CN108146635A - There is the unmanned plane and express delivery put-on method of express delivery dispensing - Google Patents
There is the unmanned plane and express delivery put-on method of express delivery dispensing Download PDFInfo
- Publication number
- CN108146635A CN108146635A CN201711393818.4A CN201711393818A CN108146635A CN 108146635 A CN108146635 A CN 108146635A CN 201711393818 A CN201711393818 A CN 201711393818A CN 108146635 A CN108146635 A CN 108146635A
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- express delivery
- unmanned
- capstan winch
- locking plate
- 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.)
- Withdrawn
Links
- 238000012384 transportation and delivery Methods 0.000 title claims abstract description 41
- 238000000034 method Methods 0.000 title claims abstract description 23
- 230000005540 biological transmission Effects 0.000 claims description 12
- 230000004044 response Effects 0.000 claims description 12
- 230000009471 action Effects 0.000 claims description 5
- 210000000988 bone and bone Anatomy 0.000 claims description 5
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 claims description 4
- 238000000203 droplet dispensing Methods 0.000 claims description 2
- 239000004677 Nylon Substances 0.000 abstract description 13
- 229920001778 nylon Polymers 0.000 abstract description 13
- 230000008569 process Effects 0.000 description 9
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 description 4
- 238000005265 energy consumption Methods 0.000 description 4
- 229910052744 lithium Inorganic materials 0.000 description 4
- 238000010586 diagram Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 230000007423 decrease Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 230000001737 promoting effect Effects 0.000 description 2
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- 210000000683 abdominal cavity Anatomy 0.000 description 1
- 238000013473 artificial intelligence Methods 0.000 description 1
- 230000004888 barrier function Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000004364 calculation method Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000005183 dynamical system Methods 0.000 description 1
- 210000005069 ears Anatomy 0.000 description 1
- 230000003628 erosive effect Effects 0.000 description 1
- 238000001125 extrusion Methods 0.000 description 1
- 230000008676 import Effects 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 238000005457 optimization Methods 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 230000003014 reinforcing effect Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
- B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
-
- 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
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Management, Administration, Business Operations System, And Electronic Commerce (AREA)
Abstract
The invention discloses a kind of unmanned planes and express delivery put-on method with express delivery dispensing, there is the unmanned plane package card to throw module, the package card throws module and includes locking plate, nylon rope, rope closing capstan winch and micromachine, wherein, the locking plate is articulated in the circular shaft between two supporting legs, and it is pre-tightened between circular shaft and locking plate using torsional spring, so that two locking plates form the layout pattern of symmetrical eight shape, the rope closing capstan winch is rotatably mounted in unmanned plane cabin, the rope closing capstan winch is driven by micromachine, the nylon rope connection locking plate and rope closing capstan winch, when rope closing capstan winch is in micromachine when being rotated by, it realizes and tightens or loosen while two nylon ropes.The present invention is realized using unmanned plane launches package in the air with certain altitude, and unmanned plane can directly make a return voyage after dispensing without landing, save a large amount of time.
Description
Technical field
The invention is related to unmanned plane transport cargo technical field, the terminal of especially a kind of courier packages launch unmanned plane and
Put-on method.
Background technology
Unmanned plane delivery will be the following effective means for solving delivery industry last one kilometer.
By taking express delivery industry as an example, lead in Shun Feng, Shen etc. in express deliveries, most express delivery product is all that quality is less than 5KG
Small bulk goods object, be very suitable for unmanned plane and dispensed.
Based on current news report, application scenarios of the current unmanned plane in delivery industry are as follows：
Express delivery and other items is placed in the cabin of unmanned plane by delivery personnel, and then unmanned plane flies under program control and unloads
Goods place is taken off since dispensing vehicle, is landed and is unloaded after unmanned plane arrives at landing place, is taking off involved in whole process
The flight of (elevated height), overhead horizontal such as drop to landing platform (height decline), unloads, goes around at several links.
