CN106184706A - A kind of H type structure can double-deformation unmanned plane - Google Patents
A kind of H type structure can double-deformation unmanned plane Download PDFInfo
- Publication number
- CN106184706A CN106184706A CN201610713838.4A CN201610713838A CN106184706A CN 106184706 A CN106184706 A CN 106184706A CN 201610713838 A CN201610713838 A CN 201610713838A CN 106184706 A CN106184706 A CN 106184706A
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- horn
- deformation
- double
- type structure
- 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.)
- Pending
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/30—Parts of fuselage relatively movable to reduce overall dimensions of aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
- B64C27/10—Helicopters with two or more rotors arranged coaxially
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Remote Sensing (AREA)
- Toys (AREA)
Abstract
The invention discloses a kind of H type structure can double-deformation unmanned plane, including body and be arranged on body both sides and the horn being parallel to each other, it is provided with lifting structure in the middle part of described body, described lifting structure is connected with the oblique T-shaped part being fixed in the middle part of horn by lateral stressed pipe, and described horn two ends are equipped with rotor assemblies.The present invention, by body added lifting structure, makes the horn of unmanned plane be capable of lifting, it is possible to preferably to adjust the center of unmanned plane, make unmanned plane can adapt to the high altitude environment of Various Complex, improve the stability of unmanned plane；Make at the unmanned plane performing shooting operation, it is possible to avoid the interference of horn, promote the shooting effect of unmanned plane；Realize the folding of unmanned plane body and horn, during transport unmanned plane, the horn of unmanned plane can be folded with body, reduce the volume of unmanned plane, directly the unmanned plane that assembly and adjustment is good is directly used during convenient use, improve the practicality of unmanned plane.
Description
Technical field
The present invention relates to unmanned air vehicle technique field, specifically refer to a kind of H type structure can double-deformation unmanned plane frame.
Background technology
UAV is called for short " unmanned plane ", and english abbreviation is " UAV ", utilizes radio robot and provides for oneself
The most manned aircraft that presetting apparatus is handled.Can be divided into from technical standpoint definition: unmanned fixed-wing aircraft, unmanned VTOL
Machine, unmanned airship, depopulated helicopter, unmanned multi-rotor aerocraft, unmanned parasol etc..It is complete that unmanned plane can carry multiple load
Become various complex task, specifically have extensive use in multiple fields such as photography, pesticide spraying, fire protection and rescue, communication, drug law enforcement.
Existing unmanned plane structure is the most single, and horn and body are fixed structure, and unmanned plane is in flight course, very
Being easily subject to the impact of external environment condition and lose stability, some unmanned planes performing shooting task need to install photographic head, by
In keeping relatively stable flight, it is easy to photograph horn, strong influence shooting effect, substantially prolongs unmanned
The activity duration of machine, add the task cost of unmanned plane.Simultaneously as body and horn is fixing, cause the body of unmanned plane
Long-pending the hugest, the most in use, need large-scale means of transport to transport, or unmanned plane is broken, using
Time, the part of unmanned plane is transported to appointed place, then assembles, after finishing assembly, in addition it is also necessary to debug, ability
Normally using, be inconvenient for, this constrains the use of unmanned plane greatly, have impact on the development of unmanned plane.
Summary of the invention
It is an object of the invention to provide a kind of stability high, horn does not affect shooting effect, and the H type knot of convenient transport
Structure can double-deformation unmanned plane frame.
The present invention is achieved through the following technical solutions: a kind of H type structure can double-deformation unmanned plane, it is characterised in that:
Including body and be arranged on body both sides and the horn being parallel to each other, in the middle part of described body, it is provided with lifting structure, described lifting
Structure is connected with the oblique T-shaped part being fixed in the middle part of horn by lateral stressed pipe, and described horn two ends are equipped with rotor assemblies.
The operation principle of the technical program is, man-machine in flight course, can make machine by the lifting structure in the middle part of body
Arm rises or falls under the effect of lateral stressed pipe 7, and rising or falling of unmanned plane horn can preferably adjust unmanned plane
Center, make unmanned plane can adapt to the high altitude environment of Various Complex, improve the stability of unmanned plane；Meanwhile, horn is upper
Rise and decline, it is possible to making the unmanned plane of execution shooting operation, it is to avoid the interference of horn, affect shooting effect.
