CN109229379A - A kind of take-away allocator based on unmanned dispatching aircraft - Google Patents
A kind of take-away allocator based on unmanned dispatching aircraft Download PDFInfo
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- CN109229379A CN109229379A CN201810955849.2A CN201810955849A CN109229379A CN 109229379 A CN109229379 A CN 109229379A CN 201810955849 A CN201810955849 A CN 201810955849A CN 109229379 A CN109229379 A CN 109229379A
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- aircraft
- take
- cavity
- away
- loading plate
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- 238000000034 method Methods 0.000 claims abstract description 35
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 18
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 17
- 238000001179 sorption measurement Methods 0.000 claims description 10
- 239000011248 coating agent Substances 0.000 claims description 6
- 238000000576 coating method Methods 0.000 claims description 6
- 238000004804 winding Methods 0.000 claims description 4
- 238000009825 accumulation Methods 0.000 claims description 3
- 229910052799 carbon Inorganic materials 0.000 claims description 3
- 238000006243 chemical reaction Methods 0.000 claims description 3
- 238000007667 floating Methods 0.000 claims description 2
- 238000005516 engineering process Methods 0.000 abstract description 3
- 238000012790 confirmation Methods 0.000 abstract 1
- 230000007613 environmental effect Effects 0.000 abstract 1
- 230000032258 transport Effects 0.000 description 36
- 239000000126 substance Substances 0.000 description 8
- 230000000694 effects Effects 0.000 description 7
- 238000013016 damping Methods 0.000 description 5
- 238000005265 energy consumption Methods 0.000 description 4
- 238000004140 cleaning Methods 0.000 description 3
- 230000005484 gravity Effects 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 239000002699 waste material Substances 0.000 description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 238000007599 discharging Methods 0.000 description 2
- 101000804902 Drosophila melanogaster Xaa-Pro aminopeptidase ApepP Proteins 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
Classifications
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- 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
-
- 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
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/30—Aircraft characterised by electric power plants
- B64D27/35—Arrangements for on-board electric energy production, distribution, recovery or storage
- B64D27/353—Arrangements for on-board electric energy production, distribution, recovery or storage using solar cells
-
- 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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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
- H02J7/34—Parallel operation in networks using both storage and other dc sources, e.g. providing buffering
- H02J7/35—Parallel operation in networks using both storage and other dc sources, e.g. providing buffering with light sensitive cells
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/60—UAVs specially adapted for particular uses or applications for transporting passengers; for transporting goods other than weapons
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Power Engineering (AREA)
- Management, Administration, Business Operations System, And Electronic Commerce (AREA)
Abstract
The invention belongs to unmanned distribution technology field, specifically a kind of take-away allocator based on unmanned dispatching aircraft, this method comprises the following steps: being made according to the order information of user to take-away；Take-away is packaged, is labelled；The idle unmanned dispatching aircraft of confirmation, and take-away is placed in unmanned dispatching aircraft；Take-away is sent into customer's hand by unmanned dispatching aircraft；The present invention can effectively improve the dispatching efficiency of take-away, and the present invention is protected from environmental small in the delivery process of take-away, while the present invention can ensure the quality taken out in delivery process, can dispense simultaneously to multiple take-aways.
Description
Technical field
The invention belongs to unmanned distribution technology field, specifically a kind of take-away dispatching based on unmanned dispatching aircraft
Method.
Background technique
Today's society takes out the prosperity of industry gradually and gets up, especially young man, usually with the quickening pace of modern life
Like ordering by network AP P；The important link taken out is exactly to dispense, and the positive rating in a shop also dispenses speed with it
It is related；And the speed dispensed is limited by the jam situation of urban road, happen vehicle flowrate it is big when, the dispatching speed of take-away drops significantly
It is low, while the dispatching taken out also is influenced by weather, the dispatching speed that the rainy day takes out is usually relatively slow, how to improve matching for take-away
Speed is sent, the waiting time for reducing customer, which becomes, takes out an industry problem urgently to be solved.
Summary of the invention
In order to make up for the deficiencies of the prior art, a kind of take-away distribution side based on unmanned dispatching aircraft proposed by the present invention
Method, this method dispense take-away using a kind of unmanned dispatching aircraft, and the congestion in road for avoiding city causes dispatching
Influence, improve the speed of dispatching, at the same solve the problems, such as the rainy day dispatching it is slow-paced, when reducing the waiting of customer
Between, customer is improved to the positive rating in shop.