Meanwhile according to physics common sense, unmanned plane in takeoff phase due to being to bear a heavy burden to take off, so takeoff speed reduces,
The time of consumption is also most, and two above problem is to limit the main problem that unmanned plane is quickly applied in delivery industry.
The scheme solved at present is, as soon as it increases the power of motor of unmanned plane rotor module or increases the quantity of rotor module,
It is using powerful unmanned plane, promotes take-off power and time, but the new problem that this mode is brought is exactly to increase energy
The consumption in source, reduces course continuation mileage.Second is that increasing the capacity of accumulator, that is, solved using more lithium battery groups,
While bringing course continuation mileage, shortcoming be sacrifice can loading object weight.
So two above problem is associated with each other, either which kind of mode does not all solve existing nothing fundamentally
The problem of man-machine dispatching.
The present invention changes traditional landing mode, studies a set of aerial dispensing technology, realizes the aerial dispensing of courier packages,
Realize the dispensing of not landing of unmanned plane.
Invention content
In order to solve the deficiencies in the prior art, the present invention provides a kind of unmanned plane with express delivery dispensing and express delivery is thrown
Method is put, realizes the aerial accurate dispensing of low energy consumption, improves and launches efficiency.
The technical solution adopted by the present invention to solve the technical problems is：
There is the unmanned plane that express delivery is launched, including
Groined type frame is a part for unmanned plane bone,
Supporting leg is a part for unmanned plane bone,
Rotor module provides flying power,
Power battery and flight control system module, provide electric energy and flight controls,
Scan camera shooting head module provides scanning and identification,
It is characterized in that, further including package card throws module, the package card throws module and includes locking plate, nylon rope, rope closing
Capstan winch and micromachine, wherein, the locking plate is articulated in the circular shaft between two supporting legs, and between circular shaft and locking plate
It is pre-tightened using torsional spring so that two locking plates form the layout pattern of symmetrical eight shape, and the rope closing capstan winch is rotatably pacified
In unmanned plane cabin, the rope closing capstan winch is driven by micromachine, the nylon rope connection locking plate and rope closing capstan winch, when
Rope closing capstan winch when being rotated by, is realized in micromachine and tightens or loosen while two nylon ropes.
It is guide plate in the lower part of locking plate.
The special express box of outfit is further included, is provided with card slot the two sides of the special express box are corresponding, it is described
Card slot is fastened with locking plate and is locked.
Express delivery put-on method, which is characterized in that using described in claims 1 to 33 have the function of express delivery launch nobody
Machine carries out air-drop dispensing, carries out following steps：
Step 1 on cargo platform, carries out barcode scanning to courier packages using the scan code system on unmanned plane, obtains express delivery
The dispatching address information of package, courier packages to be dispensed is fixed in the cabin of unmanned plane, lifting means promotes unmanned plane
To predetermined altitude；
Step 2, unmanned plane obtain instruction of taking off, and unmanned plane rotor module starts and takes off, and unmanned plane is low with dive status
The flight attitude that consumes energy flies, and when reaching near release position, state of flight is adjusted, in order to scan the address in unmanned inbox
Quick Response Code；
Step 3, unmanned plane scan the address Quick Response Code in unmanned inbox by scanning system, confirm address and nobody
Whether the address recorded in machine system is consistent, if unanimously, unmanned plane action is dropped, express delivery is launched to unmanned inbox
It is internal.
Step 4, unmanned plane return to flight, return to the dispatching origin such as express transportation vehicle according to programming route, carry out again
Secondary dispatching.
In step 3, most preferably release altitude is unmanned plane apart from 0.3 to 0.5 meter of height at the top of unmanned inbox.
The cover board that can be automatically opened there are one settings at the top of the unmanned inbox, the cover board can pass through control system
Control is opened, and described address Quick Response Code is set on the cover board.
The bottom setting sponge cushion pad of the unmanned inbox.
The lifting means includes braced frame, chain transmission system, motor and promotes platform, wherein, the rigidity structure
Setting chain transmission system in frame, the operating of motor drive chain transmission system, the promotion platform are fixed on chain transmission system
Chain on.