When carrying out the carrying of unmanned plane, horn is positioned at body both sides, and horn is fixed oblique T-shaped part, by rotating
Lateral stressed pipe connect body and oblique T-shaped part, therefore horn and body relative movement can form interior foldable structure, it is achieved nothing
The folding of man-machine body and the folder function of horn, unmanned plane body and horn, during transport unmanned plane, can be by unmanned
The horn of machine folds with body, reduces the volume of unmanned plane, convenient when using directly by unmanned plane that assembly and adjustment is good
Directly use, it is not necessary to assembled in situ and debugging, improve the use condition of unmanned plane greatly, improve the practicality of unmanned plane
Property.
In order to the present invention is better achieved, further, described lifting structure includes fixed plate, sets in the middle part of described fixed plate
Have a driving motor, and with the leading screw driving motor to be connected, described leading screw both sides further respectively have be fixed on by rotating shaft fixing
Connector on plate, described connector one end is connected with lateral stressed pipe；The most threaded lifter plate it is provided with in the middle part of leading screw,
Described lifter plate two ends are equipped with the draw bar being connected with connector free end.
In order to the present invention is better achieved, further, described driving motor is provided with driving angular wheel, and leading screw top sets
Having driven angular wheel, described driving angular wheel axis is vertical with driven angular wheel axis, and drive angular wheel with from
Dynamic angular wheel engagement.
In order to the present invention is better achieved, further, described leading screw is solid by upper and lower two pieces of force bearing plates being parallel to each other
Being scheduled in fixed plate, be equipped with rolling bearing in the middle part of described force bearing plate, described leading screw string is inserted in the rolling bearing in the middle part of force bearing plate,
And leading screw lower end fixes in the rolling bearing of lower section force bearing plate.
In order to the present invention is better achieved, further, one end of described connector is extended outside fixed plate, and be provided with
The pipe clamp that lateral stressed pipe matches, described lateral stressed pipe and connector clamping.
In order to the present invention is better achieved, further, described rotor assemblies includes the motor peace being arranged on horn two ends
Dress seat, described motor mount is provided with brushless electric machine, and described horn two ends are also equipped with the spiral driven by brushless electric machine
Oar.
In order to the present invention is better achieved, further, it is additionally provided with undercarriage below described horn.
In order to the present invention is better achieved, further, stable pull bar it is also associated with between described body and horn.
In order to the present invention is better achieved, further, described body upper is additionally provided with GPS mounting bracket.
The present invention compared with prior art, has the following advantages and beneficial effect:
(1) present invention is by body added lifting structure, makes the horn of unmanned plane be capable of lifting, it is possible to preferably to adjust
The center of unmanned plane, makes unmanned plane can adapt to the high altitude environment of Various Complex, improves the stability of unmanned plane；
(2) present invention is by realizing the lifting of unmanned plane horn, makes at the unmanned plane performing shooting operation, it is possible to avoid horn
Interference, promotes the shooting effect of unmanned plane；
(3) annexation of present invention body with horn by optimizing unmanned plane, it is achieved unmanned plane body and the folding of horn,
During transport unmanned plane, the horn of unmanned plane can be folded with body, reduce the volume of unmanned plane, convenient use
Time directly the unmanned plane that assembly and adjustment is good is directly used, it is not necessary to assembled in situ and debugging, improve making of unmanned plane greatly
By condition, improve the practicality of unmanned plane；
(4) present configuration is simple, and easy to use, manufacturing cost is relatively low, greatly facilitates the use of unmanned plane, the most extensively
Popularization and application.
Accompanying drawing explanation
By the detailed description non-limiting example made with reference to the following drawings of reading, other features of the present invention,
Purpose and advantage will be changed to substantially:
Fig. 1 is the structural representation of the present invention；
Fig. 2 is the lifting structure schematic diagram of the present invention；
Fig. 3 is lifting structure and the horn attachment structure schematic diagram of the present invention；
Fig. 4 is left view during horn of the present invention rising；
Front view when Fig. 5 is that in the present invention, horn rises；
Left view when Fig. 6 is that in the present invention, horn declines；
Front view when Fig. 7 is that in the present invention, horn declines；
Top view when Fig. 8 is that in the present invention, horn folds；
Front view when Fig. 9 is that in the present invention, horn folds.
