CN108100243A - Unmanned vehicle and its rack - Google Patents
Unmanned vehicle and its rack Download PDFInfo
- Publication number
- CN108100243A CN108100243A CN201711403687.3A CN201711403687A CN108100243A CN 108100243 A CN108100243 A CN 108100243A CN 201711403687 A CN201711403687 A CN 201711403687A CN 108100243 A CN108100243 A CN 108100243A
- Authority
- CN
- China
- Prior art keywords
- fuselage
- drive shaft
- motor
- component
- drive
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 238000009434 installation Methods 0.000 claims description 4
- 241000237858 Gastropoda Species 0.000 claims description 2
- 238000010586 diagram Methods 0.000 description 3
- 230000003416 augmentation Effects 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 239000010687 lubricating oil Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 239000013589 supplement Substances 0.000 description 1
Classifications
-
- 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
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Microelectronics & Electronic Packaging (AREA)
- Toys (AREA)
- Accessories Of Cameras (AREA)
- Studio Devices (AREA)
Abstract
The present invention relates to aircraft fields, provide a kind of unmanned vehicle and its rack, and the rack includes fuselage, fuselage drive component and horn component.The fuselage drive component is installed on the fuselage.The horn component is connected to the fuselage drive component, and the fuselage drive component can drive the fuselage compared with described 360 degree of rotations of horn component.In the present invention, the fuselage drive component can drive the fuselage compared with described 360 degree of rotations of horn component, so as to 360 degree of rotations of camera assembly that the unmanned vehicle is driven to be carried, so that the camera assembly can adjust operating position and angle as needed, so as to fulfill multi-angled shooting.
Description
【Technical field】
The present invention relates to aircraft field more particularly to a kind of unmanned vehicles and its rack 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 carries multiclass by holder and passes
Sensor or photographic device can realize image real-time Transmission, high-risk areas detecting function, be satellite remote sensing and traditional air remote sensing
Strong supplement.
Inventor has found that holder is usually mounted to the lower section of unmanned vehicle fuselage, cloud in the implementation of the present invention
The operating angle of platform can be restricted, and the photographic device that holder is carried is only used for horizontal or shoots obliquely so that takes the photograph
As the shooting angle of device is restricted.
【The content of the invention】
In order to solve the above-mentioned technical problem, the embodiment of the present invention provides a kind of rotatable unmanned vehicle of fuselage and its machine
Frame so that the picture shooting assembly that the unmanned vehicle is carried can realize multi-angled shooting.
The embodiment of the present invention solves its technical problem using following technical scheme：
A kind of rack, which is characterized in that including：Fuselage, fuselage drive component and horn component.The fuselage driving group
Part is installed on the fuselage.The horn component is connected to the fuselage drive component, and the fuselage drive component can drive institute
Fuselage is stated compared with described 360 degree of rotations of horn component.
Optionally, the fuselage drive component includes motor, worm screw, worm gear and drive shaft；
The motor is fixedly installed in the fuselage；
The worm screw and the rotation axis connection of the motor, the central axes of the worm screw turn with the rotation axis of the motor
Shaft line overlaps；
The worm gear set is arranged on the drive shaft, the worm gear and the worm engaging；
The both ends of the drive shaft are movably installed in the fuselage respectively, and the drive shaft can turn compared with the fuselage
Dynamic, the horn component is fixedly connected on the drive shaft；
During the motor operations, the motor and the worm screw can together around the worm gear and the drive shaft turns, from
And the fuselage is driven to be rotated around the drive shaft compared with the horn component.
Optionally, the outer surface of the worm screw has the first helical teeth tooth；
The outer surface of the worm gear has the second helical teeth tooth, and the first helical teeth tooth is engaged with the second helical teeth tooth.
Optionally, the worm gear is hollow cylindrical, and central axes are vertical but non-intersect with the pivot center.
Optionally, the central axes of the drive shaft are vertical but non-intersect with the pivot center.
Optionally, the fuselage drive component includes motor, the first helical gear, the second helical gear and drive shaft；
The motor is fixedly installed in the fuselage；
First helical gear is fixedly installed in the rotation axis of the motor；
Second helical gear is sheathed on the drive shaft, and first helical gear is engaged with second helical gear；
The both ends of the drive shaft are movably installed in the fuselage respectively, and the drive shaft can turn compared with the fuselage
Dynamic, the horn component is fixedly connected on the drive shaft；
During the motor operations, the motor and first helical gear can be together around the drive shaft turns, so as to band
The fuselage is moved to rotate compared with the horn component around the drive shaft.
