CN207417151U - A kind of unmanned vehicle - Google Patents
A kind of unmanned vehicle Download PDFInfo
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- CN207417151U CN207417151U CN201721295313.XU CN201721295313U CN207417151U CN 207417151 U CN207417151 U CN 207417151U CN 201721295313 U CN201721295313 U CN 201721295313U CN 207417151 U CN207417151 U CN 207417151U
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- unmanned vehicle
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Abstract
The utility model is related to aircraft fields, and providing 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 utility model, 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, it can be achieved that without dead angle pan-shot.
Description
【Technical field】
The utility model is related to aircraft field more particularly to a kind of unmanned vehicles with shooting function.
【Background technology】
UAV, abbreviation unmanned vehicle (UAV) are a kind of new concept equipments being in rapidly developing,
Have the advantages that maneuverability, rapid reaction, it is unmanned, operation require it is low.Unmanned vehicle is by carrying multiclass sensor
Or picture pick-up device, it can realize image real-time Transmission, high-risk areas detecting function, be satellite remote sensing and traditional air remote sensing has
Power is supplemented.
In current unmanned vehicle, the camera assembly visual angle of common realization pan-shot is relatively narrow, easily by fuselage
Or other carrying equipments block, it is impossible to fully meet use demand.
【Utility model content】
In order to solve the above-mentioned technical problem, the utility model embodiment provides a kind of achievable pan-shot and shoots and regards
The open unmanned vehicle in angle.
The utility model embodiment solves its technical problem using 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.
Optionally, each first camera assembly includes the first photographic device, and first photographic device is included at least
One camera lens.
Optionally, first camera assembly includes mounting rod and the first holder, 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 holder, the first photographic device installation
In first holder.
Optionally, first holder is three-axis stability augmentation holder, 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
Photographic device is fixedly installed in the rotor of first motor.
Optionally, the mounting rod is adjustable in length structure.
Optionally, 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.
Optionally, each second camera assembly includes the second holder and the second photographic device, and second holder is consolidated
Dingan County is loaded on the fuselage, and second photographic device is installed on second holder.
Optionally, 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 driving component is installed on the fuselage, and the driving component is connected with two horns, for driving
Move two horns so that the angle between two horns increases or reduces.
Optionally, the driving component includes：Driving device, movable part and actuator；
The driving device is fixedly installed in the fuselage, for the movable part to be driven 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
The hinged corresponding horn in end.
Optionally, the driving component includes screw rod；
The driving device is connected with the screw rod, for the screw rod to be driven 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.
Optionally, each actuator includes body part, first connecting portion and second connecting portion；
Two first connecting portions are extended from the one side of the body part, the end of two first connecting portions
It is arranged at intervals, the end of two first connecting portions is hinged a corresponding horn；
The opposite side of two second connecting portions from the body parts extends, 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 hinged.
Optionally, each horn includes arm body and mounting base；
The mounting base is fixed in one end of the arm body；
Two mounting bases are hinged, and each hinged one of the one end of the actuator away from the movable part is corresponding
The mounting base.
Optionally, the mounting base 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
It puts, the end of two articulated sections of one of them mounting base and the end of two articulated sections of another mounting base are handed over
For overlapping, and the end of the articulated section of two mounting bases is hinged.
Optionally, 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；
One first camera assembly is installed on the middle part of a corresponding installing arm.
Optionally, the horn component include fixed link, the fixed link include the body of rod and connector, the one of the body of rod
The hinged fuselage in end, the other end of the body of rod are hinged one end of the connector, the other end hinged one of the connector
A corresponding installing arm.
Optionally, above-mentioned unmanned vehicle includes landing gear assembly, and the landing gear assembly includes land bar and supporting rod；
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 supporting rod is fixedly installed in the installing arm, and the other end of the supporting rod 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 utility model embodiment, positioned at the fuselage
At least two first camera assemblies of opposite sides can complete 360 degree of pan-shot jointly, ensure in the same time
360 degree of full-view image is inside got, and then the 3-dimensional stereoscopic experience sense in virtual reality can be met.At least two described first
Camera assembly is installed on the horn component so that its visual angle is open, will not be blocked by the fuselage, it can be achieved that without dead angle panorama
Shooting.
【Description of the drawings】
One or more embodiments are illustrated by corresponding attached drawing, these exemplary illustrations not structure
The restriction of paired embodiment, the element for having same reference numbers label in attached drawing is expressed as similar element, unless there are special
It declares, composition does not limit the figure in attached drawing.
