CN206476093U - A kind of unmanned plane - Google Patents
A kind of unmanned plane Download PDFInfo
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- CN206476093U CN206476093U CN201621453808.6U CN201621453808U CN206476093U CN 206476093 U CN206476093 U CN 206476093U CN 201621453808 U CN201621453808 U CN 201621453808U CN 206476093 U CN206476093 U CN 206476093U
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- unmanned plane
- cantilever
- main body
- fender bracket
- fuselage main
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Abstract
The utility model discloses a kind of unmanned plane, including fuselage main body, the relative both sides of fuselage main body are provided with some cantilevers, cantilevered distal end is provided with rotor, and cantilever is bent, and cantilever is stretched during storage, with fuselage main body formation yi word pattern receiving state, in use, cantilever is bent into square, I-shaped deployed condition is formed with fuselage main body.Unmanned plane of the present utility model is by setting the cantilever that can be bent, cantilever is bent into square when in use, it is in I-shaped deployed condition to make unmanned plane, rotor is located at surrounding and provides flying power, cantilever is stretched during storage, it is in yi word pattern receiving state to make unmanned plane, is easy to store carrying, so as to solve the problem of larger inconvenience of unmanned plane volume in the market is stored.
Description
Technical field
The utility model is related to unmanned air vehicle technique field, more particularly to a kind of unmanned plane for being easy to store.
Background technology
Unmanned plane is that one kind need not carry people to fly, by the aircraft of controlled in wireless, because it can realize flight, boat
The function such as bat and detecting, can complete being not readily accomplished before many for task, therefore be developed rapidly, and at present, unmanned plane was both
Available for professional domains such as movies-making, military surveillance and public security fire-fightings, while increasingly favor for ordinary populace again, progressively send out
The instrument to be amused and diverted oneself for people is transformed into, manipulates, autodyne and takes photo by plane for flying.
However, common unmanned plane volume is bigger than normal in the market, user is allowed to be inconvenient to store and carry, have impact on makes
User carries with the experience that unmanned plane carries out recreation.
Utility model content
In view of the problem of prior art unmanned plane is inconvenient to store carrying, it is proposed that one kind of the present utility model is easy to store
Unmanned plane, to overcome above mentioned problem or to solve the above problems at least in part.
To achieve these goals, the utility model employs following technical scheme：
A kind of unmanned plane, including fuselage main body, the relative both sides of the fuselage main body are provided with some cantilevers, the cantilever
End is provided with rotor, and the cantilever is bent, and the cantilever is stretched during storage, is stored with fuselage main body formation yi word pattern
State, in use, the cantilever is bent into square, I-shaped deployed condition is formed with the fuselage main body.
Alternatively, the cantilever includes fixed arm and cursor, and the fixed arm is fixedly connected in the fuselage main body,
Its end connects the cursor by axis of rotation, and the cursor end is provided with the rotor；The fixed arm and institute
The rotating contact face of cursor is stated with the axis of the cantilever in 45 ° of angles, the vertical rotating contact face of the rotating shaft is set,
During storage the cursor go to it is in alignment with the fixed arm, when using the cursor go to the fixed arm hang down
Directly.
Alternatively, the rotating shaft side is additionally provided with spacing preiection, the axis hole side wall of the rotating shaft corresponding described spacing
Projection is provided with stopper slot, and the spacing preiection is slided in the stopper slot during axis of rotation, and the cursor is gone to
In alignment or when going to vertical with the fixed arm with the fixed arm, the spacing preiection slides to the stopper slot end
Stop sliding, it is spacing to the rotating shaft.
Alternatively, the relative both sides of the fuselage main body are respectively symmetrically provided with two cantilevers, positioned at the fuselage
The cantilever of main body homonymy is bent into square opposite to each other.
Alternatively, the rotor blade is removably attached on the cantilever.
Alternatively, the unmanned plane also includes fender bracket, and the fender bracket is enclosed on the outside of the unmanned plane, including left guarantor
Retaining frame and right fender bracket, the left fender bracket and right fender bracket are by snapping connection.
Alternatively, it is provided with the fender bracket in supporting plate, the supporting plate and is provided with fixed seat, the unmanned plane is consolidated
It is scheduled in the fixed seat, drives the fender bracket together to fly.