The technical solution adopted by the present invention to solve the technical problems is: of the present invention a kind of winged based on unmanned dispatching
The take-away allocator of row device, this method comprises the following steps:
Step 1: take-away is made according to the order information of user；
Step 2: after making take-away in step 1, take-away is packaged, is labelled；
Step 3: after packed in step 2, confirm idle unmanned dispatching aircraft, and take-away is placed on nobody and is matched
It send in aircraft；
Step 4: after placing take-away in step 3, take-away is sent into customer's hand by unmanned dispatching aircraft；
Wherein, unmanned dispatching aircraft described in step 2 includes shell, kickboard, connecting rod, loading plate, dispensing cartridge, cabin
Door, shipment device, propeller and motor one；The enclosure interior is equipped with cavity one and cavity two, and cavity one is located at cavity two
Top, one section of cavity are triangle, and two section of cavity is rectangle, and two bottom of cavity is equipped with water, and water is turning to aircraft
When or when by external active force, kickboard and loading plate remain horizontal relative to the earth under the action of water, so as to avoid goods
Object inclination, improves the safety and stability when cargo transport；The kickboard is mounted on two bottom of cavity, and kickboard floats on the water
Side；The connecting rod quantity is several, and connecting rod lower end is fixed in kickboard, and small end is equipped with spring, and spring plays one to loading plate
A cushioning effect further improves the peace of cargo transport so as to avoid cargo during transportation by biggish vibration
Full property and stability；The loading plate is located in cavity two, and loading plate is mounted on the top of kickboard by connecting rod and spring, loads
Plate is equipped with several rectangular recess one, and loading plate is for loading cargo, the setting of multiple rectangular recess one, so that aircraft can be with
Multiple cargos are dispensed simultaneously, improve dispatching efficiency；The dispensing cartridge is placed on loading plate by rectangular recess one,
Dispensing cartridge is used for arrangement of goods；The hatch door is hinged on the right side of shell, and hatch door is for closing aircraft；The shipment
Device is mounted on two top of cavity, and shipment device is used to cargo sending out aircraft；The propeller is fixed on above shell, spiral shell
Rotation paddle is for driving aircraft flight；The motor one is fixed in cavity one, and motor one is used to provide power to propeller.Work
When making, cargo to be transported is placed in dispensing cartridge, then dispensing cartridge is placed sequentially in the rectangular recess one of loading plate, square
The presence of connected in star one avoids dispensing cartridge sliding during transportation, thus stability and peace when ensure that cargo transport
Quan Xing；In transportational process, hatch door is sealed aircraft, prevents cargo from falling out aircraft, band of the propeller in motor one
Dynamic lower driving aircraft flies to destination；Water in cavity two makes kickboard and loading plate under the action of water always and the earth
It keeps horizontal, turned to so as to avoid aircraft in transportational process or by cargo run-off the straight when external forces, improves goods
The safety and stability of object during transportation, are damaged when avoiding cargo transport；Connecting rod and spring make kickboard with
Loading plate links together, while the presence of spring plays the role of damping to the cargo on loading plate and loading plate, into one
Step improves the safety and stability of cargo during transportation；After eventually arriving at destination, cargo is in discharging device
Act on lower submitting aircraft.
T-shaped sliding slot is additionally provided at the top of the cavity two, the presence of T-shaped sliding slot is mounted on sky convenient for gear and motor two
The top of chamber two, T-shaped sliding slot quantity is identical with dispensing cartridge quantity, and the right side of T-shaped sliding slot is equipped with tooth；The hatch door relative to
Same T-shaped sliding slot and tooth are equipped at the top of cavity two；The shipment device includes gear, motor two, hoist engine and drawstring；Institute
Gear is stated to be mounted in T-shaped sliding slot；The motor two is mounted on two top of cavity by gear, and motor two is used for band moving gear
It is moved along the tooth on T-shaped sliding slot；The hoist engine is mounted on the left end of motor one；Drawstring one end winding is in hoist engine
On, the drawstring other end is connected with dispensing cartridge.When work, after cargo reaches the destination, hatch door is opened, T-shaped on hatch door
Slideway links together with the T-shaped slideway on cavity two, and hoist engine winding drawstring rises dispensing cartridge, and the rotation of motor two makes
It obtains gear to move outside teeth directional shell in T-shaped sliding slot, finally removes dispensing cartridge outside shell, made by releasing drawstring
Dispensing cartridge falls to destination under the effect of gravity, so that the process of automatic shipment is realized, spiral when avoiding people's picking
Paddle damages people, while having saved the time of people's picking, so that aircraft is more intelligent.
