CN208963313U - A kind of folding mixed layout unmanned plane - Google Patents
A kind of folding mixed layout unmanned plane Download PDFInfo
- Publication number
- CN208963313U CN208963313U CN201821296745.7U CN201821296745U CN208963313U CN 208963313 U CN208963313 U CN 208963313U CN 201821296745 U CN201821296745 U CN 201821296745U CN 208963313 U CN208963313 U CN 208963313U
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- wing
- fixed
- unmanned plane
- mounting base
- folding
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Abstract
The utility model discloses a kind of folding mixed layout unmanned planes, including fuselage, fuselage two sides are provided with folding wing, at least four rotor assemblies are provided on the wing, the rotor assemblies include the connecting rod connecting with wing, the end of the connecting rod is provided with steering mechanism, is fixed with helical blade in the steering mechanism；Steering mechanism in rotor assemblies makes helical blade usable rotational direction, 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 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 mixed layout unmanned planes.
Background technique
Traditional unmanned plane during flying device generallys use the method for changing wing shape, such as curved using change angle of sweep, change aerofoil profile
The methods of degree, to adapt to the different state of flight such as landing, cruise and high-speed flight, makes every effort to obtain more satisfactory performance.But
This method mechanism complexity, function limitation, efficiency are lower, it is difficult to adapt to wider range flight environment of vehicle transformation (such as speed, weather,
Height etc.) requirement, cause traditional unmanned plane to be of limited application.
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 it is multiple turn to rotor, can
It realizes VTOL and high-performance cruise, meets the folding 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 mixed layout unmanned plane, including fuselage, fuselage two sides are provided with folding wing, the machine
It is provided at least four rotor assemblies on the wing, the rotor assemblies include the connecting rod connecting with wing and are fixed on connecting rod
On helical blade, the connecting rod end of at least one set of rotor assemblies is provided with steering mechanism, and the helical blade, which is fixed on, to be turned
To in 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 is rotatably connected by hinged seat and wing.
The utility model has the beneficial effects that
A kind of folding mixed layout unmanned plane of the utility model, the steering mechanism in rotor assemblies make helical blade
Usable rotational direction, so that unmanned plane can carry out high speed, long-time and long distance with VTOL as fixed wing aircraft
From cruise operation；And rotor assemblies and wing are foldable, and parking space becomes smaller, and 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 utility model first embodiment is unfolded；
Fig. 2 is the structural schematic diagram of the utility model rotor assemblies；
Fig. 3 is the decomposition diagram of the utility model rotor assemblies；
Fig. 4 is the folded structural schematic diagram of the utility model first embodiment；
Fig. 5 is structural schematic diagram when the utility model second embodiment is unfolded.
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. 5, a kind of folding mixed layout unmanned plane includes fuselage 1, and 1 two sides of fuselage are provided with and can roll over
Folded wing is provided at least four rotor assemblies on the wing, and the rotor assemblies include the connecting rod 2 connecting with wing
And it is fixed on the helical blade 2 in connecting rod 2,2 end of connecting rod of at least one set of rotor assemblies is provided with steering mechanism, institute
Helical blade 3 is stated to be fixed in steering mechanism.
According to first embodiment preferred in Fig. 1 to Fig. 4, each rotor assemblies are provided with steering mechanism, according to Fig. 5's
Second embodiment, two rotor assemblies on front side of fuselage are provided with steering mechanism, and two on rear side of fuselage rotor assemblies are not set
Steering mechanism is set, helical blade 3 is arranged on the pedestal of fixed-direction.According to production or design requirement, the rotor of different number
Component can freely select the steering mechanism of different number, and each steering mechanism is arranged at 2 end of connecting rod.
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 with rolling bearing 5 and same
To rotation, the outside of the mounting base 4 passes through connector and is fixed with fixed plate 6, and the fixed plate 6 presses rolling bearing 5
In mounting base 4, fall 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 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 mounting base
On 4.The two sides of the rotary drive motor 11 are provided with locating plate 10, are provided with location hole, location hole on the locating plate 10
It is inside equipped with locating shaft 12, locating shaft 12 is fixed in mounting base 4.Gag lever post 13 and locating shaft 12 all play better fixation
Effect, rotary drive motor 11 are 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 is rotatably connected by hinged seat 16 with wing.According to Fig. 1 to Fig. 5, the selection of hinged seat 16 is shipped and resell on another market matches with rotation seat
Close hinged, inner wing 14 and outer wing 15 use hinge page coordination hinge, when being actually related to, the hinged seat 16 and inner wing 14 and outer
Any structure that wing and connecting rod 2 can be made to relatively rotate can be used between the wing 15.And 15 side of rotation of inner wing 14 and outer wing
To can also rotate down, between connecting rod 2 and wing can horizontal or vertical direction, or each angle is carried out using ball link
Rotation.Wing and connecting rod 2 are respectively articulated with, and aircraft can be made to occupy smaller space in storage, carry more convenient, use
Family use is more convenient.
