CN107585306A - A kind of unmanned vehicle - Google Patents
A kind of unmanned vehicle Download PDFInfo
- Publication number
- CN107585306A CN107585306A CN201710939715.7A CN201710939715A CN107585306A CN 107585306 A CN107585306 A CN 107585306A CN 201710939715 A CN201710939715 A CN 201710939715A CN 107585306 A CN107585306 A CN 107585306A
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- Prior art keywords
- unmanned vehicle
- fuselage
- horn
- component
- hinged
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- 230000000712 assembly Effects 0.000 claims abstract description 11
- 238000000429 assembly Methods 0.000 claims abstract description 11
- 238000009434 installation Methods 0.000 claims description 3
- 239000007787 solid Substances 0.000 claims description 2
- 230000001154 acute effect Effects 0.000 claims 1
- 230000000007 visual effect Effects 0.000 abstract description 5
- 230000003416 augmentation Effects 0.000 description 5
- 238000005516 engineering process Methods 0.000 description 2
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 210000003127 knee Anatomy 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
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- 238000006467 substitution reaction Methods 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U20/00—Constructional aspects of UAVs
- B64U20/80—Arrangement of on-board electronics, e.g. avionics systems or wiring
- B64U20/87—Mounting of imaging devices, e.g. mounting of gimbals
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
- B64U10/13—Flying platforms
- B64U10/14—Flying platforms with four distinct rotor axes, e.g. quadcopters
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U60/00—Undercarriages
- B64U60/50—Undercarriages with landing legs
Abstract
The present invention relates to aircraft field, there is provided a kind of unmanned vehicle includes：Fuselage, horn component, Power Component and the first camera assembly.The horn component is installed on the fuselage；The Power Component is installed on the horn component, for providing flying power for the unmanned vehicle；At least two first camera assemblies are respectively arranged in the horn component, and the opposite sides of the fuselage respectively sets at least one first camera assembly.During the unmanned vehicle flight of the present invention, at least two first camera assemblies positioned at the opposite sides of the fuselage can complete 360 degree of pan-shot jointly, ensure to get 360 degree of full-view image within the same time.At least two first camera assemblies are installed on the horn component so that its visual angle is open, will not be blocked by the fuselage or airborne equipment, can be achieved without dead angle pan-shot.
Description
【Technical field】
The present invention relates to aircraft field, more particularly to a kind of unmanned vehicle with shoot function.
【Background technology】
UAV, abbreviation unmanned vehicle (UAV), it is a kind of new ideas equipment being in developing rapidly, its
The advantages of low is required with maneuverability, rapid reaction, unmanned, operation.Unmanned vehicle is by carrying multiclass sensor
Or picture pick-up device, it is possible to achieve image real-time Transmission, high-risk areas detecting function be satellite remote sensing to be had with traditional air remote sensing
Power is supplemented.
In current unmanned vehicle, the conventional camera assembly visual angle for realizing pan-shot is narrower, easily by fuselage
Or other carrying equipments block, it is impossible to fully meet use demand.
【The content of the invention】
In order to solve the above-mentioned technical problem, the embodiment of the present invention provides a kind of achievable pan-shot and shooting visual angle is opened
Wealthy unmanned vehicle.
The embodiment of the present invention solves its technical problem and uses following technical scheme：
A kind of unmanned vehicle, including：Fuselage, horn component, Power Component and the first camera assembly.The horn group
Part is installed on the fuselage；The Power Component is installed on the horn component, for providing flight for the unmanned vehicle
Power；At least two first camera assemblies are respectively arranged in the horn component, and the opposite sides of the fuselage is respectively set
At least one first camera assembly.
Alternatively, each first camera assembly includes the first camera device, and first camera device is included at least
One camera lens.
Alternatively, first camera assembly includes mounting rod and the first head, and one end of the mounting rod is installed on institute
Horn component is stated, the other end of the mounting rod is removably installed in first head, the first camera device installation
In first head.
