CN108438216A - Unmanned plane skeleton and unmanned plane - Google Patents
Unmanned plane skeleton and unmanned plane Download PDFInfo
- Publication number
- CN108438216A CN108438216A CN201810641204.1A CN201810641204A CN108438216A CN 108438216 A CN108438216 A CN 108438216A CN 201810641204 A CN201810641204 A CN 201810641204A CN 108438216 A CN108438216 A CN 108438216A
- Authority
- CN
- China
- Prior art keywords
- horn
- unmanned plane
- hole
- fuselage framework
- strip
- 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
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- 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
- B64C27/32—Rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
Abstract
The present invention provides a kind of unmanned plane skeleton and unmanned planes, are related to the technical field of unmanned plane, the unmanned plane skeleton, including：The quantity of fuselage framework and horn, the horn is multiple；The horn includes first end and second end, and the first end is for being fixedly mounted propeller mechanism, and the second end is flexibly connected with the peripheral side of the fuselage framework, so that distance of the second end apart from the fuselage framework is adjustable.By movable horn, the second end of horn can be made close to the fuselage framework, at this point, the first end and second end of horn is all close to fuselage framework, unmanned plane skeleton entirety occupied space reduces, and facilitates the storage and carrying of unmanned plane；When unmanned plane needs in use, movable horn, makes the second end of horn far from fuselage framework, horn expansion meets the needs of long wheelbase.
Description
Technical field
The present invention relates to the technical fields of unmanned plane, more particularly, to a kind of unmanned plane skeleton and unmanned plane.
Background technology
Unmanned plane refers to the not manned vehicle controlled using wireless remote control device and the control device of itself, such as
Unmanned helicopter, unmanned fixed-wing aircraft, unmanned parasol, multi-rotor unmanned aerial vehicle etc..In recent ten years, unmanned plane is extensive
Applied to photography of taking photo by plane, electric inspection process, environmental monitoring, forest fire protection, disaster inspection, anti-terrorism lifesaving, military surveillance, battle assessment
Equal fields can effectively overcome the shortcomings of that manned aircraft carries out aerial work, reduce purchase and maintenance cost, improve delivery
The safety of tool.
Multi-rotor unmanned aerial vehicle is in order to ensure lift and lifting capacity, it is necessary to select corresponding motor and corresponding package size
Propeller, heavy－duty require large scale propeller, it is ensured that propeller mutually mutually disjoints, and must keep certain wheelbase
Row.In the case of same wheelbase, the size of the number of axle more at most paddle just can only be smaller.Therefore it to meet big loading capacity, must just set
Meter very large-size axis parts away from more rotors, then the volume of gyroplane is also bigger.Either four axis, six axis or eight axis gyroplanes are received
Get up to be required for a huge rectangular cubic chest shipment, is not easy to case and transport to carry.
Invention content
The purpose of the present invention is to provide a kind of unmanned plane skeleton and unmanned planes, are deposited with alleviating unmanned plane in the prior art
Be inconvenient to store with carry the technical issues of.
In a first aspect, a kind of unmanned plane skeleton provided in an embodiment of the present invention, including：Fuselage framework and horn, the machine
The quantity of arm is multiple；The horn includes first end and second end, and the first end is for being fixedly mounted propeller mechanism, institute
It states second end to be flexibly connected with the peripheral side of the fuselage framework, so that distance of the second end apart from the fuselage framework
It is adjustable.
Further, the horn and the fuselage framework are hinged.
Further, the articulated shaft of the horn and the fuselage framework perpendicular to the fuselage framework upper and lower surface,
So that the horn can rotate in the face parallel with the fuselage framework.
Further, the fuselage framework includes upper plate and lower plate, and the upper plate is parallel with lower plate and interval is arranged, described
The second end of horn is hinged between the upper plate and lower plate；
Be correspondingly arranged on respectively on the upper plate and lower plate the first limit strip-shaped hole and second limit strip-shaped hole, described first
It is arc-shaped to limit strip-shaped hole and the second limit strip-shaped hole, is correspondingly arranged on the opposite sides face of the horn and described first
Limit corresponding first limit protrusion of strip-shaped hole, and the second limit protrusion corresponding with the second limit strip-shaped hole；It is described
First limit protrusion is located at described first and limits in strip-shaped hole, and can be along the first limit strip-shaped hole sliding；Described second
Limit protrusion is located at described second and limits in strip-shaped hole, and can be along the second limit strip-shaped hole sliding.