Rectangular recess two is provided on the rectangular recess one of the loading plate；The dispensing cartridge bottom is coated with magnetisable coating；
Electromagnet is provided in the rectangular recess two, electromagnet is used to adsorb dispensing cartridge or pop up.When work, magnetisable coating with
Electromagnet cooperates, so that cargo, in transport, electromagnet attracts dispensing cartridge, consolidates so that dispensing cartridge is more stable
It is scheduled on loading plate, avoids dispensing cartridge and relative motion occurs in loading plate, thus the safety during improving cargo transport
Property and stability, and then ensure that cargo during transportation and will not be damaged, it is ensured that the quality of cargo improves flight
The performance of device；Meanwhile in shipment, when the drawstring of shipment device draws dispensing cartridge, electromagnet changes polarity, makes
The rectangular recess one for obtaining the more convenient pop-up loading plate of dispensing cartridge, improves the shipment speed of shipment device.
The upper part of the housing is cone, and conical design is for reducing the resistance of wind and avoiding the accumulation of rainwater.Work
When, conical design is so that the resistance that aircraft is subject in uphill process becomes smaller, so that the energy of aircraft has been saved, into
And the effective time of aircraft is improved, meanwhile, conical design is kept away so that rainwater can not stockpile on board the aircraft
Rainwater is exempted from since long-time is accumulated on board the aircraft, has finally had part and enter in aircraft, aircraft is impacted, together
When avoid rainwater additional load caused to aircraft, to reduce the energy consumption in aircraft transportational process, further
The transport duration for improving aircraft, improves the transport capacity of aircraft.
The lower part of the shell is hemispherical, the resistance of hemispheric intensity and reduction wind designed for improving shell.
When work, hemispheric design is so that aircraft is uniformly dispersed in aircraft when by external forces, by active force
Each position improves the ability that aircraft bears ambient pressure, while hemispherical design makes the internal stress of aircraft casing
It is small, rigidity it is good, be hardly damaged, to improve the service life of aircraft；Meanwhile hemispheric design is so that aircraft is being transported
Suffered resistance is smaller during defeated, improves the flying speed of aircraft, to improve the efficiency of delivery, and then improves
The transport performance of aircraft；The reduction of resistance reduces the energy consumption in aircraft transportational process simultaneously, effectively raises flight
Device can operating time, improve the transport capacity of aircraft.
The conical position of the upper part of the housing is equipped with solar panel, and solar panel is used for conversion solar energy；
Spherical groove is also uniformly provided on the solar panel, spherical groove is for reducing solar panel to the anti-of sunlight
It penetrates；Power storage module is additionally provided in the cavity one, power storage module is used to store the electric energy of solar panel generation.When work,
The presence of solar panel makes aircraft can use the energy of sunlight in transport on daytime, to effectively save
The loss of the energy of aircraft itself, and then effective transport duration of aircraft is improved, improve the transport capacity of aircraft；
Meanwhile power storage module stores the extra electric energy that solar panel generates, and avoids the waste of electric energy, while electric power storage mould
The electric energy of block storage can also be powered aircraft at night, and aircraft is worked for a long time, effective to improve
The working efficiency and performance of aircraft；The presence of spherical groove on solar panel reduces solar panel to light
Reflection, effectively raise solar panel to the utilization rate of luminous energy, improve the electric energy of solar panel generation
Speed, to ensure that the supply to the energy of aircraft so that aircraft can efficient work for a long time, simultaneously
Improve the speed of power storage module storage electric energy；The reflection for reducing light also avoids aircraft and causes light dirty during transportation
Dye, improves the practicability of aircraft.
Activated carbon adsorption module is additionally provided on two inner wall of cavity, active carbon adsorption module is for adsorbing in cavity two
Harmful substance.When work, activated carbon adsorption module adsorbs the harmful substance in cavity two, avoids having in cavity two
Damage of the evil substance to cargo, to ensure that the quality of cargo, while ensure that the cleaning in aircraft interior space, avoids
Frequently manually aircraft interior is cleaned, has saved the loss of manpower and material resources.