Alternatively, first head is three-axis stability augmentation head, including the first motor, the second motor and the 3rd motor；
The stator of 3rd motor is removably installed in the one end of the mounting rod away from the horn component, described
The stator of rotor the second motor of connection of 3rd motor, and the stator of the rotor of the second motor the first motor of connection, described first
Camera device is fixedly installed in the rotor of first motor.
Alternatively, the mounting rod is adjustable in length structure.
Alternatively, above-mentioned unmanned vehicle includes at least one second camera assembly, and second camera assembly is installed on
The fuselage；When the unmanned vehicle is in flight attitude, second camera assembly is located at the downside of the fuselage.
Alternatively, each second camera assembly includes the second head and the second camera device, and second head is consolidated
Dingan County is loaded on the fuselage, and second camera device is installed on second head.
Alternatively, the horn component includes drive component and horn；
One end of two horns is hinged, and two horns are located at the opposite sides of the fuselage respectively；
The drive component is installed on the fuselage, and the drive component is connected with two horns, for driving
Move two horns so that angle increase or reduction between two horns.
Alternatively, the drive component includes：Drive device, movable part and actuator；
The drive device is fixedly installed in the fuselage, for driving the movable part to do linear reciprocating motion；
The quantity of the actuator is two, and one end of one of them actuator is hinged one end of the movable part,
One end of another actuator is hinged the other end of the movable part, each actuator away from the movable part one
End is hinged a corresponding horn.
Alternatively, the drive component includes screw rod；
The drive device is connected with the screw rod, for driving the screw rod to rotate；
The movable part is sheathed on the screw rod, and can be done with the rotation of the screw rod along the axis of the screw rod past
Linear motion.
Alternatively, each actuator includes body, first connecting portion and second connecting portion；
Two first connecting portions are extended from the side of the body, the end of two first connecting portions
It is arranged at intervals, the end of two first connecting portions is hinged a corresponding horn；
Two second connecting portions are extended from the opposite side of the body, the end of two second connecting portions
End is arranged at intervals, and the end of two second connecting portions is located at the both sides of the movable part, and with one end of the movable part
It is be hinged.
Alternatively, each horn includes arm body and mounting seat；
The mounting seat is fixed in one end of the arm body；
Two mounting seats are hinged, and each be hinged one of the one end of the actuator away from the movable part is corresponding
The mounting seat.
Alternatively, the mounting seat includes tube body and articulated section；
One end of the arm body is inserted and fixed in the tube body；
Two articulated sections are extended from one end of the tube body, and the space from end of two articulated sections is set
Put, the end of the end of two articulated sections of one of them mounting seat and two articulated sections of another mounting seat is handed over
For overlapping, and the end of the articulated section of two mounting seats is hinged.
Alternatively, the horn component includes installing arm, the middle part machine corresponding with one of each installing arm
One end connection of the arm away from the fuselage；
Each camera assembly is installed on the middle part of a corresponding installing arm.
Alternatively, the horn component includes fix bar, and the fix bar includes the body of rod and connector, and the one of the body of rod
End is hinged the fuselage, and the other end of the body of rod is hinged one end of the connector, the other end be hinged one of the connector
The individual corresponding installing arm.
Alternatively, above-mentioned unmanned vehicle includes landing gear assembly, and the landing gear assembly includes land bar and support bar；
One end of the land bar is fixedly installed in the installing arm, in sharp between the land bar and the installing arm
Angle；
One end of the support bar is fixedly installed in the installing arm, and the other end of the support bar is fixedly installed in described
Land bar, and it is separated by default distance with the end of the land bar.
Compared with prior art, in the unmanned vehicle flight of the embodiment of the present invention, positioned at the relative of the fuselage
At least two first camera assemblies of both sides can complete 360 degree of pan-shot jointly, ensure to obtain within the same time
360 degree of full-view image is got, and then the 3-dimensional stereoscopic experience sense in virtual reality can be met.At least two first shootings
Component is installed on the horn component so that its visual angle is open, will not be blocked by the fuselage, can be achieved to clap without dead angle panorama
Take the photograph.