Further, positioning locking structure, the positioning lock are correspondingly arranged between the horn and the fuselage framework
Only after structure locking, for making the horn keep receiving state or unfolded state.
Further, first positioning hole and second location hole are provided on the upper plate, the first positioning hole is located at institute
The outside of first limit strip-shaped hole one end is stated, the second location hole is located at the outer of the other end that described first limits strip-shaped hole
Side；
Elastic positioning pin is provided on the horn, the elastic positioning pin includes plunger and key seat, and the key seat includes
Pin hole, the plunger are slidably connected in the pin hole, and are provided with compressed spring between the plunger and the key seat, described
The length of plunger is less than the depth of the pin hole, so that the plunger is telescopically disposed in the key seat；
The first positioning hole and second location hole are located on the motion path of the plunger, so that the elastic positioning pin
Turn to the first positioning hole either second location hole when the plunger stretched from the first positioning hole or second location hole
Go out.
Further, the outer end of the plunger is bulb shape；The first positioning hole and second location hole are loudspeaker
Shape structure, the flared structure include the first opening for being located at the upper plate backwards to the lower plate one side, and positioned at described
Upper plate is open along described first to second opening direction, the tubaeform knot towards the second opening of the lower plate one side
The internal diameter of structure gradually increases, and the flared structure internal face and the upper plate are towards rounding between the one side of the lower plate
Angle.
Further, the fuselage framework includes four circumferentially arranged lateral surfaces, and the quantity of the horn is four,
Four horns are located on four lateral surfaces.
Second aspect, a kind of unmanned plane provided in an embodiment of the present invention, including above-mentioned unmanned plane skeleton.
Further, the unmanned plane further includes propeller mechanism, flies control anticollision identification device and GPS receiver.
The embodiment of the present invention brings following advantageous effect：
Unmanned plane skeleton and unmanned plane provided in an embodiment of the present invention, unmanned plane skeleton include：Fuselage framework and horn, institute
The quantity for stating horn is multiple；The horn includes first end and second end, and the first end is for being fixedly mounted propeller machine
Structure, the second end are flexibly connected with the peripheral side of the fuselage framework, so that the second end is apart from the fuselage framework
Distance it is adjustable.By movable horn, the second end of horn can be made close to the fuselage framework, at this point, the first end of horn
With second end all close to fuselage framework, unmanned plane skeleton entirety occupied space reduces, and facilitates the storage and carrying of unmanned plane；When
Unmanned plane needs in use, movable horn, makes the second end of horn far from fuselage framework, and horn is unfolded to meet the need of long wheelbase
It asks.Unmanned plane skeleton provided in an embodiment of the present invention has folding structure system that is deployable and can storing, developed dimension
Bigger, storage are smaller, folding and unfolding mode and simple to operate.
Other features and advantages of the present invention will illustrate in the following description, also, partly become from specification
It obtains it is clear that understand through the implementation of the invention.The purpose of the present invention and other advantages are in specification, claims
And specifically noted structure is realized and is obtained in attached drawing.
To enable the above objects, features and advantages of the present invention to be clearer and more comprehensible, preferred embodiment cited below particularly, and coordinate
Appended attached drawing, is described in detail below.
Description of the drawings
It, below will be to specific in order to illustrate more clearly of the specific embodiment of the invention or technical solution in the prior art
Embodiment or attached drawing needed to be used in the description of the prior art are briefly described, it should be apparent that, in being described below
Attached drawing is some embodiments of the present invention, for those of ordinary skill in the art, before not making the creative labor
It puts, other drawings may also be obtained based on these drawings.
Fig. 1 is the side view that unmanned plane skeleton provided in an embodiment of the present invention is in unfolded state；
Fig. 2 is the vertical view that unmanned plane skeleton provided in an embodiment of the present invention is in unfolded state；
Fig. 3 is the vertical view that unmanned plane skeleton provided in an embodiment of the present invention is in receiving state；
Fig. 4 is the schematic diagram that unmanned plane skeleton provided in an embodiment of the present invention is in unfolded state；
Fig. 5 is the partial enlarged view of location A in Fig. 4；
Fig. 6 is the partial sectional view of B location in Fig. 1.