Beneficial effects of the present invention are as follows:
1. a kind of take-away allocator based on unmanned dispatching aircraft of the present invention, this method using it is a kind of nobody
Dispatching aircraft dispenses take-away, avoids congestion in road influence caused by dispatching in city, improves the speed of dispatching
Degree, while solving the problems, such as that rainy day dispatching is slow-paced, reduce the waiting time of customer, improves customer to the good of shop
Comment rate.
2. a kind of take-away allocator based on unmanned dispatching aircraft of the present invention, this method use nobody match
Aircraft is sent to cooperate by water, kickboard, connecting rod, spring and the loading plate in housing hollow two, so that taking out with passing through
Cheng Zhong, kickboard and loading plate under the action of water with greatly remain horizontal, so as to avoid taking out during dispatching
It turns on one's side, it is ensured that the quality and condition of take-away, to improve the satisfaction of customer.
3. a kind of take-away allocator based on unmanned dispatching aircraft of the present invention, a kind of nothing that this method uses
People dispenses aircraft and is cooperated by the solar panel and power storage module being arranged on aircraft, so that aircraft is gathered around
Have a longer effective time, improve the distribution capacity and dispatching speed of aircraft, so as to shorten dispatching it is spent when
Between, improve dispatching efficiency.
Detailed description of the invention
Fig. 1 is flow chart of the invention；
Fig. 2 is main view of the invention；
Fig. 3 is A-A cross-sectional view in Fig. 2；
Fig. 4 is B-B cross-sectional view in Fig. 2；
In figure: shell 1, kickboard 2, connecting rod 3, loading plate 4, dispensing cartridge 5, hatch door 6, shipment device 7, propeller 8, motor one
9, T-shaped sliding slot 11, solar panel 12, power storage module 13, activated carbon adsorption module 14, electromagnet 51, gear 71, motor
2 72, hoist engine 73, drawstring 74.
Specific embodiment
It is carried out such as using take-away allocator based on unmanned dispatching aircraft of Fig. 1-Fig. 4 to an embodiment of the present invention
Lower explanation.
As shown in Figure 1 to Figure 3, a kind of take-away allocator based on unmanned dispatching aircraft of the present invention, the party
Method includes the following steps:
Step 1: take-away is made according to the order information of user；
Step 2: after making take-away in step 1, take-away is packaged, is labelled；
Step 3: after packed in step 2, confirm idle unmanned dispatching aircraft, and take-away is placed on nobody and is matched
It send in aircraft；
Step 4: after placing take-away in step 3, take-away is sent into customer's hand by unmanned dispatching aircraft；
Wherein, unmanned dispatching aircraft described in step 2 includes shell 1, kickboard 2, connecting rod 3, loading plate 4, dispensing cartridge
5, hatch door 6, shipment device 7, propeller 8 and motor 1；Cavity one and cavity two are equipped with inside the shell 1, cavity one is located at
The top of cavity two, one section of cavity are triangle, and two section of cavity is rectangle, and two bottom of cavity is equipped with water, and water to fly
When device is when turning to or by external active force, kickboard 2 and loading plate 4 remain horizontal relative to the earth under the action of water, from
And cargo tilt is avoided, improve safety and stability when cargo transport；The kickboard 2 is mounted on two bottom of cavity,
2 side of floating on the water of kickboard；3 quantity of connecting rod is several, and 3 lower end of connecting rod is fixed in kickboard 2, and 3 upper end of connecting rod is equipped with spring, bullet
Spring plays a cushioning effect to loading plate 4, so as to avoid cargo during transportation by biggish vibration, further mentions
The high safety and stability of cargo transport；The loading plate 4 is located in cavity two, and loading plate 4 is pacified by connecting rod 3 and spring
Mounted in the top of kickboard 2, loading plate 4 is equipped with several rectangular recess one, and loading plate 4 is for loading cargo, multiple rectangular recess
One setting dispenses aircraft to multiple cargos simultaneously, improves dispatching efficiency；The dispensing cartridge 5 passes through
Rectangular recess one is placed on loading plate 4, and dispensing cartridge 5 is used for arrangement of goods；The hatch door 6 is hinged on the right side of shell 1, hatch door
6 for closing aircraft；The shipment device 7 is mounted on two top of cavity, and shipment device 7, which is used to send out cargo, to fly
Row device；The propeller 8 is fixed on 1 top of shell, and propeller 8 is for driving aircraft flight；The motor 1 is fixed on sky
In chamber one, motor 1 is used to provide power to propeller 8.When work, cargo to be transported is placed in dispensing cartridge 5, then will
Dispensing cartridge 5 is placed sequentially in the rectangular recess one of loading plate 4, and the presence of rectangular recess one avoids matches during transportation
Box 5 is sent to slide, thus stability and safety when ensure that cargo transport；In transportational process, hatch door 6 carries out aircraft close
Envelope, prevents cargo from falling out aircraft, and propeller 8 drives aircraft to fly to destination under the drive of motor 1；Cavity two
Interior water makes kickboard 2 and loading plate 4 horizontal with the earth holding always under the action of water, flies so as to avoid in transportational process
Row device turns to or by cargo run-off the straight when external forces, improves the safety and stability of cargo during transportation,
It is damaged when avoiding cargo transport；Connecting rod 3 makes kickboard 2 link together with loading plate 4 with spring, while spring is deposited
To the cargo on loading plate 4 and loading plate 4 play the role of damping, further improves cargo during transportation
Safety and stability；After eventually arriving at destination, cargo sends out aircraft under the action of discharging device.