【Brief description of the drawings】
One or more embodiments are illustrative by corresponding accompanying drawing, these exemplary illustrations not structure
The restriction of paired embodiment, the element for having same reference numbers label in accompanying drawing is expressed as similar element, unless there are special
Declare, composition does not limit the figure in accompanying drawing.
Fig. 1 is a kind of stereogram for unmanned vehicle that a wherein embodiment of the invention provides；
Fig. 2 is the front view of the unmanned vehicle shown in Fig. 1；
Fig. 3 is stereogram of the fuselage with horn component of the unmanned vehicle shown in Fig. 1, wherein a part for the fuselage
It is omitted；
Fig. 4 is the side view of the fuselage shown in Fig. 3 and horn component；
Fig. 5 is along the sectional view of line A-A in Fig. 4；
Fig. 6 is the exploded view of the fuselage shown in Fig. 3 and horn component.
【Embodiment】
For the ease of understanding the present invention, below in conjunction with the accompanying drawings and specific embodiment, the present invention will be described in more detail.
It should be noted that when element is expressed " being fixed on " another element, it can directly on another element or therebetween
There may be one or more elements placed in the middle.When an element is expressed " connection " another element, it can directly be connected
It is connected to another element or there may be one or more elements placed in the middle therebetween.Term used in this specification is " vertical
", " horizontal ", "left", "right", " interior ", " outer " and similar statement for illustrative purposes only.
Unless otherwise defined, the technical field of all technologies used in this specification and scientific terminology with belonging to the present invention
The implication that is generally understood that of technical staff it is identical.It is specific to be intended merely to description for used term in the description of the invention
The purpose of embodiment, it is not intended to the limitation present invention.Term "and/or" used in this specification includes one or more related
Listed Items arbitrary and all combination.
In addition, as long as technical characteristic involved in invention described below difference embodiment is not formed each other
Conflict can be combined with each other.
Fig. 1 and Fig. 2, a kind of unmanned vehicle 100 that a wherein embodiment of the invention provides, including fuselage 10 are referred to,
Horn component 20, Power Component 30, the first camera assembly 40, the second camera assembly 50 and landing gear assembly 60.The horn
Component 20 is installed on the fuselage 10, and the Power Component 30 is installed on the horn component 20, for for the unmanned flight
Device 100 provides flying power, and two first camera assemblies 40 are respectively arranged in the horn component 20, and are located at the machine
The opposite sides of body 10, second camera assembly 50 are installed on the fuselage 10, and the landing gear assembly 60 is installed on described
Horn component 20.
Include the control circuit component being made up of electronic components such as MCU, the control circuit component bag in the fuselage 10
Include multiple control modules, e.g., for the control module for controlling the horn component 20 to pack up or put down, for control it is described nobody
The flight control modules of the flight attitude of aircraft 100, the locating module for the unmanned vehicle 100 that navigates and it is used for
Handle data processing module of the environmental information acquired in related airborne equipment etc..
Also referring to Fig. 3 to Fig. 5, the fuselage 10 opens up accepting groove 102, for horn component described in partial receipt
20。
The horn component 20 includes drive component 210, horn 220, fix bar 230 and installing arm 240.The driving group
Part 210 is arranged at the accepting groove 102 of the fuselage 10, and the drive component 210 is connected with the horn 220, to described
Horn 220 provides power, drives the horn 220 to pack up or put down.The horn 220 is connected with the installing arm 240, described
Installing arm 240 is used to install the Power Component 30, first camera assembly 40 and the landing gear assembly 60.It is described solid
The both ends of fixed pole 230 are respectively articulated with the fuselage 10 and the installing arm 240, for being applied to the horn 220 and installing arm 240
Add the pulling force towards the fuselage 10 so that the horn 220 stably can be packed up or put down.