Optionally, the central axes of the drive shaft are vertical with the pivot center of the rotation axis of the motor and intersect.
Optionally, first helical gear includes the first circular conical surface, the rotation axis of first circular conical surface and the motor
The angle of pivot center be 45 degree, first circular conical surface is equipped with teeth；
Second helical gear includes the second circular conical surface, second circular conical surface and the angle of the central axes of the drive shaft
For 45 degree, second circular conical surface is equipped with teeth, and the teeth of first circular conical surface are engaged with the teeth of second circular conical surface.
Optionally, the fuselage drive component includes motor, the first spur gear, the second spur gear and drive shaft；
The motor is fixedly installed in the fuselage；
First spur gear is fixedly installed in the rotation axis of the motor；
Second spur gear is sheathed on the drive shaft, and first spur gear is engaged with second spur gear；
The drive shaft and the rotation axis of the motor are arranged in parallel, and the both ends of the drive shaft are movably installed in institute respectively
Fuselage is stated, the drive shaft can be rotated compared with the fuselage, and the horn component is fixedly connected on the drive shaft；
During the motor operations, the motor and first spur gear can be together around the drive shaft turns, so as to band
The fuselage is moved to rotate compared with the horn component around the drive shaft.
Optionally, the fuselage drive component includes bearing block, and two bearing blocks are fixedly installed in the fuselage, institute
The both ends for stating drive shaft are movably installed in two bearing blocks respectively, and the drive shaft can be rotated compared with the bearing block.
Optionally, set in each bearing block there are one bearing, the bearing holder (housing, cover) is arranged on the drive shaft.
The embodiment of the present invention solves its technical problem and also uses following technical scheme：
A kind of unmanned vehicle, including：Motor, propeller, camera assembly and above-described rack, the motor peace
Loaded on the horn, the propeller is installed on the motor, and the camera assembly is installed on the fuselage.
Optionally, two horn components are symmetrically arranged in the opposite sides of the fuselage, and fixed peace respectively
Both ends loaded on the drive shaft.
Optionally, each horn component includes host arm and linking arm, in each horn component, the master
One end of horn is fixedly installed in one end of the drive shaft, and two linking arms are commonly connected to the host arm away from institute
State the other end of drive shaft, the host arm and two linking arm composition Y-shapeds；
The each one end of the linking arm away from the host arm is installed by one motor.
Optionally, each horn component includes host arm, and there are one the motors for the host arm installation.
Compared with prior art, in the unmanned vehicle of the embodiment of the present invention and its rack, the fuselage driving group
Part is installed on the fuselage, and the fuselage drive component is connected with the horn component, can drive the fuselage compared with described
360 degree of rotations of horn component, so as to 360 degree of rotations of camera assembly that the unmanned vehicle is driven to be carried so that described
Camera assembly can adjust operating position and angle as needed, so as to fulfill multi-angled 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 a wherein embodiment of the invention provides；
Fig. 2 is the stereogram of another angle of unmanned vehicle shown in FIG. 1；
Fig. 3 and Fig. 4 is respectively the stereogram of the another angle of unmanned vehicle shown in FIG. 1, wherein the unmanned flight
A part for the fuselage of device is omitted；
Fig. 5 is the partial enlarged view of part A in Fig. 4；
Fig. 6 is the assembling schematic diagram of the fuselage drive component of unmanned vehicle shown in FIG. 1；
Fig. 7 is the assembling schematic diagram of fuselage drive component described in some embodiments of the invention；
Fig. 8 is the assembling schematic diagram of fuselage drive component described in other embodiments of the invention.
【Specific embodiment】
For the ease of understanding the present invention, in the following with reference to the drawings and specific embodiments, 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, technical and scientific term all used in this specification is led with belonging to the technology of the present invention
The normally understood meaning of technical staff in domain is identical.It is specific to be intended merely to description for used term in the description of the invention
Embodiment purpose, be not intended to limitation the present invention.Term "and/or" used in this specification includes one or more phases
The arbitrary and all combination of the Listed Items of pass.
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.
