CN109279019A - A kind of logistics unmanned plane - Google Patents
A kind of logistics unmanned plane Download PDFInfo
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- CN109279019A CN109279019A CN201811274671.1A CN201811274671A CN109279019A CN 109279019 A CN109279019 A CN 109279019A CN 201811274671 A CN201811274671 A CN 201811274671A CN 109279019 A CN109279019 A CN 109279019A
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- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 23
- 229910052742 iron Inorganic materials 0.000 claims description 12
- 230000008602 contraction Effects 0.000 claims description 3
- 238000001514 detection method Methods 0.000 claims 1
- 238000000034 method Methods 0.000 description 20
- 230000033001 locomotion Effects 0.000 description 6
- 230000005540 biological transmission Effects 0.000 description 3
- 238000010586 diagram Methods 0.000 description 3
- 238000012360 testing method Methods 0.000 description 2
- 238000010521 absorption reaction Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000000903 blocking effect Effects 0.000 description 1
- 238000012790 confirmation Methods 0.000 description 1
- 230000001595 contractor effect Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000003116 impacting effect Effects 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 230000000750 progressive effect Effects 0.000 description 1
- 238000011160 research Methods 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
- B64D1/08—Dropping, ejecting, or releasing articles the articles being load-carrying devices
- B64D1/12—Releasing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D9/00—Equipment for handling freight; Equipment for facilitating passenger embarkation or the like
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- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05C—BOLTS OR FASTENING DEVICES FOR WINGS, SPECIALLY FOR DOORS OR WINDOWS
- E05C19/00—Other devices specially designed for securing wings, e.g. with suction cups
- E05C19/16—Devices holding the wing by magnetic or electromagnetic attraction
- E05C19/166—Devices holding the wing by magnetic or electromagnetic attraction electromagnetic
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- Mechanical Engineering (AREA)
- Warehouses Or Storage Devices (AREA)
Abstract
The invention discloses a kind of logistics unmanned planes, comprising: body, control system, power supply unit；The control system, power supply unit are placed in the inside of the body；The body includes: fuselage, wing, container；The side of the container is equipped with door-plate, the side of the door-plate and the container is hinged, the container interior opposite with the door-plate is equipped with the first telescopic rod, telescope support, the bottom of the container is equipped with sliding slot, sliding block is equipped in the sliding slot, the sliding block is fixedly connected with the bottom of the telescope support；The control system includes: processor, camera, scanning area, control device for pivoting, the first telescopic control device, the second telescopic control device, global position system.Unmanned plane during flying stability in the present invention is good, and loading is convenient, and can unload automatically.
Description
Technical field
The present invention relates to air vehicle technique field, more particularly to a kind of logistics unmanned plane.
Background technique
Currently, worse and worse, traffic jam is one huge to the condition of road surface in city with economic continuous development
Problem.This causes huge trouble to logistics personnel, increases the time of logistics transportation, has seriously affected the timeliness of logistics.
Therefore, in order to change the status of existing logistics transportation, people start selection unmanned plane delivery items, can save object in this way
The time delivered is flowed, brought a series of problem of avoiding the jams.But the existing unmanned plane for conveying articles,
One is the bottom that article is hung over to unmanned plane, the article transported in the flight course of unmanned plane in this way can ceaselessly shake
It is dynamic, it can affect to the stability of unmanned plane during flying；Another kind is the bottom setting fixed frame of unmanned plane, is transported
Article be fixed on fixed frame, this unmanned plane needs article fixation just can guarantee nobody before conveying articles
Machine article in flight course is not easy to slide, although being not in the phenomenon that article shakes.But the article after fixation binding is not
Easily be disassembled, and article be sent to after also personnel is needed to remove article, it is increased dismantling article time.
Therefore, a kind of flight stability is good at research, and it is this field skill that loading is convenient, and the unmanned plane that can be unloaded automatically
The problem of art personnel's urgent need to resolve.