The drive component 210 is installed on the fuselage 10.The drive component 210 includes：Drive device 212, screw rod
214, movable part 216 and actuator 218.The drive device 212 is fixedly installed in the fuselage 10, itself and the screw rod
214 connections, for driving the screw rod 214 to rotate.Described one end of screw rod 214 is fixedly connected with the rotating shaft of the drive device 212,
The other end is rotationally connected with the fuselage 10.The movable part 216 is sheathed on the screw rod 214, and can be with the screw rod 214
Rotation, do linear reciprocating motion along the axis of the screw rod 214.The quantity of the actuator 218 is two, one of institute
The one end for stating actuator 218 is hinged one end of the movable part 216, and one end of another actuator 218 is hinged the work
The other end of moving part 216.
In the present embodiment, the drive device 212 includes a motor, for driving the screw rod 214 to rotate, and then makes
The movable part 216 is obtained with the rotation of the screw rod 214, linear reciprocating motion is done along the axis of the screw rod 214.
It is understood that in some other embodiments, the screw rod 214 can omit, and the drive device 212 can
To be one kind in cylinder or hydraulic cylinder, the drive device 212 is connected with the movable part 216, for driving the activity
Part 216 does linear reciprocating motion.
The quantity of the horn 220 is two, has angle between two horns 220, two horns 220 divide
Not Wei Yu the fuselage 10 opposite sides.Each horn 220 includes arm body 222 and mounting seat 224, the arm body 222
One end be inserted and fixed in the mounting seat 224.Two mounting seats 224 are hinged, and each actuator 218 is remote
One end from the movable part 216 is hinged a corresponding mounting seat 224.It is described when the drive device 212 works
Drive device 212 drives the screw rod 214 to rotate, and drives axis of the movable part 216 along the screw rod 214 to do reciprocating linear
Motion, under the driving of the movable part 216, the actuator 218 drives two horns 220 to pack up or put down so that
Angle between two horns 220 is decreased or increased.
Referring to Fig. 6, each actuator 218 includes body 2180, first connecting portion 2182 and second connecting portion
2184.The first connecting portion 2182 is shaft-like, and two first connecting portions 2182 are prolonged from the side of the body 2180
Stretch, the space from end of two first connecting portions 2182 is set.Similarly, the second connecting portion 2184 is also bar
Shape, two second connecting portions 2184 are extended from the opposite side of the body 2180, two second connecting portions
2184 space from end is set.The end of two second connecting portions 2184 is located at the both sides of the movable part 216, and with institute
The one end for stating movable part 216 is hinged.
The mounting seat 224 includes tube body 2242, bearing pin 2244 and articulated section 2246.The tube body 2242 opens up
There is mounting hole (not shown), one end of the arm body 222 is inserted and fixed in the mounting hole.The quantity of the bearing pin 2244 is
Two, two bearing pins 2244 are fixedly installed in the opposite sides of the tube body 2242 respectively, each bearing pin 2244
The end of the first connecting portion 2182 corresponding with one is hinged so that the actuator 218 is articulated with the mounting seat
224.The 2246 have a generally triangular shape tabular of articulated section, quantity are two, and two articulated sections 2246 are from the tube body
2242 one end is extended, and the space from end of two articulated sections 2246 is set.The two of one of them mounting seat 224
The alternately stacked setting in end of the end of individual articulated section 2246 and two articulated sections 2246 of another mounting seat 224, and
And the end of the articulated section 2246 of two mounting seats 224 is hinged.
The fix bar 230 includes the body of rod 232 and connector 234, and one end of the body of rod 232 is hinged the fuselage 10,
The other end of the body of rod 232 is hinged one end of the connector 234, the be hinged peace dress of the other end of the connector 234
Arm 240.When unmanned vehicle 100 is in state of flight, the Power Component 30 is to the horn 220 away from the fuselage 10
One end and installing arm 240 upward pulling force is provided, the fix bar 230 provides direction to the horn 220 and installing arm 240
The pulling force of the fuselage 10, to prevent the horn 220 from further being rotated relative to the fuselage 10, so that the machine
Arm 220 is in stable state.