It please refers to Fig.1 to Fig.3, a kind of unmanned vehicle 100 that a wherein embodiment of the invention provides, including fuselage 10,
Fuselage drive component 20, horn component 30, motor 40, propeller 50 and camera assembly 60.The fuselage drive component 20 is pacified
Loaded in the fuselage 10, the fuselage drive component 20 is connected with the horn component 30, for driving 10 phase of fuselage
360 degree of rotations are done for the horn component 30.The motor 40 is installed on the horn component 30, and the propeller 50 is installed
In the motor 40, the motor 40 provides power for the propeller 50 to be driven to rotate, for the unmanned vehicle 100.
The camera assembly 60 is installed on the fuselage 10, for captured image.
Include the control circuit component being made of electronic components such as MCU, the control circuit component bag in the fuselage 10
Multiple control modules are included, e.g., for the fuselage drive component 20 to be controlled to drive the fuselage 10 compared with the horn component
30 control modules rotated, for the motor 40 to be controlled to work to control the flight of 100 flight attitude of unmanned vehicle
Control module, for the locating module for the unmanned vehicle 100 that navigates and for handling acquired in related airborne equipment
Data processing module of environmental information etc..The embodiment of the present invention for convenience of description, attached drawing are only shown and phase of the embodiment of the present invention
The component of pass.
Also referring to Fig. 4 to Fig. 6, the fuselage drive component 20 includes motor 202, worm screw 203, worm gear 204, driving
Axis 205 and bearing block 206.
The motor 202 is fixedly installed in the fuselage 10, and rotation axis is connected with the worm screw 203, and the horse
Pivot center O up to 202 rotation axis is overlapped with the central axes of the worm screw 203.The motor 202 is used to drive the worm screw
203 rotate around the pivot center O.
The worm screw 203 is cylinder, and outer surface has the first helical teeth tooth 2032, for coordinating with the worm gear 204.
The worm gear 204 is hollow cylindrical, and central axes and the pivot center O are vertical but non-intersect.The worm gear
204 outer surface has the second helical teeth tooth 2042, and the first helical teeth tooth 2032 is engaged with the second helical teeth tooth 2042.It is described
Worm gear 204 is sheathed on the drive shaft 205.
The drive shaft 205 passes through the worm gear 204, and central axes are overlapped with the central axes of the worm gear 204, the drive
The central axes of moving axis 205 are also vertical but non-intersect with the pivot center O.
The quantity of the bearing block 206 is two, is fixedly installed in the opposite sides of the fuselage 10 respectively.It is each described
It is set in bearing block 206 there are one bearing 2062, the both ends of the drive shaft 205 are each passed through the corresponding bearing
2062, and the outside of the fuselage 10 is exposed to, for connecting the horn component 30.The drive shaft 205 can be compared with described
Bearing 2062 rotates.
It is understood that in some other embodiments, the bearing block 206 can be omitted, the drive shaft 205
Both ends are directly movably installed in the fuselage 10, and lubricating oil can be added between the both ends of the drive shaft 205 and the fuselage 10,
So that the drive shaft 205 can be rotated swimmingly compared with the fuselage 10.
The quantity of the horn component 30 is two, and two horn components 30 are respectively arranged in the drive shaft 205
Both ends.Each horn component 30 includes host arm 302 and linking arm 304, described in each horn component 30
One end of host arm 302 is fixedly installed in one end of the drive shaft 205, and two linking arms 304 are commonly connected to described
The other end of the host arm 302 away from the drive shaft 205, the host arm 302 and two linking arms 304 form Y-shaped.
Two horn components 30 of 10 opposite sides of fuselage are symmetrically distributed in altogether there are four the linking arm 304, wherein two
A linking arm 304 is located at the one side of the fuselage 10, and linking arm 304 described in another two is located at the another of the fuselage 10
Side.The each one end of the linking arm 304 away from the host arm 302 is installed by the motor 40.
In the present embodiment, the quantity of the horn component 30 is two, is symmetrically arranged in the phase of the fuselage 10
To both sides, and the both ends of the drive shaft 205 are fixedly installed in respectively.The quantity of the motor 40 is four, four electricity
Machine 40 is generally aligned in the same plane, and is located at square four apex angle respectively.
It is understood that in some other embodiments, the quantity of the horn component 30 is alternatively one, the drive
One end of moving axis 205 is fixedly connected with the horn component 30, and the other end passes through the corresponding bearing 2062.
