CN207826581U - Unmanned vehicle - Google Patents
Unmanned vehicle Download PDFInfo
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- CN207826581U CN207826581U CN201721579885.0U CN201721579885U CN207826581U CN 207826581 U CN207826581 U CN 207826581U CN 201721579885 U CN201721579885 U CN 201721579885U CN 207826581 U CN207826581 U CN 207826581U
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- undercarriage
- horn
- unmanned vehicle
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- fuselage
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- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims description 17
- 238000013016 damping Methods 0.000 claims description 6
- 230000000712 assembly Effects 0.000 claims description 5
- 238000000429 assembly Methods 0.000 claims description 5
- 238000006243 chemical reaction Methods 0.000 claims description 3
- 238000005516 engineering process Methods 0.000 description 3
- 230000003190 augmentative effect Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000003287 optical effect Effects 0.000 description 2
- 230000000717 retained effect Effects 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 239000003814 drug Substances 0.000 description 1
- 229940079593 drug Drugs 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 239000013589 supplement Substances 0.000 description 1
- 230000000007 visual effect Effects 0.000 description 1
Classifications
-
- 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
- B64U60/40—Undercarriages foldable or retractable
Landscapes
- Engineering & Computer Science (AREA)
- Microelectronics & Electronic Packaging (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Accessories Of Cameras (AREA)
- Studio Devices (AREA)
Abstract
The utility model is related to unmanned vehicle technical fields, provide a kind of unmanned vehicle, including：One end of fuselage, horn, power plant, camera assembly and undercarriage, the horn is installed on the fuselage；The power plant is installed on the other end of the horn far from fuselage, the power for providing the unmanned vehicle flight；The undercarriage is installed on the other end of the horn far from the fuselage, and the camera assembly is fixed on the undercarriage, for shooting image.In the above manner, the camera in the camera assembly can be blocked to avoid by undercarriage, propeller and unmanned vehicle horn, so that the unmanned vehicle can carry out pan-shot.
Description
【Technical field】
The utility model is related to unmanned vehicle technical field more particularly to a kind of unmanned vehicles.
【Background technology】
Unmanned vehicle (UAV) is a kind of new concept equipment being in rapidly developing, with maneuverability, reaction
Quickly, unmanned, operation requires low advantage.Unmanned vehicle is by carrying multiclass sensor or picture pick-up device, Ke Yishi
Existing image real-time Transmission, high-risk areas detecting function are the strong supplements of satellite remote sensing and traditional air remote sensing.Currently, nobody
The use scope of aircraft has widened military affairs, scientific research, civilian three big field, specifically in power communication, meteorology, agricultural, sea
Ocean, he explores, photographs, preventing and reducing natural disasters, Crop Estimation, drug law enforcement anti-smuggling, border patrol, the fields application such as public security anti-terrorism it is very wide.
Current augmented reality (Augmented Reality, AR) and virtual reality (Virtual Reality, VR) technology
Development is swift and violent, also higher and higher for the demand of panoramic video shooting, is taken photo by plane using unmanned vehicle, is to obtain very
A kind of important way of the panoramic picture of real field scape.And in order to accurately obtain the image of multiple angles, fly when using nobody
When row device carries out panoramic shooting, unmanned vehicle camera mounted needs to avoid undercarriage, propeller and unmanned flight
Device horn blocks.
In the process of implementing the utility model, the inventor finds that the existing technology has at least the following problems：Existing
In unmanned vehicle, camera is hung on by holder below the fuselage of unmanned vehicle；Due to the camera shooting at the position
Head is blocked by undercarriage, propeller and unmanned vehicle horn, can not carry out panoramic shooting.
【Utility model content】
In order to solve the above-mentioned technical problem, the utility model embodiment provide it is a kind of can realize panoramic shooting nobody fly
Row device.
In order to solve the above technical problems, the utility model embodiment provides following technical scheme：
A kind of unmanned vehicle, including：Fuselage, horn, power plant, camera assembly and undercarriage, the one of the horn
End is installed on the fuselage；The power plant is installed on the other end of the horn far from the fuselage, described for providing
The power of unmanned vehicle flight；The undercarriage is installed on the other end of the horn far from the fuselage, the camera shooting group
Part is fixed on the undercarriage, for shooting image.