The quantity of the installing arm 240 is two, each installing arm 240 substantially straight-bar, its middle part and the machine
One end connection of the arm 220 away from fuselage 10.Two installing arms 240 are arranged in parallel in relative the two of the fuselage 10
Side.It is understood that in some other embodiments, the shape and set-up mode of the installing arm 240 can be according to reality
Changes in demand, for example, the installing arm 240 can be knee etc..
Referring back to Fig. 1 and Fig. 2, the Power Component 30 includes motor and is installed on the propeller of the motor, is used for
Flying power is provided for the unmanned vehicle 100.The quantity of the Power Component 30 is four, Power Component described in each two
30 are respectively arranged in the opposite end of the installing arm 240 corresponding to one.
It is understood that in some other embodiments, the quantity of the Power Component 30 can according to circumstances increase or
Reduce, for example, 6,8 etc. are reduced to 1,2 or increase to, for example, when the quantity of the Power Component 30 is two,
The installing arm 240 can be omitted, and each Power Component 30 can be fixedly installed in one of the horn 220 away from fuselage 10
End；For example, when the quantity of the Power Component 30 is 6,8, it can accordingly increase the horn 220 and the number of installing arm 240
Amount.
The quantity of first camera assembly 40 is two, and each first camera assembly 40 includes mounting rod 42, the
One head 44 and the first camera device 46.One end of the mounting rod 42 is fixedly installed in the middle part of the installing arm 240, institute
The other end for stating mounting rod 42 is removably installed in first head 44.The mounting rod 42 is adjustable in length structure,
For example, using stretching structure, to be adapted to various sizes of unmanned vehicle 100.
First head 44 is three-axis stability augmentation head, and the three-axis stability augmentation head is on three axles to described in in-flight
First camera device 46 increase surely：Course axle (Yaw), pitch axis (Pitch) and roll axis (Roll).The pitch axis is vertical
In roll axis, course axle is perpendicular to pitch axis and roll axis.
First head 44 includes：First motor, the second motor and the 3rd motor.The center of the rotor of first motor
Axle is coaxial with roll axis.The central shaft of the rotor of second motor and pitch axis are coaxial, and the central shaft of the rotor of the 3rd motor with
Course axle is coaxial.The stator of 3rd motor is removably installed in the mounting rod 42 away from the installing arm by fixed seat
240 one end, the rotor of the 3rd motor connects the stator of the second motor, and the rotor of the second motor connects determining for the first motor
Son.
It is understood that in some other embodiments, the 3rd motor can omit, and the stator of the second motor leads to
Cross the other end that fixed seat is removably installed in the mounting rod 42.
First camera device 46 is fixedly installed in the rotor of the first motor of the first head 44.The first shooting dress
Putting 46 can be first-class for camera, video camera, shooting, and it can include at least one camera lens, such as each first shooting dress
Putting 46 includes two backwards to the camera lens set.Two first camera devices 46 are generally aligned in the same plane.
It is understood that the quantity of first camera assembly 40 can be at least two, as long as the fuselage 10
Opposite sides respectively sets at least one camera assembly 40 to complete pan-shot.At least two first camera assemblies
40 the first camera device 46 is generally aligned in the same plane.
It is understood that in some other embodiments, first head 44 or single shaft head；Or institute
State the first head 44 to omit, first camera device 46 is directly mounted at the mounting rod 42.
Second camera assembly 50 includes the second head 54 and the second camera device 56, and second head 54 is installed on
The fuselage 10, second camera device 56 are installed on second head 54.In 100 flight of unmanned vehicle,
Second camera assembly 50 is located at the downside of the fuselage 10.
Second head 54 is three-axis stability augmentation head, and the three-axis stability augmentation head is on three axles to described in in-flight
Second camera device 56 increase surely：Course axle (Yaw), pitch axis (Pitch) and roll axis (Roll).The pitch axis is vertical
In roll axis, course axle is perpendicular to pitch axis and roll axis.