Each motor 40 corresponds to installation, and there are one the propellers 50.In the present embodiment, each horn group
Part 30 includes two linking arms 304, and there are one the motor 40 and a spirals for each installation of linking arm 304
Paddle 50 namely unmanned vehicle provided in this embodiment 100 include four propellers 50, are quadrotor unmanned vehicle.
It is understood that in some other embodiments, the linking arm 304 can be omitted, each host arm
302 are mounted directly that there are one the motor 40 and a propellers 50 namely the unmanned vehicle 100 to include two institutes
State propeller 50.
Referring back to Fig. 1 and Fig. 2, the picture shooting assembly 60 is installed on the fuselage 10, is filled including holder 602 and shooting
Put 604.
The holder 602 carries the filming apparatus 604.The holder 602 be three-axis stability augmentation holder, the three-axis stability augmentation
Holder to the photographic device 604 in-flight increase steady on three axis：Course axis (Yaw), pitch axis (Pitch) and is turned over
Roller bearing (Roll).The pitch axis is perpendicular to roll axis, and course axis is perpendicular to pitch axis and roll axis.
The holder 602 includes：First motor, the second motor and the 3rd motor.The central shaft of the rotor of first motor
It is coaxial with roll axis.The central shaft of the rotor of second motor and pitch axis are coaxial, and the central shaft and boat of the rotor of the 3rd motor
It is coaxial to axis.The stator of 3rd motor is removably installed in the fuselage 10, the rotor connection of the 3rd motor by fixed seat
The stator of second motor, and the rotor of the second motor connects the stator of the first motor.
It is understood that in some other embodiments, the 3rd motor can be omitted, and the stator of the second motor leads to
It crosses fixed seat and is removably installed in the fuselage 10.
The holder 602 is removably installed in the fuselage 10 by fixed seat, can facilitate the camera assembly 60
It replaces.The holder 602 can be removably installed in the fuselage 10 by structures such as buckle, screw threads.
In the present embodiment, in 100 flight of unmanned vehicle, the holder 602 is located under the fuselage 10
Side, it is to be understood that in some other implementations, the holder 602 can be mounted on the fuselage 10 according to actual demand
Any position.
The photographic device 604 is fixedly installed in the rotor of the first motor of the holder 602.The photographic device 604
It can be camera, video camera, camera etc., at least one camera lens can be included, such as each photographic device 604 includes
Two backwards to the camera lens set.
It is understood that in some other embodiments, the holder 602 or uniaxial holder；Alternatively, the cloud
Platform 602 omits, and the photographic device 604 is directly mounted at the fuselage 10.
In the unmanned vehicle 100 in use, the motor 40 works, the propeller 50 is driven to rotate, is described
Unmanned vehicle 100 provides flying power.In 100 flight of unmanned vehicle, the camera assembly 60 can be located at institute
The lower section of fuselage 10 is stated, to horizontally or obliquely direction being descended to shoot.It is described when needing to shoot the top of fuselage 10
Unmanned vehicle 100 controls the motor 202 to work, and the rotation axis of the motor 202 drives the worm screw 203, is the snail
Wheel 204 and drive shaft 205 provide rotary power.Since the horn component 30 is fixedly connected on the drive shaft 205, the spiral shell
Rotation paddle 50 provides the thrust opposite with the direction of rotation of the drive shaft 205 for the horn component 30 so that the drive shaft
205 and worm gear 204 remain stationary as.In the case where the drive shaft 205 and worm gear 204 remain stationary as, the first helical teeth tooth
2032 engage with the second helical teeth tooth 2042, and the rotary power that the motor 202 provides causes the worm screw 203 and motor
202 rotate around the worm gear 204 and drive shaft 205, so that the fuselage 10 can do 180 degree rotation, the camera assembly
60 are located at the top of the fuselage 10, upward direction can be shot, without being blocked by the fuselage 10.Similarly, the machine
Body 10 can do 360 degree of rotations, can arbitrarily adjust operating position and the angle of the camera assembly 60.