Alternatively, the relative both sides of the fuselage main body are provided with projection, and the fixed seat is the imitation-shaped groove of upper opening
The correspondence raised neck is provided with structure, its side wall, the projection is caught in the neck, the unmanned plane is fixed
In the fixed seat.
Alternatively, the fender bracket includes side wall of the horizontal direction around the unmanned plane, the both sides up and down of the side wall
It is provided with the catch net of ventilation.
Alternatively, the both sides of the edge up and down of the side wall are provided with threading in string holes, the string holes and form the catch net.
The beneficial effects of the utility model are：
There is provided a kind of unmanned plane for being easy to store, by setting the cantilever that can be bent, cantilever is bent when in use
Shape at a right angle, it is in I-shaped deployed condition to make unmanned plane, and rotor is located at surrounding and provides flying power, stretches cantilever during storage,
It is in yi word pattern receiving state to make unmanned plane, is easy to store carrying, so as to solve the larger inconvenience of unmanned plane volume in the market
The problem of storage.
Brief description of the drawings
A kind of unmanned plane receiving state schematic diagram that Fig. 1 provides for the utility model one embodiment；
Fig. 2 is bent into the schematic diagram of square for a kind of unmanned plane cantilever that the utility model one embodiment is provided；
Rotating contact face signal when Fig. 3 stretches for a kind of unmanned plane cantilever that the utility model one embodiment is provided
Figure；
Rotating contact faces of the Fig. 4 for a kind of unmanned plane cantilever bending that the utility model one embodiment is provided when at a right angle
Schematic diagram；
A kind of unmanned plane deployed condition schematic diagram that Fig. 5 provides for the utility model one embodiment；
Fig. 6 installs schematic diagram during fender bracket for a kind of unmanned plane that the utility model one embodiment is provided；
A kind of fuselage main body for unmanned plane that Fig. 7 provides for the utility model one embodiment and the fixed seat of fender bracket are solid
Determine schematic diagram；
A kind of signal of the fender bracket installation state for unmanned plane that Fig. 8 provides for the utility model one embodiment
Figure；
In figure：1st, fuselage main body；11st, it is raised；2nd, fixed arm；3rd, cursor；4th, rotor motor；5th, rotating contact face；51、
Rotating shaft；52nd, spacing preiection；53rd, stopper slot；6th, rotor blade；7th, left fender bracket；71st, supporting plate；72nd, fixed seat；73rd, neck；
8th, right fender bracket.
Embodiment
Core concept of the present utility model is：The form that the cantilever of unmanned plane is set to bend, when in use will
Cantilever is bent into square, unmanned plane is flown in I-shaped deployed condition, stretches cantilever during storage, makes the unmanned plane be in
Yi word pattern receiving state, is carried consequently facilitating storing.
It is new to this practicality below in conjunction with accompanying drawing to make the purpose of this utility model, technical scheme and advantage clearer
Type embodiment is described in further detail.
Fig. 1-8 shows a preferred embodiment of the utility model unmanned plane, and with reference to Fig. 1-8, the utility model is implemented
The unmanned plane of example, including fuselage main body 1, the relative both sides of fuselage main body 1 are provided with some cantilevers, and cantilevered distal end is provided with rotation
The wing, cantilever is bent, and cantilever is stretched during storage, yi word pattern receiving state is formed with fuselage main body 1, as shown in figure 1, now straight line
The unmanned plane of shape is easy to pack up carrying；In use, cantilever is bent into square, I-shaped deployed condition is formed with fuselage main body 1,
Shown in Fig. 4, now rotor is deployed in fuselage main body surrounding, and rotation provides the power of unmanned plane during flying.It is bent by setting
Cantilever, using cantilever bending and stretch, unmanned plane is switched between I-shaped deployed condition and yi word pattern receiving state,
While not influenceing the unmanned plane to use, it is easy to the storage of unmanned plane to carry.
In the present embodiment, rotor includes rotor motor 4 and rotor blade 6, and rotor blade 6 is removably attached to cantilever
On, rotor blade 6 pulled down into storages when storing, is conducive to reducing volume, saving space, can also avoid rotor blade 6 due to
Extruding is impaired.