Summary of the invention
In view of this, the present invention provides one kind to be put into cargo conveniently, cargo can be taken out automatically, the good object of safety
Flow unmanned plane.
To achieve the goals above, the present invention adopts the following technical scheme:
A kind of logistics unmanned plane, comprising: body, control system, power supply unit；The control system, power supply unit are placed in institute
The inside of body is stated, the body, control system are electrically connected with the power supply unit；The body include: fuselage, wing,
Container, the wing are fixed on the side wall of the fuselage, and the container is fixed on the bottom of the fuselage；The side of the container
Equipped with door-plate, the side of the door-plate and the container is hinged, and the container interior opposite with the door-plate is equipped with
First telescopic rod, telescope support, the bottom of the container are equipped with sliding slot, are equipped with sliding block in the sliding slot, the sliding block with it is described
The bottom of telescope support is fixedly connected；The control system includes: processor, camera, scanning area, control device for pivoting,
One telescopic control device, the second telescopic control device, global position system, the processor, camera, scanning area, rotation control
Device processed, the first telescopic control device, the second telescopic control device, global position system are electrically connected with the power supply unit,
The control device for pivoting, the first telescopic control device, the second telescopic control device are connected with the processor, the camera shooting
Head, scanning area, global position system and ground control terminal are wirelessly connected, the control device for pivoting and the fixed company of the door-plate
It connects, first telescopic control device is fixedly connected with first telescopic rod, and second telescopic control device is stretched with described
Contracting bracket is fixedly connected, and the camera and scanning area are placed in the side wall of the fuselage.
For above content, the bottom hung of middle fuselage of the present invention is used to hold the container of cargo, can save to cargo
The process for carrying out bundled fixed, facilitates loading, picking；When needing picking, door-plate, which opens telescope support stretching, extension, will drive sliding block
Sliding, while driving cargo to the external mobile of container, the first telescopic rod is stretched simultaneously, when cargo is moved to goods completely
When the outside of case, the first telescopic rod and telescope support stop stretching, at this point, the first telescopic rod keeps different, telescope support
Band movable slider is shunk, and the first telescopic rod stops cargo mobile with telescope support, and then during telescope support is shunk,
Slide cargo from sliding block, the first telescopic rod is carrying out contractile motion after telescope support is shunk completely, realizes cargo
Automatically the process delivered keeps delivery process time saving and energy saving without manually delivering to cargo.Rotation control dress in control system
The process of control door-plate rotary opening closing is set, the first telescopic control device controls the stretching motion of the first telescopic rod, the second telescopic rod
Control telescope support stretching motion, control system realize to the intelligent control of unmanned plane make unmanned plane may be implemented transport,
Deliver the process of cargo.
Preferably, the camera and scanning area are placed in the side wall of the fuselage and are placed in the same side with the door-plate.It takes the photograph
As head can detect the environment around unmanned plane, the picture that camera takes can be transferred to ground control terminal, ground control
End processed according to the actual situation manipulates unmanned plane；Scanning area is scanned the mark of delivery station, and scanning result is transmitted
To ground control terminal, judge whether to deliver here.
Preferably, the bottom of the fuselage connects multiple connecting rods, and the fuselage is fixedly connected with container by the connecting rod.
Container is attached by connecting rod can prevent container shaking during unmanned plane during flying from impacting to unmanned plane during flying.
Preferably, there are two the door-plate is set, side wall of two door-plates respectively with the container is hinged.
Preferably, the control device for pivoting is fixedly connected with two door-plates.Two door-plates pass through rotating device
Control can carry out the rotation around hinged side wall, and then realize the opening and closing of cargo box door.
Preferably, the side wall of one of them door-plate is equipped with iron block, and the side wall of another door-plate is equipped with electromagnetism
Iron, the iron block are set to the position that two door-plates are in contact with electromagnet.Electromagnet, which is powered, makes two doors with iron block absorption
Plate closing is close, and cargo box door is not easy to be opened, and the cargo in container will not drop out, and does not adsorb mutually with iron block after electromagnet power-off,
The opening of cargo box door may be implemented by the control of control device for pivoting.