Wherein: 1 motor mount, 2 brushless electric machines, 3 horns, 4 undercarriages, 5 stablize pull bar, and 6 is the most T-shaped
Part, 7 lateral stressed pipes, 8 propellers, 9 lifting structures, 91 fixed plates, 92 connectors, 93 drive conical tooth
Wheel, 94 leading screws, 95 lifter plates, 96 driven angular wheels, 97 draw bars, 98 force bearing plates, 99 rotating shafts, 10
GPS mounting bracket, 11 bodies.
Detailed description of the invention
Embodiments of the invention are described below in detail, and the example of described embodiment is shown in the drawings, the most from start to finish
Same or similar label represents same or similar element or has the element of same or like function.Below with reference to attached
The embodiment that figure describes is exemplary, is only used for explaining the present invention, and is not considered as limiting the invention.
In describing the invention, it is to be understood that term " " center ", " longitudinally ", " laterally ", " on ", D score,
Orientation or the position relationship of the instruction such as "front", "rear", "left", "right", " vertically ", " level ", " top ", " end ", " interior ", " outward " are
Based on orientation shown in the drawings or position relationship, it is for only for ease of the description present invention and simplifies description rather than instruction or dark
The device or the element that show indication must have specific orientation, with specific azimuth configuration and operation, therefore it is not intended that right
The restriction of the present invention.
In describing the invention, it should be noted that unless otherwise clearly defined and limited, term " is installed ", " phase
Even ", " connection " should be interpreted broadly, for example, it may be fixing connection, it is also possible to be to removably connect, or be integrally connected；Can
To be mechanical connection, it is also possible to be electrical connection；Can also be to be joined directly together, it is also possible to be to be indirectly connected to by intermediary, can
To be the connection of two element internals.For the ordinary skill in the art, above-mentioned term can be understood with concrete condition
Concrete meaning in the present invention.
Embodiment 1:
The primary structure of the present embodiment, as it is shown in figure 1, include body 11 and be arranged on body 11 both sides and the machine being parallel to each other
Arm 3, is provided with lifting structure 9 in the middle part of described body 11, described lifting structure 9 passes through lateral stressed pipe 7 and is fixed in the middle part of horn 3
Oblique T-shaped part 6 connect, described horn 3 two ends are equipped with rotor assemblies.
Detailed description of the invention is, unmanned plane, in flight course, can make horn 3 by the lifting structure 9 in the middle part of body 11
Rise or fall under the effect of lateral stressed pipe 7, such as Fig. 4, shown in Fig. 5, Fig. 6, Fig. 7, rising or falling of unmanned plane horn 3
Can preferably adjust the center of unmanned plane, make unmanned plane can adapt to the high altitude environment of Various Complex, improve unmanned plane
Stability；Meanwhile, the raising and lowering of horn 3, it is possible to make the unmanned plane of execution shooting operation, it is to avoid the interference of horn 3, impact
Shooting effect.
When carrying out the carrying of unmanned plane, horn 3 is positioned at body 11 both sides, and horn 3 is fixed oblique T-shaped part 6, by can
The lateral stressed pipe 7 rotated connects body 11 and oblique T-shaped part 6, and therefore horn 3 and body 11 relative movement can form interior folding
Structure, it is achieved the body 11 of unmanned plane and the folder function of horn 3, such as Fig. 8, shown in Fig. 9, unmanned plane body 11 and horn 3
Fold, during transport unmanned plane, the horn 3 of unmanned plane can be folded with body 11, reduce the volume of unmanned plane,
Directly the unmanned plane that assembly and adjustment is good is directly used during convenient use, it is not necessary to assembled in situ and debugging, improve nothing greatly
Man-machine use condition, improves the practicality of unmanned plane.
Embodiment 2:
The present embodiment, on the basis of above-described embodiment, further defines the concrete structure of lifting structure 9, as in figure 2 it is shown,
Described lifting structure 9 includes fixed plate 91, is provided with driving motor, and the silk being connected with driving motor in the middle part of described fixed plate 91
Thick stick 94, described leading screw 94 both sides further respectively have the connector 92 being fixed in fixed plate 91 by rotating shaft 99, described connector
92 one end are connected with lateral stressed pipe 7；The most threaded lifter plate 95, described lifter plate 95 two ends it are provided with in the middle part of leading screw 94
It is equipped with the draw bar 97 being connected with connector 92 free end.