Second head 54 includes：First motor, the second motor and the 3rd motor.The center of the rotor of first motor
Axle is coaxial with roll axis.The central shaft of the rotor of second motor and pitch axis are coaxial, and the central shaft of the rotor of the 3rd motor with
Course axle is coaxial.The stator of 3rd motor is installed on the fuselage 10, the electricity of rotor connection second of the 3rd motor by fixed seat
The stator of machine, and the rotor of the second motor connects the stator of the first motor.It is understood that in some other embodiments,
3rd motor can omit, and the stator of the second motor is installed on the fuselage 10 by fixed seat.
Second camera device 56 is fixedly installed in the rotor of the first motor of second head 54.Described second takes the photograph
Picture device 56 can be first-class for camera, video camera, shooting, and it can include at least one camera lens, such as each described second takes the photograph
As device 56 includes two backwards to the camera lens set.
It is understood that the quantity of second camera assembly 50 is not limited to one, can be corresponding according to the actual requirements
Increase, such as 2 or 4 are increased to, 2 or 4 second camera assemblies 50 are all installed on the fuselage 10.
It is understood that in some other embodiments, second head 54 or single shaft head；Or institute
State the second head 54 to omit, second camera device 56 is directly mounted at the fuselage 10.
Referring back to Fig. 3 to Fig. 5, the landing gear assembly 60 includes land bar 602 and support bar 604.The land bar
602 one end is fixedly installed in one end of the installing arm 240, in sharp between the land bar 602 and the installing arm 240
Angle, one end of the support bar 604 are fixedly installed in the installing arm 240, and the other end of the support bar 604 is fixedly installed in
The land bar 602, and it is separated by default distance with the end of the land bar 602.Described in the support bar 604 and part
It is triangle to fall bar 602 and the part installing arm 240, in 100 land of unmanned vehicle, the undercarriage group
Part 60 can consolidate the support unmanned vehicle 100.
It is understood that in some other embodiments, the landing gear assembly 60 may also include drive device, described
Drive device can be cylinder or hydraulic cylinder, and it is installed on the installing arm 240, and one end of the support bar 604 is installed on described
Drive device, the other end are installed on the land bar 602, and one end of the land bar 602 is articulated with the installing arm 240.Make
Used time, the drive device can drive the support bar 604 for linear motion along the axis of its drive rod, described so as to drive
Fall bar 602 to rotate relative to the installing arm 240 so that the land bar 602 can be laid down or pack up.
In 100 flight of unmanned vehicle, positioned at two first shootings of the opposite sides of the fuselage 10
Component 40 can complete 360 degree of pan-shot jointly, ensure to get 360 degree of full-view image within the same time, and then
The 3-dimensional stereoscopic experience sense in virtual reality can be met.Two first camera assemblies 40 are installed on the horn component 20, its
Visual angle is open, will not be blocked by the fuselage 10 or carrying equipment, and can realize no dead angle pan-shot.
In addition, the mounting rod 42 is adjustable in length structure, the various sizes of unmanned vehicle can be adapted to
100。
Moreover, the drive component 210 can drive two horns 220 so that the folder between two horns 220
Angle increases or reduced, so as to can adjust the spacing between two first camera assemblies 40, to adapt to different photographing requests.
Finally it should be noted that：The above embodiments are merely illustrative of the technical solutions of the present invention, rather than its limitations；At this
Under the thinking of invention, it can also be combined between the technical characteristic in above example or different embodiments, step can be with
Realized with random order, and many other changes of the different aspect of the present invention as described above be present, for simplicity, they do not have
Have and provided in details；Although the present invention is described in detail with reference to the foregoing embodiments, the ordinary skill people of this area
Member should be understood：It can still modify to the technical scheme described in foregoing embodiments, or to which part skill
Art feature carries out equivalent substitution；And these modifications or replacement, the essence of appropriate technical solution is departed from each reality of the present invention
Apply the scope of a technical scheme.