Icon：100- fuselage frameworks；110- upper plates；111- first limits strip-shaped hole；112- first positioning holes；Under 120-
Plate；200- horns；The first limit protrusions of 210-；220- plungers；300- articulated shafts；400- flared structures.
Specific implementation mode
Technical scheme of the present invention is clearly and completely described below in conjunction with attached drawing, it is clear that described implementation
Example is a part of the embodiment of the present invention, instead of all the embodiments.Based on the embodiments of the present invention, ordinary skill
The every other embodiment that personnel are obtained without making creative work, shall fall within the protection scope of the present invention.
In the description of the present invention, it should be noted that such as occur term "center", "upper", "lower", "left", "right",
The orientation or positional relationship of "vertical", "horizontal", "inner", "outside" etc., instruction is that orientation based on ... shown in the drawings or position are closed
System, is merely for convenience of description of the present invention and simplification of the description, not indicating or implying the indicated device or element must have
Specific orientation, with specific azimuth configuration and operation, therefore be not considered as limiting the invention.In addition, such as there is art
Language " first ", " second ", " third " are used for description purposes only, and are not understood to indicate or imply relative importance.
In addition, in the description of the embodiment of the present invention unless specifically defined or limited otherwise, term " connected " " connects
Connect " it shall be understood in a broad sense, for example, it may be being fixedly connected, it may be a detachable connection, or be integrally connected；It can be machine
Tool connects, and can also be electrical connection；It can be directly connected, can also can be indirectly connected through an intermediary two members
Connection inside part.For the ordinary skill in the art, it can understand above-mentioned term in the present invention with concrete condition
Concrete meaning.
As Figure 1-Figure 4, unmanned plane skeleton provided in an embodiment of the present invention, including：Fuselage framework 100 and horn 200,
The quantity of the horn 200 is multiple；The horn 200 includes first end and second end, and the first end is for being fixedly mounted
Propeller mechanism, the second end are flexibly connected with the peripheral side of the fuselage framework 100, so that the second end is apart from institute
The distance for stating fuselage framework 100 is adjustable.By movable horn 200, the second end of horn 200 can be made close to the fuselage framework
100, at this point, the first end and second end of horn 200 is all close to fuselage framework 100, unmanned plane skeleton entirety occupied space reduces
, facilitate the storage and carrying of unmanned plane；When unmanned plane needs in use, movable horn 200, keeps the second end of horn 200 remote
From fuselage framework 100, the expansion of horn 200 meets the needs of long wheelbase.Unmanned plane skeleton provided in an embodiment of the present invention, having can
Expansion and the folding structure system that can be stored, developed dimension bigger store smaller, folding and unfolding mode and side easy to operate
Just.
Unmanned plane skeleton provided in an embodiment of the present invention makes horn 200 and fuselage framework by way of movable horn 200
100 occur relative motion, to make horn 200 be unfolded or storage, the carrying for making unmanned plane be more prone to.
Specifically, horn 200 can be rotation connection with fuselage framework 100, by way of rotation, by horn 200
Outer end is rotated to the outside of fuselage framework 100, and horn 200 is made to be unfolded, the occupied space bigger of unmanned plane skeleton entirety, on the contrary
, it is rotated back, horn 200 is stored.
It is not limited to the mode of rotation, it can also be by the way of flexible, for example, between horn 200 and fuselage framework 100
It is correspondingly arranged on sliding equipment, horn 200 can be made to be retracted into fuselage framework 100, or is projected to outside fuselage framework 100,
It can equally reach and change unmanned plane skeleton entirety the space occupied.
The direction of rotation can be rotation along the horizontal plane, or rotation vertically.For example, horn 200
It can rotate in the horizontal direction, multiple horns 200 rotate general 90 degree of expansion along direction clockwise or counter-clockwise；Or
Person, horn 200 can also vertically plane direction rotation, horn 200 is arranged on the side of fuselage framework 100, horn 200
It can rotate, be accommodated in below fuselage framework 100 to the bottom surface direction of fuselage framework 100, or to the top of fuselage framework 100
Face direction rotates, and is accommodated in the top surface of fuselage framework 100, in use, can also reach storage to level in rotation 180 degree and subtract
The effect of few space hold.