Preferably, with reference to Fig. 1-4, cantilever includes fixed arm 2 and cursor 3, and fixed arm 2 is fixedly connected on fuselage main body 1
On, its end rotates connection cursor 3 by rotating shaft 51 (be located at cantilever in), and the end of cursor 3 is provided with rotor (rotor in figure
Blade 6 has been pulled down)；The rotating contact face 5 of fixed arm 2 and cursor 3 is with the axis of cantilever in 45 ° of angles, and rotating shaft 51 is vertically revolved
Switching contacting surface 5 is set, and cursor 3 goes in alignment with fixed arm 2 during storage, and cursor 3 is gone to and fixed arm 2 when using
Vertically.
Rotating contact face schematic diagram when Fig. 3 stretches for cantilever, Fig. 4 is rotating contact face when cantilever is bent into square
Schematic diagram, referring to Fig. 3-4, the side of rotating shaft 51 is additionally provided with correspondence spacing preiection on spacing preiection 52, the axis hole side wall of rotating shaft 51
52 are provided with stopper slot 53, and spacing preiection 52 is slided in stopper slot 53 when rotating shaft 51 is rotated, as shown by arrows in FIG..Work as rotation
Arm 3 goes in alignment or when going to vertical with fixed arm 2 with fixed arm 2, and spacing preiection 52 slides to the end of stopper slot 53 and stopped
Sliding stop, countershaft 51 is spacing, the bending of cantilever is deployed and is stretched storage and be accurately positioned.In the present embodiment, stopper slot 53 is opened
The downside of rotating shaft 51 is located at, by upward power during due to rotor wing rotation flight, spacing preiection 52 can be avoided in stopper slot 53
Retract.
Preferably, in the present embodiment, the relative both sides of fuselage main body 1 are respectively symmetrically provided with two cantilevers, positioned at fuselage
The cantilever of the homonymy of main body 1 is bent into square opposite to each other, rotor thereon is deployed respectively to both sides.
Preferably, the unmanned plane of the present embodiment also includes fender bracket, and fender bracket is enclosed on the outside of unmanned plane, makes unmanned plane whole
Body is located in fender bracket, and rotor can be protected not damaged in air crash, can also prevent unmanned plane from contacting with people to hurt sb.'s feelings, especially suitable
With people's SUAV closer to the distance when operation, as shown in figs 6-8, fender bracket includes left fender bracket 7 and right fender bracket 8,
Left fender bracket 7 and right fender bracket 8 are connected together by snapping connection after being respectively fitted over from unmanned plane both sides on the outside of unmanned plane.
Preferably, supporting plate 71 is provided with fender bracket, as shown in fig. 7, supporting plate 71 is fixed in left fender bracket 7, branch
Fixed seat 72 is provided with fagging 71, during flight, unmanned plane is fixed in fixed seat 72, drives fender bracket together to fly.
Specifically, the relative both sides of fuselage main body 1 are provided with projection 11, and fixed seat 72 is the imitation-shaped groove knot of upper opening
The neck 73 of respective protrusions 11 is provided with structure, the shape adaptation with fuselage main body 1, its side wall, under shown in arrow in figure
Unmanned plane is pressed, projection 11 is caught in neck 73, unmanned plane is fixed in fixed seat 72.
Preferably, fender bracket includes horizontal direction around the side wall of unmanned plane, and the both sides up and down of side wall are provided with ventilation
Catch net, side wall can realize that horizontal direction is well isolated from unmanned plane, it is to avoid unmanned plane is wounded and hurted sb.'s feelings, and both sides are set up and down
Catch net while shielding, also do not obstruct air-flow, do not interfere with the flight of unmanned plane rotor.Specifically, side wall
Both sides of the edge up and down be provided with string holes, string holes threading formation catch net, threading may also help in the left fender bracket 7 of sizing and the right side
The shape of fender bracket 8, prevents the two out of shape.
It is described above, embodiment only of the present utility model, under above-mentioned teaching of the present utility model, this area
Technical staff can carry out other improvement or deformation on the basis of above-described embodiment.It will be understood by those skilled in the art that
Above-mentioned specific descriptions are more preferable explanation the purpose of this utility model, and protection domain of the present utility model should be with claim
Protection domain be defined.
Claims (10)
1. a kind of unmanned plane, including fuselage main body, it is characterised in that the relative both sides of the fuselage main body are provided with some outstanding
Arm, the cantilevered distal end is provided with rotor, and the cantilever is bent, and the cantilever is stretched during storage, with the fuselage main body shape
Into yi word pattern receiving state, in use, the cantilever is bent into square, I-shaped expansion shape is formed with the fuselage main body
State.
