CN206087287U - Express delivery unmanned aerial vehicle - Google Patents
Express delivery unmanned aerial vehicle Download PDFInfo
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- CN206087287U CN206087287U CN201621032903.9U CN201621032903U CN206087287U CN 206087287 U CN206087287 U CN 206087287U CN 201621032903 U CN201621032903 U CN 201621032903U CN 206087287 U CN206087287 U CN 206087287U
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- cargo hold
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Abstract
The utility model relates to an express delivery unmanned aerial vehicle. The utility model provides a pair of express delivery unmanned aerial vehicle includes many rotor unmanned aerial vehicle body and cargo hold, many rotor unmanned aerial vehicle body center department is through two pan tilt connected cargo holds, two cloud platforms include the axis of ordinates and cross axle, the axis of ordinates is through first articulated piece and many these body couplings of rotor unmanned aerial vehicle, the cross axle is perpendicular with the axis of ordinates, and the cross axle is articulated with the axis of ordinates, the cross axle passes through the articulated piece of second and connects the cargo hold. The utility model provides an express delivery unmanned aerial vehicle is connected with the cargo hold through two cloud platforms that set up, can come through the rotation of cross axle and the axis of ordinates automatic balance cargo hold because of cargo weight or shape distribution disequilibrium lead to the focus change for whole express delivery unmanned aerial vehicle flight safety steady more.
Description
Technical field
This utility model is related to unmanned plane field, and in particular to express delivery unmanned plane field.
Background technology
Unmanned plane is used for express delivery, due to low cost, efficiency high, VTOL, flexible operation, is more and more weighed
Depending on.
In prior art, unmanned plane express delivery technical scheme is to be fixedly connected goods with multi-rotor unmanned aerial vehicle, is combined as one
Individual entirety, due to the scrambling of each transport goods, i.e. weight and shape is differed, cause as overall many rotors without
Man-machine center of gravity is not fixed.And center of gravity is particularly important for multi-rotor unmanned aerial vehicle, its stability and mobility are directly affected, because
This, under prior art, is required for carrying out counterweight to goods before each cargo transport, to fix unmanned plane center of gravity,
Also goods is fixed in addition, in case goods is moved during unmanned plane during flying and causes the center of gravity of unmanned plane to be sent out
It is raw to change.The efficiency for so allowing for unmanned plane express delivery is substantially reduced.
Utility model content
For defect of the prior art, this utility model provides a kind of stability and mobility not by goods weight and shape
The express delivery unmanned plane that shape affects.
A kind of express delivery unmanned plane that this utility model is provided includes multi-rotor unmanned aerial vehicle body and cargo hold；Many rotors without
Connect the cargo hold by two axle heads at man-machine body central；The two axles head includes the longitudinal axis and transverse axis；The longitudinal axis leads to
Cross the first hinged block to be connected with multi-rotor unmanned aerial vehicle body；The transverse axis and axis oriented normal, the transverse axis is hinged with the longitudinal axis；It is described
Transverse axis connects the cargo hold by the second hinged block.
That is multi-rotor unmanned aerial vehicle body is connected at its center the cargo hold of arrangement of goods by two axle heads,
Two axle heads are horizontally and vertically made up of axially vertical, longitudinal axis two ends and cargo hold top connection, horizontally and vertically between be hinged,
I.e. transverse axis can be hinged by hinged block, or be hinged by hinge hole around the axial-rotation of the longitudinal axis.Such goods
When the article deposited in cabin is uneven, self-balancing can be carried out by the rotation between horizontally and vertically, so that unmanned plane
It is more steady.
Preferably, through hole is set described in above-mentioned express delivery unmanned plane on transverse axis, and the through hole is axially perpendicular to transverse axis axial direction,
The longitudinal axis penetrates the through hole and is hinged with transverse axis.
That is, used as jointed shaft, in penetrating the through hole arranged on transverse axis, transverse axis can be around the axle of the longitudinal axis for the longitudinal axis itself
To rotation.So it is not required to additional articulated mounting to be capable of achieving to be hinged purpose, and horizontally and vertically connects more close and firm so that nothing
Man-machine entirety is more stable, and weight is lighter.