The promotion platform includes L shaped plate and fixed plate, and wherein fixed plate is fixed on chain, in the lower edge of fixed plate
Be articulated and connected L shaped plate.
The unmanned inbox is open design.
The beneficial effects of the invention are as follows：
Realize that aerial launch with certain altitude is wrapped up using unmanned plane, unmanned plane, can be direct after dispensing without landing
It makes a return voyage, saves a large amount of time.According to measuring and calculating, each single dispatching can save the power consumption of energy consumption 10% or so, save
20% or so distribution time reduces distribution cost with very big realistic meaning for promoting dispatching efficiency.
Description of the drawings
Fig. 1 is the principle of the present invention schematic diagram.
Fig. 2 is unmanned plane Special-purpose lifting equipment structure chart.
Fig. 3 is promotes platform and chain installation connection stereogram.
Fig. 4 is promotes platform schematic diagram.
Fig. 5 is unmanned plane stereogram.
Fig. 6 is the stereogram of rope closing capstan winch.
Fig. 7 launches package schematic diagram for unmanned plane.
Fig. 8 is the stereogram of express box.
Fig. 9 is the sectional view of express box.
Figure 10 is unmanned inbox stereogram.
Figure 11 a, Figure 11 b, Figure 11 c are unmanned plane launch process.
In figure：100 Special-purpose lifting equipment, 110 braced frames, 120 chain transmission systems, 121 sprocket wheels, 122 sprocket shafts,
123 chains, 124 chain expansion tightening wheels, 130 motors, 140 promote platform, 141L shape plates, 142 fixed plates, 143 strip holes, 200 nothings
It is man-machine, 210 groined type frames, 220 supporting legs, 230 rotor modules, 240 control system modules, 250 scan camera shooting head modules,
260 package cards throw module, 261 locking plates, 2611 guide plates, 262 nylon ropes, 263 rope closing capstan winches, 2631 teeth, 2632 nylon ropes
Fastening point, 300 cargo platforms, 400 unmanned inboxes, 410 cover boards, 420 address Quick Response Codes, 440 door openings, 430 sponge cushion pads.
Specific embodiment
Basic ideas introduction：
Based in traditional unmanned plane dispatching cargo, takeoff phase needs to consume a large amount of electric energy, is analyzed from principle, this
Part electric energy is converted into the gravitional force of cargo, that is to say, that unmanned plane needs to overcome cargo in itself in takeoff phase and nobody
The weight of machine in itself, according to formula:Ep=mgh, it is known that, consumption and dead weight, the goods weight and height of taking off of unmanned plane electric energy
Related, the utilization ratio that the electric energy in usual lithium battery is converted to unmanned plane workmanship only has 30% or so, so this discrete consuming
A large amount of electric energy of unmanned plane.In level flight stage, energy consumption is less, it is only necessary to overcome air drag, decline stage, consumption
Can be less, because the dead weight of unmanned plane and cargo can provide downward gravitional force, it might even be possible to by circuit to unmanned plane
Electric power system compensates.Meanwhile when unmanned plane dispenses courier packages, unmanned plane needs to go around after landing, and energy consumption is larger, this hair
Bright is exactly that technical problem in the prior art is solved in terms of the two.
Embodiment one, according to Fig. 1,
In the present invention, business is dispensed based on a certain range of unmanned plane, so-called a certain range, which is often referred to compare, to be less than
In normal the continuation of the journey range, such as 5 kilometer ranges of unmanned plane, the corresponding country is generally in the range of an industrial park or CBD
Office building concentration zones or an inhabitation section, according to domestic inhabitation and office present situation, the limited selection 2 of a certain range is public
In range in dispensed.It is described in detail with reference to its specific delivery process.