Referring to Fig. 7, in some embodiments, the worm screw 203 in the fuselage drive component 20 can be replaced by first
Helical gear 203a, the worm gear 204 can be replaced by the second helical gear 204a.The first helical gear 203a is fixedly installed in institute
State the rotation axis of motor 202, the first helical gear 203a include the first circular conical surface 2032a, the first circular conical surface 2032a with
The angle of the pivot center O of the rotation axis of the motor 202 is 45 degree, and the first circular conical surface 2032a is equipped with teeth.Described
Two helical gear 204a are sheathed on the drive shaft 205, and the second helical gear 204a includes the second circular conical surface 2042a, and described the
Two circular conical surface 2042a and the angle of the central axes of the drive shaft 205 are 45 degree, and the second circular conical surface 2042a is equipped with teeth,
The teeth of the first circular conical surface 2032a are engaged with the teeth of the second circular conical surface 2042a.The axis of the drive shaft 205
Line is vertical with the pivot center O and intersects, and the first helical gear 203a is engaged with the second helical gear 204a.The horse
Up to during 202 work, the drive shaft 205 and the second helical gear 204a are remained stationary as, and the motor 202 and described first is tiltedly
Gear 203a is rotated around the drive shaft 205, and the fuselage 10 is driven to be rotated around the drive shaft 205.
Referring to Fig. 8, in further embodiments, the worm screw 203 in the fuselage drive component 20 can be replaced by
One spur gear 203b, the worm gear 204 can be replaced by the second spur gear 204b.The rotation axis of the motor 202 can with it is described
Drive shaft 205 is arranged in parallel, and the first spur gear 203b is fixedly installed in the rotation axis of the motor 202, and described second is straight
Gear 204b is sheathed on the drive shaft 205, and the first spur gear 203b is engaged with the second spur gear 204b, the horse
Up to during 202 work, the drive shaft 205 and the second spur gear 204b are remained stationary as, and the motor 202 and described first is directly
Gear 203b is rotated around the drive shaft 205, and the fuselage 10 is driven to be rotated around the drive shaft 205.
It is understood that in some other embodiments, the fuselage drive component 20 or belt transmission, i.e. institute
The rotation axis and the drive shaft 205 for stating motor 202 are arranged in parallel, and the rotation axis of the motor 202 passes through belt and the drive
Moving axis 205 connects；Alternatively, the fuselage drive component 20 can also use other kinds of drive, as long as the machine can be driven
Body 10 rotates 360 degree compared with the drive shaft 205 and the horn component 30.
In the present embodiment, the fuselage drive component 20 is installed on the fuselage 10, the fuselage drive component 20 with
The horn component 30 connects, and the fuselage 10 can be driven to do 360 degree of rotations compared with the horn component 30, so as to drive
The camera assembly 60 does 360 degree of rotations so that and the camera assembly 60 can adjust operating position and angle as needed, so as to
Realize multi-angled shooting.
Another embodiment of the present invention also provides a kind of rack, and the fuselage 10 including above-described embodiment, the fuselage drive
Dynamic component 20 and horn component 30.The fuselage drive component 20 is installed in the fuselage 10, the fuselage drive component
20 are connected with the horn component 30, for the fuselage 10 to be driven to do 360 degree of rotations compared with the horn component 30.
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
It under the thinking of invention, can also be combined between the technical characteristic in above example or different embodiment, step can be with
It is realized with random order, and there are many other variations of different aspect present invention as described above, 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 field
Member should be understood：It can still modify to the technical solution recorded 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 not made to depart from each reality of the present invention
Apply the scope of a technical solution.
Claims (15)
1. a kind of rack, which is characterized in that including：
Fuselage (10)；
Fuselage drive component (20) is installed on the fuselage (10)；
Horn component (30), is connected to the fuselage drive component (20), and the fuselage drive component (20) can drive described
Fuselage (10) is compared with described (30) 360 degree of rotations of horn component.
2. rack according to claim 1, which is characterized in that the fuselage drive component (20) includes motor (202), snail
Bar (203), worm gear (204) and drive shaft (205)；
The motor (202) is fixedly installed in the fuselage (10)；
The worm screw (203) and the rotation axis connection of the motor (202), central axes and the motor of the worm screw (203)
(202) pivot center (O) of rotation axis overlaps；
The worm gear (204) is sheathed on the drive shaft (205), and the worm gear (204) is engaged with the worm screw (203)；
The both ends of the drive shaft (205) are movably installed in the fuselage (10) respectively, and the drive shaft (205) can be compared with institute
Fuselage (10) rotation is stated, the horn component (30) is fixedly connected on the drive shaft (205)；
During motor (202) work, the motor (202) and the worm screw (203) can be together around the worm gear (204) and institutes
Drive shaft (205) rotation is stated, so as to drive the fuselage (10) around the drive shaft (205) compared with the horn component (30)
It rotates.