Preferably, the electromagnet is connected with switch controlling device, the switch controlling device and power supply unit electricity
Connection, the switch controlling device are also electrically connected with the processor.Switch controlling device can control the power on/off of electromagnet, place
Manage the opening and closing of device meeting control switch control device.
Preferably, the telescope support includes: the second telescopic rod, bracket, the top of second telescopic rod and the bracket
Portion is connected, and the bottom of the bracket is fixedly connected with the sliding block.
Preferably, the height of the container base slider is not less than the height of the container bottom.It just can guarantee cunning in this way
Block can drive cargo to move together in sliding process, preferably realize the automatic process for delivering cargo.
Preferably, weight sensor, the weight sensor and the processing is arranged in the bottom of the container
Device electrical connection.The weight of loading is certain in container, and overburden can impact the flight of unmanned plane, weight detecting
Sensor can detect the weight of cargo, if the weight of cargo is more than the maximum value of preset goods weight in processor,
Processor can control the stretching, extension of the second telescopic control device, and telescope support can release cargo, so that unmanned plane is more intelligent, use
It is more safe.
Beneficial effects of the present invention:
(1) unmanned plane in the present invention connects container by connecting rod, and cargo is placed in container, can prevent the shaking of cargo,
The time required for fixed cargo is reduced, so that the flight of unmanned plane is more steady, it is safer, load the process of cargo more
It is time saving and energy saving.
(2) mistake that cargo is delivered automatically may be implemented by the telescopic process of the first telescopic rod and telescope support in container
Journey, without human intervention, so that the delivery process of cargo is simpler, it is convenient.
Detailed description of the invention
In order to more clearly explain the embodiment of the invention or the technical proposal in the existing technology, to embodiment or will show below
There is attached drawing needed in technical description to be briefly described, it should be apparent that, the accompanying drawings in the following description is only this
The embodiment of invention for those of ordinary skill in the art without creative efforts, can also basis
The attached drawing of offer obtains other attached drawings.
Fig. 1 attached drawing is the overall structure diagram of unmanned plane provided by the invention.
Fig. 2 attached drawing is container interior structural schematic diagram provided by the invention.
Fig. 3 attached drawing is the side view of one of door-plate provided by the invention.
Fig. 4 attached drawing is the side view of another door-plate provided by the invention.
Fig. 5 attached drawing is the structural schematic diagram of control system provided by the invention.
Wherein, in figure,
1- body；
11- fuselage；12- wing；
13- container；
131- door-plate；
1311- electromagnet；1312- iron block；
The first telescopic rod of 132-；
133- telescope support；
The second telescopic rod of 1331-；1332- bracket；
134- sliding slot；135- sliding block；136- weight sensor；
2- camera；3- scanning area；4- connecting rod.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
The embodiment of the invention discloses a kind of logistics unmanned planes, comprising: body 1, control system, power supply unit；Control system
System, power supply unit are placed in the inside of body 1, and body 1, control system are electrically connected with power supply unit；Body 1 includes: fuselage
11, wing 12, container 13, wing 12 are fixed on the side wall of fuselage 11, and container 13 is fixed on the bottom of fuselage 11；The one of container 13
Side is equipped with door-plate 131, and door-plate 131 and the side of container 13 be hinged, and the interior opposite with door-plate 131 of container 13 is equipped with the
One telescopic rod 132, telescope support 133, the bottom of container 13 are equipped with sliding slot 134, are equipped with sliding block 135, sliding block 135 in sliding slot 134
It is fixedly connected with the bottom of telescope support 133；Control system include: processor, camera 2, scanning area 3, control device for pivoting,
First telescopic control device, the second telescopic control device, global position system, processor, camera 2, scanning area 3, rotation control
Device processed, the first telescopic control device, the second telescopic control device, global position system are electrically connected with power supply unit, are rotated
Control device, the first telescopic control device, the second telescopic control device are connected with processor, camera 2, scanning area 3, satellite
Positioning system and ground control terminal are wirelessly connected, and control device for pivoting is fixedly connected with door-plate 131, the first telescopic control device and
First telescopic rod 132 is fixedly connected, and the second telescopic control device is fixedly connected with telescope support 133, camera 2 and scanning area 3
It is placed in the side wall of fuselage 11.