In some embodiments, the camera assembly includes holder and photographic device, and the holder carries the camera shooting dress
It sets, the holder is fixedly connected with the undercarriage.
In some embodiments, the holder includes：Holder, pitching spindle motor and roll spindle motor, the holder include
Pedestal and two linking arms, the pedestal are fixedly connected with the other end of the undercarriage far from the horn, two companies
The one end for connecing arm is fixedly connected with the pedestal, and the pitching spindle motor is installed on the linking arm far from the another of the pedestal
One end；The roll spindle motor is rotatablely connected with the pitching spindle motor.
In some embodiments, the pitching spindle motor is installed on one of them described linking arm far from the another of the pedestal
One end；The photographic device includes shell and camera lens module, and the shell is connect with the pitching spindle motor, and with described in two
The other end of another in linking arm is hinged, and the pitching spindle motor is for driving the shell around pitch axes；The cross
Roller motor is installed in the shell, and is connect with the camera lens module, and the roll spindle motor is for driving the camera lens
Module is dynamic around roll shaft rotation relative to the shell.
In some embodiments, the junction of the camera assembly and the fuselage is provided with damping device, described
Damping device includes the first connecting plate, shock-absorbing ball and the second connecting plate, and the shock-absorbing ball is set to first connecting plate and institute
It states between the second connecting plate；First connecting plate is fixedly connected with the lateral surface of the fuselage, second connecting plate and institute
Holder is stated to be fixedly connected.
In some embodiments, the other end of the horn far from the fuselage is provided with storage tank, the undercarriage
One end or the undercarriage can be all accommodated in the storage tank；The undercarriage includes main part and support portion,
One end of the support portion is connect with the main part, and the support portion is vertical with the main part；The undercarriage can
It is rotated relative to the horn, so that the undercarriage is converted between the first and second location status；The first position state
It is vertical with the horn for the main part of the undercarriage；The second position state be the undercarriage main part with it is described
Horn is parallel or on same straight line.
In some embodiments, the junction of the undercarriage and the horn is provided with driving device, the driving dress
It sets for driving the undercarriage to be rotated relative to the horn, so that the undercarriage is between the first and second location status
Conversion；The undercarriage includes main part and support portion, and one end of the support portion is connect with the main part, and the branch
Support part is vertical with the main part；The first position state is that the main part of the undercarriage is vertical with the horn；It is described
Second position state is that the main part of the undercarriage is parallel with the horn or on same straight line.
In some embodiments, the junction of the undercarriage and the horn is provided with position limiting structure, so that described
Undercarriage is positively retained at any one of first and second location status；The undercarriage includes main part and support portion, the support
The one end in portion is connect with the main part, and the support portion is vertical with the main part；The first position state is institute
The main part for stating undercarriage is vertical with the horn；The second position state is the main part of the undercarriage and the horn
It is parallel or on same straight line.
In some embodiments, one end of the support portion and the main part are hinged.
In some embodiments, the unmanned vehicle be quadrotor unmanned vehicle, the horn altogether there are four, it is described
There are four camera assembly is total, the camera assembly is corresponded with the horn；The line of four camera assemblies constitutes one
Rectangle.
In some embodiments, the camera assembly includes holder and photographic device, and the holder is fixedly connected on described
The other end of the horn far from the fuselage, the holder carry the photographic device.
Compared with prior art, a kind of unmanned vehicle of the utility model embodiment, including：Fuselage, horn, power
One end of device, camera assembly and undercarriage, the horn is installed on the fuselage；The power plant is installed on the horn
The other end far from the fuselage, the power for providing the unmanned vehicle flight；The undercarriage is installed on the machine
The other end of the arm far from the fuselage, the camera assembly is fixed on the undercarriage, for shooting image.By with top
Formula, the camera in the camera assembly can be blocked to avoid by undercarriage, propeller and unmanned vehicle horn, with
The unmanned vehicle is allow to carry out pan-shot.
