CN108313259A - A kind of unmanned plane - Google Patents
A kind of unmanned plane Download PDFInfo
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- CN108313259A CN108313259A CN201810149869.0A CN201810149869A CN108313259A CN 108313259 A CN108313259 A CN 108313259A CN 201810149869 A CN201810149869 A CN 201810149869A CN 108313259 A CN108313259 A CN 108313259A
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- China
- Prior art keywords
- fuselage
- state
- unmanned plane
- horn
- unfolded
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Classifications
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- 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
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/061—Frames
- B64C1/063—Folding or collapsing to reduce overall dimensions, e.g. foldable tail booms
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- 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
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/068—Fuselage sections
- B64C1/069—Joining arrangements therefor
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- 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
- B64C1/16—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like specially adapted for mounting power plant
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- 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
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Remote Sensing (AREA)
- Toys (AREA)
Abstract
The present invention provides a kind of unmanned plane, including the first fuselage, the second fuselage and the first horn and the second horn for carrying power plant, the first horn are flexibly connected with the first fuselage, and the first supporting part for installing power plant is provided on the first horn；Second horn is flexibly connected with the second fuselage, and the second supporting part for installing power plant is provided on the second horn；First fuselage is flexibly connected with the second fuselage, and when unmanned plane is in state of flight, the first fuselage can be unfolded to be in the first unfolded state relative to the second fuselage；When unmanned plane is in non-state of flight, it is in first folded state that the first fuselage, which can be rotated relative to the second fuselage and is bonded with the second fuselage,；First fuselage can be rotated relative to the second fuselage, and the first fuselage is made to switch between the first unfolded state and first folded state.Overall volume when unmanned plane is in non-state of flight can be reduced in this way.
Description
Technical field
The present invention relates to air vehicle technique field more particularly to a kind of unmanned planes.
Background technology
Unmanned plane, that is, UAV requires low excellent with maneuverability, rapid reaction, unmanned flight, operation
Point.And various loads, such as camera can be loaded on unmanned plane, image real-time Transmission may be implemented, and can extensive use
In fire-fighting, military affairs, the fields such as energy, police service, exploration and meteorology are handed over, to realize cruise shooting and the monitoring to designated area.
Currently, unmanned plane is multiaxis unmanned plane mostly, such as four axis, six axis etc., and since horn is outside with respect to fuselage
It is arranged radially, causes the overall volume of unmanned plane bigger, occupied space is also bigger, it is difficult to accomplish convenient transportation and take
Band.As it can be seen that existing unmanned plane has that overall volume is larger.
Invention content
The embodiment of the present invention provides a kind of unmanned plane, and it is larger that there are overall volumes to solve the problems, such as existing unmanned plane.
An embodiment of the present invention provides a kind of unmanned plane, including the first fuselage, the second fuselage and for carrying power dress
The first horn and the second horn set, wherein：
First horn is flexibly connected with first fuselage, is provided on first horn described dynamic for installing
First supporting part of power apparatus；
Second horn is flexibly connected with second fuselage, is provided on second horn described dynamic for installing
Second supporting part of power apparatus；
First fuselage is flexibly connected with second fuselage, when the unmanned plane is in state of flight, described first
Fuselage can be unfolded to be in the first unfolded state relative to second fuselage；When the unmanned plane is in non-state of flight, described
It is in first folded state that one fuselage, which can be rotated relative to second fuselage and is bonded with second fuselage,；
Wherein, first fuselage can be rotated relative to second fuselage, make first fuselage in the first expansion
Switch between state and first folded state.
Optionally, when the unmanned plane is in state of flight, first horn can be relative to the first fuselage exhibition
It is in the second unfolded state to open；When the unmanned plane is in non-state of flight, first horn can be relative to first machine
Body, which is rotated and collapsed, is presented the second folded state；First horn can be rotated relative to first fuselage, make described
One horn switches between second unfolded state and second folded state；
When the unmanned plane is in state of flight, second horn can be unfolded to be in third relative to second fuselage
Unfolded state；When the unmanned plane is in non-state of flight, second horn can rotate simultaneously relative to second fuselage
It collapses and third folded state is presented；Second horn can be rotated relative to second fuselage, and second horn is made to exist
Switch between the third unfolded state and the third folded state.