Claims (16)
- A kind of 1. unmanned vehicle (100), it is characterised in that including：Fuselage (10)；Horn component (20), the horn component (20) are installed on the fuselage (10)；Power Component (30), the Power Component (30) are installed on the horn component (20), for for the unmanned vehicle (100) flying power is provided；First camera assembly (40), at least two first camera assemblies (40) are respectively arranged in the horn component (20), The opposite sides of the fuselage (10) respectively sets at least one first camera assembly (40).
- 2. unmanned vehicle (100) according to claim 1, it is characterised in that each first camera assembly (40) Including the first camera device (46), first camera device (46) includes at least one camera lens.
- 3. unmanned vehicle (100) according to claim 2, it is characterised in that first camera assembly (40) includes Mounting rod (42) and the first head (44), one end of the mounting rod (42) are installed on the horn component (20), the installation The other end of bar (42) is removably installed in first head (44), and first camera device (46) is installed on described One head (44).
- 4. unmanned vehicle (100) according to claim 3, it is characterised in that first head (44) increases for three axles Steady head, including the first motor, the second motor and the 3rd motor；The stator of 3rd motor is removably installed in the one end of the mounting rod (42) away from the horn component (20), The rotor of 3rd motor connects the stator of the second motor, and the rotor of the second motor connects the stator of the first motor, described First camera device (46) is fixedly installed in the rotor of first motor.
- 5. the unmanned vehicle (100) according to claim 3 or 4, it is characterised in that the mounting rod (42) is that length can Adjust structure.
- 6. the unmanned vehicle (100) according to any one of claim 1 to 5, it is characterised in that including at least one second Camera assembly (50), second camera assembly (50) are installed on the fuselage (10)；It is in the unmanned vehicle (100) During flight attitude, second camera assembly (50) is located at the downside of the fuselage (10).
- 7. unmanned vehicle (100) according to claim 6, it is characterised in that each second camera assembly (50) Including the second head (54) and the second camera device (56), second head (54) is installed on the fuselage (10), and described Two camera devices (56) are installed on second head (54).
- 8. the unmanned vehicle (100) according to any one of claim 1 to 7, it is characterised in that the horn component (20) Including drive component (210) and horn (220)；One end of two horns (220) is hinged, and two horns (220) are located at the phase of the fuselage (10) respectively To both sides；The drive component (210) is installed on the fuselage (10), and the drive component (210) and two horns (220) connect, for driving two horns (220) so that the angle between two horns (220) increases or subtracted It is small.
- 9. unmanned vehicle (100) according to claim 8, it is characterised in that the drive component (210) includes：Drive Dynamic device (212), movable part (216) and actuator (218)；The drive device (212) is fixedly installed in the fuselage (10), for driving the movable part (216) to do reciprocating linear Motion；The quantity of the actuator (218) is two, and one end of one of them actuator (218) is hinged the movable part (216) one end, one end of another actuator (218) are hinged the other end of the movable part (216), each drive The one end of moving part (218) away from the movable part (216) is hinged a corresponding horn (220).
- 10. unmanned vehicle (100) according to claim 9, it is characterised in that the drive component (210) includes spiral shell Bar (214)；The drive device (212) is connected with the screw rod (214), for driving the screw rod (214) to rotate；The movable part (216) is sheathed on the screw rod (214), and can be with the rotation of the screw rod (214), along the screw rod (214) axis does linear reciprocating motion.
- 11. the unmanned vehicle (100) according to claim 9 or 10, it is characterised in that each actuator (218) Including body (2180), first connecting portion (2182) and second connecting portion (2184)；Two first connecting portions (2182) are extended from the side of the body (2180), two first connections The space from end in portion (2182) is set, and the end of two first connecting portions (2182) is hinged a corresponding horn (220)；Two second connecting portions (2184) are extended from the opposite side of the body (2180), and two described second connect The space from end of socket part (2184) is set, and the end of two second connecting portions (2184) is located at the movable part (216) Both sides, and be hinged with one end of the movable part (216).