Preferably, above-mentioned express delivery unmanned plane also includes undercarriage；The undercarriage is reclinate strip；The cargo hold
It is shaped as cuboid, undercarriage is set on vertical four ribs of the cargo hold.
That is, cargo hold is cuboid, when goods does not place inequality, the pressure to four sides can be converted into, and
Reclinate strip is set on the rib of four vertical directions, when so landing, the face two when certain one side is under pressure
Two undercarriages on bar vertical edge can contact ground so that also more steady during its landing.
Preferably, longitudinal axis two ends described in above-mentioned express delivery unmanned plane are hinged with multi-rotor unmanned aerial vehicle body by described first
Block connects；First hinged block is two, and on first hinged block hinge hole is arranged；The longitudinal axis two ends respectively penetrate two
In hinge hole on individual first hinged block.
That is, around the axial-rotation of hinge hole in the hinge hole that can arrange on the first hinged block of the longitudinal axis,
The freedom of movement between cargo hold and multi-rotor unmanned aerial vehicle body can so be increased, goods is further reduced and loaded inequality to nothing
The impact of man-machine stability.
Preferably, transverse axis two ends are connected with cargo hold by second hinged block described in above-mentioned express delivery unmanned plane；It is described
Second hinged block is two, and on second hinged block hinge hole is arranged；The transverse axis two ends respectively penetrate two second and are hinged
In hinge hole on block.
That is around the axial-rotation of hinge hole in the hinge hole that transverse axis can be arranged on the second hinged block.So may be used
To increase the freedom of movement between cargo hold and multi-rotor unmanned aerial vehicle body, further reduce goods and load inequality to unmanned plane
The impact of stability.
Preferably, above-mentioned express delivery unmanned plane also includes the first servomotor and the second servomotor；The first servo electricity
Machine controls transverse axis around its axial rotation；The second Serve Motor Control longitudinal axis is around its axial rotation.
That is rotation horizontally and vertically is controlled by servomotor, so can ensure that cargo hold self-balancing
Shi Buhui oscillates so that unmanned plane during flying is more stable.
It is further preferred that above-mentioned express delivery unmanned plane also includes controller and gyro sensor；The gyro sensors
Device is placed in the cargo hold top, for measuring cargo hold horizontality；The controller feeds back according to the gyro sensor
Signal controls the rotation of first servomotor and the second servomotor, for realizing that the balance of cargo hold is controlled.
That is, the gyro sensor feedback that the rotation of the servomotor is installed by controller according to cargo hold top
Poised state signal be controlled, can so realize the autobalance of whole cargo hold.
Preferably, undercarriage described in above-mentioned express delivery unmanned plane and cargo hold integrated design.I.e. undercarriage is installed on cargo hold
On, with cargo hold integrated design, can so mitigate the weight of unmanned plane body, in landing, four undercarriages can also be same
When land because cargo hold remains horizontality.
In sum, the express delivery unmanned plane that this utility model is provided, is connected by the two axle heads for arranging with cargo hold, can
Ground gravity center shift is caused because of goods weight or distribution of shapes imbalance come autobalance cargo hold by rotation horizontally and vertically,
So that whole express delivery unmanned plane during flying is more steady safe.
Description of the drawings
In order to be illustrated more clearly that this utility model specific embodiment or technical scheme of the prior art, below will be right
The accompanying drawing to be used needed for specific embodiment or description of the prior art is briefly described.In all of the figs, it is similar
Element or part are typically identified by similar reference.In accompanying drawing, each element or part might not be according to actual ratios
Draw.
One of schematic diagram of express delivery unmanned plane that Fig. 1 is provided for the embodiment of this utility model one；
The two of the schematic diagram of the express delivery unmanned plane that Fig. 2 is provided for the embodiment of this utility model one.
Specific embodiment
The embodiment of technical solutions of the utility model is described in detail below in conjunction with accompanying drawing.Following examples are only
For clearly illustrating the technical solution of the utility model, therefore example is only used as, and this practicality can not be limited with this
New protection domain.
It should be noted that unless otherwise stated, technical term used in this application or scientific terminology should be this reality
The ordinary meaning understood with new one of ordinary skill in the art.