Optionally, it is provided on first fuselage and holds for the first of accommodating the first horn that the second folded state is presented
Between emptying；The second accommodating space for accommodating the second horn that third folded state is presented is provided on second fuselage.
Optionally, the quantity of first horn is two, and the quantity of first accommodating space is two；Described second
The quantity of horn is two；The quantity of second accommodating space is two.
Optionally, the flight coordinate-system of the unmanned plane includes roll axis, course axis and pitch axis, the roll axis with
Plane where the pitch axis is the first reference plane of the unmanned plane, and the roll axis is institute with plane where the course axis
State the second reference plane of unmanned plane；
Wherein, when the unmanned plane is in non-state of flight, first accommodating space and the second accommodating space phase
First reference plane is symmetrical arranged, relatively described second reference plane of two first accommodating spaces is symmetrical arranged, described
Relatively described second reference plane of two the second accommodating spaces is symmetrical arranged.
Optionally, when the unmanned plane is in non-state of flight, direction of first horn in the roll axis direction
It is identical in the direction of roll axis direction as second horn.
Optionally, when first fuselage relative to second fuselage is unfolded that the first unfolded state is presented, described first
First supporting part of horn is identical as the direction of the second supporting part of the second horn；First fuselage is relative to described
The rotation of two fuselages be bonded with second fuselage when being in first folded state, the first supporting part of first horn and described the
The direction of second supporting part of two horns is opposite.
Optionally, the unmanned plane further includes fuselage shaft, and first fuselage passes through the fuselage shaft and described the
Two fuselages are rotatablely connected.
Optionally, the unmanned plane further includes holder, and the holder is arranged on the first fuselage or the second fuselage；When described
When first fuselage relative to second fuselage is unfolded that the first unfolded state is presented, the holder, which is in, appears state, when described
When first fuselage is bonded with second fuselage in first folded state relative to second fuselage rotation, the holder is in
Hidden state.
Optionally, the unmanned plane further includes：First support portion and the second support portion, wherein first support portion is set
It sets on the first fuselage, second support portion is arranged on the second fuselage；
When first fuselage relative to second fuselage is unfolded that the first unfolded state is presented, first support portion
It is in holding state with the second support portion；
It is bonded in first folded state with second fuselage when first fuselage is rotated relative to second fuselage
When, first support portion and the second support portion are in hidden state.
Optionally, the power plant is rotor assemblies.
Optionally, the rotor assemblies include be arranged first supporting part on the second supporting part motor and set
Set the propeller on the motor.
Optionally, the propeller is detachable paddle.
In this way, in the embodiment of the present invention, including the first fuselage, the second fuselage and for carrying power plant first
Horn and the second horn, wherein：First horn is flexibly connected with first fuselage, is arranged on first horn useful
In the first supporting part for installing the power plant；Second horn is flexibly connected with second fuselage, second machine
The second supporting part for installing the power plant is provided on arm；First fuselage connects with the second fuselage activity
It connects, when the unmanned plane is in state of flight, first fuselage can be unfolded relative to second fuselage in the first expansion shape
State；When the unmanned plane is in non-state of flight, first fuselage can rotate and described the relative to second fuselage
The fitting of two fuselages is in first folded state；Wherein, first fuselage can be rotated relative to second fuselage, make described
One fuselage switches between the first unfolded state and first folded state.It, can be in this way when unmanned plane is in non-state of flight
It is in folded state by the way that the first fuselage to be bonded with respect to the second fuselage, to reduce the overall volume of unmanned plane.
Description of the drawings
In order to illustrate the technical solution of the embodiments of the present invention more clearly, needed in being described below to the embodiment of the present invention
Attached drawing to be used is briefly described, it should be apparent that, drawings in the following description are only some embodiments of the invention,
For those of ordinary skill in the art, without having to pay creative labor, it can also obtain according to these attached drawings
Obtain other attached drawings.
Fig. 1 is one of the structural schematic diagram of unmanned plane provided in an embodiment of the present invention；
Fig. 2 is the second structural representation of unmanned plane provided in an embodiment of the present invention；
Fig. 3 is the third structural representation of unmanned plane provided in an embodiment of the present invention；
Fig. 4 is the four of the structural schematic diagram of unmanned plane provided in an embodiment of the present invention.