As shown in Fig. 2 and Fig. 4, T-shaped sliding slot 11 is additionally provided at the top of the cavity two, the presence of T-shaped sliding slot 11 is convenient for
Gear 71 and motor 2 72 are mounted on the top of cavity two, and T-shaped 11 quantity of sliding slot is identical with 5 quantity of dispensing cartridge, T-shaped sliding slot
11 right side is equipped with tooth；The hatch door 6 is relative to being equipped with same T-shaped sliding slot 11 and tooth at the top of cavity two；The shipment dress
Setting 7 includes gear 71, motor 2 72, hoist engine 73 and drawstring 74；The gear 71 is mounted in T-shaped sliding slot 11；The electricity
Machine 2 72 is mounted on two top of cavity by gear 71, and motor 2 72 is used for moving gear 71 along the tooth on T-shaped sliding slot 11
It is mobile；The hoist engine 73 is mounted on the left end of motor 1；On hoist engine 73, drawstring 74 is another for 74 one end of drawstring winding
One end is connected with dispensing cartridge 5.When work, after cargo reaches the destination, hatch door 6 is opened, the T-shaped slideway on hatch door 6 with
T-shaped slideway on cavity two links together, and hoist engine 73 winds drawstring 74 and dispensing cartridge 5 is made to increase, and motor 2 72 rotates
So that gear 71 moves outside teeth directional shell 1 in T-shaped sliding slot 11, finally dispensing cartridge 5 is removed outside shell 1, by putting
Drawstring 74 makes dispensing cartridge 5 fall to destination under the effect of gravity out, to realize the process of automatic shipment, avoids people
Picking when propeller 8 people are damaged, while the time of people's picking has been saved, so that aircraft is more intelligent.
As shown in Fig. 2, being provided with rectangular recess two on the rectangular recess one of the loading plate 4；5 bottom of dispensing cartridge applies
Be magnetic coating；Electromagnet 51 is provided in the rectangular recess two, electromagnet 51 is used to adsorb dispensing cartridge 5 or pop up.
When work, magnetisable coating and electromagnet 51 cooperate, so that cargo, in transport, electromagnet 51 attracts dispensing cartridge 5, thus
So that dispensing cartridge 5 is more stably fixed on loading plate 4, avoids dispensing cartridge 5 and relative motion occurs in loading plate 4, thus
The safety and stability during cargo transport are improved, and then ensure that cargo will not be damaged during transportation,
The quality for ensuring cargo improves the performance of aircraft；Meanwhile in shipment, when 74 pairs of drawstring dispatchings of shipment device 7
When box 5 is drawn, electromagnet 51 changes polarity, so that the rectangular recess one for popping up loading plate 4 that dispensing cartridge 5 is more convenient,
Improve the shipment speed of shipment device 7.