【Description of the drawings】
One or more embodiments are illustrated by the picture in corresponding attached drawing, these exemplary theorys
The bright restriction not constituted to embodiment, the element with same reference numbers label is expressed as similar element in attached drawing, removes
Non- to have special statement, composition does not limit the figure in attached drawing.
Fig. 1 is a kind of structural schematic diagram for unmanned vehicle that one embodiment of the utility model provides；
Fig. 2 is the structural schematic diagram of camera assembly in unmanned vehicle shown in FIG. 1；
Fig. 3 is the exploded view of photographic device and roll spindle motor in camera assembly shown in Fig. 2；
Fig. 4 is the vertical view of unmanned vehicle shown in FIG. 1；
Fig. 5 is the side view of unmanned vehicle shown in FIG. 1, and the wherein unmanned vehicle is in first position state；
Fig. 6 is the side view of unmanned vehicle shown in FIG. 1, and the wherein unmanned vehicle is in second position state.
【Specific implementation mode】
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
Upper or placed in the middle there may be one or more therebetween elements.When an element is expressed " electrical connection " another element, it
It can be directly to another element or may exist one or more elements placed in the middle therebetween.This specification is made
The orientation or positional relationship of the instructions such as term "upper", "lower", "inner", "outside", " bottom " is orientation based on ... shown in the drawings
Or position relationship, be merely for convenience of describing the present invention and simplifying the description, do not indicate or imply the indicated device or
Element must have a particular orientation, with specific azimuth configuration and operation, therefore should not be understood as the limit to the utility model
System.In addition, term " first ", " second " " third " etc. are used for description purposes only, it is not understood to indicate or imply relatively heavy
The property wanted.
Unless otherwise defined, technical and scientific term all used in this specification and the skill for belonging to the utility model
The normally understood meaning of technical staff in art field is identical.Term used in the description of the utility model is intended merely to
The purpose for describing specific embodiment is not intended to limitation the utility model.Term "and/or" used in this specification includes
Any and all combinations of one or more relevant Listed Items.
In addition, as long as technical characteristic involved in the utility model difference embodiment disclosed below is each other not
Constituting conflict can be combined with each other.
As shown in Figure 1, a kind of unmanned vehicle 100 that one embodiment of the utility model provides, including：Fuselage 10, horn
20, one end of power plant 30, camera assembly 40 and undercarriage 50, the horn 20 is installed on the fuselage 10.The power
Device 30 is installed on the other end of the horn 20 far from the fuselage 10, for providing the flight of the unmanned vehicle 100
Power.The undercarriage 50 is installed on the other end of the horn 20 far from the fuselage 10, and the camera assembly 40 is fixed on
The undercarriage 50, for shooting image.Above-mentioned unmanned vehicle 100 can be rotor unmanned aircraft, fixed-wing nobody fly
The unmanned vehicle that row device or fixed-wing are mixed with rotor.Wherein, rotor unmanned aircraft is concretely：Single rotor nobody fly
Row device, DCB Specimen unmanned vehicle, three rotor unmanned aircrafts, quadrotor unmanned vehicle, six rotor unmanned aircrafts and eight
Rotor unmanned aircraft etc..
In the present embodiment, by taking the unmanned vehicle 100 is quadrotor unmanned vehicle as an example, to the unmanned vehicle
100 concrete structure is described in detail.
Specifically, the number of the horn 20 is four, one end of four horns 20 is fixed with the fuselage 10
Connection.The fuselage 10 and horn 20 are substantially in " ten " font, that is, non-conterminous two horns 20 are located at same straight line
On, and two adjacent horns 20 are mutually perpendicular to.
Specifically, the number of the power plant 30 is four, it is separate that the power plant 30 is installed on the horn 20
The other end of the fuselage 10, the power for providing the flight of the unmanned vehicle 100.Four power plants 30 and four
A horn 20 corresponds.The power plant 30 includes motor and propeller, and the motor is fixed on the horn 20
The other end far from the fuselage 10, the motor are connect with the propeller, and the propeller is driven to rotate.