For above content, the process of flight and the loading, unloading of unmanned plane is controlled in the present invention by control system,
Unmanned plane is needed goods handling to express delivery release position, and express delivery release position is designed with special identifier, by scanning area 3 to special mark
Knowledge is scanned, and the information of scanning area 3 can be transferred to ground control terminal, and ground control terminal sentences the mark scanned
It is disconnected, if to need the place launched, if release position then issues the instruction for needing to launch to processor, if not release position is then
The instruction for continually looking for release position is issued to processor, the setting of scanning area can guarantee the accuracy of release position, reduce and launch
The error rate of cargo.
Further, camera 2 and scanning area 3 are placed in the side wall of fuselage 11 and are placed in the same side with door-plate 131.Camera
2 can be shot with the cargo handling process of the opening and closing of end of door plate 131 and cargo, and the picture transmission taken is controlled to ground
End, ground control terminal can in real time be monitored the flight of unmanned plane, launch process.
Further, there are two door-plate 131 is set, side wall of two door-plates 131 respectively with container 13 is hinged, rotation control
Device is fixedly connected with two door-plates 131.Control device for pivoting can control door-plate 131 and rotate around hinged side wall.
Further, the side wall of one of door-plate 131 is equipped with iron block 1312, and the side wall of another door-plate 131 is equipped with
Electromagnet 1311, iron block 1312 are set to the position that two door-plates 131 are in contact with electromagnet 1311.Meeting after electromagnet 1311 is powered
Adsorb iron block 1312, energizations of electromagnet 1311 can make being fixed after two door-plates 131 closures, prevent cargo from container
It is thrown out of in 13, and simple by the fixed form that electromagnet 1311 adsorbs iron block 1312, it is easy to operate.
Further, electromagnet 1311 is connected with switch controlling device, and switch controlling device is electrically connected with power supply unit, opens
Control device is closed also to be electrically connected with processor.
Further, telescope support 133 includes: the second telescopic rod 1331, bracket 1332, the second telescopic rod 1331 and bracket
1332 top is connected, and the bottom of bracket 1332 is fixedly connected with sliding block 135.Preferably, 13 bottom of container sets that there are two sliding
Slot 134 is equipped with a sliding block 135 in each sliding slot 134, and bracket 1332 is connected with two sliding blocks 135, the second telescopic rod 1331
Stretching motion can drive bracket 1332 to move, and then slide in sliding slot 134 with movable slider 135.
Further, the height of 13 base slider 135 of container is not less than the height of 13 bottom of container.It can guarantee sliding block
Cargo can be mobile with sliding block 135 when 135 movement.
Further, weight sensor 136, weight sensor 136 and processor is arranged in the bottom of container 13
Electrical connection.Weight sensor 136 weighs to the cargo in container 13, prevents transported cargo overweight, guarantees nothing
The safety of man-machine flight.
The course of work:
After loading cargo, wing 12, which is powered, to be rotated, and is flown, global position system can be according to predetermined routes
It flies, camera 2 can shoot the environment around unmanned plane, by the picture transmission of shooting to ground control terminal,
Ground control terminal according to picture the case where, the route of flight is adjusted at any time, when unmanned plane during flying to specified delivery point, delivery point
It is equipped with special identifier, is scanned by 3 pairs of marks of scanning area, by the content transmission scanned to ground control terminal, if
Delivery point mistake, then unmanned plane continues flight searching delivery point；If delivery point is correct, ground control terminal can be sent out to processor
The instruction of cargo is unloaded out, carries out automatic unloading cargo under the control of a processor, after completion of discharge, unmanned plane is returned by former road
It returns, the cargo of unloading can be delivered staff a little and be delivered to corresponding location.