Firstly, it is necessary to a highest building A of height is selected then to be built as basic carrier in the range of dispatching
A set of unmanned plane Special-purpose lifting equipment 100 is installed in the side of object, lifting means using electric energy or engine as power, no
Consume the lithium battery energy of unmanned plane in itself.The lifting means has following ability：Pass through the dynamical system other than unmanned plane 200
Unmanned plane is promoted to the top of lifting means with hoisting mechanism, which is usually less than the height built, in order to nobody
The release of machine is with taking off, but nor absolute, even if height of the top of lifting means less than building, as long as by rationally setting
Meter can reach the reasonable takeoff condition of unmanned plane.
Unmanned plane 200 loads cargo (the typically less than courier packages of 5KG) should be at the ground of lifting means bottom
It carries out, the effect of lifting means is to carry out unmanned plane and its cargo elevated height, and the consumption of energy is by nothing in lifting process
Motor other than man-machine electric power system provides, this process does not consume unmanned plane self electric quantity.
After reaching predetermined altitude, unmanned plane 200 is released and takes off, due in the range, the height highest of building,
So unmanned plane tool, there are one the action dived downwards, unmanned plane does not consume energy substantially in process of subduction.When unmanned plane to bow
It rushes after posture flies to the about 2 meters of positions in release position top and adjusts posture, courier packages are discharged by way of air-drop, realization is not landed
It launches, unmanned plane can return to after dispensing.
The structure of lifting means 100 is described below, referring to figs. 2 to Fig. 4.
Including braced frame 110, chain transmission system, motor, platform etc. is promoted, wherein, braced frame 110 is using vertical
It assembles to be formed with lateral aluminium alloy extrusions, there is that certain corrosive nature, prevent by raindrop erosion.In braced frame 110
Chain transmission system 120 is set, and chain transmission system includes sprocket wheel 121, sprocket shaft 122, chain 123, chain guide and chain
Expansion tightening wheel 124, middle sprocket are four groups, are separately positioned on four corners, and chain 123 formed " mouth " font, motor around one week
130 by driving 122 drive chain system of a sprocket shaft therein to operate, that is to say, that under the drive of motor 130, chain
Item 123 is continuously rotated.Chain guide is set in 123 side of chain at vertical position, for the guiding of chain, is prevented
Only there is big deformation.In lower position, setting chain expansion tightening wheel 124, for the tensioning of chain transmission system.
Platform 140 is promoted, including L shaped plate 141 and fixed plate 142, wherein in fixed plate 142 there is strip hole 143, pass through
Screw or bolt assembly will be fixed by being fixed on chain, are wherein provided with and are picked up the ears on chain 123, for fixing fixed plate.
At least two, chain carries out good fixation to fixed plate.It is flexibly connected and (hingedly connected by round pin in the lower edge of fixed plate
Connect) L shaped plate 141, reinforcing rib is set in L shaped plate, improves integral strength.In the promotion side of chain, L shaped plate is maintained at upright
State, on another vertical plane, L shaped plate is in folded state, has the effect for reducing storage space.
Security protection can be carried out in the periphery of lifting means 100, usual way is to set protective cover, that is, make
It is protected with a shell, unmanned plane import is reserved at top, unmanned plane outlet is reserved at top.
Unmanned plane launches function introduction automatically, and with reference to figure 5 and Fig. 7, unmanned plane 200 includes groined type frame 210, supporting leg
220th, rotor module 230, power battery and flight control system module 240, scan camera shooting head module 250 and package card throw module
260, groined type frame therein is the bone frame of unmanned plane, for fixing other modules, power battery and flight control system
Module of uniting is mounted in groined type frame, and using shell protection, reduces the windage in flight course.Rotor module is mounted on well
Around glyph framework, especially corner provides power by 8 rotor modules 230 of setting for unmanned plane.