- 12. unmanned vehicle (100) according to claim 9, it is characterised in that each horn (220) includes arm Body (222) and mounting seat (224)；The mounting seat (224) is fixed in one end of the arm body (222)；Two mounting seats (224) are hinged, each one end of the actuator (218) away from the movable part (216) It is hinged a corresponding mounting seat (224).
- 13. unmanned vehicle (100) according to claim 12, it is characterised in that the mounting seat (224) includes body Portion (2242) and articulated section (2246)；One end of the arm body (222) is inserted and fixed in the tube body (2242)；Two articulated sections (2246) are extended from one end of the tube body (2242), two articulated sections (2246) Space from end set, the ends of two articulated sections (2246) of one of them mounting seat (224) and another described peace Fill the alternately stacked setting in end of two articulated sections (2246) of seat (224), and the hinge of two mounting seats (224) The end of socket part (2246) is hinged.
- 14. the unmanned vehicle (100) according to claim any one of 8-13, it is characterised in that the horn component (20) installing arm (240) is included, the middle part horn (220) corresponding with one of each installing arm (240) is away from institute State one end connection of fuselage (10)；One camera assembly (40) is installed on the middle part of a corresponding installing arm (240).
- 15. unmanned vehicle (100) according to claim 14, it is characterised in that the horn component (20) includes solid Fixed pole (230), the fix bar (230) include the body of rod (232) and connector (234), and one end of the body of rod (232) is hinged institute State fuselage (10), the other end of the body of rod (232) is hinged one end of the connector (234), the connector (234) it is another One end is hinged a corresponding installing arm (240).
- 16. the unmanned vehicle (100) according to claims 14 or 15, it is characterised in that including landing gear assembly (60), The landing gear assembly (60) includes land bar (602) and support bar (604)；One end of the land bar (602) is fixedly installed in the installing arm (240), the land bar (602) and the installation It is at an acute angle between arm (240)；One end of the support bar (604) is fixedly installed in the installing arm (240), and the other end of the support bar (604) is consolidated Dingan County is loaded on the land bar (602), and is separated by default distance with the end of the land bar (602).
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710939715.7A CN107585306A (en) | 2017-09-30 | 2017-09-30 | A kind of unmanned vehicle |
| PCT/CN2018/086725 WO2019062139A1 (en) | 2017-09-30 | 2018-05-14 | Unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710939715.7A CN107585306A (en) | 2017-09-30 | 2017-09-30 | A kind of unmanned vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107585306A true CN107585306A (en) | 2018-01-16 |
Family
ID=61052921
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710939715.7A Pending CN107585306A (en) | 2017-09-30 | 2017-09-30 | A kind of unmanned vehicle |
Country Status (2)
| Country | Link |
|---|---|
| CN (1) | CN107585306A (en) |
| WO (1) | WO2019062139A1 (en) |
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| WO2019062139A1 (en) * | 2017-09-30 | 2019-04-04 | 深圳市道通智能航空技术有限公司 | Unmanned aerial vehicle |
| CN110341947A (en) * | 2019-06-25 | 2019-10-18 | 武汉科技大学 | A kind of quadrotor that multidirectional can be verted |
| CN112995516A (en) * | 2019-05-30 | 2021-06-18 | 深圳市道通智能航空技术股份有限公司 | Focusing method and device, aerial camera and unmanned aerial vehicle |
| CN113335496A (en) * | 2021-06-19 | 2021-09-03 | 国网浙江省电力有限公司浦江县供电公司 | Be applied to unmanned aerial vehicle horn subassembly that electric power cruises |
| CN113335516A (en) * | 2021-06-19 | 2021-09-03 | 国网浙江省电力有限公司浦江县供电公司 | Be applied to unmanned aerial vehicle that electric power cruises |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| WO2023144994A1 (en) * | 2022-01-28 | 2023-08-03 | 三共木工株式会社 | Aircraft and method for manufacturing aircraft |
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| WO2019062139A1 (en) | 2019-04-04 |
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