Specifically, as shown in Fig. 2, the camera assembly 40 includes holder 41 and photographic device 42, the holder 41 carries
The photographic device 42 (is taken the photograph with the fixation for realizing photographic device 42 or the posture for arbitrarily adjusting photographic device 42 for example, changing
As the height of device 42, inclination angle and/or direction) and photographic device 42 is made to be stably held in the posture of setting.The camera shooting
Device 42 can be specifically：Camera, video camera, camera etc..The holder 41 can be uniaxial holder, twin shaft holder or three axis clouds
Platform.
The camera assembly 40 and the junction of the fuselage 10 are provided with damping device (not shown), the damping
Device includes the first connecting plate (not shown), shock-absorbing ball and the second connecting plate (not shown), and the shock-absorbing ball is set to described the
Between one connecting plate and the second connecting plate.First connecting plate is fixedly connected with the lateral surface of the fuselage 10, and described second
Connecting plate is fixedly connected with the holder 41.
In the present embodiment, there are four the camera assembly 40 is total to, the camera assembly 40 is a pair of with the horn 20 1
It answers.It is understood that in some other embodiment, the number of the camera assembly 40 can also be five or five with
On, wherein four camera assemblies 40 are corresponded with the horn 20, remaining camera assembly 40 can be according to the demand of actual conditions
And it is set to any position of unmanned vehicle 100.
There are four the undercarriage 50 is total, corresponded with the horn 20.One end of the undercarriage 50 with it is described
The other end of the horn 20 far from the fuselage 10 is hinged, and the other end of the undercarriage 50 is landing end, for it is described nobody
Machine 100 contacts when landing with ground.
As shown in Figures 2 and 3, in the present embodiment, the holder 41 is twin shaft holder.The holder 41 includes：Holder
411, pitching spindle motor 412 and roll spindle motor 413.The holder 411 is substantially U-shaped, including pedestal 4111 and two connections
One end of arm 4112, two linking arms 4112 is fixedly connected with the pedestal 4111, and the pitching spindle motor 412 only has
One, it is installed on the other end of one of them in two linking arms 4112.The roll spindle motor 413 and the pitching
Spindle motor 412 is rotatablely connected.
It is understood that in some other embodiment, the holder 41 includes two pitching spindle motors 412,
Each pitching spindle motor 412 is installed on the other end of a corresponding linking arm 4112.
The photographic device 42 includes shell 421 and camera lens module 422, the shell 421 and the pitching spindle motor 412
Connection, and it is hinged with another the other end in two linking arms 4112, and the pitching spindle motor 412 is described for driving
Shell 421 is around pitch axes.The roll spindle motor 413 is installed in the shell 421, and with the camera lens module 422
Connection, the roll spindle motor 413 is for driving the camera lens module 422 dynamic around roll shaft rotation relative to the shell 421.
As shown in figure 4, in the present embodiment, the line of four camera lens modules 422 constitutes an a rectangle (camera lens mould
Group 422 only with two adjacent 422 lines of camera lens module).Two camera lens moulds being located on two non-conterminous horns 20
The optical axis of group 422 is always positioned in same plane.The optical axis of two adjacent camera lens modules 422 is always positioned at orthogonal two
In a plane.Four camera lens modules 422 can cooperate and cooperate, to take around unmanned vehicle 100 360 degree
Panoramic picture.
The camera assembly 40 is set to the other end of the horn 20, may make camera assembly 40 that can preferably avoid
Undercarriage, propeller, horn and fuselage block so that camera assembly 40 can obtain larger range of scenery or image.This
Outside, four camera assemblies 40 can also jointly shoot same target, due to camera lens module 422 in four camera assemblies 40
Shooting angle it is different, therefore the image that four camera lens modules 422 shoot same target can be used for quickly carrying out above-mentioned target
3D modeling and/or drafting relief map etc..Based on above structure feature, may make the unmanned vehicle 100 engineering survey,
The fields such as mapping and disaster emergency rescue play a significant role.