Package card throws module 260 and includes locking plate 261, nylon rope 262, rope closing capstan winch 263 and micromachine, wherein, lock
Only plate 261 is mounted on by way of pivot joint on circular shaft I, and is pre-tightened between circular shaft I and locking plate using torsional spring so that two
Locking plate 261 is symmetrically formed the layout pattern of eight shape.Corresponding courier packages use special express box, the two of express box
Side is corresponding to be provided with card slot K1, and card slot is made of two inclined-planes, with reference to figure 8 and Fig. 9, when card slot K1 is stuck in two locking plates
When between 261, accommodated by locking plate and being formed from clamping action to courier packages for torsional spring, realize locking, the effect of card slot
It is to prevent the landing of courier packages.It is guide plate 2611 in the lower part of locking plate 261, guide plate 2611 is the surface of arc,
During being flared out under pullling of the locking plate in nylon rope, courier packages slide, and during landing, guide plate is fast
Pass the guiding in package offer vertical direction so that the upright state of courier packages falls, corresponding to coordinate unmanned receive in release position
Part case.Rope closing capstan winch 263 is rotatably mounted in the abdominal cavity of unmanned plane center, is horizontally disposed with, is provided on rope closing capstan winch 263
Nylon rope fastening point 2632, two nylon ropes are set with the tooth 2631 of micromachine line shaft cooperation and on rope closing capstan winch
It is fastened on rope closing capstan winch clockwise, when rope closing capstan winch when being rotated by, realizes two nylon ropes in micromachine
While tighten or loosen.
Unmanned inbox 400 with reference to figure 10, can automatically open at the top of intelligent unmanned inbox there are one settings
Cover board 410, the cover board can be controlled by control system and opened, and address Quick Response Code 420 is provided on the cover board at top,
The Quick Response Code of addressee information is exactly represented, after unmanned plane reaches 0.5 meter of height and position above the inbox, unmanned plane passes through
After scan camera shooting head scans the Quick Response Code, after address comparison is dispensed in UAV system, package is launched if consistent, meanwhile,
The top blind flange of inbox automatically opens so that courier packages are smoothly dropped into unmanned inbox, and addressee can then pass through
The door opening 440 of side takes out the package of oneself.To avoid colliding with, sponge cushion pad is set in the bottom of unmanned inbox 400
430, carry out security protection.The cover board that the unmanned inbox of plain edition then omits top, direct open design, at top may be used
Edge placement paste address of the addressee Quick Response Code, if meet fixed condition directly launch.
The present invention is to reduce the electric power storage electric energy loss of unmanned plane and to improve the dispatching efficiency of unmanned plane as basic design mesh
, detailed statement is carried out to the present invention using above-mentioned delivery system combination procedure below.
The control system of unmanned plane has logical calculated ability and certain artificial intelligence.
According to above-mentioned purpose, the step of realizing of the invention, is as follows：
Express delivery vehicle etc. is loaded near the platform of express delivery by step 1, sets cargo platform 300, on cargo platform 300,
Barcode scanning is carried out to courier packages K using the scan code system on unmanned plane 200, obtains the information such as the dispatching address of courier packages, it will
Express delivery to be dispensed is fixed in the cabin of unmanned plane, and then unmanned plane is pushed to the bottom of lifting means and is promoted on platform 140,
Unmanned plane 200 is promoted to top by lifting means, in the process, can continuously be promoted progress sequence on platform and be loaded nobody
Machine 200；Above-mentioned cargo platform 300 carries out filling courier packages using manual or automated equipment.
Step 2, when unmanned plane under the action of promoting platform after the top position of lifting means is delivered to, at top
Unmanned plane, trigger element either barcode scanning or receive control system instruction by way of obtain instruction of taking off, received Fetion
After number, 200 rotor module of unmanned plane starts and takes off, and (is highly tens of meters of high-altitudes, usually exists since unmanned plane is in high point
Within 100), unmanned plane is dispensed according to the dispatching address of control system, in the process, the height above sea level of usual point to be dispensed
Degree, so unmanned plane 200 is dive status, in low power consuming state of flight, is launched less than the height above sea level of takeoff point when reaching
When near point, state of flight is adjusted, in order to scan address Quick Response Code；
Step 3, unmanned plane 200 scan the address Quick Response Code in unmanned inbox 400 by scanning system, confirm address
Whether consistent with the address that is recorded in UAV system, if consistent, unmanned plane 200 sends out control instruction, controls unmanned addressee
Case 400 opens top door-plate, while unmanned plane 200 acts, and is dropped, and express delivery is launched to unmanned inbox, then
Fast unmanned inbox is closed；Launch process is with reference to figure 11a-11c.