3. rack according to claim 2, which is characterized in that the outer surface of the worm screw (203) has the first helical teeth tooth
(2032)；
The outer surface of the worm gear (204) has the second helical teeth tooth (2042), the first helical teeth tooth (2032) and described second
Helical teeth tooth (2042) engages.
4. the rack according to Claims 2 or 3, which is characterized in that the worm gear (204) be hollow cylindrical, axis
Line and the pivot center (O) are vertical but non-intersect.
5. according to claim 2 to 4 any one of them rack, which is characterized in that the central axes of the drive shaft (205) and institute
It is vertical but non-intersect to state pivot center (O).
6. rack according to claim 1, which is characterized in that the fuselage drive component (20) includes motor (202), the
One helical gear (203a), the second helical gear (204a) and drive shaft (205)；
The motor (202) is fixedly installed in the fuselage (10)；
First helical gear (203a) is fixedly installed in the rotation axis of the motor (202)；
Second helical gear (204a) is sheathed on the drive shaft (205), first helical gear (203a) and described second
Helical gear (204a) engages；
The both ends of the drive shaft (205) are movably installed in the fuselage (10) respectively, and the drive shaft (205) can be compared with institute
Fuselage (10) rotation is stated, the horn component (30) is fixedly connected on the drive shaft (205)；
During motor (202) work, the motor (202) and first helical gear (203a) can be together around the drive shafts
(205) rotate, so as to which the fuselage (10) be driven to be rotated around the drive shaft (205) compared with the horn component (30).
7. rack according to claim 6, which is characterized in that the central axes of the drive shaft (205) and the motor
(202) pivot center (O) of rotation axis is vertical and intersects.
8. the rack according to claim 6 or 7, which is characterized in that first helical gear (203a) includes the first circular cone
Face (2032a), first circular conical surface (2032a) and the angle of the pivot center (O) of the rotation axis of the motor (202) are 45
Degree, first circular conical surface (2032a) are equipped with teeth；
Second helical gear (204a) includes the second circular conical surface (2042a), second circular conical surface (2042a) and the driving
The angle of the central axes of axis (205) is 45 degree, and second circular conical surface (2042a) is equipped with teeth, first circular conical surface
The teeth of (2032a) are engaged with the teeth of second circular conical surface (2042a).
9. rack according to claim 1, which is characterized in that the fuselage drive component (20) includes motor (202), the
One spur gear (203b), the second spur gear (204b) and drive shaft (205)；
The motor (202) is fixedly installed in the fuselage (10)；
First spur gear (203b) is fixedly installed in the rotation axis of the motor (202)；
Second spur gear (204b) is sheathed on the drive shaft (205), first spur gear (203b) and described second
Spur gear (204b) engages；
The drive shaft (205) and the rotation axis of the motor (202) are arranged in parallel, the both ends difference of the drive shaft (205)
The fuselage (10) is movably installed in, the drive shaft (205) can rotate compared with the fuselage (10), the horn component
(30) it is fixedly connected on the drive shaft (205)；
During motor (202) work, the motor (202) and first spur gear (203b) can be together around the drive shafts
(205) rotate, so as to which the fuselage (10) be driven to be rotated around the drive shaft (205) compared with the horn component (30).
10. according to claim 2 to 9 any one of them rack, which is characterized in that the fuselage drive component (20) includes axis
Bearing (206), two bearing blocks (206) are fixedly installed in the fuselage (10), the both ends difference of the drive shaft (205)
Two bearing blocks (206) are movably installed in, the drive shaft (205) can rotate compared with the bearing block (206).
11. rack according to claim 10, which is characterized in that bearing there are one being set in each bearing block (206)
(2062), the bearing (2062) is sheathed on the drive shaft (205).
12. a kind of unmanned vehicle (100), which is characterized in that including：Motor (40), propeller (50), camera assembly (60) with
And rack as described in any one of claim 1 to 11, the motor (40) are installed on the horn (30), the propeller
(50) motor (40) is installed on, the camera assembly (60) is installed on the fuselage (10).