Preferably, the articulated shaft 300 of the horn 200 and the fuselage framework 100 is perpendicular to the fuselage framework 100
Upper and lower surface, so that the horn 200 can rotate in the face parallel with the fuselage framework 100.Using turning in the horizontal plane
Dynamic mode, on the one hand, the angle of rotation is smaller, and maximum only needs to rotate general 90 degree, second aspect, horizontal rotation
Pivot design more vertically rotates simpler.
Fuselage framework 100 includes upper plate 110 and lower plate 120, and the upper plate 110 is parallel with lower plate 120 and interval is arranged, institute
The second end for stating horn 200 is hinged between the upper plate 110 and lower plate 120；It is right respectively on the upper plate 110 and lower plate 120
It should be provided with the first limit strip-shaped hole 111 and second limit strip-shaped hole, the first limit strip-shaped hole 111 and second limits bar shaped
Hole is arc-shaped, is correspondingly arranged on the opposite sides face of the horn 200 and the first limit strip-shaped hole 111 corresponding the
One limit protrusion 210, and the second limit protrusion corresponding with the second limit strip-shaped hole；First limit protrusion 210
In the first limit strip-shaped hole 111, and it can be slided along the first limit strip-shaped hole 111；Second limit convex
It rises and is located in the second limit strip-shaped hole, and can be along the second limit strip-shaped hole sliding.When horn 200 rotates
It waits, the first limit protrusion 210 and the second limit protrusion are slidably connected at the limit bar shaped of the first limit strip-shaped hole 111 and second respectively
In hole, the articulated shaft 300 between horn 200 and fuselage framework 100 plays a certain protective role, if being not provided with positive stop strip
If shape hole and protrusion, 300 independent stress of articulated shaft is easy to cause horn 200 and is broken with fuselage framework 100.
Further, it is correspondingly arranged on positioning locking structure between the horn 200 and the fuselage framework 100, works as machine
When arm 200 is turned out to unfolded state, locking structure is opened, horn 200 is made to be maintained at the state of expansion；Similarly, lock is closed
Only structure rotates horn 200, when horn 200 inwardly turns to receiving state, opens locking structure, horn 200 is made to be maintained at
Receiving state.
As shown in figure 5, specifically, be provided with first positioning hole 112 and second location hole on the upper plate 110, described
A positioning hole 112 is located at the described first outside for limiting 111 one end of strip-shaped hole, and the second location hole is located at described first and limits
The outside of the other end of position strip-shaped hole 111；Elastic positioning pin is provided on the horn 200, the elastic positioning pin includes
Plunger 220 and key seat, the key seat include pin hole, and the plunger 220 is slidably connected in the pin hole, and the plunger 220
Compressed spring is provided between the key seat, the length of the plunger 220 is less than the depth of the pin hole, so that the plunger
220 are telescopically disposed in the key seat；The first positioning hole 112 and second location hole are located at the fortune of the plunger 220
On dynamic path.When plunger 220 is in first positioning hole 112, horn 200 is in receiving state, by pressing plunger 220, makes pin
First 220 are retracted into key seat, then rotate horn 200, and plunger 220 is against upper plate 110 under by the elastic force of compressed spring
In the one side of plate 120, with horn 200 rotate unfolded state when, plunger 220 turns at second location hole, is compressed
The elastic force of spring acts on, and plunger 220 is stretched out from second location hole, at this point, horn 200 can not be rotated again.Pass through location hole
With the cooperation of elastic positioning pin, horn 200 is made to be maintained at receiving state and unfolded state.
As shown in fig. 6, it is further, for the switching state for keeping horn 200 more convenient, the outer end of the plunger 220
Portion is bulb shape；The first positioning hole 112 and second location hole are flared structure 400, and the flared structure 400 wraps
The first opening backwards to 120 one side of the lower plate positioned at the upper plate 110 is included, and positioned at the upper plate 110 towards under described
Second opening of 120 one side of plate, is open along described first to second opening direction, the internal diameter of the flared structure 400
Gradually increase, and 400 internal face of the flared structure and the upper plate 110 are towards rounding between the one side of the lower plate 120
Angle.Operator presses with finger plunger 220, makes the top of plunger 220 less than the first opening, then firmly rotates horn 200, pin
First 220 bulb can be contradicted with the inner wall of inclined flared structure 400, to by along the power on inclined-plane resolve into it is horizontal and
Power in vertical direction presses downward to plunger 220 in key seat, it is easier to horn 200 be made to rotate.