Specific implementation mode
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation describes, it is clear that described embodiments are some of the embodiments of the present invention, instead of all the embodiments.Based on this hair
Embodiment in bright, the every other implementation that those of ordinary skill in the art are obtained without creative efforts
Example, shall fall within the protection scope of the present invention.
In the description of the present invention, it should be noted that term "upper", "left", "right", "front", "rear", " is erected at "lower"
Directly ", the orientation of the instructions such as "inner", "outside" and position relationship are orientation based on ... shown in the drawings and position relationship, merely to just
In description invention and simplify description, does not indicate or imply the indicated device or element must have a particular orientation, with spy
Fixed azimuth configuration and operation, therefore be not considered as limiting the invention.In addition, term " first ", " second ", " third "
It is used for description purposes only, is not understood to indicate or imply relative importance.
In the description of the present invention, it should be noted that unless otherwise clearly defined and limited, term " installation ", " phase
Even ", " connection " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection, or be integrally connected；
It can be mechanical connection, can also be electrical connection；Can be directly connected, can also be indirectly connected through an intermediary, can
To be the connection in two elements.For the ordinary skill in the art, it can understand that above-mentioned term exists with concrete condition
Concrete meaning in the present invention.
Fig. 1 is one of the structural schematic diagram of unmanned plane provided in an embodiment of the present invention；Fig. 2 is provided in an embodiment of the present invention
The second structural representation of unmanned plane；Fig. 3 is the third structural representation of unmanned plane provided in an embodiment of the present invention；Fig. 4 is this
The four of the structural schematic diagram for the unmanned plane that inventive embodiments provide.
As shown in Figures 1 to 4, the embodiment of the present invention provides a kind of unmanned plane 100, including the first fuselage 10, the second fuselage
20 and the first horn 30 and the second horn 40 for carrying power plant, wherein：
First horn 30 is flexibly connected with first fuselage 10, is provided on first horn 30 for installing
First supporting part 31 of the power plant；
Second horn 40 is flexibly connected with second fuselage 20, is provided on second horn 40 for installing
Second supporting part 41 of the power plant；
First fuselage 10 is flexibly connected with second fuselage 20, when the unmanned plane 100 is in state of flight, institute
Stating the first fuselage 10 can be unfolded to be in the first unfolded state relative to second fuselage 20；The unmanned plane 100 is in non-flight
When state, it is in the first folding that first fuselage 10, which can be rotated relative to second fuselage 20 and is bonded with second fuselage 20,
Overlapping state；
Wherein, first fuselage 10 can be rotated relative to second fuselage 20, make first fuselage 10
Switch between one unfolded state and first folded state.
In embodiments of the present invention, unmanned plane 100 further includes fuselage shaft, and the first fuselage 10 can pass through fuselage shaft and the
Two fuselages 20 are rotatablely connected.As shown in Figure 1, when unmanned plane 100 is in state of flight, the first fuselage 10 can be with respect to the second machine
Body 20 is unfolded, and is in the first unfolded state, it is preferred that the first fuselage 10 can rotate 180 ° relative to the second fuselage, in the first expansion
State；As shown in Fig. 2, when unmanned plane 100 is in non-state of flight, the first fuselage 10 can be rotated relative to the second fuselage 20 with
The fitting of second fuselage 20 is in first folded state.
In present embodiment, after the first fuselage 10 is bonded with the second fuselage 20, it can be arranged first by engaging
First fuselage 10 and the second fuselage 20 are maintained fit-state by the buckle structure 50 on fuselage 10 and the second fuselage 20；And it needs
It, then can be by unclamping buckle structure 50 when controlling the first fuselage 10 in the first unfolded state, and control 10 phase of the first fuselage
Second fuselage 20 is rotated.And first fuselage 10 can be rotated relative to the second fuselage 20, make the first fuselage 10 first be unfolded shape
Switch between state and first folded state.