Loading process: when not having cargo in container 13, the weight that weight sensor 136 detects is 0, weight inspection
Survey the data that can will test of sensor 136 and be transferred to processor, at this time processor can control switch control device disconnect, then this
When electromagnet 1311 it is not charged, loading personnel can open at any time container 13 two door-plates 131 be packed into cargo, when cargo load
After, weight sensor 136 can detect the weight for being loaded into cargo, and the information that will test is transferred in processor, if
The weight measured is greater than the weight value set in processor, then processor can control the second telescopic control device and be stretched, the
Two telescopic control devices can control the second telescopic rod 1331 and be stretched, and the second telescopic rod 1331 will drive sliding block 135 to container
13 outsides are mobile, prompt this cargo of loading personnel overweight, and after the second telescopic rod 1331 stretches to the limit, processor can be controlled
The contraction of the second telescopic control device is made, the second telescopic control device controls the second telescopic rod 1331 and shrinks；If the cargo loaded
Weight be less than the weight value that sets in processor, then processor will not issue any instruction.
Unload the process of cargo: after confirmation reaches specified delivery service area, processor meeting control switch control device is disconnected
It opens, electromagnet 1311 powers off at this time, and processor can control control device for pivoting rotation, and control device for pivoting controls two door-plates
131 rotate to two sides, and the door of container 13 is opened, and processor can control the first telescopic control device and the second telescopic control device
Stretching is carried out simultaneously, at this point, the first telescopic rod 132 and the second telescopic rod 1331 are stretched, when cargo is moved completely
When to the outside of container 13, the first telescopic rod 132 and telescope support 133 stop stretching, at this point, the first telescopic rod 132 is protected
To hold motionless, processor controls the second telescopic rod 1331 and carries out contractive action, and also the second telescopic rod 1331 of institute is shunk sliding block 135, and the
One telescopic rod 132 plays the role of blocking to cargo, separates cargo from sliding block 135, when the second telescopic rod 1331 is complete
After full contraction, processor controls the first telescopic rod 132 again and carries out contractile motion, realizes the process that cargo is delivered automatically.It has delivered
Cheng Hou, processor control control device for pivoting rotation, and control device for pivoting controls two rotations of door-plate 131 and is closed, and 13, container
After closure, control device for pivoting sends to processor and instructs, processor control switch control device closure, at this time electromagnet 1311
It is powered, 131 tight close of door-plate of container 13.
Each embodiment in this specification is described in a progressive manner, the highlights of each of the examples are with other
The difference of embodiment, the same or similar parts in each embodiment may refer to each other.For device disclosed in embodiment
For, since it is corresponded to the methods disclosed in the examples, so being described relatively simple, related place is said referring to method part
It is bright.
The foregoing description of the disclosed embodiments enables those skilled in the art to implement or use the present invention.
Various modifications to these embodiments will be readily apparent to those skilled in the art, as defined herein
General Principle can be realized in other embodiments without departing from the spirit or scope of the present invention.Therefore, of the invention
It is not intended to be limited to the embodiments shown herein, and is to fit to and the principles and novel features disclosed herein phase one
The widest scope of cause.