Fig. 1 is a kind of stereogram for unmanned vehicle that the utility model wherein embodiment provides；
Fig. 2 is the front view of unmanned vehicle shown in FIG. 1；
Fig. 3 is stereogram of the fuselage with horn component of unmanned vehicle shown in FIG. 1, wherein a part for the fuselage
It is omitted；
Fig. 4 is the side view of 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 fuselage shown in Fig. 3 and horn component.
【Specific embodiment】
For the ease of understanding the utility model, in the following with reference to the drawings and specific embodiments, the utility model is carried out more detailed
Thin explanation.It should be noted that when element is expressed " being fixed on " another element, it can be directly in another element
Above or therebetween there may be one or more elements placed in the middle.When an element is expressed " connection " another element, it can
To be directly to another element or there may be one or more elements placed in the middle therebetween.This specification is used
Term " vertical ", " horizontal ", "left", "right", " interior ", " outer " and similar statement for illustrative purposes only.
Unless otherwise defined, technology of all technical and scientific terms used in this specification with belonging to the utility model
The normally understood meaning of technical staff in field is identical.It is intended merely to retouch in the term used in the description of the utility model
The purpose of specific embodiment is stated, is not intended to limitation the utility model.Term "and/or" used in this specification includes one
The arbitrary and all combination of a or multiple relevant Listed Items.
In addition, as long as technical characteristic involved in the utility model difference embodiment disclosed below is each other not
Forming conflict can be combined with each other.
It please refers to Fig.1 and Fig. 2, a kind of unmanned vehicle 100 that the utility model wherein embodiment provides, including fuselage
10, horn component 20, Power Component 30, the first camera assembly 40, the second camera assembly 50 and landing gear assembly 60.It is described
Horn component 20 is installed on the fuselage 10, and the Power Component 30 is installed on the horn component 20, for for it is described nobody
Aircraft 100 provides flying power, and two first camera assemblies 40 are respectively arranged in the horn component 20, and positioned at institute
The opposite sides of fuselage 10 is stated, second camera assembly 50 is installed on the fuselage 10, and the landing gear assembly 60 is installed on
The horn component 20.
Include the control circuit component being made of electronic components such as MCU, the control circuit component bag in the fuselage 10
Include multiple control modules, e.g., for controlling the control module that the horn component 20 is packed up or put down, for control it is described nobody
The flight control modules of 100 flight attitude of aircraft, for the unmanned vehicle 100 that navigates locating module and be used for
Data processing module of environmental information acquired in the related airborne equipment of processing etc..
Also referring to Fig. 3 to Fig. 5, the fuselage 10 opens up container 102, for horn component described in partial receipt
20。
The horn component 20 includes drive component 210, horn 220, fixed link 230 and installing arm 240.The driving group
Part 210 is arranged at the container 102 of the fuselage 10, and the driving component 210 is connected with the horn 220, to described
Horn 220 provides power, and the horn 220 is driven 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 the horn 220 and installing arm 240
Apply the pulling force towards the fuselage 10 so that the horn 220 steadily can be packed up or put down.
The driving component 210 is installed on the fuselage 10.The driving component 210 includes：Driving device 212, screw rod
214, movable part 216 and actuator 218.The driving device 212 is fixedly installed in the fuselage 10, with the screw rod
214 connections, for the screw rod 214 to be driven to rotate.Described 214 one end of screw rod is fixedly connected with the shaft of the driving 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 driving device 212 includes a motor, for the screw rod 214 to be driven to rotate, and then
So that rotation of the movable part 216 with 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 be omitted, the driving device 212 can
To be one kind in cylinder or hydraulic cylinder, the driving 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 base 224, the arm body 222
One end be inserted and fixed in the mounting base 224.Two mounting bases 224 are hinged, and each actuator 218 is remote
One end from the movable part 216 is hinged a corresponding mounting base 224.It is described when the driving device 212 works
Driving device 212 drives the screw rod 214 to rotate, and the axis of the movable part 216 along the screw rod 214 is driven to do back and forth directly
Line moves, and under the driving of the movable part 216, the actuator 218 drives two horns 220 to pack up or put down, and makes
The angle obtained between two horns 220 is decreased or increased.
Referring to Fig. 6, each actuator 218 includes body part 2180, first connecting portion 2182 and second connecting portion
2184.The first connecting portion 2182 is rod-shaped, and two first connecting portions 2182 are prolonged from the one side of the body part 2180
It stretches, the space from end of two first connecting portions 2182 is set.Similarly, the second connecting portion 2184 is also bar
Shape, the opposite side of two second connecting portions 2184 from the body parts 2180 extend, 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 base 224 includes tube body 2242, axis 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 axis pin 2244 is
Two, two axis pins 2244 are fixedly installed in the opposite sides of the tube body 2242 respectively, each axis 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 base
224.The 2246 have a generally triangular shape plate 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 base 224
The alternately stacked setting in end of the end of a articulated section 2246 and two articulated sections 2246 of another mounting base 224, and
And the end of the articulated section 2246 of two mounting bases 224 is hinged.