In the description of the present application, it is to be understood that term " horizontal stroke ", " vertical ", " vertical ", " downward ", "left", "right",
The orientation or position relationship of the instruction such as "front", "rear", " top " is based on orientation shown in the drawings or position relationship, merely to just
In description this utility model and simplified description, rather than indicate or imply that the device or element of indication there must be specifically side
Position, with specific azimuth configuration and operation, therefore it is not intended that to restriction of the present utility model.
Additionally, term " first ", " second " etc. are only used for describing purpose, and it is not intended that indicating or implying relatively important
Property or the implicit quantity for indicating indicated technical characteristic.
In this application, unless otherwise clearly defined and limited, term " connection " should be interpreted broadly, for example, can be with
It is to be fixedly connected, or be detachably connected, or it is integral；Can be mechanically connected, or electrically connect；Can be straight
Connect connected, it is also possible to be indirectly connected to by intermediary, can be connection or the phase interaction of two elements of two element internals
With relation.For the ordinary skill in the art, can as the case may be understand above-mentioned term in this utility model
In concrete meaning.
The preferred embodiment provided according to Fig. 1 and Fig. 2 carries out as described below：
A kind of express delivery unmanned plane that this utility model is provided includes：Multi-rotor unmanned aerial vehicle body 1 and cargo hold 2；Many rotations
The center of wing unmanned plane body 1 connects the cargo hold 2 by two axle heads 3；The two axles head 3 includes the longitudinal axis 32 and transverse axis
31；The longitudinal axis 32 is connected by the first hinged block 5 with multi-rotor unmanned aerial vehicle body 1；Transverse axis 31 is vertical with the longitudinal axis 32, transverse axis 31 with it is vertical
Axle 32 is hinged；Transverse axis 31 connects the cargo hold 2 by the second hinged block 6.Through hole is set on transverse axis 31, and the through hole is axially vertical
In transverse axis 31 axially, the longitudinal axis 32 penetrates the through hole and is hinged with transverse axis 31.
Above-mentioned express delivery unmanned plane also includes undercarriage 4；The undercarriage 4 is reclinate strip；The shape of the cargo hold 2
For cuboid, undercarriage 4 is set on 2 vertical four ribs of the cargo hold.Undercarriage 4 and the integrated design of cargo hold 2.
The two ends of the longitudinal axis 32 are connected first hinged block 5 with multi-rotor unmanned aerial vehicle body 1 by first hinged block 5
Two, hinge hole is set on first hinged block 5；The two ends of the longitudinal axis 32 respectively penetrate the hinge on two the first hinged blocks 5
In connecing hole.The two ends of transverse axis 31 are connected second hinged block 6 for two, described second with cargo hold 2 by second hinged block 6
Hinge hole is set on hinged block 6；The two ends of the transverse axis 31 are respectively penetrated in the hinge hole on two the second hinged blocks 6.
Above-mentioned express delivery unmanned plane also includes the first servomotor, the second servomotor, controller and gyro sensor；Institute
The first Serve Motor Control transverse axis 31 is stated around its axial rotation；The second Serve Motor Control longitudinal axis 32 is around its axial rotation；
The gyro sensor is placed in the top of the cargo hold 2, for measuring cargo hold horizontality；The controller is passed according to gyroscope
The signal of sensor feedback controls the rotation of first servomotor and the second servomotor, so as to control transverse axis 31 and the longitudinal axis 32
It is rotated to keep the balance of cargo hold 2 around its respective axial direction.
So, this utility model is capable of achieving unmanned plane stability and motor-driven by the rotary motion of transverse axis 31 and the longitudinal axis 32
Property is not affected by goods weight and shape.
Unmanned plane, when needing to change attitude, controls cargo hold 2 and locates all the time during transport goods by two axle head 3
In horizontality, so as to the mobility and stability that ensure unmanned plane are not affected by the weight of cargo hold 2 and the center of gravity of cargo hold 2.Its master
Adjustment when four kinds of attitudes of unmanned plane change is shown as, is described as follows with reference to Fig. 1：
A. when unmanned plane flight forward, unmanned plane turns forward, and the transverse axis 31 of two axle heads 3 is relative to the second hinged block
6 turn clockwise, and make cargo hold 2 be in horizontality.
B. when unmanned plane flies backward or slows down forward, unmanned plane is tilted backwards, the transverse axis 31 of two axle heads 3 relative to
The rotate counterclockwise of second hinged block 6, makes cargo hold 2 be in horizontality.