13. unmanned vehicle (100) according to claim 12, which is characterized in that two horn components (30) point
The opposite sides of the fuselage (10) is not symmetrically disposed on, and is fixedly installed in the both ends of the drive shaft (205) respectively.
14. unmanned vehicle (100) according to claim 13, which is characterized in that each horn component (30) bag
Host arm (302) and linking arm (304) are included, in each horn component (30), one end of the host arm (302) is fixed
One end of the drive shaft (205) is installed on, it is separate that two linking arms (304) are commonly connected to the host arm (302)
The other end of the drive shaft (205), the host arm (302) and two linking arm (304) composition Y-shapeds；
The each one end of the linking arm (304) away from the host arm (302) is installed by one motor (40).
15. unmanned vehicle (100) according to claim 13, which is characterized in that each horn component (30) bag
Host arm (302) is included, there are one the motors (40) for host arm (302) installation.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711403687.3A CN108100243A (en) | 2017-12-22 | 2017-12-22 | Unmanned vehicle and its rack |
| PCT/CN2018/109765 WO2019119939A1 (en) | 2017-12-22 | 2018-10-11 | Unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711403687.3A CN108100243A (en) | 2017-12-22 | 2017-12-22 | Unmanned vehicle and its rack |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108100243A true CN108100243A (en) | 2018-06-01 |
Family
ID=62212205
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711403687.3A Pending CN108100243A (en) | 2017-12-22 | 2017-12-22 | Unmanned vehicle and its rack |
Country Status (2)
| Country | Link |
|---|---|
| CN (1) | CN108100243A (en) |
| WO (1) | WO2019119939A1 (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2019119939A1 (en) * | 2017-12-22 | 2019-06-27 | 深圳市道通智能航空技术有限公司 | Unmanned aerial vehicle |
| WO2022157778A1 (en) * | 2021-01-21 | 2022-07-28 | Trim Robotics Ltd. | Dynamic drive |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0918748A (en) * | 1995-06-29 | 1997-01-17 | Nec Corp | Motor-driven universal head |
| CN101063510A (en) * | 2007-04-02 | 2007-10-31 | 北京科技大学 | Electric-controlled head |
| US20140034775A1 (en) * | 2012-08-02 | 2014-02-06 | Neurosciences Research Foundation | Vehicle capable of stabilizing a payload when in motion |
| CN104763867A (en) * | 2014-10-11 | 2015-07-08 | 天津汇讯视通科技有限公司 | Transmission structure of monitoring apparatus |
| CN205381396U (en) * | 2016-02-01 | 2016-07-13 | 梁伟 | Ware of taking photo by plane flies |
| CN106029502A (en) * | 2015-04-24 | 2016-10-12 | 深圳市大疆创新科技有限公司 | Gimbal and unmanned aerial vehicle using same |
| WO2017132990A1 (en) * | 2016-02-05 | 2017-08-10 | Autel Robotics Co.,Ltd | Multirotor aircraft |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103921933A (en) * | 2013-01-10 | 2014-07-16 | 深圳市大疆创新科技有限公司 | Deformation structure of air vehicle and micro air vehicle |
| JP5997342B1 (en) * | 2015-09-29 | 2016-09-28 | 京商株式会社 | Multicopter toy |
| CN105235899B (en) * | 2015-11-17 | 2017-05-03 | 温州市通翔智能科技有限公司 | Deformable unmanned aerial vehicle |
| WO2017132796A1 (en) * | 2016-02-01 | 2017-08-10 | Autel Robotics Co., Ltd | A multirotor aircraft and a method for controlling the multirotor aircraft |
| CN107444606B (en) * | 2017-09-15 | 2023-10-27 | 汤新哲 | Novel aircraft and aircraft system |
| CN108100243A (en) * | 2017-12-22 | 2018-06-01 | 深圳市道通智能航空技术有限公司 | Unmanned vehicle and its rack |
| CN207956048U (en) * | 2017-12-22 | 2018-10-12 | 深圳市道通智能航空技术有限公司 | Unmanned vehicle and its rack |
-
2017
- 2017-12-22 CN CN201711403687.3A patent/CN108100243A/en active Pending
-
2018
- 2018-10-11 WO PCT/CN2018/109765 patent/WO2019119939A1/en active Application Filing