Since when unmanned plane 100 is in non-state of flight, 10 opposite second fuselage 20 of the first fuselage is unfolded, and can make nothing
Man-machine 100 overall volume is excessive, by rotating the first fuselage 10, the first fuselage 10 is made to be bonded the setting of the second fuselage 20, can be with
Overall volume of the unmanned plane 100 in non-state of flight is effectively reduced, and then user is facilitated to transport and take unmanned plane 100
Band.
In order to further decrease overall volume of the unmanned plane 100 in non-state of flight, the first horn 30 can be bonded
First fuselage 10 is arranged, and the second horn 40 is bonded the setting of the second fuselage 20.
As shown in Figures 1 and 2, when unmanned plane 100 is in state of flight, the first horn 30 can be relative to the first fuselage 10
In the second unfolded state；When unmanned plane 100 is in non-state of flight, the first horn 30 can rotate simultaneously relative to the first fuselage 10
It is in the second folded state to collapse；And first horn 30 can be rotated relative to the first fuselage 10, enable the first horn 30 second
Switch between unfolded state and the second folded state.Preferably, it is provided on the first fuselage 10 and the second folding is presented for accommodating
First accommodating space 11 of the first horn 30 of state, in this way when unmanned plane 100 is in non-state of flight, the first horn 30 can
It is accommodated in the first accommodating space 11 of the first fuselage 10, it is opposite to be fitted on the first fuselage 10, nobody can be further decreased
Machine 100 is in the overall volume in non-state of flight.
Similarly, when unmanned plane 100 is in state of flight, the second horn 40 can be in third exhibition relative to the second fuselage 20
Open state；When unmanned plane 100 is in non-state of flight, the second horn 40 can be rotated relative to the second fuselage 20 and be collapsed in the
Three folded states；And second horn 40 can be rotated relative to the second fuselage 20, enable the second horn 40 in third unfolded state
Switch between third folded state.Preferably, it is provided on the second fuselage 20 and is presented the of third folded state for accommodating
Second accommodating space 21 of two horns 40, in this way when unmanned plane 100 is in non-state of flight, the second horn 40 can be accommodated in
It is opposite to be fitted on the second fuselage 20 in second accommodating space 21 of two fuselages 20, can further decrease unmanned plane 100
Overall volume when non-state of flight.
In the present embodiment, the quantity of the first horn 30 is two, and the quantity of the first accommodating space 11 is two；Second
The quantity of horn 40 is two, and the quantity of the second accommodating space 21 is two.
As shown in Figure 1, the flight coordinate-system of unmanned plane 100 includes roll axis (X-axis), course axis (Y-axis) and pitch axis
(Z axis), in the present embodiment, roll axis (X-axis) and the first reference plane that plane where pitch axis (Z axis) is unmanned plane 100,
Roll axis (X-axis) and the second reference plane that plane where course axis (Y-axis) is unmanned plane 100.
Wherein, when unmanned plane 100 is in non-state of flight, the first accommodating space 11 and the second accommodating space 21 opposite first
Reference plane is symmetrical arranged, and two 11 opposite second reference planes of the first accommodating space are symmetrical arranged, two 21 phases of the second accommodating space
Second reference plane is symmetrical arranged.
It should be noted that when unmanned plane 100 is in non-state of flight, the first horn 30 is in the roll axis (X-axis)
Direction of the direction in direction with the second horn 40 in roll axis (X-axis) direction is identical.
Optionally, it is described when first fuselage 10 relative to second fuselage 20 is unfolded that the first unfolded state is presented
First supporting part 31 of the first horn 30 is identical as the direction of the second supporting part 41 of second horn 40；First fuselage
10 rotate relative to second fuselage 20 and are bonded with second fuselage 20 when being in first folded state, first horn 30
The first supporting part 31 it is opposite with the direction of the second supporting part 41 of second horn 40.
In the embodiment of the present invention, when the first fuselage 10 relative to the second fuselage 20 is unfolded that the first unfolded state is presented, that is, work as
When unmanned plane 100 is in state of flight, the first supporting part 31 by the way that the first horn 30 is arranged is held with the second of the second horn 40
The direction in load portion 41 is identical, can make to be mounted on the first supporting part 31 and the power plant on the second supporting part 41 towards phase
Together, even if the power traction direction of unmanned plane 100 is consistent, the flying quality of unmanned plane 100 can be effectively promoted, can also be saved
The consumed energy of flight.