Step 4, unmanned plane return to flight, return to the dispatching origin such as express transportation vehicle according to programming route, carry out again
Secondary dispatching.
Optimize flight path, carrying out automatic calculate according to the height software for calculation in UAV system takes off highly, for example,
The height of inbox can be then taken off after unmanned plane rises to 6 meters of positions in the height of opposite 5 meters of delivery point, save flight
Time.
Optimization expense route, when encountering in flight path with barrier, best scheme is that takeoff point is higher than obstacle
The high point of object reduces the power consumption of lithium battery in loading flight course.
The above-described embodiments are merely illustrative of preferred embodiments of the present invention, not to the model of the present invention
It encloses and is defined, under the premise of design spirit of the present invention is not departed from, various changes of the relevant technical staff in the field to the present invention
Shape and improvement, should all be determined by claims of the present invention in protection domain.
Claims (10)
1. there is the unmanned plane that express delivery is launched, including
Groined type frame is a part for unmanned plane bone,
Supporting leg is a part for unmanned plane bone,
Rotor module provides flying power,
Power battery and flight control system module, provide electric energy and flight controls,
Scan camera shooting head module provides scanning and identification,
It is characterized in that, further including package card throws module, the package card throws module and includes locking plate, rope, rope closing capstan winch and micro-
Type motor, wherein, the locking plate is articulated in the circular shaft between two supporting legs, and torsional spring is used between circular shaft and locking plate
It pre-tightens so that two locking plates form the layout of symmetrical eight shape, and the rope closing capstan winch is rotatably mounted on unmanned plane machine
In cabin, the rope closing capstan winch is driven by micromachine, the rope connection locking plate and rope closing capstan winch, when rope closing capstan winch is in micro electric
When being rotated by of machine is realized and tightens or loosen while two ropes.
2. the unmanned plane according to claim 1 that there is express delivery and launch, which is characterized in that be in the lower part of locking plate
Guide plate.
3. the unmanned plane according to claim 1 that there is express delivery and launch, which is characterized in that further include the special of outfit
Express box is provided with card slot the two sides of the special express box are corresponding, and the card slot is fastened with locking plate and locked.
4. express delivery put-on method, which is characterized in that utilize the unmanned plane that there is express delivery and launch described in claims 1 to 33
Air-drop dispensing is carried out, carries out following steps：
Step 1 on cargo platform, carries out barcode scanning to courier packages using the scan code system on unmanned plane, obtains courier packages
Dispatching address information, courier packages to be dispensed are fixed in the cabin of unmanned plane, unmanned plane is promoted to pre- by lifting means
Fixed height；
Step 2, unmanned plane obtain instruction of taking off, and unmanned plane rotor module starts and takes off, and unmanned plane is with dive status low power consuming
Flight attitude flies, and when reaching near release position, adjusts state of flight, in order to scan the two dimension of the address in unmanned inbox
Code；
Step 3, unmanned plane scan the address Quick Response Code in unmanned inbox by scanning system, confirm address and unmanned plane system
Whether the address recorded in system is consistent, if unanimously, package card throws module action, is dropped, express delivery is launched to unmanned addressee
Inside case.
Step 4, unmanned plane return to flight, return to the dispatching origin such as express transportation vehicle according to programming route, are matched again
It send.
5. express delivery put-on method according to claim 4, which is characterized in that in step 3, most preferably release altitude is
Unmanned plane is apart from 0.3 to 0.5 meter of height at the top of unmanned inbox.
6. express delivery put-on method according to claim 4, which is characterized in that at the top of the unmanned inbox there are one settings
The cover board that can be automatically opened, the cover board can be controlled by control system and opened, and described address Quick Response Code is set on the cover board.