If first positioning hole 112 or second location hole are the constant through-hole of internal diameter, because upper plate 110 has centainly
Thickness, user need use some protrusions, the top of plunger 220, which is depressed into the lower surface of upper plate 110 or less just, to be made
Horn 200 rotates, and needs inconvenient by foreign object.
Further, the fuselage framework 100 includes four circumferentially arranged lateral surfaces, the quantity of the horn 200
It it is four, four horns 200 are located on four lateral surfaces.The case where unmanned plane skeleton is not limited to four arms,
The form for being prepared into six arms or eight arms can also be designed.
Above-mentioned location structure can also be accordingly arranged in lower plate 120, identical as above-mentioned set-up mode, only set
The position set is different.
Alternatively, on upper plate 110 and lower plate 120, and positioning knot is correspondingly arranged in the opposing sides of horn 200
Structure, although structure is complicated, locating effect is more preferable, and horn 200 is more stablized.
A kind of unmanned plane provided in an embodiment of the present invention, including above-mentioned unmanned plane skeleton.Unmanned plane skeleton includes：Fuselage
The quantity of skeleton 100 and horn 200, the horn 200 is multiple；The horn 200 includes first end and second end, and described the
For propeller mechanism to be fixedly mounted, the second end is flexibly connected with the peripheral side of the fuselage framework 100 for one end, so that
Distance of the second end apart from the fuselage framework 100 is adjustable.By movable horn 200, the second end of horn 200 can be made
Close to the fuselage framework 100, at this point, the first end and second end of horn 200 is all close to fuselage framework 100, unmanned plane skeleton
Whole occupied space reduces, and facilitates the storage and carrying of unmanned plane；When unmanned plane needs in use, movable horn 200, makes machine
The second end of arm 200 meets the needs of long wheelbase far from fuselage framework 100, the expansion of horn 200.Nothing provided in an embodiment of the present invention
There is man-machine skeleton folding structure system that is deployable and can storing, developed dimension bigger to store smaller, folding and unfolding side
Formula and simple to operate.
Further, the unmanned plane further includes propeller mechanism, flies control anticollision identification device and GPS receiver.Spiral
Paddle mechanism is mounted on horn 200, and flying control anticollision identification device and GPS receiver can be arranged in fuselage framework 100.
Finally it should be noted that：Embodiment described above, only specific implementation mode of the invention, to illustrate the present invention
Technical solution, rather than its limitations, scope of protection of the present invention is not limited thereto, although with reference to the foregoing embodiments to this hair
It is bright to be described in detail, it will be understood by those of ordinary skill in the art that：Any one skilled in the art
In the technical scope disclosed by the present invention, it can still modify to the technical solution recorded in previous embodiment or can be light
It is readily conceivable that variation or equivalent replacement of some of the technical features；And these modifications, variation or replacement, do not make
The essence of corresponding technical solution is detached from the spirit and scope of technical solution of the embodiment of the present invention, should all cover the protection in the present invention
Within the scope of.Therefore, the protection scope of the present invention shall be subject to the protection scope of the claims.
Claims (10)
1. a kind of unmanned plane skeleton, which is characterized in that including：The quantity of fuselage framework and horn, the horn is multiple；It is described
Horn includes first end and second end, and the first end is for being fixedly mounted propeller mechanism, the second end and the fuselage
The peripheral side of skeleton is flexibly connected, so that distance of the second end apart from the fuselage framework is adjustable.
2. unmanned plane skeleton according to claim 1, which is characterized in that the horn is hinged with the fuselage framework.
3. unmanned plane skeleton according to claim 2, which is characterized in that the articulated shaft of the horn and the fuselage framework
Perpendicular to the upper and lower surface of the fuselage framework, so that the horn can rotate in the face parallel with the fuselage framework.