2. unmanned plane as claimed in claim 1, it is characterised in that the cantilever includes fixed arm and cursor, the fixation
Arm is fixedly connected in the fuselage main body, and its end connects the cursor by axis of rotation, and the cursor end is set
It is equipped with the rotor；The rotating contact face of the fixed arm and the cursor is in 45 ° of angles with the axis of the cantilever, described
The vertical rotating contact face of rotating shaft is set, during storage the cursor go to it is in alignment with the fixed arm, when using
The cursor goes to vertical with the fixed arm.
3. unmanned plane as claimed in claim 2, it is characterised in that the rotating shaft side is additionally provided with spacing preiection, described turn
The correspondence spacing preiection is provided with stopper slot on the axis hole side wall of axle, and the spacing preiection is in the limit during axis of rotation
Slided in the groove of position, the cursor go to it is in alignment or when going to vertical with the fixed arm with the fixed arm, it is described
Spacing preiection, which slides to the stopper slot end, to be stopped sliding, spacing to the rotating shaft.
4. unmanned plane as claimed in claim 1, it is characterised in that the relative both sides of the fuselage main body are respectively symmetrically provided with
Two cantilevers, the cantilever positioned at the fuselage main body homonymy is bent into square opposite to each other.
5. unmanned plane as claimed in claim 1, it is characterised in that the rotor blade is removably attached to the cantilever
On.
6. unmanned plane as claimed in claim 1, it is characterised in that the unmanned plane also includes fender bracket, the fender bracket bag
It is trapped among on the outside of the unmanned plane, including left fender bracket and right fender bracket, the left fender bracket and right fender bracket are by snapping connection.
7. unmanned plane as claimed in claim 6, it is characterised in that supporting plate, the supporting plate are provided with the fender bracket
On be provided with fixed seat, the unmanned plane is fixed in the fixed seat, drives the fender bracket together to fly.
8. unmanned plane as claimed in claim 7, it is characterised in that the relative both sides of the fuselage main body are provided with projection, institute
State and the correspondence raised neck is provided with the profiling slot structure that fixed seat is upper opening, its side wall, the projection is caught in
In the neck, the unmanned plane is fixed in the fixed seat.
9. unmanned plane as claimed in claim 6, it is characterised in that the fender bracket includes horizontal direction around the unmanned plane
Side wall, the both sides up and down of the side wall are provided with the catch net of ventilation.
10. unmanned plane as claimed in claim 9, it is characterised in that the both sides of the edge up and down of the side wall are provided with string holes, institute
State threading in string holes and form the catch net.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621453808.6U CN206476093U (en) | 2016-12-27 | 2016-12-27 | A kind of unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621453808.6U CN206476093U (en) | 2016-12-27 | 2016-12-27 | A kind of unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206476093U true CN206476093U (en) | 2017-09-08 |
Family
ID=59750484
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621453808.6U Active CN206476093U (en) | 2016-12-27 | 2016-12-27 | A kind of unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206476093U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106741839A (en) * | 2016-12-27 | 2017-05-31 | 歌尔科技有限公司 | A kind of unmanned plane |
| NO20180080A1 (en) * | 2018-01-17 | 2019-07-18 | Griff Aviation As | An unmanned aerial vehicle having rotating wing lift generating means, advantageously a multicopter with a unitary main fuselage and foldable rotor arms. |
-
2016
- 2016-12-27 CN CN201621453808.6U patent/CN206476093U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106741839A (en) * | 2016-12-27 | 2017-05-31 | 歌尔科技有限公司 | A kind of unmanned plane |
| NO20180080A1 (en) * | 2018-01-17 | 2019-07-18 | Griff Aviation As | An unmanned aerial vehicle having rotating wing lift generating means, advantageously a multicopter with a unitary main fuselage and foldable rotor arms. |
| NO344274B1 (en) * | 2018-01-17 | 2019-10-21 | Griff Aviation As | An unmanned aerial vehicle having rotating wing lift generating means, advantageously a multicopter with a unitary main fuselage and foldable rotor arms. |
| US11993373B2 (en) | 2018-01-17 | 2024-05-28 | Griff Aviation As | Unmanned aerial vehicle |
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