7. express delivery put-on method according to claim 6, which is characterized in that the bottom setting sponge of the unmanned inbox
Cushion pad.
8. express delivery put-on method according to claim 4, which is characterized in that the lifting means includes braced frame, chain
Transmission system, motor and platform is promoted, wherein, setting chain transmission system in the braced frame, motor drive chain passes
Dynamic system operating, the promotion platform are fixed on the chain of chain transmission system.
9. express delivery put-on method according to claim 8, which is characterized in that the promotion platform includes L shaped plate and fixation
Plate, wherein fixed plate are fixed on chain, and be articulated and connected L shaped plate in the lower edge of fixed plate.
10. express delivery put-on method according to claim 4, which is characterized in that the unmanned inbox is open design.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711393818.4A CN108146635A (en) | 2017-12-21 | 2017-12-21 | There is the unmanned plane and express delivery put-on method of express delivery dispensing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711393818.4A CN108146635A (en) | 2017-12-21 | 2017-12-21 | There is the unmanned plane and express delivery put-on method of express delivery dispensing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108146635A true CN108146635A (en) | 2018-06-12 |
Family
ID=62464887
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711393818.4A Withdrawn CN108146635A (en) | 2017-12-21 | 2017-12-21 | There is the unmanned plane and express delivery put-on method of express delivery dispensing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108146635A (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109001124A (en) * | 2018-07-03 | 2018-12-14 | 中能能控（北京）科技有限公司 | A kind of remote sensing monitoring device, system and method based on unmanned plane |
| CN109533341A (en) * | 2018-09-20 | 2019-03-29 | 广东工业大学 | A kind of logistics aircraft and cargo hold and logistics aircraft and cargo hold automatic butt, the control system and control method that separate |
| CN110091992A (en) * | 2019-05-22 | 2019-08-06 | 成都工业学院 | Cargo launches the control method of case, unmanned plane and chamber door |
| CN110968105A (en) * | 2018-09-29 | 2020-04-07 | 比亚迪股份有限公司 | Cargo transportation method, cargo transportation device, cargo transportation medium, and electronic apparatus |
| CN111977234A (en) * | 2020-07-13 | 2020-11-24 | 李隆锦 | Unmanned aerial vehicle parcel assembly system |
| CN113525686A (en) * | 2021-07-20 | 2021-10-22 | 三明学院 | Unmanned aerial vehicle and throwing device thereof |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204990395U (en) * | 2015-10-15 | 2016-01-20 | 冯雨桐 | Intelligence delivery system based on unmanned aerial vehicle |
| CN105923163A (en) * | 2016-06-01 | 2016-09-07 | 北京小米移动软件有限公司 | Transportation shelf and unmanned aerial vehicle |
| US20160257423A1 (en) * | 2014-09-09 | 2016-09-08 | Joseph Martin | Unmanned Aerial Delivery System |
| CN106542087A (en) * | 2016-11-01 | 2017-03-29 | 顺丰科技有限公司 | A kind of frame of multi-rotor unmanned aerial vehicle |
| CN106809393A (en) * | 2016-10-21 | 2017-06-09 | 北京京东尚科信息技术有限公司 | A kind of freight transportation method based on unmanned plane |
-
2017
- 2017-12-21 CN CN201711393818.4A patent/CN108146635A/en not_active Withdrawn
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20160257423A1 (en) * | 2014-09-09 | 2016-09-08 | Joseph Martin | Unmanned Aerial Delivery System |
| CN204990395U (en) * | 2015-10-15 | 2016-01-20 | 冯雨桐 | Intelligence delivery system based on unmanned aerial vehicle |
| CN105923163A (en) * | 2016-06-01 | 2016-09-07 | 北京小米移动软件有限公司 | Transportation shelf and unmanned aerial vehicle |
| CN106809393A (en) * | 2016-10-21 | 2017-06-09 | 北京京东尚科信息技术有限公司 | A kind of freight transportation method based on unmanned plane |