4. unmanned plane skeleton according to claim 3, which is characterized in that the fuselage framework includes upper plate and lower plate, institute
State that upper plate is parallel with lower plate and interval setting, the second end of the horn is hinged between the upper plate and lower plate；
The first limit strip-shaped hole and the second limit strip-shaped hole, first limit are correspondingly arranged on the upper plate and lower plate respectively
Strip-shaped hole and the second limit strip-shaped hole are arc-shaped, are correspondingly arranged on the opposite sides face of the horn and first limit
Corresponding first limit protrusion of strip-shaped hole, and the second limit protrusion corresponding with the second limit strip-shaped hole；Described first
Limit protrusion is located at described first and limits in strip-shaped hole, and can be along the first limit strip-shaped hole sliding；Second limit
Protrusion is located at described second and limits in strip-shaped hole, and can be along the second limit strip-shaped hole sliding.
5. unmanned plane skeleton according to claim 4, which is characterized in that corresponding between the horn and the fuselage framework
It is provided with positioning locking structure, after the positioning locking Structural lock stops, for making the horn keep receiving state or expansion
State.
6. unmanned plane skeleton according to claim 5, which is characterized in that be provided with first positioning hole and on the upper plate
Two location holes, the first positioning hole are located at the described first outside for limiting strip-shaped hole one end, and the second location hole is located at
The outside of the other end of the first limit strip-shaped hole；
Elastic positioning pin is provided on the horn, the elastic positioning pin includes plunger and key seat, and the key seat includes pin hole,
The plunger is slidably connected in the pin hole, and compressed spring is provided between the plunger and the key seat, the plunger
Length be less than the pin hole depth so that the plunger is telescopically disposed in the key seat；
The first positioning hole and second location hole are located on the motion path of the plunger, so that the elastic positioning pin rotates
To the first positioning hole either second location hole when the plunger stretched out from the first positioning hole or second location hole.
7. unmanned plane skeleton according to claim 6, which is characterized in that the outer end of the plunger is bulb shape；It is described
First positioning hole and second location hole are flared structure, and the flared structure includes being located at the upper plate under described
Plate one side first opening, and positioned at the upper plate towards the lower plate one side second opening, along described first be open to
Second opening direction, the internal diameter of the flared structure gradually increase, and the flared structure internal face with it is described on
Plate is towards rounded corner between the one side of the lower plate.
8. unmanned plane skeleton according to claim 1, which is characterized in that the fuselage framework includes circumferentially arranged four
The quantity of a lateral surface, the horn is four, and four horns are located on four lateral surfaces.
9. a kind of unmanned plane, which is characterized in that including the unmanned plane skeleton described in claim 1-8 any one.
10. unmanned plane according to claim 9, which is characterized in that the unmanned plane further includes propeller mechanism, flies to control and prevent
Hit identification device and GPS receiver.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810641204.1A CN108438216A (en) | 2018-06-20 | 2018-06-20 | Unmanned plane skeleton and unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810641204.1A CN108438216A (en) | 2018-06-20 | 2018-06-20 | Unmanned plane skeleton and unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108438216A true CN108438216A (en) | 2018-08-24 |
Family
ID=63206660
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810641204.1A Pending CN108438216A (en) | 2018-06-20 | 2018-06-20 | Unmanned plane skeleton and unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108438216A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109760830A (en) * | 2019-03-20 | 2019-05-17 | 郑荣桂 | A kind of three support leg module combined type rotor wing unmanned aerial vehicles of environment survey |
