | 2018-08-13 | A kind of folding three rotors mixed layout unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208963312U true CN208963312U (en) | 2019-06-11 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821296691.4U Active CN208963312U (en) | 2018-08-13 | 2018-08-13 | A kind of folding three rotors mixed layout unmanned plane |
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| CN (1) | CN208963312U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109018332A (en) * | 2018-08-13 | 2018-12-18 | 珠海天晴航空航天科技有限公司 | A kind of folding three rotors mixed layout unmanned plane |
-
2018
- 2018-08-13 CN CN201821296691.4U patent/CN208963312U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109018332A (en) * | 2018-08-13 | 2018-12-18 | 珠海天晴航空航天科技有限公司 | A kind of folding three rotors mixed layout unmanned plane |
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| CP02 | Change in the address of a patent holder |
Address after: Room 102, floor 1, 3 workshop, No. 6898, Zhuhai Avenue, Hongqi Town, Jinwan District, Zhuhai City, Guangdong Province Patentee after: ZHUHAI TIANQING AEROSPACE TECHNOLOGY Co.,Ltd. Address before: 519000 Guangdong Province, Zhuhai city planning exhibition hall on the third floor of the aviation city Jinwan District 312-30 room Patentee before: ZHUHAI TIANQING AEROSPACE TECHNOLOGY Co.,Ltd. |