As it can be seen in figures 5 and 6, one end of the undercarriage 50 and the other end of the horn 20 are hinged, the undercarriage 50
It is fixedly connected with the pedestal 4111 of the holder 41.The undercarriage 50 includes main part 51 and support portion 52, the support portion
52 one end is fixedly connected with the main part 51, and the support portion 52 is vertical with the main part 51.The support portion
52 support the unmanned vehicle 100 when landing for the unmanned vehicle 100.The undercarriage 50 can be relative to the machine
Arm 20 rotates, so that the undercarriage 50 is converted between two kinds of location status.The one of which position of the undercarriage 50
State (also referred to as first position state) is：The main part 51 of the undercarriage 50 is vertical with the horn 20；When described
When undercarriage 50 is in the position, the camera assembly 40 is located at the underface of the power plant 30, the camera assembly 40
In photographic device 42 can take the scene of the lower section of the unmanned vehicle 100 in all directions；But due to power plant 30
Positioned at the top of camera assembly 40, photographic device 42 is located at the scape of 100 top of the unmanned vehicle or oblique upper to shoot
As can then be blocked, can not be shot in all directions by power plant 30.Another location status of the undercarriage 50
(also referred to as second position state) is：The main part 51 of the undercarriage 50 is parallel with the horn 20 or in always
On line.When the undercarriage 50 is in the position, the camera assembly 40 is located at the horn 20 and is away from fuselage 10 most
At a distance, the camera assembly 40 is located at side of the power plant 30 far from the fuselage 10 at this time.The camera assembly 40
In photographic device 42 can take the scene of the unmanned vehicle 100 oblique upper and top in all directions；But camera shooting dress
42 scenes for being located at 100 lower section of the unmanned vehicle to shoot are set, then may be blocked by undercarriage on fuselage 10,
It can not be shot in all directions.In the present embodiment, the undercarriage 50 and the junction of the horn 20 are provided with limit
Structure (not shown), so that the undercarriage 50 is positively retained at any one of two kinds of location status.Using this, nobody flies
When row device 100, user manually can operate the undercarriage 50 according to use demand, to switch the location status of the undercarriage 50,
To change specific location of the camera assembly 40 on the horn 20, so that the camera assembly 40 can basis
The demand of actual photographed adjusts on better camera site, and has the better visual field.
It is understood that in some other embodiment, the undercarriage 50 includes main part 51 and support portion 52, institute
One end and the main part 51 for stating support portion 52 are hinged (that is, the support portion 52 can be relative to 51 rotary folding of the main part
Folded or expansion).When the undercarriage 50 is in first position state, the support portion 52 is rotated relative to the main part 51
It folds so that the support portion 52 is Chong Die with the main part 51.It is described when the undercarriage 50 is in second position state
Support portion 52 is unfolded relative to the main part 51 so that the support portion 52 is perpendicular to the main part 51.
It is understood that in some other embodiment, the other end of the horn 20, which is provided with storage tank, (schemes not
Show), one end of the undercarriage 50 or the undercarriage 50 are entirely located in the storage tank.The undercarriage 50 can phase
The horn 20 is rotated, so that the undercarriage 50 is converted between two kinds of location status.
It is understood that in some other embodiment, the undercarriage 50 and the junction of the horn 20 are arranged
There are driving device (not shown), the driving device to be used to that the undercarriage 50 to be driven to rotate relative to the horn 20, so that
The undercarriage 50 is obtained to convert between two kinds of location status.The driving device concretely motor, cylinder or pneumatic horse
It reaches.
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 there are many other variations of the different aspect of 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 understand that：Its still can with technical scheme described in the above embodiments is modified,
Or equivalent replacement of some of the technical features；And these modifications or replacements, do not make the sheet of corresponding technical solution
Matter is detached from the range of various embodiments of the utility model technical solution.
Claims (10)
1. a kind of unmanned vehicle (100), which is characterized in that including：Fuselage (10), horn (20), power plant (30), camera shooting
One end of component (40) and undercarriage (50), the horn (20) is installed on the fuselage (10)；Power plant (30) peace
The other end far from the fuselage (10) loaded on the horn (20), for providing the dynamic of the unmanned vehicle (100) flight
Power；The undercarriage (50) is installed on the other end of the horn (20) far from the fuselage (10), the camera assembly (40)
It is fixed on the undercarriage (50), for shooting image.