In present embodiment, the power plant of unmanned plane 100 can be rotor assemblies, wherein the rotor assemblies include setting
The propeller set the motor on the first supporting part 31 and the second supporting part 41 and be arranged on motor.
Since the blade of propeller is longer, in order to further decrease overall volume of the unmanned plane 100 under non-state of flight,
Can be detachable paddle by Design of Propeller.
Optionally, unmanned plane 100 provided in an embodiment of the present invention further includes holder 60, and holder 60 can be arranged in the first machine
On body 10, it can also be arranged on the second fuselage 20；As shown in figure 4, when opposite second fuselage 20 expansion of the first fuselage 10 is presented the
When one unfolded state, holder 60 manifests dewiness state；As shown in Fig. 2, when the first fuselage 10 is relative to the second fuselage 20 rotation and the
When the fitting of two fuselages 20 is in first folded state, holder 60 is in hidden state.
In present embodiment, for example, holder 60 is arranged on the first fuselage 10, the second fuselage 20 then corresponds to holder 60 and is equipped with
The container of holder 60 is accommodated, is bonded in this way in first with the second fuselage 20 when the first fuselage 10 is rotated relative to the second fuselage 20
When folded state, holder 60 protrudes from the part of the first fuselage 10, can be housed in the container of the second fuselage 20, and in hidden
Tibetan state.
Similarly, when holder 60 is arranged on the second fuselage 20, the first fuselage 10 then corresponds to holder 60 and is equipped with receiving holder 60
Container, be bonded in this way with the second fuselage 20 in first folded state when the first fuselage 10 is rotated relative to the second fuselage 20
When, holder 60 protrudes from the part of the second fuselage 20, can be housed in the container of the first fuselage 10, and is in hidden state.
Optionally, unmanned plane 100 provided in an embodiment of the present invention further includes the first support portion 71 and the second support portion 72,
In, the first support portion 71 is arranged on the first fuselage 10, and the second support portion 72 is arranged on the second fuselage 20, wherein first
Support part 71 can be in " n " type, and the second support portion 72 can also be in " n " type.
When unmanned plane 100 rests in ground, the first support portion 71 and the second support portion 72 can play and unmanned plane are made
100 effect.
Specifically, when the first fuselage 10 relative to the second fuselage 20 is unfolded that the first unfolded state is presented, the first support portion
71 and second support portion 72 be in holding state；When the first support portion 71 and the second support portion 72 are in holding state,
First support portion 71 and 72 opposite unmanned plane 100 of the second support portion are arranged in " V " type, to play better supporting role.
When the first fuselage 10 is rotated relative to the second fuselage 20 to be bonded in first folded state with the second fuselage 20, first
Support portion 71 and the second support portion 72 are in hidden state.
In this way, when unmanned plane 100 is in non-state of flight, the first support portion 71 and the second support portion 72 can be distinguished
It is housed on the first fuselage 10 and the second fuselage 20, the first support portion 71 and the second support portion 72 is made to be in hidden state, from
And unmanned plane 100 can be further decreased in the overall volume in non-state of flight.
It should be noted that during the expansion of unmanned plane 100, first unclamp for fixing the first fuselage 10 and the second machine
The buckle structure 50 of body 20, and control the first fuselage 10 and rotated relative to the second fuselage 20, it is in the first unfolded state, it is preferred that can
To control the first fuselage 10 180 ° are rotated relative to the second fuselage 20；Then, the first horn 30 of control is rotated relative to the first fuselage 10,
It is rotated relative to the second fuselage 20 in the second unfolded state, and the second horn 40 of control, is in third unfolded state, shape is finally unfolded
State is as shown in Figure 1.
In the folding process of unmanned plane 100, the first horn 30 of first control control is rotated relative to the first fuselage 10, is in second
Folded state, and the second horn 40 of control are rotated relative to the second fuselage 20, are in third folded state；Then, it is controlled in control
First fuselage 10 is rotated relative to the second fuselage 20, is in first folded state, is finally engaged buckle structure 50, make the first fuselage 10 with
The fitting of second fuselage 20 is fixed, and final folded state is as shown in Figure 2.