The horn of unmanned plane is when lifting, and by driving motor to drive leading screw 94 to rotate, leading screw 94 provides for lifter plate 95 and turns
Power, owing to leading screw 94 is fixed in fixed plate 91, therefore the lifter plate 95 in the middle part of leading screw 94 moves up and down on leading screw 94.By
Being connected by the free end of draw bar more than 97 connector 92 in lifter plate 95, therefore the free end of connector 92 is with in connector 92
The rotating shaft 99 in portion rotates for axle, and the lateral stressed pipe 7 being connected with connector 92 other end then drives horn 3 to realize rising
Process with declining, realizes the raising and lowering of unmanned plane horn 3 therefrom.Other parts of the present embodiment and above-described embodiment
Identical, repeat no more.
Embodiment 3:
The present embodiment, on the basis of above-described embodiment, further defines the annexation driving motor with leading screw 94, as
Shown in Fig. 2, described driving motor is provided with driving angular wheel 93, and leading screw 94 top is provided with driven angular wheel 96, described driving
Angular wheel 93 axis is vertical with driven angular wheel 96 axis, and drives angular wheel 93 to engage with driven angular wheel 96.
Drive motor to drive leading screw 94 to rotate by the way of driving angular wheel 93 to engage with driven angular wheel 96, and drive taper
Gear 93 axis is vertical with driven angular wheel 96 axis, so makes the installation site driving motor and leading screw 94 the cleverest
Live, preferably realize the lifting of unmanned plane horn 3.Other parts of the present embodiment are same as the previously described embodiments, repeat no more.
Embodiment 4:
The present embodiment, on the basis of above-described embodiment, further defines the connected mode of leading screw 94 and fixed plate 91, as
Shown in Fig. 2, described leading screw 94 is fixed in fixed plate 91 by upper and lower two pieces of force bearing plates being parallel to each other 98, described force bearing plate 98
Middle part is equipped with rolling bearing, and described leading screw 94 string is inserted in the rolling bearing in the middle part of force bearing plate 98, and leading screw 94 lower end is in lower section
The rolling bearing of force bearing plate 98 is fixed.Thus, the flexible rotating of leading screw 94 can be realized, and the position of leading screw 94 will not become
Change, facilitate the reciprocal lifting of lifter plate 95, also lifter plate 95 has been played certain restriction effect simultaneously.Other of the present embodiment
Part is same as the previously described embodiments, repeats no more.
Embodiment 5:
The present embodiment, on the basis of above-described embodiment, further defines the annexation of lifting structure 9 and horn 3, as
Shown in Fig. 3, one end of described connector 92 is extended outside fixed plate 91, and is provided with the pipe clamp matched with lateral stressed pipe 7, institute
State lateral stressed pipe 7 and connector 92 clamping.Other parts of the present embodiment are same as the previously described embodiments, repeat no more.
Embodiment 6:
The present embodiment, on the basis of above-described embodiment, further defines the concrete structure of rotor assemblies, as it is shown in figure 1,
Described rotor assemblies includes the motor mount 1 being arranged on horn 3 two ends, and described motor mount 1 is provided with brushless electric machine
2, described horn 3 two ends are also equipped with the propeller 8 driven by brushless electric machine 2.Other parts of the present embodiment and above-mentioned enforcement
Example is identical, repeats no more.
Embodiment 7:
The present embodiment, on the basis of above-described embodiment, also sets up undercarriage 4 further below described horn 3.Described
The frame 4 that falls mainly is made up of two vertical tubes and a transverse tube, and transverse tube is fixed by tee T and two vertical tubes, the freedom of two vertical tubes
Holding and be connected by the retainer ring on horn 3 is fixing with horn 3, it act as after unmanned plane lands providing for unmanned plane supporting.
Other parts of the present embodiment are same as the previously described embodiments, repeat no more.
Embodiment 8:
The present embodiment, on the basis of above-described embodiment, has additional between described body 11 and horn 3 further and stably draws
Bar 5.Described pull bar 5 one end of stablizing is rotationally connected with the stabilizing ring being fixed on horn by Universal connector, and the other end is solid with body
Fixed connection, it is ensured that in horn 3 lifting process, the stability of body 11.Other parts of the present embodiment and above-described embodiment phase
With, repeat no more.