| CN106542087A (en) * | 2016-11-01 | 2017-03-29 | 顺丰科技有限公司 | A kind of frame of multi-rotor unmanned aerial vehicle |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109001124A (en) * | 2018-07-03 | 2018-12-14 | 中能能控（北京）科技有限公司 | A kind of remote sensing monitoring device, system and method based on unmanned plane |
| CN109533341A (en) * | 2018-09-20 | 2019-03-29 | 广东工业大学 | A kind of logistics aircraft and cargo hold and logistics aircraft and cargo hold automatic butt, the control system and control method that separate |
| CN109533341B (en) * | 2018-09-20 | 2023-05-16 | 广东工业大学 | Logistics aircraft and cargo hold, control system and control method for automatic docking and detaching of logistics aircraft and cargo hold |
| CN110968105A (en) * | 2018-09-29 | 2020-04-07 | 比亚迪股份有限公司 | Cargo transportation method, cargo transportation device, cargo transportation medium, and electronic apparatus |
| CN110091992A (en) * | 2019-05-22 | 2019-08-06 | 成都工业学院 | Cargo launches the control method of case, unmanned plane and chamber door |
| CN111977234A (en) * | 2020-07-13 | 2020-11-24 | 李隆锦 | Unmanned aerial vehicle parcel assembly system |
| CN111977234B (en) * | 2020-07-13 | 2022-02-11 | 广州雪贝儿美妆用品有限公司 | Unmanned aerial vehicle parcel assembly system |
| CN113525686A (en) * | 2021-07-20 | 2021-10-22 | 三明学院 | Unmanned aerial vehicle and throwing device thereof |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN108146635A (en) | There is the unmanned plane and express delivery put-on method of express delivery dispensing | |
| CN108128447B (en) | Terminal goods delivery method based on unmanned aerial vehicle and low-energy-consumption unmanned aerial vehicle delivery system | |
| US10352306B2 (en) | Wind turbine nacelle | |
| CN102619702B (en) | For promoting elevator system and the method for the rotor blade of wind turbine | |
| US12006911B2 (en) | Nacelle for a wind turbine | |
| CN108934165A (en) | Suspension type transport and path management system | |
| CN101754915A (en) | Container lifting method and system for implementation thereof | |
| US20220403829A1 (en) | A nacelle for a wind turbine | |
| CN109178744A (en) | Unmanned plane delivery terminal station and unmanned plane delivery system | |
| CN109178982A (en) | A kind of handler for harbour container | |
| EP3880954B1 (en) | Multirotor wind turbine comprising a logistics system | |
| CN102803710B (en) | Wind turbine generator service by airship | |
| CN108177778B (en) | Unmanned aerial vehicle for standard express continuous delivery, batch delivery model and delivery method | |
| CN112208957A (en) | Intelligent finished grain storage and transportation integrated container with self-generating device | |
| CN116118937A (en) | Battery box arrangement pattern suitable for roll-on roll-off ship | |
| US20210301791A1 (en) | Wind turbine component transport arrangement | |
| CN209193391U (en) | Mobile Cargo device | |
| CN209160965U (en) | A kind of logistics unmanned plane airport | |
| CN209506748U (en) | Unmanned plane delivery terminal station and unmanned plane delivery system | |
| CN219619372U (en) | Photovoltaic power plant fortune dimension is with small-size airship | |
| CN211810304U (en) | Auxiliary device for quickly assembling and disassembling luggage | |
| CN117163278B (en) | Hanging modularized integral cargo hold and upper single-wing cargo aircraft | |
| CN216508084U (en) | Emergency rescue flood prevention vehicle for power transmission line | |
| CN210883575U (en) | Intelligent finished grain storage and transportation integrated container with self-generating device | |
| WO2010145664A1 (en) | Wind turbine generator airship flying concept |
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 | ||
| WW01 | Invention patent application withdrawn after publication | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20180612 |