As shown in Fig. 2, 1 top of shell is cone, conical design is used to reduce the resistance of wind and avoids rainwater
Accumulation.When work, conical design is so that the resistance that aircraft is subject in uphill process becomes smaller, to save flight
The energy of device, and then the effective time of aircraft is improved, meanwhile, conical design is so that rainwater can not fly
It is stockpiled on device, avoids rainwater since long-time is accumulated on board the aircraft, finally have part and enter in aircraft, to aircraft
It impacts, while avoiding rainwater and additional load is caused to aircraft, to reduce the energy in aircraft transportational process
Consumption, further improves the transport duration of aircraft, improves the transport capacity of aircraft.
As shown in Fig. 2, the lower part of the shell 1 be hemispherical, it is hemispheric designed for improve shell 1 intensity with subtract
The resistance of small wind.When work, hemispheric design is so that aircraft uniformly disperses when by external forces, by active force
At each position of aircraft, the ability that aircraft bears ambient pressure is improved, while hemispherical design makes aircraft shell
The internal stress of body 1 is small, rigidity is good, is hardly damaged, to improve the service life of aircraft；Meanwhile hemispheric design makes
Aircraft suffered resistance is smaller during transportation, the flying speed of aircraft is improved, to improve the effect of delivery
Rate, and then improve the transport performance of aircraft；The reduction of resistance reduces the energy consumption in aircraft transportational process simultaneously, effectively
Improve aircraft can operating time, improve the transport capacity of aircraft.
As shown in Fig. 2, the conical position on 1 top of shell is equipped with solar panel 12, solar panel 12
For conversion solar energy；Spherical groove is also uniformly provided on the solar panel 12, spherical groove is for reducing solar energy
Reflection of the solar panel 12 to sunlight；Power storage module 13 is additionally provided in the cavity one, power storage module 13 is for storing solar energy
The electric energy that solar panel 12 generates.When work, the presence of solar panel 12 can use aircraft in transport on daytime
The energy of sunlight to effectively save the loss of the energy of aircraft itself, and then improves effective fortune of aircraft
Defeated duration improves the transport capacity of aircraft；Meanwhile the extra electric energy that solar panel 12 is generated of power storage module 13 into
Row storage avoids the waste of electric energy, while the electric energy that power storage module 13 stores can also be powered aircraft at night, make
Obtaining aircraft can work for a long time, effectively raise the working efficiency and performance of aircraft；On solar panel 12
The presence of spherical groove reduce the reflection of 12 pairs of light of solar panel, effectively raise 12 pairs of light of solar panel
The utilization rate of energy improves the speed of the electric energy of the generation of solar panel 12, to ensure that the confession to the energy of aircraft
Give so that aircraft can efficient work for a long time, while improving the speed that power storage module 13 stores electric energy；Subtract
The reflection of small light also avoids aircraft and causes light pollution during transportation, improves the practicability of aircraft.
As shown in Fig. 2, being additionally provided with activated carbon adsorption module 14 on two inner wall of cavity, active carbon adsorption module is for inhaling
Harmful substance in attached cavity two.When work, activated carbon adsorption module 14 adsorbs the harmful substance in cavity two, avoids
Damage of the harmful substance to cargo in cavity two to ensure that the quality of cargo, while ensure that aircraft interior sky
Between cleaning, avoid and frequently manually aircraft interior cleaned, saved the loss of manpower and material resources.
Concrete operations process is as follows:
When work, cargo to be transported is placed in dispensing cartridge 5, then dispensing cartridge 5 is placed sequentially in the square of loading plate 4
In connected in star one, the presence of rectangular recess one avoids the sliding of dispensing cartridge 5 during transportation, to ensure that cargo transport
When stability and safety；In transportational process, hatch door 6 is sealed aircraft, prevents cargo from falling out aircraft, spiral
Paddle 8 drives aircraft to fly to destination under the drive of motor 1；Water in cavity two makes kickboard 2 and loading plate 4 in water
Under the action of keep horizontal with the earth always, turned to so as to avoid aircraft in transportational process or by cargo when external forces
Run-off the straight improves the safety and stability of cargo during transportation, is damaged when avoiding cargo transport；Connecting rod
3 kickboards 2 made with spring link together with loading plate 4, while the presence of spring is to the cargo on loading plate 4 and loading plate 4
Play the role of damping, further improves the safety and stability of cargo during transportation, it is more on loading plate 4
The setting of group rectangular recess, dispenses aircraft to multiple cargos simultaneously, improves dispatching efficiency；It transports simultaneously
When interacted by the magnetisable coating of electromagnet 51 and 5 bottom of dispensing cartridge so that dispensing cartridge 5 is adsorbed by electromagnet 51, thus
It further ensure that the stability and safety when cargo transport；After eventually arriving at destination, hatch door 6 is opened, on hatch door 6
T-shaped slideway link together with the T-shaped slideway on cavity two, hoist engine 73 wind drawstring 74 pull dispensing cartridge 5, electromagnetism
51 reversing of iron makes dispensing cartridge 5 pop up rectangular recess one, after dispensing cartridge 5 is drawn high certain altitude by drawstring 74, motor 2 72
Rotation finally removes dispensing cartridge 5 outside shell 1 so that gear 71 moves outside teeth directional shell 1 in T-shaped sliding slot 11, leads to
Crossing releasing drawstring 74 makes dispensing cartridge 5 fall to destination under the effect of gravity, to realize the process of automatic shipment, avoids
Propeller 8 damages people when people's picking, while having saved the time of people's picking, so that aircraft more intelligence
Energy.