Embodiment 9:
The present embodiment, on the basis of above-described embodiment, sets up GPS mounting bracket 10 on described body 11 top further.Increase
If GPS mounting bracket 10 is convenient, GPS device is arranged on the body 11 of unmanned plane, increases positioning function for unmanned plane.This reality
Other parts executing example are same as the previously described embodiments, repeat no more.
It is understood that according to an embodiment of the invention H type structure can double-deformation unmanned plane rack construction,
Operation principle and the work process of the such as parts such as brushless electric machine 2 and undercarriage 4 are all prior aries, and are the technology of this area
Known to personnel, the most no longer it is described in detail.
Although an embodiment of the present invention has been shown and described, it will be understood by those skilled in the art that: not
Depart from and these embodiments can be carried out multiple change under the principle of the present invention and objective, revise, replace and modification, the present invention's
Scope is limited by claim and equivalent thereof.
Claims (9)
1. a H type structure can double-deformation unmanned plane, it is characterised in that: include body (11) and be arranged on body (11)
Both sides and the horn (3) being parallel to each other, described body (11) middle part is provided with lifting structure (9), and described lifting structure (9) is by horizontal stroke
Being connected with the oblique T-shaped part (6) being fixed on horn (3) middle part to stressed tube (7), described horn (3) two ends are equipped with rotor assemblies.
A kind of H type structure the most according to claim 1 can double-deformation unmanned plane, it is characterised in that: described lifting knot
Structure (9) includes that fixed plate (91), described fixed plate (91) middle part are provided with driving motor, and the leading screw being connected with driving motor
(94), described leading screw (94) both sides further respectively have the connector (92) being fixed in fixed plate (91) by rotating shaft (99), institute
State connector (92) one end to be connected with lateral stressed pipe (7)；Leading screw (94) middle part is provided with the most threaded lifter plate (95),
Described lifter plate (95) two ends are equipped with the draw bar (97) being connected with connector (92) free end.
A kind of H type structure the most according to claim 2 can double-deformation unmanned plane, it is characterised in that: described drive electricity
Machine is provided with driving angular wheel (93), and leading screw (94) top is provided with driven angular wheel (96), described driving angular wheel (93)
Axis is vertical with driven angular wheel (96) axis, and drives angular wheel (93) to engage with driven angular wheel (96).
A kind of H type structure the most according to claim 3 can double-deformation unmanned plane, it is characterised in that: described leading screw
(94) being fixed in fixed plate (91) by upper and lower two pieces of force bearing plates being parallel to each other (98), described force bearing plate (98) middle part is all provided with
There are rolling bearing, described leading screw (94) string to insert in the rolling bearing at force bearing plate (98) middle part, and leading screw (94) lower end is held in lower section
The rolling bearing of power plate (98) is fixed.
5. according to a kind of H type structure described in any one of claim 2 ~ 4 can double-deformation unmanned plane, it is characterised in that: institute
Fixed plate (91) is extended outward in the one end stating connector (92), and is provided with the pipe clamp matched with lateral stressed pipe (7), described horizontal stroke
To stressed tube (7) and connector (92) clamping.
6. according to a kind of H type structure described in any one of claim 1 ~ 4 can double-deformation unmanned plane, it is characterised in that: institute
State rotor assemblies and include being arranged on the motor mount (1) at horn (3) two ends, described motor mount (1) is provided with brushless
Motor (2), described horn (3) two ends are also equipped with the propeller (8) driven by brushless electric machine (2).
7. according to a kind of H type structure described in any one of claim 1 ~ 4 can double-deformation unmanned plane, it is characterised in that: institute
State horn (3) lower section and be additionally provided with undercarriage (4).
8. according to a kind of H type structure described in any one of claim 1 ~ 4 can double-deformation unmanned plane, it is characterised in that: institute
State and between body (11) and horn (3), be also associated with stable pull bar (5).