Claims (10)
1. a kind of logistics unmanned plane characterized by comprising body (1), control system, power supply unit；The control system,
Power supply unit is placed in the inside of the body (1), and the body (1), control system are electrically connected with the power supply unit；
The body (1) includes: fuselage (11), wing (12), container (13), and the wing (12) is fixed on the fuselage (11)
Side wall, the container (13) is fixed on the bottom of the fuselage (11)；
The side of the container (13) is equipped with door-plate (131), and the door-plate (131) and the side of the container (13) are hinged,
The container (13) and the door-plate (131) opposite interior are equipped with the first telescopic rod (132), telescope support (133), institute
The bottom for stating container (13) is equipped with sliding slot (134), is equipped with sliding block (135) in the sliding slot (13), the sliding block (135) with it is described
The bottom of telescope support (133) is fixedly connected；
The control system includes: processor, camera (2), scanning area (3), control device for pivoting, the first extension and contraction control dress
Set, the second telescopic control device, global position system, the processor, camera (2), scanning area (3), control device for pivoting,
First telescopic control device, the second telescopic control device, global position system are electrically connected with the power supply unit, the rotation
Control device, the first telescopic control device, the second telescopic control device are connected with the processor, and the camera (2) is swept
It retouches area (3), global position system and ground control terminal to be wirelessly connected, the control device for pivoting and the door-plate (131) are fixed
Connection, first telescopic control device is fixedly connected with first telescopic rod (132), second telescopic control device and
The telescope support (133) is fixedly connected, and the camera (2) and scanning area (3) are placed in the side wall of the fuselage (11).
2. a kind of logistics unmanned plane according to claim 1, which is characterized in that the camera (2) and scanning area (3) are set
In the fuselage (11) side wall and be placed in the same side with the door-plate (131).
3. a kind of logistics unmanned plane according to claim 1, which is characterized in that the bottom connection of the fuselage (11) is multiple
Connecting rod (4), the fuselage (11) are fixedly connected with container (13) by the connecting rod (4).
4. a kind of logistics unmanned plane according to claim 1 or 2, which is characterized in that there are two the door-plate (131) sets,
Side wall of two door-plates (131) respectively with the container (13) is hinged.
5. a kind of logistics unmanned plane according to claim 4, which is characterized in that described in the control device for pivoting and two
Door-plate (131) is fixedly connected.
6. a kind of logistics unmanned plane according to claim 4, which is characterized in that the side of one of them door-plate (131)
Wall is equipped with iron block (1312), the side wall of another door-plate (131) is equipped with electromagnet (1311), the iron block (1312) with
Electromagnet (1311) is set to the position that two door-plates (131) are in contact.
7. a kind of logistics unmanned plane according to claim 6, which is characterized in that the electromagnet (1311) is connected with switch
Control device, the switch controlling device are electrically connected with the power supply unit, the switch controlling device also with the processor
Electrical connection.
8. a kind of logistics unmanned plane according to claim 1, which is characterized in that the telescope support (133) includes: second
Telescopic rod (1331), bracket (1332) are connected at the top of second telescopic rod (1331) and the bracket (1332), described
The bottom of bracket (1332) is fixedly connected with the sliding block (135).
9. a kind of logistics unmanned plane according to claim 1 or 8, which is characterized in that container (13) base slider
(135) height is not less than the height of the container (13) bottom.