C. when to the left side flies unmanned plane, unmanned plane is tilted to the left, and the longitudinal axis 32 of two axle heads 3 is hinged relative to first
Block 5 turns clockwise, and makes cargo hold 2 be in horizontality.
D. when to the right side flies unmanned plane, unmanned plane is tilted to the right, and the longitudinal axis 32 of two axle heads 3 is hinged relative to first
The rotate counterclockwise of block 5, makes cargo hold 2 be in horizontality.
Finally it should be noted that：Various embodiments above is only illustrating the technical solution of the utility model, rather than it is limited
System；Although being described in detail to this utility model with reference to foregoing embodiments, one of ordinary skill in the art should
Understand：It still can modify to the technical scheme described in foregoing embodiments, either to which part or whole
Technical characteristic carries out equivalent；And these are changed or are replaced, the essence for not making appropriate technical solution departs from this practicality newly
The scope of each embodiment technical scheme of type, it all should cover in the middle of the scope of claim of the present utility model and description.
Claims (8)
1. a kind of express delivery unmanned plane, it is characterised in that include：
Multi-rotor unmanned aerial vehicle body and cargo hold；
Connect the cargo hold by two axle heads at the multi-rotor unmanned aerial vehicle body central；
The two axles head includes the longitudinal axis and transverse axis；
The longitudinal axis is connected by the first hinged block with multi-rotor unmanned aerial vehicle body；
The transverse axis and axis oriented normal, the transverse axis is hinged with the longitudinal axis；
The transverse axis connects the cargo hold by the second hinged block.
2. express delivery unmanned plane according to claim 1, it is characterised in that
Through hole is set on the transverse axis, and the through hole is axially perpendicular to transverse axis axial direction, and the longitudinal axis penetrates the through hole and transverse axis
It is hinged.
3. express delivery unmanned plane according to claim 1, it is characterised in that also include：
Undercarriage；
The undercarriage is reclinate strip；
The cargo hold is shaped as cuboid, and on vertical four ribs of the cargo hold undercarriage is arranged.
4. express delivery unmanned plane according to claim 1, it is characterised in that
The longitudinal axis two ends are connected with multi-rotor unmanned aerial vehicle body by first hinged block；
First hinged block is two, and on first hinged block hinge hole is arranged；
The longitudinal axis two ends are respectively penetrated in the hinge hole on two the first hinged blocks.
5. express delivery unmanned plane according to claim 1, it is characterised in that
The transverse axis two ends are connected with cargo hold by second hinged block；
Second hinged block is two, and on second hinged block hinge hole is arranged；
The transverse axis two ends are respectively penetrated in the hinge hole on two the second hinged blocks.
6. express delivery unmanned plane according to claim 1, it is characterised in that also include：
First servomotor and the second servomotor；
The first Serve Motor Control transverse axis is around its axial rotation；
The second Serve Motor Control longitudinal axis is around its axial rotation.
7. express delivery unmanned plane according to claim 6, it is characterised in that also include：
Controller and gyro sensor；
The gyro sensor is placed in the cargo hold top, for measuring cargo hold horizontality；
The controller controls first servomotor and the second servo electricity according to the signal that the gyro sensor feeds back
The rotation of machine, for realizing that the balance of cargo hold is controlled.