9. according to a kind of H type structure described in any one of claim 1 ~ 4 can double-deformation unmanned plane, it is characterised in that: institute
State body (11) top and be additionally provided with GPS mounting bracket (10).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610713838.4A CN106184706A (en) | 2016-08-24 | 2016-08-24 | A kind of H type structure can double-deformation unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610713838.4A CN106184706A (en) | 2016-08-24 | 2016-08-24 | A kind of H type structure can double-deformation unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106184706A true CN106184706A (en) | 2016-12-07 |
Family
ID=57524883
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610713838.4A Pending CN106184706A (en) | 2016-08-24 | 2016-08-24 | A kind of H type structure can double-deformation unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106184706A (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106697276A (en) * | 2017-01-23 | 2017-05-24 | 南京大学 | Double-sided flightable multi-rotor aircraft and operation method thereof |
| CN106945817A (en) * | 2017-05-02 | 2017-07-14 | 珠海市双捷科技有限公司 | Multi-rotor unmanned aerial vehicle |
| CN108190029A (en) * | 2018-02-09 | 2018-06-22 | 广东莱盛隆电子股份有限公司 | A kind of fog machine |
| CN109018328A (en) * | 2018-08-03 | 2018-12-18 | 广东电网有限责任公司 | One kind four axis, eight rotor wing unmanned aerial vehicle and flight instruments |
| CN110844058A (en) * | 2020-01-06 | 2020-02-28 | 天津微深科技有限公司 | Modular morphing aircraft |
| RU204990U1 (en) * | 2021-03-26 | 2021-06-22 | Федеральное государственное бюджетное образовательное учреждение высшего образования "Казанский национальный исследовательский технический университет им. А.Н. Туполева - КАИ" | Drone transformer |
| DE102020200746A1 (en) | 2020-01-22 | 2021-07-22 | Volkswagen Aktiengesellschaft | Multicopter and method for operating a multicopter |
| WO2024077523A1 (en) * | 2022-10-12 | 2024-04-18 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101992854A (en) * | 2010-11-03 | 2011-03-30 | 中国科学院长春光学精密机械与物理研究所 | Foldable six-axis multi-rotor aircraft |
| CN202319771U (en) * | 2011-11-07 | 2012-07-11 | 上海工程技术大学 | Air-land dual-purpose aircraft |
| CN103921933A (en) * | 2013-01-10 | 2014-07-16 | 深圳市大疆创新科技有限公司 | Deformation structure of air vehicle and micro air vehicle |
| CN204341415U (en) * | 2014-12-04 | 2015-05-20 | 北方天途航空技术发展（北京）有限公司 | Quick demounting many rotor wing unmanned aerial vehicles horn joint sleeve assembly |
| CN105539821A (en) * | 2015-12-11 | 2016-05-04 | 广州鼎飞航空科技有限公司 | Deformable folding structure of multi-rotor type aircraft |
| CN205469807U (en) * | 2016-03-11 | 2016-08-17 | 尖蜂航空科技有限公司 | Six spool collapsible plant protection machines |
| CN205454605U (en) * | 2016-03-29 | 2016-08-17 | 佛山市顺德区顺茵绿化设计工程有限公司 | Maintenance of equipment is construct on golf course lawn |
| CN205469772U (en) * | 2016-04-06 | 2016-08-17 | 成都普蓝特科技有限公司 | It is preceding to little volume unmanned aerial vehicle of folded form |
| CN205906203U (en) * | 2016-08-24 | 2017-01-25 | 四川建筑职业技术学院 | H type structure can two -way deformation unmanned aerial vehicle |
-
2016
- 2016-08-24 CN CN201610713838.4A patent/CN106184706A/en active Pending
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101992854A (en) * | 2010-11-03 | 2011-03-30 | 中国科学院长春光学精密机械与物理研究所 | Foldable six-axis multi-rotor aircraft |
| CN202319771U (en) * | 2011-11-07 | 2012-07-11 | 上海工程技术大学 | Air-land dual-purpose aircraft |
| CN103921933A (en) * | 2013-01-10 | 2014-07-16 | 深圳市大疆创新科技有限公司 | Deformation structure of air vehicle and micro air vehicle |
| CN204341415U (en) * | 2014-12-04 | 2015-05-20 | 北方天途航空技术发展（北京）有限公司 | Quick demounting many rotor wing unmanned aerial vehicles horn joint sleeve assembly |
| CN105539821A (en) * | 2015-12-11 | 2016-05-04 | 广州鼎飞航空科技有限公司 | Deformable folding structure of multi-rotor type aircraft |