In this way, when unmanned plane 100 is in non-state of flight, it can be by the way that 10 opposite second fuselage 20 of the first fuselage be pasted
It is in folded state to close, and the first horn 30 is made to be accommodated in the first accommodating space 11 of the first fuselage 10, and makes the second horn
40 are accommodated in the second accommodating space 21 of the second fuselage 20, to reduce the overall volume of unmanned plane.
The above description is merely a specific embodiment, but scope of protection of the present invention is not limited thereto, any
Those familiar with the art in the technical scope disclosed by the present invention, can easily think of the change or the replacement, and should all contain
Lid is within protection scope of the present invention.Therefore, protection scope of the present invention should be subject to the protection scope in claims.
Claims (13)
1. a kind of unmanned plane, which is characterized in that including the first fuselage, the second fuselage and for carrying power plant first
Horn and the second horn, wherein：
First horn is flexibly connected with first fuselage, is provided on first horn for installing the power dress
The first supporting part set；
Second horn is flexibly connected with second fuselage, is provided on second horn for installing the power dress
The second supporting part set；
First fuselage is flexibly connected with second fuselage, when the unmanned plane is in state of flight, first fuselage
It can be unfolded to be in the first unfolded state relative to second fuselage；When the unmanned plane is in non-state of flight, first machine
It is in first folded state that body, which can be rotated relative to second fuselage and is bonded with second fuselage,；
Wherein, first fuselage can be rotated relative to second fuselage, make first fuselage in the first unfolded state
Switch between first folded state.
2. unmanned plane according to claim 1, which is characterized in that when the unmanned plane is in state of flight, described first
Horn can be unfolded to be in the second unfolded state relative to first fuselage；It is described when the unmanned plane is in non-state of flight
First horn, which can be rotated and be collapsed relative to first fuselage, is presented the second folded state；First horn can be opposite
It is rotated in first fuselage, first horn is made to be cut between second unfolded state and second folded state
It changes；
When the unmanned plane is in state of flight, second horn can be unfolded to be unfolded in third relative to second fuselage
State；When the unmanned plane is in non-state of flight, second horn can rotate and collapse relative to second fuselage
Third folded state is presented；Second horn can be rotated relative to second fuselage, make second horn described
Switch between third unfolded state and the third folded state.
3. unmanned plane according to claim 2, which is characterized in that be provided on first fuselage and be presented for accommodating
First accommodating space of the first horn of eighty percent discount overlapping state；It is provided on second fuselage and third rugosity is presented for accommodating
Second accommodating space of the second horn of state.
4. unmanned plane according to claim 3, which is characterized in that the quantity of first horn be two, described first
The quantity of accommodating space is two；The quantity of second horn is two；The quantity of second accommodating space is two.
5. unmanned plane according to claim 4, which is characterized in that the flight coordinate-system of the unmanned plane includes roll
Axis, course axis and pitch axis, the roll axis and the first reference plane that plane where the pitch axis is the unmanned plane, it is described
Roll axis and the second reference plane that plane where the course axis is the unmanned plane；
Wherein, when the unmanned plane is in non-state of flight, first accommodating space institute opposite with second accommodating space
It states the first reference plane to be symmetrical arranged, relatively described second reference plane of two first accommodating spaces is symmetrical arranged, described two
Relatively described second reference plane of second accommodating space is symmetrical arranged.
6. unmanned plane according to claim 5, which is characterized in that when the unmanned plane is in non-state of flight, described
One horn is identical in the direction of roll axis direction as second horn in the direction of the roll axis direction.
7. unmanned plane according to claim 1, which is characterized in that first fuselage is unfolded relative to second fuselage
When the first unfolded state is presented, the first supporting part of first horn and the second supporting part of second horn are towards phase
Together；It is described when first fuselage is bonded with second fuselage in first folded state relative to second fuselage rotation
First supporting part of the first horn is opposite with the direction of the second supporting part of the second horn.
8. unmanned plane according to claim 1, which is characterized in that the unmanned plane further includes fuselage shaft, and described first
Fuselage is rotatablely connected by the fuselage shaft and second fuselage.