8. express delivery unmanned plane according to claim 3, it is characterised in that
The undercarriage and cargo hold integrated design.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621032903.9U CN206087287U (en) | 2016-08-31 | 2016-08-31 | Express delivery unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621032903.9U CN206087287U (en) | 2016-08-31 | 2016-08-31 | Express delivery unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206087287U true CN206087287U (en) | 2017-04-12 |
Family
ID=58475277
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621032903.9U Active CN206087287U (en) | 2016-08-31 | 2016-08-31 | Express delivery unmanned aerial vehicle |
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| Country | Link |
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| CN (1) | CN206087287U (en) |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107399435A (en) * | 2017-07-05 | 2017-11-28 | 广东容祺智能科技有限公司 | A kind of express delivery receive-transmit system based on unmanned plane |
| CN107600413A (en) * | 2017-09-08 | 2018-01-19 | 厦门大学 | The rotor of multi-chamber microminiature container-type four transports unmanned plane |
| CN107656546A (en) * | 2017-10-16 | 2018-02-02 | 郑州云海信息技术有限公司 | Utilize the method and apparatus of cloud data platform management unmanned plane |
| CN107757917A (en) * | 2017-10-09 | 2018-03-06 | 黄文佳 | Remote control express delivery box |
| CN108438542A (en) * | 2017-10-09 | 2018-08-24 | 黄文佳 | A kind of express delivery box |
| CN108725817A (en) * | 2018-06-05 | 2018-11-02 | 广东工业大学 | A kind of four axis unmanned planes with stabilization function |
| CN109533303A (en) * | 2018-11-27 | 2019-03-29 | 上海交通大学 | Split type full landform multi-rotor aerocraft with collision prevention function |
| CN109677617A (en) * | 2019-01-22 | 2019-04-26 | 广州市妙伊莲科技有限公司 | A kind of stable type unmanned flight's transport device for logistics distribution |
| CN111942592A (en) * | 2020-07-13 | 2020-11-17 | 李隆锦 | Multi-cabin logistics unmanned aerial vehicle transportation system |
| CN112046221A (en) * | 2020-09-21 | 2020-12-08 | 西南大学 | Dual-purpose unmanned aerial vehicle in air and ground |
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2016
- 2016-08-31 CN CN201621032903.9U patent/CN206087287U/en active Active
Cited By (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107399435A (en) * | 2017-07-05 | 2017-11-28 | 广东容祺智能科技有限公司 | A kind of express delivery receive-transmit system based on unmanned plane |
| CN107600413A (en) * | 2017-09-08 | 2018-01-19 | 厦门大学 | The rotor of multi-chamber microminiature container-type four transports unmanned plane |
| CN108482655B (en) * | 2017-10-09 | 2019-12-06 | 浙江龙腾电工器材有限公司 | Express delivery box |
| CN107757917A (en) * | 2017-10-09 | 2018-03-06 | 黄文佳 | Remote control express delivery box |
| CN108438542A (en) * | 2017-10-09 | 2018-08-24 | 黄文佳 | A kind of express delivery box |
| CN108482655A (en) * | 2017-10-09 | 2018-09-04 | 黄文佳 | A kind of express delivery box |
| CN108438542B (en) * | 2017-10-09 | 2020-05-01 | 瑞安市如果建材有限公司 | Express delivery box |
| CN107656546A (en) * | 2017-10-16 | 2018-02-02 | 郑州云海信息技术有限公司 | Utilize the method and apparatus of cloud data platform management unmanned plane |
| CN108725817A (en) * | 2018-06-05 | 2018-11-02 | 广东工业大学 | A kind of four axis unmanned planes with stabilization function |
| CN109533303A (en) * | 2018-11-27 | 2019-03-29 | 上海交通大学 | Split type full landform multi-rotor aerocraft with collision prevention function |
| CN109533303B (en) * | 2018-11-27 | 2020-09-15 | 上海交通大学 | Split type all-terrain multi-rotor aircraft with anti-collision function |
| CN109677617A (en) * | 2019-01-22 | 2019-04-26 | 广州市妙伊莲科技有限公司 | A kind of stable type unmanned flight's transport device for logistics distribution |
| CN111942592A (en) * | 2020-07-13 | 2020-11-17 | 李隆锦 | Multi-cabin logistics unmanned aerial vehicle transportation system |
| CN112046221A (en) * | 2020-09-21 | 2020-12-08 | 西南大学 | Dual-purpose unmanned aerial vehicle in air and ground |
| CN112046221B (en) * | 2020-09-21 | 2022-12-23 | 西南大学 | Dual-purpose unmanned aerial vehicle in air and ground |
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Effective date of registration: 20240402 Address after: 518000, Building 1, Building B, 1003, Shangzhi Science and Technology Park, No. 380 Guangming Avenue, Tangwei Community, Fenghuang Street, Guangming District, Shenzhen, Guangdong Province Patentee after: Shenzhen Yunzhikong Intelligent Equipment Co.,Ltd. Country or region after: China Address before: 5118000, C-10G, Xihai Mingzhu Garden, Taoyuan Road, Nanshan District, Shenzhen, Guangdong Province Patentee before: Ma Yanting Country or region before: China |
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