In the process, conical design is so that the resistance that aircraft is subject in uphill process becomes smaller, to save winged
The energy of row device, and then the effective time of aircraft is improved, meanwhile, conical design is so that rainwater can not fly
It is stockpiled on device, avoids rainwater since long-time is accumulated on board the aircraft, finally have part and enter in aircraft, to aircraft
It impacts, while avoiding rainwater and additional load is caused to aircraft, to reduce the energy in aircraft transportational process
Consumption, further improves the transport duration of aircraft, improves the transport capacity of aircraft.
Hemispheric design so that aircraft suffered resistance is smaller during transportation, improve the flight speed of aircraft
Degree, to improve the efficiency of delivery, and then improves the transport performance of aircraft；Aircraft has been saved in the reduction of resistance simultaneously
Energy consumption in transportational process, effectively raise aircraft can operating time, improve the transport capacity of aircraft.
The presence of solar panel 12 makes aircraft can use the energy of sunlight in transport on daytime, to have
The loss of the energy for having saved aircraft itself of effect, and then effective transport duration of aircraft is improved, improve aircraft
Transport capacity；Meanwhile the extra electric energy that power storage module 13 generates solar panel 12 stores, and avoids electric energy
Waste, at the same power storage module 13 store electric energy aircraft can also be powered at night, allow aircraft for a long time
Work, effectively raise the working efficiency and performance of aircraft；The presence of spherical groove on solar panel 12 subtracts
The small reflection of 12 pairs of light of solar panel, effectively raises solar panel 12 to the utilization rate of luminous energy, improves
The speed for the electric energy that solar panel 12 generates, to ensure that the supply to the energy of aircraft, so that aircraft
Can efficient work for a long time, while improving the speed that power storage module 13 stores electric energy；The reflection for reducing light also avoids
Aircraft causes light pollution during transportation, improves the practicability of aircraft.
Activated carbon adsorption module 14 adsorbs the harmful substance in cavity two, avoids the harmful substance in cavity two
Damage to cargo to ensure that the quality of cargo, while ensure that the cleaning in aircraft interior space, avoid frequent
Manually aircraft interior is cleaned, has saved the loss of manpower and material resources.
More than, it is illustrated about one embodiment of the present invention, but the present invention is not limited to the above embodiments, not
Various changes are able to carry out in the range of disengaging present subject matter.
(A) in the above-described embodiment, kickboard and loading plate are linked together by connecting rod and spring, is realized to loading
The connection and damping of plate, but not limited to this, directly kickboard and loading plate can also be linked together by spring, be realized to dress
The connection and damping of support plate.
Industrial applicibility
According to the present invention, the method can effectively improve the dispatching speed of take-away, while guarantee to take out in delivery process
In quality, so that this take-away allocator based on unmanned dispatching aircraft is useful in unmanned distribution technology field.