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0918748A (en) * | 1995-06-29 | 1997-01-17 | Nec Corp | Motor-driven universal head |
| CN101063510A (en) * | 2007-04-02 | 2007-10-31 | 北京科技大学 | Electric-controlled head |
| US20140034775A1 (en) * | 2012-08-02 | 2014-02-06 | Neurosciences Research Foundation | Vehicle capable of stabilizing a payload when in motion |
| CN104763867A (en) * | 2014-10-11 | 2015-07-08 | 天津汇讯视通科技有限公司 | Transmission structure of monitoring apparatus |
| CN106029502A (en) * | 2015-04-24 | 2016-10-12 | 深圳市大疆创新科技有限公司 | Gimbal and unmanned aerial vehicle using same |
| WO2016169035A1 (en) * | 2015-04-24 | 2016-10-27 | 深圳市大疆创新科技有限公司 | Gimbal and unmanned aerial vehicle using same |
| CN205381396U (en) * | 2016-02-01 | 2016-07-13 | 梁伟 | Ware of taking photo by plane flies |
| WO2017132990A1 (en) * | 2016-02-05 | 2017-08-10 | Autel Robotics Co.,Ltd | Multirotor aircraft |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2019119939A1 (en) * | 2017-12-22 | 2019-06-27 | 深圳市道通智能航空技术有限公司 | Unmanned aerial vehicle |
| WO2022157778A1 (en) * | 2021-01-21 | 2022-07-28 | Trim Robotics Ltd. | Dynamic drive |
Also Published As
| Publication number | Publication date |
|---|---|
| WO2019119939A1 (en) | 2019-06-27 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN104508346B (en) | Non-orthogonal axes carrier | |
| CN108698682B (en) | Unmanned aerial vehicle, frame, kit, assembly method and operation method thereof | |
| CN107585306A (en) | A kind of unmanned vehicle | |
| US11305875B2 (en) | Mult-functional compartment | |
| US10081441B2 (en) | Tilt-ball turret with gimbal lock avoidance | |
| KR101783545B1 (en) | Camera Gimbal Syatem of Unmanned Flight Vehicle for VR 360 degree Omnidirectional Photographing | |
| US20200387173A1 (en) | Flight control method and device for multi-rotor unmanned aerial vehicle, and multi-rotor unmanned aerial vehicle | |
| CN107685872A (en) | Unmanned vehicle | |
| CN108235702A (en) | A kind of holder, unmanned plane and its control method | |
| CN108100284A (en) | A kind of holder, camera assembly and unmanned vehicle | |
| CN107521714A (en) | Head and the unmanned plane with this head | |
| CN207417151U (en) | A kind of unmanned vehicle | |
| US20150053833A1 (en) | Pan-tilt mount system for image sensor | |
| CN108332023B (en) | Two-axis and three-axis pan-tilt and shooting equipment thereof | |
| CN108100243A (en) | Unmanned vehicle and its rack | |
| CN107108043B (en) | Unmanned vehicle and unmanned vehicle are taken photo by plane method | |
| CN108216593A (en) | Undercarriage and the unmanned vehicle with this undercarriage | |
| CN206202711U (en) | A kind of head and unmanned plane | |
| WO2019128401A1 (en) | Undercarriage and unmanned aerial vehicle provided with same | |
| CN207956048U (en) | Unmanned vehicle and its rack | |
| CN108146618A (en) | Undercarriage and the unmanned vehicle with this undercarriage | |
| CN107719685A (en) | Head, picture shooting assembly and unmanned vehicle | |
| WO2017088514A1 (en) | Aerial vehicle and ball head thereof | |
| US10843816B2 (en) | Photographic assembly and unmanned aerial vehicle having same | |
| CN109844394A (en) | A kind of control method and holder of holder |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| CB02 | Change of applicant information | ||
| CB02 | Change of applicant information |
Address after: 518055 Guangdong city of Shenzhen province Nanshan District Xili Street Xueyuan Road No. 1001 Chi Yuen Building 9 layer B1 Applicant after: Shenzhen daotong intelligent Aviation Technology Co.,Ltd. Address before: 518055 Guangdong city of Shenzhen province Nanshan District Xili Street Xueyuan Road No. 1001 Chi Yuen Building 9 layer B1 Applicant before: AUTEL ROBOTICS Co.,Ltd. |