| CN205469807U (en) * | 2016-03-11 | 2016-08-17 | 尖蜂航空科技有限公司 | Six spool collapsible plant protection machines |
| CN205454605U (en) * | 2016-03-29 | 2016-08-17 | 佛山市顺德区顺茵绿化设计工程有限公司 | Maintenance of equipment is construct on golf course lawn |
| CN205469772U (en) * | 2016-04-06 | 2016-08-17 | 成都普蓝特科技有限公司 | It is preceding to little volume unmanned aerial vehicle of folded form |
| CN205906203U (en) * | 2016-08-24 | 2017-01-25 | 四川建筑职业技术学院 | H type structure can two -way deformation unmanned aerial vehicle |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106697276A (en) * | 2017-01-23 | 2017-05-24 | 南京大学 | Double-sided flightable multi-rotor aircraft and operation method thereof |
| CN106945817A (en) * | 2017-05-02 | 2017-07-14 | 珠海市双捷科技有限公司 | Multi-rotor unmanned aerial vehicle |
| CN106945817B (en) * | 2017-05-02 | 2023-10-20 | 珠海市双捷科技有限公司 | Multi-rotor unmanned aerial vehicle |
| CN108190029A (en) * | 2018-02-09 | 2018-06-22 | 广东莱盛隆电子股份有限公司 | A kind of fog machine |
| CN109018328A (en) * | 2018-08-03 | 2018-12-18 | 广东电网有限责任公司 | One kind four axis, eight rotor wing unmanned aerial vehicle and flight instruments |
| CN110844058A (en) * | 2020-01-06 | 2020-02-28 | 天津微深科技有限公司 | Modular morphing aircraft |
| DE102020200746A1 (en) | 2020-01-22 | 2021-07-22 | Volkswagen Aktiengesellschaft | Multicopter and method for operating a multicopter |
| DE102020200746B4 (en) | 2020-01-22 | 2022-03-31 | Volkswagen Aktiengesellschaft | Multicopter and method of operating a multicopter |
| RU204990U1 (en) * | 2021-03-26 | 2021-06-22 | Федеральное государственное бюджетное образовательное учреждение высшего образования "Казанский национальный исследовательский технический университет им. А.Н. Туполева - КАИ" | Drone transformer |
| WO2024077523A1 (en) * | 2022-10-12 | 2024-04-18 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN106184706A (en) | A kind of H type structure can double-deformation unmanned plane | |
| CN205906203U (en) | H type structure can two -way deformation unmanned aerial vehicle | |
| CN110053435B (en) | Foldable amphibious four-rotor aircraft | |
| CN207403934U (en) | Multi-rotor unmanned aerial vehicle | |
| US8342440B2 (en) | Miniature robotic vehicle with ground and flight capability | |
| CN104743110B (en) | A kind of collapsible air-drop unmanned plane | |
| CN106184729A (en) | A kind of many rotor wing unmanned aerial vehicles | |
| CN102556336A (en) | Wing fast unfolding device for folding-wing unmanned plane | |
| CN109533323B (en) | Miniature flapping wing aircraft with single-degree-of-freedom foldable wings | |
| CN104443380B (en) | A kind of eight word track flapping wing mechanism and micro flapping wing air vehicles | |
| CN207683779U (en) | Portable unmanned machine coaxial double-oar fold mechanism | |
| CN106887807A (en) | For the inspection robot of overhead transmission line | |
| CN206775621U (en) | A kind of lightweight oblique photograph head | |
| CN204548502U (en) | A kind of collapsible air-drop unmanned plane | |
| CN206012942U (en) | A kind of Multi-axis aircraft folded piece with auto-lock function | |
| CN106240800A (en) | A kind of unmanned plane folding wing | |
| CN209938948U (en) | Coaxial rotor unmanned aerial vehicle of folded cascade | |
| JP2020040566A (en) | Flight device | |
| CN109552614A (en) | Portable aircraft | |
| TWM524313U (en) | Unmanned aerial vehicle | |
| CN205076033U (en) | Electronic foot rest folding device | |
| CN106564583A (en) | Aerial-photography unmanned aerial vehicle convenient to store | |
| CN209427025U (en) | Posture is adjustable rotor mechanism | |
| CN207826537U (en) | A kind of dynamic rotor structure of new type foldable oil | |
| CN110550198A (en) | Rock wall fixed point type unmanned aerial vehicle |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20161207 |