2. unmanned vehicle (100) according to claim 1, which is characterized in that
The camera assembly (40) includes holder (41) and photographic device (42), and the holder (41) carries the photographic device
(42), the holder (41) is fixedly connected with the undercarriage (50).
3. unmanned vehicle (100) according to claim 2, which is characterized in that
The holder (41) includes：Holder (411), pitching spindle motor (412) and roll spindle motor (413), the holder (411)
Including pedestal (4111) and two linking arms (4112), the pedestal (4111) is with the undercarriage (50) far from the horn
(20) the other end is fixedly connected, and one end of two linking arms (4112) is fixedly connected with the pedestal (4111), institute
State the other end that pitching spindle motor (412) is installed on the separate pedestal (4111) of the linking arm (4112)；The roll axis
Motor (413) is rotatablely connected with the pitching spindle motor (412).
4. unmanned vehicle (100) according to claim 3, which is characterized in that
It is another far from the pedestal (4111) that the pitching spindle motor (412) is installed on one of them described linking arm (4112)
End；
The photographic device (42) includes shell (421) and camera lens module (422), and the shell (421) is electric with the pitch axis
Machine (412) connects, and hinged with another the other end in two linking arms (4112), the pitching spindle motor (412)
For driving the shell (421) to be rotated around pitch axis (P)；The roll spindle motor (413) is installed on the shell (421)
It is interior, and connect with the camera lens module (422), the roll spindle motor (413) is for driving the camera lens module (422) opposite
It is rotated around roll axis (R) in the shell (421).
5. unmanned vehicle (100) according to claim 2, which is characterized in that
The junction of the camera assembly (40) and the fuselage (10) is provided with damping device, and the damping device includes first
Connecting plate, shock-absorbing ball and the second connecting plate, the shock-absorbing ball are set between first connecting plate and second connecting plate；
First connecting plate is fixedly connected with the lateral surface of the fuselage (10), second connecting plate and the holder (41)
It is fixedly connected.
6. unmanned vehicle (100) according to claim 1, which is characterized in that
The other end of the horn (20) far from the fuselage (10) is provided with storage tank, one end of the undercarriage (50) or
The undercarriage (50) can all be accommodated in the storage tank；
The undercarriage (50) includes main part (51) and support portion (52), one end and the main part of the support portion (52)
(51) it connects, and the support portion (52) is vertical with the main part (51)；
The undercarriage (50) can rotate relative to the horn (20), so that the undercarriage (50) is in the first and second position
It is converted between state；
The first position state is that the main part (51) of the undercarriage (50) is vertical with the horn (20)；
The second position state is that the main part (51) of the undercarriage (50) is parallel with the horn (20) or in same
On straight line.
7. unmanned vehicle (100) according to claim 1, which is characterized in that
The junction of the undercarriage (50) and the horn (20) is provided with driving device, and the driving device is for driving institute
It states undercarriage (50) to rotate relative to the horn (20), so that the undercarriage (50) is between the first and second location status
Conversion；
The undercarriage (50) includes main part (51) and support portion (52), one end and the main part of the support portion (52)
(51) it connects, and the support portion (52) is vertical with the main part (51)；
The first position state is that the main part (51) of the undercarriage (50) is vertical with the horn (20)；
The second position state is that the main part (51) of the undercarriage (50) is parallel with the horn (20) or in same
On straight line.
8. unmanned vehicle (100) according to claim 1, which is characterized in that
The undercarriage (50) and the junction of the horn (20) are provided with position limiting structure, so that the undercarriage (50) can
It is maintained at any one of first and second location status；
The undercarriage (50) includes main part (51) and support portion (52), one end and the main part of the support portion (52)
(51) it connects, and the support portion (52) is vertical with the main part (51)；
The first position state is that the main part (51) of the undercarriage (50) is vertical with the horn (20)；
The second position state is that the main part (51) of the undercarriage (50) is parallel with the horn (20) or in same
On straight line.