The fixed link 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, and the other end of the connector 234 hingedly pacifies the dress
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 fixed link 230 provides direction to the horn 220 and installing arm 240
The pulling force of the fuselage 10, the horn 220 to be prevented further to be rotated compared with the fuselage 10, so that described
Horn 220 is in stable state.
The quantity of the installing arm 240 is two, each installing arm 240 substantially straight-bar, 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 opposite 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 curved bar 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 a corresponding installing arm 240.
It is understood that in some other embodiments, the quantity of the Power Component 30 can according to circumstances increase or
It reduces, 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 holder 44 and the first photographic 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 holder 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 holder 44 is three-axis stability augmentation holder, and the three-axis stability augmentation holder is on three axis to described in in-flight
First photographic device 46 increase steady：Course axis (Yaw), pitch axis (Pitch) and roll axis (Roll).The pitch axis is vertical
In roll axis, course axis is perpendicular to pitch axis and roll axis.
First holder 44 includes：First motor, the second motor and the 3rd motor.The center of the rotor of first motor
Axis 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 axis 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 be omitted, 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 photographic device 46 is fixedly installed in the rotor of the first motor of the first holder 44.The first camera shooting dress
It can be camera, video camera, camera etc. to put 46, can include at least one camera lens, such as each first camera shooting dress
Putting 46 includes two backwards to the camera lens set.Two first photographic 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 that pan-shot can be completed.At least two first camera assemblies
40 the first photographic device 46 is generally aligned in the same plane.
It is understood that in some other embodiments, first holder 44 or uniaxial holder；Alternatively, institute
It states the first holder 44 to omit, first photographic device 46 is directly mounted at the mounting rod 42.
Second camera assembly 50 includes the second holder 54 and the second photographic device 56, and second holder 54 is installed on
The fuselage 10, second photographic device 56 are installed on second holder 54.In 100 flight of unmanned vehicle,
Second camera assembly 50 is located at the downside of the fuselage 10.
Second holder 54 is three-axis stability augmentation holder, and the three-axis stability augmentation holder is on three axis to described in in-flight
Second photographic device 56 increase steady：Course axis (Yaw), pitch axis (Pitch) and roll axis (Roll).The pitch axis is vertical
In roll axis, course axis is perpendicular to pitch axis and roll axis.
Second holder 54 includes：First motor, the second motor and the 3rd motor.The center of the rotor of first motor
Axis 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 axis is coaxial.The stator of 3rd motor is installed on the fuselage 10, the second electricity of rotor connection 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 be omitted, and the stator of the second motor is installed on the fuselage 10 by fixed seat.
Second photographic device 56 is fixedly installed in the rotor of the first motor of second holder 54.Described second takes the photograph
Picture device 56 can be camera, video camera, camera etc., 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, it can be corresponding according to actual demand
Increase, such as increase to 2 or 4,2 or 4 second camera assemblies 50 are all installed on the fuselage 10.
It is understood that in some other embodiments, second holder 54 or uniaxial holder；Alternatively, institute
It states the second holder 54 to omit, second photographic 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 supporting rod 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 supporting rod 604 are fixedly installed in the installing arm 240, and the other end of the supporting rod 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 supporting rod 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 driving device, described
Driving device can be cylinder or hydraulic cylinder, be installed on the installing arm 240, and one end of the supporting rod 604 is installed on described
Driving 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 driving device can drive the supporting rod 604 for linear motion along the axis of its drive rod, described so as to drive
Fall bar 602 to rotate compared with 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 camera 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,
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 driving component 210 can drive two horns 220 so that between two horns 220
Angle increases or reduces, will to adapt to different shootings so as to can adjust the spacing between two first camera assemblies 40
It asks.
Finally it should be noted that：Above example is only to illustrate the technical solution of the utility model, rather than its limitations；
Under the thinking of the utility model, it can also be combined between the technical characteristic in above example or different embodiments,
Step can be realized with random order, and many other variations of the different aspect there are the utility model as described above, be
Simplicity, they do not provide in details；Although the utility model is described in detail with reference to the foregoing embodiments, this
The those of ordinary skill in field should be understood：It can still modify to the technical solution recorded in foregoing embodiments,
Or equivalent substitution is carried out to which part technical characteristic；And these are changed or are replaced, and do not make the sheet of appropriate technical solution
Matter departs from the scope of various embodiments of the utility model technical solution.