10. a kind of logistics unmanned plane according to claim 1, which is characterized in that weight is arranged in the bottom of the container (13)
Quantity detection sensor (136), the weight sensor (136) are electrically connected with the processor.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811274671.1A CN109279019A (en) | 2018-10-30 | 2018-10-30 | A kind of logistics unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811274671.1A CN109279019A (en) | 2018-10-30 | 2018-10-30 | A kind of logistics unmanned plane |
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| Publication Number | Publication Date |
|---|---|
| CN109279019A true CN109279019A (en) | 2019-01-29 |
Family
ID=65174905
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811274671.1A Withdrawn CN109279019A (en) | 2018-10-30 | 2018-10-30 | A kind of logistics unmanned plane |
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| CN (1) | CN109279019A (en) |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110481766A (en) * | 2019-08-15 | 2019-11-22 | 天津中德应用技术大学 | Have the function of to dispense unmanned plane |
| CN110550199A (en) * | 2019-09-03 | 2019-12-10 | 南京唐壹信息科技有限公司 | Cantilever type agricultural transportation unmanned aerial vehicle |
| CN110775278A (en) * | 2019-11-13 | 2020-02-11 | 吉林大学 | Small-sized logistics unmanned aerial vehicle for terminal air transportation network |
| CN111546970A (en) * | 2020-05-11 | 2020-08-18 | 青岛工学院 | Express delivery system based on unmanned |
| CN111847011A (en) * | 2020-08-04 | 2020-10-30 | 辽宁省交通高等专科学校 | Port cargo fast loading and unloading system based on Internet of things technology |
| CN112093056A (en) * | 2020-10-13 | 2020-12-18 | 成都康拓兴业科技有限责任公司 | Goods pushing and taking-off device for unmanned helicopter goods delivery |
| CN112758330A (en) * | 2020-12-25 | 2021-05-07 | 安徽翼讯飞行安全技术有限公司 | Unmanned aerial vehicle commodity circulation goods linkage of high group spare |
| CN115743636A (en) * | 2022-11-09 | 2023-03-07 | 安徽工程大学 | Civil multi-rotor unmanned aerial vehicle and control and scheduling method thereof |
| WO2023135713A1 (en) * | 2022-01-13 | 2023-07-20 | 株式会社エアロネクスト | Aircraft, load landing method, and terrestrial vehicle |
-
2018
- 2018-10-30 CN CN201811274671.1A patent/CN109279019A/en not_active Withdrawn
Cited By (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110481766A (en) * | 2019-08-15 | 2019-11-22 | 天津中德应用技术大学 | Have the function of to dispense unmanned plane |
| CN110550199A (en) * | 2019-09-03 | 2019-12-10 | 南京唐壹信息科技有限公司 | Cantilever type agricultural transportation unmanned aerial vehicle |
| CN110775278B (en) * | 2019-11-13 | 2021-08-31 | 吉林大学 | Small-sized logistics unmanned aerial vehicle for terminal air transportation network |
| CN110775278A (en) * | 2019-11-13 | 2020-02-11 | 吉林大学 | Small-sized logistics unmanned aerial vehicle for terminal air transportation network |
| CN111546970A (en) * | 2020-05-11 | 2020-08-18 | 青岛工学院 | Express delivery system based on unmanned |
| CN111847011B (en) * | 2020-08-04 | 2022-09-02 | 广州拓威天海国际物流有限公司 | Port cargo fast loading and unloading system based on Internet of things technology |
| CN111847011A (en) * | 2020-08-04 | 2020-10-30 | 辽宁省交通高等专科学校 | Port cargo fast loading and unloading system based on Internet of things technology |
| CN112093056A (en) * | 2020-10-13 | 2020-12-18 | 成都康拓兴业科技有限责任公司 | Goods pushing and taking-off device for unmanned helicopter goods delivery |
| CN112093056B (en) * | 2020-10-13 | 2021-10-29 | 成都康拓兴业科技有限责任公司 | Goods pushing and taking-off device for unmanned helicopter goods delivery |
| CN112758330A (en) * | 2020-12-25 | 2021-05-07 | 安徽翼讯飞行安全技术有限公司 | Unmanned aerial vehicle commodity circulation goods linkage of high group spare |
| WO2023135713A1 (en) * | 2022-01-13 | 2023-07-20 | 株式会社エアロネクスト | Aircraft, load landing method, and terrestrial vehicle |
| CN115743636A (en) * | 2022-11-09 | 2023-03-07 | 安徽工程大学 | Civil multi-rotor unmanned aerial vehicle and control and scheduling method thereof |
| CN115743636B (en) * | 2022-11-09 | 2023-06-30 | 安徽工程大学 | Civil multi-rotor unmanned aerial vehicle and control and scheduling method thereof |
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Application publication date: 20190129 |