9. the unmanned vehicle (100) according to any one of claim 6-8, which is characterized in that
One end of the support portion (52) is hinged with the main part (51).
10. the unmanned vehicle (100) according to any one of claim 1-8, which is characterized in that
The unmanned vehicle (100) be quadrotor unmanned vehicle, the horn (20) altogether there are four, the camera assembly
(40) there are four altogether, the camera assembly (40) corresponds with the horn (20)；
The line of four camera assemblies (40) constitutes a rectangle.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721579885.0U CN207826581U (en) | 2017-11-22 | 2017-11-22 | Unmanned vehicle |
| PCT/CN2018/105660 WO2019100821A1 (en) | 2017-11-22 | 2018-09-14 | Unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721579885.0U CN207826581U (en) | 2017-11-22 | 2017-11-22 | Unmanned vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207826581U true CN207826581U (en) | 2018-09-07 |
Family
ID=63386667
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721579885.0U Active CN207826581U (en) | 2017-11-22 | 2017-11-22 | Unmanned vehicle |
Country Status (2)
| Country | Link |
|---|---|
| CN (1) | CN207826581U (en) |
| WO (1) | WO2019100821A1 (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2019100825A1 (en) * | 2017-11-22 | 2019-05-31 | 深圳市道通智能航空技术有限公司 | Unmanned aerial vehicle |
| WO2019100821A1 (en) * | 2017-11-22 | 2019-05-31 | 深圳市道通智能航空技术有限公司 | Unmanned aerial vehicle |
| CN109969384A (en) * | 2019-04-11 | 2019-07-05 | 西南交通大学 | The method of fixed-wing unmanned plane undercarriage conversion fixed fin |
| CN111476818A (en) * | 2020-02-28 | 2020-07-31 | 江苏理工学院 | Multi-camera low-altitude unmanned aerial vehicle target tracking device and tracking method |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN113602512A (en) * | 2021-07-30 | 2021-11-05 | 广西电网有限责任公司电力科学研究院 | Airborne binocular type power transmission line crossing point monitoring device and monitoring method thereof |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2017128317A1 (en) * | 2016-01-29 | 2017-08-03 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle and aerial photographing method for unmanned aerial vehicle |
| CN206407152U (en) * | 2016-12-22 | 2017-08-15 | 昊翔电能运动科技(昆山)有限公司 | The unmanned plane of servo driving head rotation |
| CN207631492U (en) * | 2017-11-22 | 2018-07-20 | 深圳市道通智能航空技术有限公司 | Unmanned vehicle |
| CN207826581U (en) * | 2017-11-22 | 2018-09-07 | 深圳市道通智能航空技术有限公司 | Unmanned vehicle |
| CN207631491U (en) * | 2017-11-22 | 2018-07-20 | 深圳市道通智能航空技术有限公司 | Unmanned vehicle |
-
2017
- 2017-11-22 CN CN201721579885.0U patent/CN207826581U/en active Active
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- 2018-09-14 WO PCT/CN2018/105660 patent/WO2019100821A1/en active Application Filing
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2019100825A1 (en) * | 2017-11-22 | 2019-05-31 | 深圳市道通智能航空技术有限公司 | Unmanned aerial vehicle |
| WO2019100821A1 (en) * | 2017-11-22 | 2019-05-31 | 深圳市道通智能航空技术有限公司 | Unmanned aerial vehicle |
| CN109969384A (en) * | 2019-04-11 | 2019-07-05 | 西南交通大学 | The method of fixed-wing unmanned plane undercarriage conversion fixed fin |
| CN111476818A (en) * | 2020-02-28 | 2020-07-31 | 江苏理工学院 | Multi-camera low-altitude unmanned aerial vehicle target tracking device and tracking method |
| CN111476818B (en) * | 2020-02-28 | 2024-02-27 | 江苏理工学院 | Low-altitude unmanned aerial vehicle target tracking device with multiple cameras and tracking method |
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| Publication number | Publication date |
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| WO2019100821A1 (en) | 2019-05-31 |
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