Claims (7)
1. a kind of take-away allocator based on unmanned dispatching aircraft, it is characterised in that: this method comprises the following steps:
Step 1: take-away is made according to the order information of user；
Step 2: after making take-away in step 1, take-away is packaged, is labelled；
Step 3: after packed in step 2, confirm idle unmanned dispatching aircraft, and take-away is placed on unmanned dispatching and is flown
In row device；
Step 4: after placing take-away in step 3, take-away is sent into customer's hand by unmanned dispatching aircraft；
Wherein, unmanned dispatching aircraft described in step 2 includes shell (1), kickboard (2), connecting rod (3), loading plate (4), matches
Send box (5), hatch door (6), shipment device (7), propeller (8) and motor one (9)；Be equipped with inside the shell (1) cavity one with
Cavity two, cavity one are located at the top of cavity two, and one section of cavity is triangle, and two section of cavity is rectangle, two bottom of cavity
Equipped with water；The kickboard (2) is mounted on two bottom of cavity, kickboard (2) side of floating on the water；Connecting rod (3) quantity is several, connecting rod
(3) lower end is fixed on kickboard (2), and connecting rod (3) upper end is equipped with spring；The loading plate (4) is located in cavity two, loading plate
(4) top of kickboard (2) is mounted on by connecting rod (3) and spring, loading plate (4) is equipped with several rectangular recess one, loading plate
(4) for loading cargo；The dispensing cartridge (5) is placed on loading plate (4) by rectangular recess one, and dispensing cartridge (5) is for putting
Set cargo；The hatch door (6) is hinged on the right side of shell (1), and hatch door (6) is for closing aircraft；The shipment dress
It sets (7) and is mounted on two top of cavity, shipment device (7) is used to cargo sending out aircraft；The propeller (8) is fixed on shell
(1) top, propeller (8) is for driving aircraft flight；The motor one (9) is fixed in cavity one, and motor one (9) is used for
Power is provided to propeller (8).
2. a kind of take-away allocator based on unmanned dispatching aircraft according to claim 1, it is characterised in that: described
It is additionally provided at the top of cavity two T-shaped sliding slot (11), T-shaped sliding slot (11) quantity is identical with dispensing cartridge (5) quantity, T-shaped sliding slot
(11) right side is equipped with tooth；The hatch door (6) is relative to being equipped with same T-shaped sliding slot (11) and tooth at the top of cavity two；It is described
Shipment device (7) includes gear (71), motor two (72), hoist engine (73) and drawstring (74)；The gear (71) is mounted on T word
In shape sliding slot (11)；The motor two (72) is mounted on two top of cavity by gear (71), and motor two (72) is used for band movable tooth
It is mobile along the tooth on T-shaped sliding slot (11) to take turns (71)；The hoist engine (73) is mounted on the left end of motor one (9)；The drawing
The winding of (74) one end restrict on hoist engine (73), drawstring (74) other end is connected with dispensing cartridge (5).
3. a kind of take-away allocator based on unmanned dispatching aircraft according to claim 1, it is characterised in that: described
Rectangular recess two is provided on the rectangular recess one of loading plate (4)；Dispensing cartridge (5) bottom is coated with magnetisable coating；The square
It is provided in connected in star two electromagnet (51), electromagnet (51) is used to adsorb dispensing cartridge (5) or pop up.
4. a kind of take-away allocator based on unmanned dispatching aircraft according to claim 1, it is characterised in that: described
Shell (1) top is cone, and conical design is for reducing the resistance of wind and avoiding the accumulation of rainwater.
5. a kind of take-away allocator based on unmanned dispatching aircraft according to claim 1, it is characterised in that: described
The lower part of shell (1) is hemispherical, the resistance of hemispheric intensity and reduction wind designed for improving shell (1).
6. a kind of take-away allocator based on unmanned dispatching aircraft according to claim 1, it is characterised in that: described
The conical position on shell (1) top is equipped with solar panel (12), and solar panel (12) is used for conversion solar energy；Institute
It states and is also uniformly provided with spherical groove on solar panel (12), spherical groove is for reducing solar panel (12) to the sun
The reflection of light；It is additionally provided in the cavity one power storage module (13), power storage module (13) is for storing solar panel (12)
The electric energy of generation.
7. a kind of take-away allocator based on unmanned dispatching aircraft according to claim 1, it is characterised in that: described
It is additionally provided on two inner wall of cavity activated carbon adsorption module (14), active carbon adsorption module is used to adsorb the nuisance in cavity two
Matter.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810955849.2A CN109229379B (en) | 2018-08-21 | 2018-08-21 | Takeaway distribution method based on unmanned distribution aircraft |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810955849.2A CN109229379B (en) | 2018-08-21 | 2018-08-21 | Takeaway distribution method based on unmanned distribution aircraft |
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| CN109229379B CN109229379B (en) | 2020-12-08 |
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| CN109229379B (en) | 2020-12-08 |
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