9. unmanned plane according to claim 1, which is characterized in that the unmanned plane further includes holder, the holder setting
On the first fuselage or the second fuselage；When the first unfolded state of presentation is unfolded relative to second fuselage in first fuselage
When, the holder, which is in, appears state, when first fuselage is pasted relative to second fuselage rotation with second fuselage
When closing in first folded state, the holder is in hidden state.
10. unmanned plane according to claim 1, which is characterized in that the unmanned plane further includes：First support portion and second
Support portion, wherein first support portion is arranged on the first fuselage, and second support portion is arranged on the second fuselage；
When first fuselage relative to second fuselage is unfolded that the first unfolded state is presented, first support portion and the
Two support portions are in holding state；
When first fuselage is rotated relative to second fuselage to be bonded in first folded state with second fuselage, institute
It states the first support portion and the second support portion is in hidden state.
11. unmanned plane according to claim 1, which is characterized in that the power plant is rotor assemblies.
12. unmanned plane according to claim 11, which is characterized in that the rotor assemblies include that setting is held described first
Motor on load portion and the second supporting part and the propeller being arranged on the motor.
13. unmanned plane according to claim 12, which is characterized in that the propeller is detachable paddle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109606610A (en) * | 2018-10-24 | 2019-04-12 | 浙江大年科技有限公司 | A kind of geometry folding unmanned plane |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN205554584U (en) * | 2016-02-22 | 2016-09-07 | 深圳市大疆创新科技有限公司 | Unmanned vehicles and frame thereof |
| CN205707370U (en) * | 2016-05-25 | 2016-11-23 | 江西科技学院 | Portable and collapsible unmanned plane |
| US20160340021A1 (en) * | 2015-01-04 | 2016-11-24 | Beijing Zero Zero Infinity Technology Co., Ltd | Foldable drone |
| CN205738048U (en) * | 2016-06-03 | 2016-11-30 | 任政威 | A kind of folding four rotor wing unmanned aerial vehicles |
| CN206407103U (en) * | 2016-12-19 | 2017-08-15 | 昊翔电能运动科技(昆山)有限公司 | Folding multi-rotor unmanned aerial vehicle |
| CN107097931A (en) * | 2017-05-11 | 2017-08-29 | 珠海天晴航空航天科技有限公司 | A kind of unmanned plane horn folding device |
| CN206664918U (en) * | 2017-04-14 | 2017-11-24 | 中博宇图信息科技有限公司 | A kind of unmanned machine frame of axle of novel foldable four |
-
2018
- 2018-02-13 CN CN201810149869.0A patent/CN108313259A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20160340021A1 (en) * | 2015-01-04 | 2016-11-24 | Beijing Zero Zero Infinity Technology Co., Ltd | Foldable drone |
| CN205554584U (en) * | 2016-02-22 | 2016-09-07 | 深圳市大疆创新科技有限公司 | Unmanned vehicles and frame thereof |
| CN205707370U (en) * | 2016-05-25 | 2016-11-23 | 江西科技学院 | Portable and collapsible unmanned plane |
| CN205738048U (en) * | 2016-06-03 | 2016-11-30 | 任政威 | A kind of folding four rotor wing unmanned aerial vehicles |
| CN206407103U (en) * | 2016-12-19 | 2017-08-15 | 昊翔电能运动科技(昆山)有限公司 | Folding multi-rotor unmanned aerial vehicle |
| CN206664918U (en) * | 2017-04-14 | 2017-11-24 | 中博宇图信息科技有限公司 | A kind of unmanned machine frame of axle of novel foldable four |
| CN107097931A (en) * | 2017-05-11 | 2017-08-29 | 珠海天晴航空航天科技有限公司 | A kind of unmanned plane horn folding device |
Non-Patent Citations (1)
| Title |
|---|
| 英童书坊编纂中心: "《百科大探秘 现代兵器大探秘》", 30 January 2017 * |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109606610A (en) * | 2018-10-24 | 2019-04-12 | 浙江大年科技有限公司 | A kind of geometry folding unmanned plane |
| CN109606610B (en) * | 2018-10-24 | 2022-03-11 | 浙江大年科技有限公司 | Unmanned aerial vehicle is folded to geometry |
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