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 (7)
1. a kind of folding mixed layout unmanned plane, it is characterised in that: including fuselage (1), fuselage (1) two sides are provided with and can roll over
Folded wing is provided at least four rotor assemblies on the wing, and the rotor assemblies include the connecting rod connecting with wing
(2) and the helical blade (3) that is fixed on connecting rod (2), connecting rod (2) end of at least one set of rotor assemblies, which is provided with, to be turned
To mechanism, the helical blade (3) is fixed in steering mechanism.
2. folding mixed layout unmanned plane according to claim 1, it is characterised in that: the steering mechanism includes peace
It fills seat (4), the two sides of mounting base (4) are provided with rolling bearing (5), are provided with rotary drive motor in the mounting base (4)
(11), the rotary shaft of the rotary drive motor (11) passes through mounting base (4) and connect and rotate in same direction with rolling bearing (5), institute
It states and is arranged on rolling bearing (5) connecting plate (7), 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 helical blade (3) pass through rotary electric machine (9) drive.
3. folding mixed layout unmanned plane according to claim 2, it is characterised in that: outside the mounting base (4)
Side passes through connector and is fixed with fixed plate (6), and the fixed plate (6) presses against rolling bearing (5) on mounting base (4).
4. folding mixed layout unmanned plane according to claim 2, it is characterised in that: the rotary drive motor
(11) two sides are provided with locating plate (10), are provided with location hole on the locating plate (10), positioning hole is equipped with locating shaft
(12), locating shaft (12) is fixed on mounting base (4).
5. folding mixed layout unmanned plane according to claim 2, it is characterised in that: the rotary drive motor
(11) surrounding 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 mixed layout unmanned plane according to claim 1, it is characterised in that: the wing includes and fuselage
(1) inner wing (14) connected, inner wing (14) outside are hinged with the outer wing (15) of turnover folding.
7. folding mixed layout unmanned plane according to claim 1, it is characterised in that: the connecting rod (2) passes through
Hinged seat (16) is rotatably connected with wing.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821296745.7U CN208963313U (en) | 2018-08-13 | 2018-08-13 | A kind of folding mixed layout unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821296745.7U CN208963313U (en) | 2018-08-13 | 2018-08-13 | A kind of folding mixed layout unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208963313U true CN208963313U (en) | 2019-06-11 |
Family
ID=66752807
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821296745.7U Active CN208963313U (en) | 2018-08-13 | 2018-08-13 | A kind of folding mixed layout unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208963313U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110588967A (en) * | 2019-10-21 | 2019-12-20 | 武汉思众空间信息科技有限公司 | Aircraft and aircraft system |
| CN113460286A (en) * | 2021-09-06 | 2021-10-01 | 西安羚控电子科技有限公司 | Wing folding and locking mechanism of flight device |
-
2018
- 2018-08-13 CN CN201821296745.7U patent/CN208963313U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110588967A (en) * | 2019-10-21 | 2019-12-20 | 武汉思众空间信息科技有限公司 | Aircraft and aircraft system |
| CN113460286A (en) * | 2021-09-06 | 2021-10-01 | 西安羚控电子科技有限公司 | Wing folding and locking mechanism of flight device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| 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. |
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| CP02 | Change in the address of a patent holder | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20220729 Address after: 110000 first floor of plant, No. 37-3, Shenbei Road, Shenbei New District, Shenyang City, Liaoning Province Patentee after: Shenyang Tianqing Aerospace Technology Co.,Ltd. Address before: 519000 Room 102, floor 1, No. 3 plant, No. 6898, Zhuhai Avenue, Hongqi Town, Jinwan District, Zhuhai City, Guangdong Province Patentee before: ZHUHAI TIANQING AEROSPACE TECHNOLOGY CO.,LTD. |
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| TR01 | Transfer of patent right |