Claims (16)
1. a kind of unmanned vehicle (100), which is characterized 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, which is characterized in that each first camera assembly (40)
Including the first photographic device (46), first photographic device (46) includes at least one camera lens.
3. unmanned vehicle (100) according to claim 2, which is characterized in that first camera assembly (40) includes
Mounting rod (42) and the first holder (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 holder (44), and first photographic device (46) is installed on described
One holder (44).
4. unmanned vehicle (100) according to claim 3, which is characterized in that first holder (44) increases for three axis
Steady holder, 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 photographic device (46) is fixedly installed in the rotor of first motor.
5. unmanned vehicle (100) according to claim 3, which is characterized in that the mounting rod (42) is adjustable for length
Whole structure.
6. unmanned vehicle (100) according to claim 1, which is characterized in that including at least one second camera assembly
(50), second camera assembly (50) is installed on the fuselage (10)；Flight attitude is in the unmanned vehicle (100)
When, second camera assembly (50) is located at the downside of the fuselage (10).
7. unmanned vehicle (100) according to claim 6, which is characterized in that each second camera assembly (50)
Including the second holder (54) and the second photographic device (56), second holder (54) is installed on the fuselage (10), and described
Two photographic devices (56) are installed on second holder (54).
8. unmanned vehicle (100) according to any one of claims 1 to 7, which is characterized 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 driving component (210) is installed on the fuselage (10), and the driving component (210) and two horns
(220) connect, for driving two horns (220) so that the angle between two horns (220) increases or subtracts
It is small.
9. unmanned vehicle (100) according to claim 8, which is characterized in that the driving component (210) includes：It drives
Dynamic device (212), movable part (216) and actuator (218)；
The driving device (212) is fixedly installed in the fuselage (10), for the movable part (216) to be driven to do reciprocating linear
Movement；
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, which is characterized in that the driving component (210) includes spiral shell
Bar (214)；
The driving device (212) is connected with the screw rod (214), for the screw rod (214) to be driven 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. unmanned vehicle (100) according to claim 9, which is characterized in that each actuator (218) includes
Body part (2180), first connecting portion (2182) and second connecting portion (2184)；
Two first connecting portions (2182) are extended from the one side of the body part (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)；
The opposite side of two second connecting portion (2184) from the body parts (2180) extends, 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, which is characterized in that each horn (220) includes arm
Body (222) and mounting base (224)；
The mounting base (224) is fixed in one end of the arm body (222)；
Two mounting bases (224) are hinged, each one end of the actuator (218) away from the movable part (216)
A hinged corresponding mounting base (224).
13. unmanned vehicle (100) according to claim 12, which is characterized in that the mounting base (224) includes tube 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 base (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 bases (224)
The end of socket part (2246) is hinged.
14. unmanned vehicle (100) according to claim 8, which is characterized in that the horn component (20) includes installation
Arm (240), the separate fuselage (10) of the middle part horn (220) corresponding with one of each installing arm (240)
One end connects；
One first camera assembly (40) is installed on the middle part of a corresponding installing arm (240).
15. unmanned vehicle (100) according to claim 14, which is characterized in that the horn component (20) includes solid
Fixed pole (230), the fixed link (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. unmanned vehicle (100) according to claim 14, which is characterized in that described including landing gear assembly (60)
Landing gear assembly (60) includes land bar (602) and supporting rod (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 supporting rod (604) is fixedly installed in the installing arm (240), and the other end of the supporting rod (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).
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107585306A (en) * | 2017-09-30 | 2018-01-16 | 深圳市道通智能航空技术有限公司 | A kind of unmanned vehicle |
| CN108839810A (en) * | 2018-06-20 | 2018-11-20 | 智飞智能装备科技东台有限公司 | A kind of mapping unmanned flight's machine |
| WO2024021640A1 (en) * | 2022-07-29 | 2024-02-01 | 深圳市大疆创新科技有限公司 | Control method and apparatus, aircraft, mobile platform, and storage medium |
| WO2024077523A1 (en) * | 2022-10-12 | 2024-04-18 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle |
-
2017
- 2017-09-30 CN CN201721295313.XU patent/CN207417151U/en active Active
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107585306A (en) * | 2017-09-30 | 2018-01-16 | 深圳市道通智能航空技术有限公司 | A kind of unmanned vehicle |
| 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 |
| CN108839810A (en) * | 2018-06-20 | 2018-11-20 | 智飞智能装备科技东台有限公司 | A kind of mapping unmanned flight's machine |
| WO2024021640A1 (en) * | 2022-07-29 | 2024-02-01 | 深圳市大疆创新科技有限公司 | Control method and apparatus, aircraft, mobile platform, and storage medium |
| WO2024077523A1 (en) * | 2022-10-12 | 2024-04-18 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle |
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