| CN110171562A (en) * | 2019-05-24 | 2019-08-27 | 孙思为 | A kind of unmanned plane rotor control structure |
| CN110972471A (en) * | 2018-09-28 | 2020-04-07 | 深圳市大疆创新科技有限公司 | Arm subassembly reaches unmanned aerial vehicle including this arm subassembly |
| CN113795424A (en) * | 2020-06-01 | 2021-12-14 | 深圳市大疆创新科技有限公司 | Arm subassembly and unmanned vehicles |
| CN114336977A (en) * | 2022-01-11 | 2022-04-12 | 四川新迎顺信息技术股份有限公司 | Intelligent inspection application system and method based on AI image recognition |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN205707297U (en) * | 2016-04-19 | 2016-11-23 | 牛睿 | Fixed-wing unmanned plane |
| CN206634196U (en) * | 2017-04-06 | 2017-11-14 | 罗元彬 | A kind of new unmanned plane |
| JP2018030560A (en) * | 2016-08-26 | 2018-03-01 | 株式会社クボタ | Agriculture multicopter |
| CN208291475U (en) * | 2018-06-20 | 2018-12-28 | 广东电网有限责任公司 | Unmanned plane skeleton and unmanned plane |
-
2018
- 2018-06-20 CN CN201810641204.1A patent/CN108438216A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN205707297U (en) * | 2016-04-19 | 2016-11-23 | 牛睿 | Fixed-wing unmanned plane |
| JP2018030560A (en) * | 2016-08-26 | 2018-03-01 | 株式会社クボタ | Agriculture multicopter |
| CN206634196U (en) * | 2017-04-06 | 2017-11-14 | 罗元彬 | A kind of new unmanned plane |
| CN208291475U (en) * | 2018-06-20 | 2018-12-28 | 广东电网有限责任公司 | Unmanned plane skeleton and unmanned plane |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110972471A (en) * | 2018-09-28 | 2020-04-07 | 深圳市大疆创新科技有限公司 | Arm subassembly reaches unmanned aerial vehicle including this arm subassembly |
| CN109760830A (en) * | 2019-03-20 | 2019-05-17 | 郑荣桂 | A kind of three support leg module combined type rotor wing unmanned aerial vehicles of environment survey |
| CN109760830B (en) * | 2019-03-20 | 2020-10-20 | 山东天衢精密工业有限公司 | Environment surveying is with three leg module combination formula rotor unmanned aerial vehicle that prop |
| CN110171562A (en) * | 2019-05-24 | 2019-08-27 | 孙思为 | A kind of unmanned plane rotor control structure |
| CN113795424A (en) * | 2020-06-01 | 2021-12-14 | 深圳市大疆创新科技有限公司 | Arm subassembly and unmanned vehicles |
| CN114336977A (en) * | 2022-01-11 | 2022-04-12 | 四川新迎顺信息技术股份有限公司 | Intelligent inspection application system and method based on AI image recognition |
| CN114336977B (en) * | 2022-01-11 | 2024-05-03 | 四川新迎顺信息技术股份有限公司 | Intelligent inspection application system and method based on AI image recognition |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN108438216A (en) | Unmanned plane skeleton and unmanned plane | |
| US10710701B2 (en) | Foldable multi-rotor UAV | |
| CN208291475U (en) | Unmanned plane skeleton and unmanned plane | |
| CN206437202U (en) | Unmanned plane | |
| CN107000834B (en) | More rotor unmanned aircrafts | |
| CN102556336A (en) | Wing fast unfolding device for folding-wing unmanned plane | |
| WO2018094707A1 (en) | Air-drop container, and unmanned aerial vehicle | |
| CN107074353A (en) | Uas | |
| CN207129131U (en) | A kind of folding portable unmanned plane | |
| CN110877710A (en) | Mooring rotor unmanned aerial vehicle capable of being automatically folded and unfolded | |
| CN109703735A (en) | A kind of unmanned plane horn automatic folding device | |
| CN210191813U (en) | Unmanned aerial vehicle of collapsible rotor | |
| CN109278981B (en) | Miniature foldable three-dimensional live-action modeling unmanned aerial vehicle | |
| TWM524313U (en) | Unmanned aerial vehicle | |
| CN211685581U (en) | Intelligent rescue guiding device of hospital | |
| CN205696215U (en) | A kind of luggage case being provided with folding wheel | |
| CN210401653U (en) | Backpack type laser radar scanning system | |
| EP3564119A1 (en) | Multi-rotor unmanned aerial vehicle | |
| CN206797713U (en) | One kind is used for unmanned plane of taking photo by plane | |
| CN205866263U (en) | Assembled luggage case | |
| CN209410320U (en) | A kind of hollow vertical touching lever fold mechanism | |
| CN206885330U (en) | Horn, Power Component and unmanned plane | |
| WO2019029387A1 (en) | Aerial vehicle and arm assembly and frame thereof | |
| CN110053757A (en) | Cantilever coupling apparatus for unmanned vehicle and the unmanned vehicle using this | |
| CN206218198U (en) | Intake type aircraft |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination |