CN207466965U - Unmanned plane - Google Patents
Unmanned plane Download PDFInfo
- Publication number
- CN207466965U CN207466965U CN201721434546.3U CN201721434546U CN207466965U CN 207466965 U CN207466965 U CN 207466965U CN 201721434546 U CN201721434546 U CN 201721434546U CN 207466965 U CN207466965 U CN 207466965U
- Authority
- CN
- China
- Prior art keywords
- horn
- component
- fuselage
- unmanned plane
- shaft
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
- 238000003032 molecular docking Methods 0.000 claims description 11
- 238000000034 method Methods 0.000 abstract description 4
- 230000000694 effects Effects 0.000 description 3
- 230000004308 accommodation Effects 0.000 description 2
- 230000006978 adaptation Effects 0.000 description 2
- 238000013461 design Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000005452 bending Methods 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 230000008030 elimination Effects 0.000 description 1
- 238000003379 elimination reaction Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 238000011017 operating method Methods 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 238000012384 transportation and delivery Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Landscapes
- Agricultural Machines (AREA)
Abstract
A kind of unmanned plane, the unmanned plane include：Fuselage, the first horn component for being set to the fore-body and the second horn component set on the fuselage afterbody, the first horn component includes the first horn, the second horn component includes the second horn, first horn and second horn are rotationally connected with the fuselage respectively, so that the first horn component and the second horn component are in unfolded state or folded state；Wherein, when the first horn component and the second horn component are in folded state, first horn and second horn are arranged side by side in the horizontal direction.The utility model devises a kind of horn folding unmanned plane, and the folded form of the unmanned plane is simple and reliable, and after folding horn, unmanned function is realized space-minimized, and the protectiveness of horn is enhanced, can to avoid in storage and transportational process horn be damaged.
Description
Technical field
The utility model is related to unmanned air vehicle technique field, more particularly to a kind of horn folding unmanned plane.
Background technology
Unmanned plane because have the advantages that maneuverability, rapid reaction, unmanned flight, operation require it is low all, also widely should
For military, scientific research and civil three big field, to perform transport, delivery, monitoring, investigation, exploration, the bat in each field application
The tasks such as take the photograph.
It is usually fixed in existing unmanned plane to carry the horn of Power Component by the modes such as being bonded or being integrally formed
In fuselage, cause horn can not disassemble with slave or slave with disassemble needs by tool and relatively complicated
And cause user that can not dismantle, very big inconvenience is so brought to storage of the unmanned plane in off working state and transport, easily
Horn and Power Component is caused to damage.
Utility model content
The utility model proposes a kind of unmanned planes of the foldable setting of horn to solve above-mentioned technical problem.
According to the utility model embodiment in a first aspect, provide a kind of unmanned plane, including：Fuselage, be set to it is described
First horn component of fore-body and the second horn component set on the fuselage afterbody, the first horn component packet
Include the first horn, the second horn component includes the second horn, first horn and second horn company of rotation respectively
The fuselage is connected to, so that the first horn component and the second horn component are in unfolded state or folded state；
Wherein, when the first horn component and the second horn component are in folded state, first horn and described
Second horn is arranged side by side in the horizontal direction.
Optionally, the first rotating shaft of the first horn component and the second shaft of the second horn component are put down same
On face, wherein, the center line where the first rotating shaft intersects with the center line where the second shaft.
Optionally, the fuselage includes fuselage main body and the lug boss protruded out below the fuselage main body；Its
In, the first horn component is rotationally connected with the lug boss, and the second horn component is rotationally connected with the fuselage master
Body.
Optionally, the first horn component and the second horn component are two, two the first horn groups
Part is set on the both sides of the lug boss, and two the second horn components are set in the fuselage main body；
Wherein, when the first horn component and the second horn component are in folded state, two described first
Horn fits in the both sides of the lug boss, and two second horns are located at the outside of first horn of homonymy.
Optionally, the fuselage further includes the docking section being set on the lug boss, and the first horn component also wraps
Include the first rotating shaft that first horn is connected to the docking section, wherein, first horn using the first rotating shaft as
Shaft rotation is moved.
Optionally, the docking section is equipped with the first axis hole being connected with the first rotating shaft, wherein, described first
The angle α of the axial direction of axis hole and the central shaft of the fuselage is 56 °.
Optionally, the first horn component further includes the stopper section for being set to the fuselage, and the stopper section is located at institute
On the rotation path for stating the first horn；
Wherein, when first horn is unfolded state, first horn is connected to the stopper section；When described
When one horn is folded state, first horn fits in the fuselage main body.
Optionally, the fuselage further includes the rotary shaft rack for being set to the fuselage main body, and the second horn component is also
The second shaft including second horn to be connected to the rotary shaft rack, wherein, second horn passes through described second
Shaft is connected to the medial surface of the rotary shaft rack and is moved using second shaft as shaft rotation.
Optionally, the rotary shaft rack is equipped with the second axis hole coordinated with second shaft, wherein, second axis
The angle β of the axial direction in hole and the central shaft of the fuselage is 118 °.
Optionally, the second horn component further includes the limited block on second horn, the rotary shaft rack
It is equipped with limiting slot；
Wherein, when second horn is unfolded state, the limited block is matched in the limiting slot with limiting；When
When second horn is folded state, second horn is set adjacent to first horn of homonymy.
Optionally, the first horn component further includes the first driving means being set on the lug boss, and described
One driving device is connected to first horn and driving the first horn rotation, so that first horn is in expansion shape
State or folded state；And/or
The second horn component further includes the second driving device being set in the fuselage main body, second driving
Device is connected to second horn and driving second horn rotation so that second horn be in unfolded state or
Folded state.
The technical solution that the embodiment of the utility model provides can include the following benefits：The utility model devises
A kind of horn folding unmanned plane, the folded form of the unmanned plane is simple and reliable, and after folding horn, unmanned function realizes space
Minimize, and the protectiveness of horn enhanced, can to avoid in storage and transportational process horn be damaged.
It should be understood that above general description and following detailed description are only exemplary and explanatory, not
The utility model can be limited.
Description of the drawings
It is required in being described below to embodiment 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, it should be apparent that, the accompanying drawings in the following description is only some realities of the utility model
Example is applied, it for those of ordinary skill in the art, without having to pay creative labor, can also be attached according to these
Figure obtains other attached drawings.
Fig. 1 is a kind of structure diagram of unmanned plane shown in one exemplary embodiment of the utility model；
Fig. 2 is a kind of bottom view of unmanned plane shown in one exemplary embodiment of the utility model；
Fig. 3 is the structure diagram that horn is unfolded in a kind of unmanned plane shown in one exemplary embodiment of the utility model；
Fig. 4 is structural representation when horn folds in a kind of unmanned plane shown in one exemplary embodiment of the utility model
Figure；
Fig. 5 is that the second horn is connect with rotary shaft rack in a kind of unmanned plane shown in one exemplary embodiment of the utility model
Partial cutaway schematic view；
Fig. 6 is the structural representation after horn folds in a kind of unmanned plane shown in one exemplary embodiment of the utility model
Figure.
Specific embodiment
The following is a combination of the drawings in the embodiments of the present utility model, and the technical scheme in the embodiment of the utility model is carried out
It clearly and completely describes, it is clear that the described embodiments are only a part of the embodiments of the utility model rather than whole
Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are without making creative work
All other embodiments obtained shall fall within the protection scope of the present invention.
Below in conjunction with the accompanying drawings, it elaborates to the structure of the unmanned plane of the utility model, in the absence of conflict, under
Feature in the embodiment and embodiment stated can be combined with each other.
As shown in figures 1 to 6, the unmanned plane 100 of the utility model embodiment includes：Fuselage 1 is set to 1 forepart of fuselage
The first horn component 22 and the second horn component 33 set on 1 rear portion of fuselage.First horn component 22 includes the first horn
21, the second horn component 33 includes the second horn 31, and the first horn 21 and the second horn 31 are rotationally connected with fuselage 1 respectively, with
The first horn component 22 and the second horn component 33 is made to be in unfolded state or folded state.The unmanned plane of the utility model
100 by the foldable setting of horn, can realize that unmanned plane 100 is space-minimized after horn folding, convenient for user's storage and
Transport, so as to protect unmanned plane 100.
Specifically, which at work, maximum spread is expanded to by the first horn 21 and the second horn 31
(as shown in Figure 3), i.e. the first horn component 22 and the second horn component 33 are in unfolded state.Unmanned plane 100 when not working,
First horn 21 and the second horn 31 are rotated relative to fuselage 1 so that the first horn 21 and the second horn 31 fit in fuselage 1
Side (as shown in Figure 6), i.e. the first horn component 22 and the second horn component 33 are in folded state.
Wherein, when the first horn component 22 and the second horn component 33 are in folded state, 21 He of the first horn
Second horn 31 is arranged side by side, i.e., is arranged side by side in same plane.Preferably, the first horn 21 and the second horn 31 are in level side
It is arranged side by side upwards.Wherein, it should be noted that horizontal direction herein is in the state of being ajusted with fuselage 1.The present embodiment
In, the both sides of fuselage 1 are respectively provided with the first horn 21 and the second horn 31, the first horn 21 and the second horn 31 of 1 both sides of fuselage
It is arranged side by side.Further, in order to make the compact overall structure of unmanned plane 100, the first horn 21 and the second horn 31 abut
Fitting, and whole fitting and fuselage 1.
As shown in Figures 1 to 6, the fuselage 1 of unmanned plane 100 includes fuselage main body 11 and convex from the lower section of fuselage main body 11
The lug boss 12 of stretching, which is located at the centre position of fuselage main body 11, such that lug boss 12 and fuselage main body
11 cooperations are so that the both sides of lug boss 12 form accommodation space.Wherein, in the first horn component 22 and the second horn component 33
During in folded state, first horn 21 and the second horn 31 of 1 the same side of fuselage can abreast be located in accommodation space, from
And the effect of the first horn 21 of protection and the second horn 31 can be further functioned as.
In the present embodiment, the first horn component 22 is rotationally connected with lug boss 12, and the second horn component 33 is rotatablely connected
In fuselage main body 11.This kind of fit system, during so that the first horn component 22 being in folded state, the first horn 21 fits in convex
Portion 12 is played, when the first horn component 22 is in folded state, the second horn 31 fits in the first horn 21.
In an alternative embodiment, the first horn component 22 and the second horn component 33 are two, two the first machines
Arm component 22 is set on the both sides of lug boss 12, and two the second horn components 33 are set in fuselage main body 11.Wherein, in the first horn
When 22 and second horn component 33 of component is in folded state, two the first horns 21 fit in the both sides of lug boss 12, two
Second horn 31 is located at the outside of the first horn 21 of homonymy.Below with unmanned plane 100 for 42 unmanned plane 100 of quadrotor (i.e.
Including two the first horns 21 and two the second horns 31) for, it describes in detail to the unmanned plane 100 of the utility model.
Correspondingly, which further includes the docking section 121 being set on lug boss 12, to match with the first horn 21
Close connection.The first horn component 22 further includes the first rotating shaft 22 that the first horn 21 is connected to docking section 121, the first horn
21 are moved with first rotating shaft 22 for shaft rotation.Wherein, docking section 121 is equipped with the first axis hole being connected with first rotating shaft 22, the
The connection of one shaft 22 is limited in first axis hole, and can be rotated in the first axis hole, in the present embodiment, the first axis hole
Axial (i.e. the axial direction of first rotating shaft 22) and the angle α of the central shaft 101 of fuselage 1 are 56 °, such that the first horn 21 is being rolled over
During overlapping state there is preferably expanded angle and fuselage 1 can be fitted in folded state, meeting unmanned plane 100 can realize
Space-minimized design requirement.
Further, which further includes the stopper section 13 for being set to fuselage 1, and stopper section 13 is located at first
On the rotation path of horn 21.Wherein, when the first horn 21 is unfolded state, the first horn 21 is connected to stopper section 13, with
Limit the rotational angle of the first horn 21；When the first horn 21 is folded state, the first horn 21 fits in fuselage main body 11.
In the present embodiment, by the limitation of stopper section 13, when the first horn 21 is in unfolded state, which is in water
Square upwards, spacing between 42 component 4 of rotor is maximum at this time, can farthest reduce between multiple 42 components 4 of rotor
Interference.
In an alternative embodiment, which further includes the rotary shaft rack 14 for being set to fuselage main body 11, to second
Horn 31 is connected.The second horn component 33 further includes the second shaft that the second horn 31 is connected to rotary shaft rack 14
32, the second horn 31 is connected to the medial surface of rotary shaft rack 14 by the second shaft 32 and is moved with the second shaft 32 for shaft rotation.This
In embodiment, which is set to the side of fuselage main body 11, to adapt to connect with the second horn component 33.Its
In, the second horn 31 is connected to the medial surface of rotary shaft rack 14, the second machine of protection can be played when the second horn 31 folds
The effect of arm 31.
Wherein, rotary shaft rack 14 is equipped with the second axis hole coordinated with the second shaft 32, the axial direction (i.e. second of the second axis hole
The axial direction of shaft 32) with the angle β of the central shaft 101 of fuselage 1 it is 118 °, such that the second horn 31 has in folded state
There is preferably expanded angle and the first horn 21 can be fitted in folded state, space can be realized by meeting unmanned plane 100
The design requirement of minimum.
Further, the second horn component 33 further includes the limited block 34 on the second horn 31, on rotary shaft rack 14
Equipped with limiting slot 141.Certainly, which can also be set on rotary shaft rack 14, and limiting slot is located on the second horn 31.Its
In, when the second horn 31 is unfolded state, limited block 34 is matched with limiting in limiting slot 141, so as to make the second horn 31
It is locked as unfolded state；When the second horn 31 is folded state, the second horn 31 is set adjacent to the first horn 21 of homonymy.
In one optional embodiment, which may be used the frame mode of flexible lock pin, which can use in outer masterpiece
In lower the second horn of retraction 31, the surface of the second horn 31 can be popped up after external force elimination.The top of the flexible lock pin is circle
Head dummy structure, such that the second horn 31, in the external force effect by certain dynamics, limited block 34 can be from limiting slot 141
It inside detaches, so as to so that the second horn 31 folds.
In the utility model, which is set to the side of fuselage main body 11, and bending extends to fuselage main body
11 lower section, so that the second shaft 32 of the 22 and second horn component 33 of first rotating shaft of the first horn component 22 is in same level
On face, it can so meet the first horn 21 and the second horn 31 is arranged side by side.Wherein, the center line where first rotating shaft 22 with
Center line where second shaft 32 intersects.
In a further alternative embodiment, the first horn component 22 further includes the first driving dress being set on lug boss 12
It puts, which can replace above-mentioned docking section 121.Wherein, first driving means be connected to the first horn 21 and
The first horn 21 can be driven to rotate so that the first horn 21 is in unfolded state or folded state, i.e., by controller to
First driving means send control signal, drive 21 Automatic-expanding of the first horn or auto-folder by first driving means, not only
The operating procedure of user can be simplified, and increase the fun of using and degree of intelligence of product.
Further, which further includes the second driving device being set in fuselage main body 11, with
The rotary shaft rack 14 of two horns 31 connection can use the second driving device to replace, which is connected to the second horn
31 and driving the second horn 31 rotate so that the second horn 31 is in unfolded state or folded state.I.e. by controller to
Second driving device sends control signal, and 31 Automatic-expanding of the second horn or auto-folder are driven by the second driving device.Wherein,
First horn, 21 and second horn 31 can be unfolded or be folded simultaneously simultaneously by control ground, so as to which unmanned plane 100 be made to be in work
Make state or off working state.
Wherein, the axial direction of the drive shaft of the first driving means is identical with the axial direction of the first axis hole of docking section 121, and second
The axial direction of the drive shaft of driving device is identical with the axial direction of the second axis hole, so as to meet the first horn component 22 and the second machine
The first horn 21 and the second horn 31 simultaneously is arranged side by side in the work of 33 Automatic-expanding of arm component or auto-folder.In this practicality
In novel, the driving device that the first horn 21 of driving and the second horn 31 are turned folding and be unfolded can be coordinated to be suitable for this reality
With novel first driving means and the second driving device, do not limit specifically herein.
The unmanned plane 100 further includes the rotation of the free end for being respectively arranged at the first horn 21 and the free end of the second horn 31
42 component 4 of the wing.42 component 4 of rotor includes actuator 41 and is connected to the rotor 42 of actuator 41, is driven by actuator 41
The rotation of rotor 42, so as to fulfill the flight function of unmanned plane 100.In the present embodiment, actuator 41 can be driving motor,
The end of first horn 21 and the second horn 31 is equipped with the driving motor.
Further, the rotor 42 of the utility model is folding paddle, wherein, the foldable setting of blade in rotor 42.
The first horn 21 and the second horn 31 are arranged such that when folding, the blade of the rotor 42, which can also fold, to be packed up, so as to
The blade can be protected, while realizes the space-minimized of unmanned plane 100.
Wherein, the bottom of the first horn 21 is equipped with the first foot stool 23 to land for unmanned plane 100, the bottom of the second horn 31
Portion can also be equipped with the second foot stool 33 to land for unmanned plane 100.First foot stool 23 is located at the driving on the first horn 21
The lower section of part 41, the second foot stool 33 are located at the lower section of the actuator 41 on the second horn 31.In the present embodiment, due to the first horn
21 fit in lug boss 12, thus the first foot stool 23 on first horn 21 could be provided as relative to the first horn 21 rotate with
It folds, consequently facilitating the folding of the first horn 21.Second horn 31 is located on the outside of the first horn 21, therefore the second horn 31
Second foot stool 33 can be folded with or be set close to the side of fuselage main body 11 according to demand.
The utility model devises a kind of horn folding unmanned plane, and the folded form of the unmanned plane is simple and reliable, folding
After folded horn, unmanned function realization is space-minimized, and the protectiveness of horn is enhanced, can be to avoid in storage and transportational process
Middle horn is damaged.
Those skilled in the art will readily occur to this practicality after considering specification and putting into practice utility model disclosed herein
Novel other embodiments.This application is intended to cover any variations, uses, or adaptations of the utility model, these
Variations, uses, or adaptations follow the general principle of the utility model and including undocumented skills of the utility model
Common knowledge or conventional techniques in art field.Description and embodiments are considered only as illustratively, the utility model
True scope and spirit are pointed out by claims hereof.
It should be understood that the accurate knot that the utility model is not limited to be described above and be shown in the drawings
Structure, and various modifications and changes may be made without departing from the scope thereof.The scope of the utility model only will by appended right
It asks to limit.
Claims (11)
1. a kind of unmanned plane, which is characterized in that including：Fuselage, the first horn component, the Yi Jishe for being set to the fore-body
In the second horn component of the fuselage afterbody, the first horn component includes the first horn, the second horn component packet
The second horn is included, first horn and second horn are rotationally connected with the fuselage respectively, so that first horn
Component and the second horn component are in unfolded state or folded state；Wherein, in the first horn component and described
When second horn component is in folded state, first horn and second horn are arranged side by side in the horizontal direction.
2. unmanned plane according to claim 1, which is characterized in that the first rotating shaft of the first horn component and described the
Second shaft of two horn components in the same plane, wherein, where center line where the first rotating shaft and the second shaft
Center line intersect.
3. unmanned plane according to claim 1, which is characterized in that the fuselage includes fuselage main body and from the machine
The lug boss protruded out below body main body；Wherein, the first horn component is rotationally connected with the lug boss, second machine
Arm component is rotationally connected with the fuselage main body.
4. unmanned plane according to claim 3, which is characterized in that the first horn component and the second horn component
It it is two, two the first horn components are set on the both sides of the lug boss, and two the second horn components are set on institute
It states in fuselage main body；
Wherein, when the first horn component and the second horn component are in folded state, two first horns
The both sides of the lug boss are fitted in, two second horns are located at the outside of first horn of homonymy.
5. unmanned plane according to claim 4, which is characterized in that the fuselage, which further includes, to be set on the lug boss
Docking section, the first horn component further include the first rotating shaft that first horn is connected to the docking section, wherein, institute
The first horn is stated to move as shaft rotation using the first rotating shaft.
6. unmanned plane according to claim 5, which is characterized in that the docking section is equipped with to be coordinated with the first rotating shaft
First axis hole of connection, wherein, the angle α of the axial direction of first axis hole and the central shaft of the fuselage is 56 °.
7. unmanned plane according to claim 4, which is characterized in that the first horn component, which further includes, is set to the machine
The stopper section of body, the stopper section are located on the rotation path of first horn；
Wherein, when first horn is unfolded state, first horn is connected to the stopper section；When first machine
When arm is folded state, first horn fits in the fuselage main body.
8. unmanned plane according to claim 4, which is characterized in that the fuselage, which further includes, is set to the fuselage main body
Rotary shaft rack, the second horn component further include the second shaft that second horn is connected to the rotary shaft rack,
In, second horn is connected to the medial surface of the rotary shaft rack and using second shaft as axis by second shaft
Rotation.
9. unmanned plane according to claim 8, which is characterized in that the rotary shaft rack is equipped with matches with second shaft
The second axis hole closed, wherein, the angle β of the axial direction of second axis hole and the central shaft of the fuselage is 118 °.
10. unmanned plane according to claim 8, which is characterized in that the second horn component is further included set on described
Limited block on two horns, the rotary shaft rack are equipped with limiting slot；
Wherein, when second horn is unfolded state, the limited block is matched in the limiting slot with limiting；When described
When second horn is folded state, second horn is set adjacent to first horn of homonymy.
11. unmanned plane according to claim 3, which is characterized in that the first horn component further include be set to it is described
First driving means on lug boss, the first driving means are connected to first horn and driving first horn turns
It is dynamic, so that first horn is in unfolded state or folded state；And/or
The second horn component further includes the second driving device being set in the fuselage main body, second driving device
Second horn and driving the second horn rotation are connected to, so that second horn is in unfolded state or folding
State.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721434546.3U CN207466965U (en) | 2017-10-31 | 2017-10-31 | Unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721434546.3U CN207466965U (en) | 2017-10-31 | 2017-10-31 | Unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207466965U true CN207466965U (en) | 2018-06-08 |
Family
ID=62265997
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721434546.3U Expired - Fee Related CN207466965U (en) | 2017-10-31 | 2017-10-31 | Unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207466965U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111212782A (en) * | 2018-06-26 | 2020-05-29 | 深圳市大疆创新科技有限公司 | Unmanned plane |
-
2017
- 2017-10-31 CN CN201721434546.3U patent/CN207466965U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111212782A (en) * | 2018-06-26 | 2020-05-29 | 深圳市大疆创新科技有限公司 | Unmanned plane |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN108513556A (en) | Unmanned plane | |
| CN107614374B (en) | Rack, unmanned vehicle and its application method of unmanned vehicle | |
| CN205854469U (en) | Unmanned helicopter | |
| CN106394885B (en) | The portable folding method of quadrotor unmanned plane | |
| CN207403934U (en) | Multi-rotor unmanned aerial vehicle | |
| CN106184729A (en) | A kind of many rotor wing unmanned aerial vehicles | |
| CN104986324B (en) | A kind of rotary locking mechanism and the plant protection unmanned plane with which | |
| CN109018349A (en) | A kind of multi-rotor unmanned aerial vehicle system suitable for stablizing dispensing under the conditions of high-speed flight | |
| CN105620719B (en) | A kind of municipal gardens folding wings unmanned plane | |
| US20180208291A1 (en) | Unmanned aerial vehicle with linkage foldable arms | |
| CN109896004A (en) | A kind of unmanned plane of scalable horn | |
| CN105460211B (en) | A kind of flight instruments | |
| CN207450247U (en) | A kind of foldable rotatable spherical unmanned plane | |
| CN207466965U (en) | Unmanned plane | |
| CN106005413A (en) | Diverse foldable unmanned aerial vehicle | |
| CN110155316A (en) | A kind of coaxial twin screw vertically taking off and landing flyer of Moving mass control and its control method | |
| CN206734619U (en) | It is a kind of that there is the unmanned plane for folding protective cover | |
| CN206358357U (en) | Multi-rotor aerocraft | |
| CN106828878A (en) | Examine and beat one unmanned plane | |
| CN109000521A (en) | Rudder wingfold device, micro missile and rudder wingfold method | |
| CN206407103U (en) | Folding multi-rotor unmanned aerial vehicle | |
| CN107856856A (en) | A kind of Flyable spherical robot | |
| CN204078065U (en) | A kind of unmanned airplane empennage foldable structure | |
| CN108463394A (en) | The controlling equipment of aerodynamics trap | |
| CN109305322A (en) | A kind of foldable more large-scale unmanned planes of rotor heavy duty of cage type |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180608 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |