CN111559505A - Intelligent express logistics device for flying and transporting - Google Patents
Intelligent express logistics device for flying and transporting Download PDFInfo
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- CN111559505A CN111559505A CN202010426133.0A CN202010426133A CN111559505A CN 111559505 A CN111559505 A CN 111559505A CN 202010426133 A CN202010426133 A CN 202010426133A CN 111559505 A CN111559505 A CN 111559505A
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- Prior art keywords
- block
- cavity
- transmission
- charging
- spring
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS 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
- B64D1/10—Stowage arrangements for the devices in aircraft
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L53/00—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles
- B60L53/10—Methods of charging batteries, specially adapted for electric vehicles; Charging stations or on-board charging equipment therefor; Exchange of energy storage elements in electric vehicles characterised by the energy transfer between the charging station and the vehicle
- B60L53/14—Conductive energy transfer
- B60L53/16—Connectors, e.g. plugs or sockets, specially adapted for charging electric vehicles
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L2200/00—Type of vehicles
- B60L2200/10—Air crafts
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/70—Energy storage systems for electromobility, e.g. batteries
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/7072—Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02T90/10—Technologies relating to charging of electric vehicles
- Y02T90/14—Plug-in electric vehicles
Abstract
The invention discloses an intelligent express delivery logistics device for flying transportation, which comprises a lower shell, wherein a charging cavity with an upward opening is arranged in the lower shell, conductive rods fixedly arranged in the left and right end walls of the charging cavity are arranged in bilateral symmetry of the charging cavity, one side, far away from the center line of the charging cavity, of each conductive rod is electrically connected with a storage power supply, one side, far away from the center line of the charging cavity, of each storage power supply is electrically connected with a transmission pipe, the upper end of each transmission pipe is fixedly provided with a solar power generation board which is bilaterally symmetrical along the center line of the charging cavity, the single express delivery corresponds to the single transportation, the loss of express delivery is prevented, the safety of the express delivery can be ensured to the maximum extent, the express delivery can be delivered to the addressees at the fastest speed at the first time, excessive manual processes and intervention cannot be carried out in the middle, and the damage and loss probability of express, and inside shock-absorbing function that is equipped with can not bump the express delivery case because of jolting of flight.
Description
Technical Field
The invention relates to the technical field of logistics transportation, in particular to an intelligent logistics device for flying and transporting express.
Background
Most of express delivery at the present stage is carried by manpower together to reduce cost, but individual express delivery such as some company contracts and other emergencies are needed to be sent at the fastest speed, the express delivery is difficult to achieve, although the express delivery can be carried out smoothly and emergently in the fastest time, a plurality of processes can be carried out in the middle of the express delivery, except the express delivery in the same city, the express delivery in other cities is difficult to reach in the same day, so that the addressees are delayed to receive the express delivery to cause economic loss, the timeliness can not be guaranteed compared with manual transportation, and the express delivery can be delayed due to various accidents always occurring in ground transportation.
The application illustrates an intelligence flight transportation express delivery logistics device can solve the above-mentioned problem.
Disclosure of Invention
Aiming at the defects of the technology, the invention provides an intelligent express delivery logistics device for flying and transporting, which can overcome the defects.
The invention discloses an intelligent express delivery logistics device for flight transportation, which comprises a lower shell, wherein a charging cavity with an upward opening is arranged in the lower shell, conductive rods fixedly installed in the left end wall and the right end wall of the charging cavity are arranged in the charging cavity in a bilateral symmetry manner, one side, far away from the center line of the charging cavity, of each conductive rod is electrically connected with a storage power supply, one side, far away from the center line of the charging cavity, of each storage power supply is electrically connected with a transmission pipe, and the upper end of each transmission pipe is fixedly provided with a solar power generation panel which is bilaterally symmetrical along the center line of the charging cavity; the upper end of the solar power generation panel extends out of the upper end face of the lower shell, extension cavities communicated with the charging cavity are arranged along the center line of the charging cavity in a bilateral symmetry mode, a linking cavity is arranged below the extension cavities in a communicating mode, one side, far away from the center line of the charging cavity, of the linking cavity is provided with a lower pressure cavity in a communicating mode, an upper pressure groove with an upward opening is arranged above the lower pressure cavity in a communicating mode, waterproof components are arranged in the extension cavities in the bilateral symmetry mode and comprise waterproof blocks installed in the side, close to the center line of the charging cavity, of the extension cavities in a sliding mode, one side, far away from the center line of the charging cavity, of each waterproof block is fixedly connected with a guide block, and one end, far away from the center line of the charging cavity, of each guide block extends; the terminal surface has set firmly fixed connection piece under the guide block, the fixed connection piece lower extreme has set firmly slidable mounting and has been in extend the lower sliding block in the chamber lower extreme wall, the installation of terminal surface internal rotation is equipped with rotatory pivot before the lower sliding block, the last rotation mounting of rotatory pivot is equipped with the connecting rod, the connecting rod is kept away from the installation of charging chamber central line one end rear end face internal rotation is equipped with the rotation pivot, it is equipped with slidable mounting and is in to rotate pivot rear end the lower moving block of holding down the pressure intracavity, the moving block lower extreme has set firmly pressure spring down, pressure spring sets firmly in the chamber lower extreme wall of holding down, the moving block upper end extends to down go up the pressure tank in set firmly and move the piece.
Preferably, an insulating spring is fixedly arranged on the lower end face of the charging cavity, a conductive block is fixedly arranged above the insulating spring, a power transmission block is arranged at the upper end of the conductive block in a power connection mode, and the left end and the right end of the conductive block are in power connection with the conductive rods in bilateral symmetry.
Preferably, a flying transport block is arranged above the lower shell, support foot blocks which are bilaterally symmetrical along the central line of the flying transport block are fixedly arranged on the lower end face of the flying transport block, the support foot blocks fall into the upper pressure groove and fall on the upper end face of the upper moving block, a charging head fixedly arranged on the lower end face of the flying transport block is arranged in the middle of the support foot blocks which are bilaterally symmetrical, the charging head is electrically connected with the electricity transmission block to charge the device, a placing cavity with an opening facing left is arranged in the flying transport block, a fixed spring is fixedly arranged on the right end face of the placing cavity, a pressure block is fixedly arranged at the left end of the fixed spring, an ultrasonic identification controller is fixedly arranged on the upper end face of the flying transport block, an ultrasonic transmitter fixedly arranged on the left end face of the flying transport block is fixedly connected with the left end of the ultrasonic identification controller, an input device fixedly arranged in the upper end face of the flying transport block is arranged on the, the lower end of the input device is fixedly connected with an identification controller, and a transmission cavity is arranged in the upper end wall of the placing cavity.
Preferably, a transmission spring is fixedly arranged in the upper end wall of the transmission cavity, a transmission sliding block is fixedly arranged at the lower end of the transmission spring, the transmission sliding block is slidably arranged in the upper end wall of the transmission cavity, a transmission shaft is rotatably arranged in the lower end face of the transmission sliding block, a transmission gear is fixedly arranged on the transmission shaft, the lower end of the transmission shaft is rotatably arranged in the upper end face of a magnet, an electromagnet fixedly arranged in the lower end wall of the transmission cavity is arranged below the magnet, a rotating gear is arranged on the right side of the transmission gear and fixedly arranged on a driving shaft, the lower end of the driving shaft is in power connection with a motor fixedly arranged in the lower end wall of the transmission cavity, a connecting gear is arranged on the left side of the transmission gear and fixedly arranged on the transmission shaft, a rotating shaft is fixedly connected, the switch door right-hand member face has set firmly left coupling spring, left side coupling spring right-hand member has set firmly left clamp tight piece, place the chamber around the symmetry be equipped with fixed mounting place linking spring on the end wall around the chamber, linking spring is close to place chamber central line one end and has set firmly the removal and press from both sides tight piece, place and set firmly the recognizer of making a video recording on the chamber upper end wall.
Preferably, two sliding cavities are arranged in the upper end wall of the placing cavity in an array mode and are communicated through a screw rod cavity, the opening of the screw rod cavity faces right, a screw rod is rotatably arranged on the left end wall of the screw rod cavity, a rotating block is fixedly arranged outside the right end of the screw rod extending out of the flying transport block, a clamping and fixing component is arranged in the sliding cavity and comprises a movable thread block which is in threaded connection with the screw rod, a connecting rotating shaft is rotatably arranged on the front end surface of the movable threaded block, a connecting block is rotatably arranged on the connecting rotating shaft, the left side of the connecting rotating shaft is provided with a connecting rotating shaft which is rotatably arranged in the rear end surface of the connecting block, the rear end of the connecting rotating shaft is rotatably arranged in the front end surface of the upper sliding block, the lower end of the upper sliding block extends to the placing cavity and is fixedly provided with an upper connecting spring, and the lower end of the upper connecting spring is fixedly provided with an upper clamping block.
The beneficial effects are that: the express box has the advantages that the express is correspondingly transported in a single way, the express is prevented from being lost, the express box can be transported in a flying way, the safety of the express can be guaranteed to the maximum extent, the express can be delivered to a receiver at the fastest speed in the first time, excessive manual processes and intervention cannot be performed in the middle, the damage and the loss probability of express articles are avoided, the shock absorption function is arranged in the express box, and the express box cannot be impacted due to the bumping of the flying way.
Drawings
In order to more clearly illustrate the embodiments of the invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the invention, and it is obvious for those skilled in the art that other drawings can be obtained based on these drawings without creative efforts.
FIG. 1 is a schematic structural diagram of an embodiment of the present invention;
FIG. 2 is a schematic view of A-A of FIG. 1 according to an embodiment of the present invention;
FIG. 3 is an enlarged schematic view of the structure at B in FIG. 1 according to an embodiment of the present invention;
fig. 4 is an enlarged schematic view of the structure at C in fig. 1 according to the embodiment of the present invention.
Detailed Description
All of the features disclosed in this specification, or all of the steps in any method or process so disclosed, may be combined in any combination, except combinations and/or steps that are mutually exclusive.
The invention will now be described in detail with reference to fig. 1-4, for convenience of description, the following orientations will now be defined: the up, down, left, right, and front-back directions described below correspond to the up, down, left, right, and front-back directions in the projection relationship of fig. 1 itself.
The invention relates to an intelligent express logistics device for flight transportation, which comprises a lower shell 22, wherein a charging cavity 72 with an upward opening is arranged in the lower shell 22, conductive rods 12 fixedly arranged in the left and right end walls of the charging cavity 72 are arranged in the charging cavity 72 in a bilateral symmetry manner, one side, far away from the center line of the charging cavity 72, of each conductive rod 12 is electrically connected with a storage power supply 11, one side, far away from the center line of the charging cavity 72, of each storage power supply 11 is electrically connected with a transmission pipe 10, the upper end of each transmission pipe 10 is fixedly provided with a solar power generation plate 25 which is bilaterally symmetrical along the center line of the charging cavity 72, the upper end of each solar power generation plate 25 extends out of the upper end surface of the lower shell 22, extension cavities 53 which are communicated with the charging cavity 72 are arranged in a bilateral symmetry manner along the center line of the charging cavity 72, a connection cavity 50 is communicated below the extension cavities 53, and one side, far away from the center line of the, the upper portion of the lower pressure cavity 16 is communicated with an upper pressure groove 21 with an upward opening, the extending cavity 53 is bilaterally symmetrical, a waterproof assembly is arranged in the extending cavity 53 and comprises a waterproof block 55 which is slidably mounted in the extending cavity 53 and close to the charging cavity 72 on one side of the central line, one side, far away from the central line, of the charging cavity 72, the waterproof block 55 is fixedly connected with a guide block 54, one end, far away from the central line, of the charging cavity 72 extends into the end wall, far away from the central line, of the extending cavity 53, the lower end face of the guide block 54 is fixedly provided with a fixed connecting block 52, the lower end of the fixed connecting block 52 is fixedly provided with a lower sliding block 51 which is slidably mounted in the end wall, far away from the central line, of the extending cavity 53, the front end face of the lower sliding block 51 is rotatably mounted with a rotating shaft 49, the rotating shaft 49 is rotatably mounted on the rotating shaft 49 and provided with, the rear end of the rotating shaft 19 is rotatably provided with a lower moving block 18 which is slidably arranged in the lower pressure cavity 16, the lower end of the lower moving block 18 is fixedly provided with a pressure spring 17, the pressure spring 17 is fixedly arranged in the lower end wall of the lower pressure cavity 16, and the upper end of the lower moving block 18 extends to the upper pressure groove 21 and is fixedly provided with an upper moving block 23.
Beneficially, an insulating spring 15 is fixedly arranged on the lower end face of the charging cavity 72, a conductive block 14 is fixedly arranged above the insulating spring 15, a conductive block 13 is electrically connected to the upper end of the conductive block 14, and the left end and the right end of the conductive block 14 are electrically connected to the conductive rod 12 which is symmetrical left and right.
Beneficially, a flying transport block 26 is arranged above the lower shell 22, a support foot block 24 which is bilaterally symmetrical along the central line of the flying transport block 26 is fixedly arranged on the lower end surface of the flying transport block 26, the support foot block 24 falls in the upper pressure groove 21 and falls on the upper end surface of the upper moving block 23, a charging head 56 which is fixedly arranged on the lower end surface of the flying transport block 26 is arranged in the middle of the support foot block 24 which is bilaterally symmetrical, the charging head 56 is electrically connected with the power transmission block 13 to charge the device, a placing cavity 30 with an opening facing to the left is arranged in the flying transport block 26, a fixed spring 45 is fixedly arranged on the right end surface of the placing cavity 30, a pressure block 44 is fixedly arranged at the left end of the fixed spring 45, an ultrasonic identification controller 58 is fixedly arranged on the upper end surface of the flying transport block 26, an ultrasonic emitter 57 which is fixedly arranged on the left end surface of the flying transport block 26 is connected and controlled by the, the right side of the ultrasonic identification controller 58 is provided with an input device 35 fixedly installed in the upper end face of the flying transport block 26, the lower end of the input device 35 is fixedly connected with an identification controller 34, the upper end wall of the placing cavity 30 is internally provided with a transmission cavity 59, the camera shooting identifier 42 identifies the delivery address on the express box and then automatically plans a route, then the device flies away from the lower shell 22, the ultrasonic emitter 57 starts to generate ultrasonic waves in flight and transmits the ultrasonic waves to the ultrasonic identification controller 58, and the ultrasonic identification controller 58 controls the device to turn to prevent the obstacle from colliding in flight.
Advantageously, a transmission spring 61 is fixedly arranged in the upper end wall of the transmission cavity 59, a transmission sliding block 60 is fixedly arranged at the lower end of the transmission spring 61, the transmission sliding block 60 is slidably arranged in the upper end wall of the transmission cavity 59, a transmission shaft 63 is rotatably arranged in the lower end face of the transmission sliding block 60, a transmission gear 64 is fixedly arranged on the transmission shaft 63, the lower end of the transmission shaft 63 is rotatably arranged in the upper end face of a magnet 69, an electromagnet 68 fixedly arranged in the lower end wall of the transmission cavity 59 is arranged below the magnet 69, a rotation gear 65 is arranged on the right side of the transmission gear 64, the rotation gear 65 is fixedly arranged on a driving shaft 66, the lower end of the driving shaft 66 is in power connection with a motor 67 fixedly arranged in the lower end wall of the transmission cavity 59, a connecting gear 70 is arranged on the left side of the transmission gear 64, the connecting, the terminal surface has set firmly switch door 27 under the axis of rotation 46, switch door 27 right-hand member face has set firmly left coupling spring 28, left side coupling spring 28 right-hand member has set firmly left clamp piece 29, it is equipped with fixed mounting to place chamber 30 front and back symmetry and link up spring 48 on the end wall of placing chamber 30 front and back, link up spring 48 and be close to place chamber 30 central line one end and have set firmly and remove clamp piece 47, it has set firmly to make a video recording recognizer 42 on the end wall of placing chamber 30, when discerning far address, can automatic planning route according to self electric quantity, fall to the express delivery distribution point of all parts of the country down carry out automatic charging on the lower casing 22, flight transportation piece 26 falls to when going up the casing 22, support foot piece 24 fall earlier to go up in the pressure groove 21 and drive go up the removal piece 23 and move down, thereby it drives to go up removal piece 23 move down 18 moves down and compresses pressure A spring 17, wherein the lower moving block 18 moves downwards to drive the lower moving block 51 to move away from the side of the center line of the charging chamber 72 through the connecting rod 20, the lower moving block 51 moves downwards to drive the guide block 54 to move away from the side of the center line of the charging chamber 72 through the fixed connecting block 52, the guide block 54 moves away from the side of the center line of the charging chamber 72 to drive the waterproof block 55 to move away from the side of the center line of the charging chamber 72, the waterproof block 55 moves away from the side of the center line of the charging chamber 72 to open the upward opening of the charging chamber 72 and to move the charging head 56 to the charging chamber 72 and electrically connect with the conductive block 13 and drive the conductive block 13 to move downwards, the conductive block 13 moves downwards to drive the conductive block 14 to move downwards, the conductive block 14 moves downwards to compress the insulating spring 15 and electrically connect with the conductive rod 12, and the flying transport block 26 is rapidly charged by the storage power source 11 which is bilaterally symmetrical, and when the charging is completed, the flying transport block 26 flies away from the lower case 22 again.
Beneficially, the two sliding cavities 38 are arranged in the upper end wall of the placing cavity 30 in an array, the sliding cavities 38 are communicated through a screw rod cavity 62, the opening of the screw rod cavity 62 faces right, a screw rod 39 is arranged on the left end wall of the screw rod cavity 62 in a rotationally mounted manner, a rotating block 43 is fixedly arranged at the right end of the screw rod 39 and extends out of the right end of the flight transportation block 26, a clamping and fixing component is arranged in the sliding cavity 38 and comprises a moving screw block 41 in threaded connection with the screw rod 39, a connecting rotating shaft 40 is arranged on the front end face of the moving screw block 41 in a rotationally mounted manner, a connecting block 37 is arranged on the connecting rotating shaft 40 in a rotationally mounted manner, a connecting rotating shaft 36 is arranged on the left side of the connecting shaft 40 in the rear end face of the connecting block 37 in a rotationally mounted manner, the rear end of the connecting rotating shaft 36 is rotatably mounted in the front end face of the upper sliding, the lower end of the upper connecting spring 32 is fixedly provided with an upper clamping block 31, a courier inputs a password into the input unit 35, the recognition controller 34 controls the motor 67 to be started in the forward direction and to electrify the electromagnet 68 after sensing correct recognition, the electromagnet 68 is electrified to generate magnetic force, the electromagnet 68 generates magnetic force to adsorb the magnet 69 to move downwards, the magnet 69 moves downwards to drive the transmission shaft 63 to move downwards, the transmission shaft 63 moves downwards to drive the transmission sliding block 60 and the transmission gear 64 to move downwards, the transmission sliding block 60 moves downwards to stretch the transmission spring 61, the transmission gear 64 moves downwards to be meshed with the rotating gear 65 and the connecting gear 70, the motor 67 is started to drive the driving shaft 66 to rotate, and the driving shaft 66 rotates to drive the rotating gear 65 to rotate, thereby the running gear 65 rotates and drives drive gear 64 rotates, thereby drive gear 64 rotates and drives connecting gear 70 rotates, thereby connecting gear 70 rotates and drives transmission shaft 71 rotates, thereby transmission shaft 71 rotates and drives axis of rotation 46 rotates, thereby axis of rotation 46 rotates and drives switch door 27 rotates, thereby switch door 27 rotates through left coupling spring 28 drive left clamp block 29 rotates out place in the chamber 30.
In the initial state: the waterproof block 55 seals the upward opening of the charging cavity 72, and the upper moving block 23 seals the upward opening of the upper pressure tank 21.
When the work is started: 1. the courier inputs a password in the input unit 35, then the recognition controller 34 senses correct recognition and controls the motor 67 to be started in a forward direction and to enable the electromagnet 68 to be electrified, the electromagnet 68 is electrified to generate a magnetic force, the electromagnet 68 generates a magnetic force to attract the magnet 69 to move downwards, the magnet 69 moves downwards to drive the transmission shaft 63 to move downwards, the transmission shaft 63 moves downwards to drive the transmission slide block 60 and the transmission gear 64 to move downwards, the transmission slide block 60 moves downwards to stretch the transmission spring 61, the transmission gear 64 moves downwards to be in gear engagement with the rotating gear 65 and the connecting gear 70, meanwhile, the motor 67 is started to drive the driving shaft 66 to rotate, and the driving shaft 66 rotates to drive the rotating gear 65 to rotate, thereby the running gear 65 rotates and drives drive gear 64 rotates, thereby drive gear 64 rotates and drives connecting gear 70 rotates, thereby connecting gear 70 rotates and drives transmission shaft 71 rotates, thereby transmission shaft 71 rotates and drives axis of rotation 46 rotates, thereby axis of rotation 46 rotates and drives switch door 27 rotates, thereby switch door 27 rotates through left coupling spring 28 drive left clamp block 29 rotates out place in the chamber 30.
2. Then, the express box is placed in the placing cavity 30, pushed into the placing cavity 30 and drives the movable clamping block 47 to move to the side far away from the central line of the placing cavity 30, so as to compress the connecting spring 48, so that the express is not subjected to too large an extrusion force to prevent damage to the express, simultaneously, the pressure block 44 is driven to move to the right and the fixed spring 45 is driven to compress so that the express is not subjected to too large an extrusion force to prevent damage to the express, then the rotating block 43 is manually rotated, the rotating block 43 is rotated to drive the lead screw 39 to rotate, the lead screw 39 is rotated to drive the movable threaded block 41 to move to the left, the movable threaded block 41 moves to the left through the connecting block 37 so as to drive the upper sliding block 33 to move downwards, and the upper sliding block 33 moves downwards through the upper connecting spring 32 so as to drive the upper clamping block 31 to move downwards, the upper clamping block 31 moves downwards to contact with the express box and then compresses the upper connecting spring 32 to prevent the express from being damaged by too large extrusion force, then the courier inputs a password in the input device 35 again, and then the recognition controller 34 controls the motor 67 to start reversely after second induction recognition, so that the motor 67 starts reversely to drive the driving shaft 66 to rotate reversely, the driving shaft 66 rotates reversely to drive the rotating gear 65 to rotate reversely, the rotating gear 65 rotates reversely to drive the transmission gear 64 to rotate reversely, the transmission gear 64 rotates reversely to drive the connecting gear 70 to rotate reversely, the connecting gear 70 rotates reversely to drive the transmission shaft 71 to rotate reversely, and the transmission shaft 71 rotates reversely to drive the rotating shaft 46 to rotate reversely, the rotating shaft 46 rotates reversely to drive the opening and closing door 27 to rotate reversely, the opening and closing door 27 rotates reversely through the left connecting spring 28 to drive the left clamping block 29 to rotate reversely into the placing cavity 30, then the electromagnet 68 is controlled to be powered off, the electromagnet 68 is powered off to generate no magnetic force, the electromagnet 68 generates no magnetic force to no longer adsorb the magnet 69 and to make the magnet move upwards under the pulling force of the transmission spring 61, the magnet 69 moves upwards to drive the transmission shaft 63 to move upwards, the transmission shaft 63 moves upwards to drive the transmission sliding block 60 and the transmission gear 64 to move upwards, and the transmission gear 64 moves upwards to separate the rotating gear 65 and the connecting gear 70.
3. The camera identifier 42 automatically plans a route by identifying the delivery address on the delivery box, and the device flies off the lower housing 22, the ultrasonic transmitter 57 is activated to generate ultrasonic waves to be transmitted to the ultrasonic identification controller 58 during flight, and the ultrasonic identification controller 58 controls the device to turn to prevent the device from colliding with an obstacle during flight.
4. When the camera recognizer 42 recognizes a far address, the camera recognizer falls to express distribution points across the country according to the self electric quantity during automatic route planning, the lower shell 22 is automatically charged, the flight transportation block 26 falls to the lower shell 22, the support foot block 24 firstly falls to the upper pressure tank 21 and drives the upper moving block 23 to move downwards, the upper moving block 23 moves downwards to drive the lower moving block 18 to move downwards and compress the pressure spring 17, the lower moving block 18 moves downwards to drive the lower moving block 51 to move away from the center line of the charging cavity 72, the lower moving block 51 moves downwards to drive the guide block 54 to move away from the center line of the charging cavity 72, and the guide block 54 moves away from the center line of the charging cavity 72 to drive the waterproof block 55 to move away from the center line of the charging cavity 72 The wire moves on one side, the waterproof block 55 moves away from the center line side of the charging cavity 72 to open the upward opening of the charging cavity 72, the charging head 56 moves to the charging cavity 72 and is electrically connected with the conductive block 13, the conductive block 13 is driven to move downwards, the conductive block 13 moves downwards to drive the conductive block 14 to move downwards, the conductive block 14 moves downwards to compress the insulating spring 15 and is electrically connected with the conductive rod 12, the storage power source 11 which is symmetrical left and right is used for rapidly charging the flight transportation block 26, and after the charging is completed, the flight transportation block 26 flies away from the lower shell 22 again.
5. Then, the recipient flies to the address directly, the recipient inputs the mobile phone tail number into the input device 35, then the recognition controller 34 senses correct recognition and controls the motor 67 to be started in the forward direction and to electrify the electromagnet 68, the electromagnet 68 is electrified to generate magnetic force, the electromagnet 68 generates magnetic force to attract the magnet 69 to move downwards, the magnet 69 moves downwards to drive the transmission shaft 63 to move downwards, the transmission shaft 63 moves downwards to drive the transmission sliding block 60 and the transmission gear 64 to move downwards, the transmission sliding block 60 moves downwards to stretch the transmission spring 61, the transmission gear 64 moves downwards to be meshed with the rotating gear 65 and the connecting gear 70, meanwhile, the motor 67 is started to drive the driving shaft 66 to rotate, and the driving shaft 66 rotates to drive the rotating gear 65 to rotate, thereby the running gear 65 rotates and drives drive gear 64 rotates, thereby drive gear 64 rotates and drives connecting gear 70 rotates, thereby connecting gear 70 rotates and drives transmission shaft 71 rotates, thereby transmission shaft 71 rotates and drives axis of rotation 46 rotates, thereby axis of rotation 46 rotates and drives switch door 27 rotates, thereby switch door 27 rotates through left coupling spring 28 drive left side clamp block 29 rotates out place in the chamber 30, then follow place and take out the express delivery case in the chamber 30. Then, a mobile phone tail number is input into the input device 35 again, and then the recognition controller 34 controls the motor 67 to start reversely after the second induction recognition, so that the motor 67 starts reversely to drive the driving shaft 66 to rotate reversely, the driving shaft 66 rotates reversely to drive the rotating gear 65 to rotate reversely, the rotating gear 65 rotates reversely to drive the transmission gear 64 to rotate reversely, the transmission gear 64 rotates reversely to drive the connecting gear 70 to rotate reversely, the connecting gear 70 rotates reversely to drive the transmission shaft 71 to rotate reversely, the transmission shaft 71 rotates reversely to drive the rotating shaft 46 to rotate reversely, the rotating shaft 46 rotates reversely to drive the switch door 27 to rotate reversely, the switch door 27 rotates reversely to drive the left clamping block 29 to rotate reversely into the placing cavity 30 through the left connecting spring 28, then the electromagnet 68 is controlled to be powered off, the electromagnet 68 is powered off so as not to generate magnetic force, the electromagnet 68 does not generate magnetic force so as not to adsorb the magnet 69, and the magnet is pulled by the transmission spring 61 so as to move upwards, the magnet 69 moves upwards so as to drive the transmission shaft 63 to move upwards, the transmission shaft 63 moves upwards so as to drive the transmission sliding block 60 and the transmission gear 64 to move upwards, and the transmission gear 64 moves upwards so as to be separated from the rotating gear 65 and the connecting gear 70.
6. The solar panel 25 absorbs solar energy under the irradiation of the sun and converts the solar energy into electric energy, and then the electric energy is stored in the storage power source 11 through the transmission pipe 10, and the flying transport block 26 is rapidly charged by the storage power source 11 which is bilaterally symmetrical through the charging head 56 and the power transmission block 13 and the conductive block 14 and the conductive rod 12.
The above description is only an embodiment of the invention, but the scope of the invention is not limited thereto, and any changes or substitutions that are not thought of through the inventive work should be included in the scope of the invention. Therefore, the protection scope of the invention should be subject to the protection scope defined by the claims.
Claims (5)
1. The utility model provides an intelligence flight transportation express delivery logistics device, includes casing down, its characterized in that: a charging cavity with an upward opening is formed in the lower shell, conducting rods fixedly mounted in the left end wall and the right end wall of the charging cavity are arranged in the charging cavity in a bilateral symmetry mode, one side, away from the center line of the charging cavity, of each conducting rod is electrically connected with a storage power supply, one side, away from the center line of the charging cavity, of each storage power supply is electrically connected with a transmission pipe, and solar power generation panels which are bilaterally symmetrical along the center line of the charging cavity are fixedly arranged at the upper end of each transmission pipe; the upper end of the solar power generation panel extends out of the upper end face of the lower shell, extension cavities communicated with the charging cavity are arranged along the center line of the charging cavity in a bilateral symmetry mode, a linking cavity is arranged below the extension cavities in a communicating mode, one side, far away from the center line of the charging cavity, of the linking cavity is provided with a lower pressure cavity in a communicating mode, an upper pressure groove with an upward opening is arranged above the lower pressure cavity in a communicating mode, waterproof components are arranged in the extension cavities in the bilateral symmetry mode and comprise waterproof blocks installed in the side, close to the center line of the charging cavity, of the extension cavities in a sliding mode, one side, far away from the center line of the charging cavity, of each waterproof block is fixedly connected with a guide block, and one end, far away from the center line of the charging cavity, of each guide block extends; the terminal surface has set firmly fixed connection piece under the guide block, the fixed connection piece lower extreme has set firmly slidable mounting and has been in extend the lower sliding block in the chamber lower extreme wall, the installation of terminal surface internal rotation is equipped with rotatory pivot before the lower sliding block, the last rotation mounting of rotatory pivot is equipped with the connecting rod, the connecting rod is kept away from the installation of charging chamber central line one end rear end face internal rotation is equipped with the rotation pivot, it is equipped with slidable mounting and is in to rotate pivot rear end the lower moving block of holding down the pressure intracavity, the moving block lower extreme has set firmly pressure spring down, pressure spring sets firmly in the chamber lower extreme wall of holding down, the moving block upper end extends to down go up the pressure tank in set firmly and move the piece.
2. The intelligent flying transportation express delivery logistics device of claim 1, wherein: the charging device is characterized in that an insulating spring is fixedly arranged on the lower end face of the charging cavity, a conductive block is fixedly arranged above the insulating spring, a power transmission block is arranged at the upper end of the conductive block in a power connection mode, and the left end and the right end of the conductive block are in power connection with the conductive rods in bilateral symmetry.
3. The intelligent flying transportation express delivery logistics device of claim 1, wherein: a flying transport block is arranged above the lower shell, support foot blocks which are bilaterally symmetrical along the central line of the flying transport block are fixedly arranged on the lower end face of the flying transport block, the support foot blocks fall into the upper pressure groove and fall on the upper end face of the upper moving block, a charging head fixedly arranged on the lower end face of the flying transport block is arranged in the middle of the support foot blocks which are bilaterally symmetrical, the charging head is electrically connected with the power transmission block to charge the device, a placing cavity with an opening facing left is arranged in the flying transport block, a fixed spring is fixedly arranged on the right end face of the placing cavity, a pressure block is fixedly arranged at the left end of the fixed spring, an ultrasonic identification controller is fixedly arranged on the upper end face of the flying transport block, an ultrasonic transmitter fixedly arranged on the left end face of the flying transport block is connected and arranged on the left end face of the ultrasonic identification controller, and an input device fixedly arranged in the upper end face of the flying transport block, the lower end of the input device is fixedly connected with an identification controller, and a transmission cavity is arranged in the upper end wall of the placing cavity.
4. The intelligent flying transportation express delivery logistics device of claim 1, wherein: the upper end wall of the transmission cavity is fixedly provided with a transmission spring, the lower end of the transmission spring is fixedly provided with a transmission sliding block, the transmission sliding block is slidably arranged in the upper end wall of the transmission cavity, the lower end face of the transmission sliding block is internally and rotatably provided with a transmission shaft, the transmission shaft is fixedly provided with a transmission gear, the lower end of the transmission shaft is rotatably arranged in the upper end face of a magnet, the lower part of the magnet is provided with an electromagnet fixedly arranged in the lower end wall of the transmission cavity, the right side of the transmission gear is provided with a rotating gear fixedly arranged on a driving shaft, the lower end of the driving shaft is in power connection with a motor fixedly arranged in the lower end wall of the transmission cavity, the left side of the transmission gear is provided with a connecting gear fixedly arranged on the transmission shaft, the, the switch door right-hand member face has set firmly left coupling spring, left side coupling spring right-hand member has set firmly left clamp tight piece, place the chamber around the symmetry be equipped with fixed mounting place linking spring on the end wall around the chamber, linking spring is close to place chamber central line one end and has set firmly the removal and press from both sides tight piece, place and set firmly the recognizer of making a video recording on the chamber upper end wall.
5. The intelligent flying transportation express delivery logistics device of claim 1, wherein: two sliding cavities are arranged in the upper end wall of the placing cavity in an array mode and are communicated through a screw rod cavity, the opening of the screw rod cavity faces right, a screw rod is rotatably arranged on the left end wall of the screw rod cavity, a rotating block is fixedly arranged outside the right end of the screw rod extending out of the flying transport block, a clamping and fixing component is arranged in the sliding cavity and comprises a movable thread block which is in threaded connection with the screw rod, a connecting rotating shaft is rotatably arranged on the front end surface of the movable threaded block, a connecting block is rotatably arranged on the connecting rotating shaft, the left side of the connecting rotating shaft is provided with a connecting rotating shaft which is rotatably arranged in the rear end surface of the connecting block, the rear end of the connecting rotating shaft is rotatably arranged in the front end surface of the upper sliding block, the lower end of the upper sliding block extends to the placing cavity and is fixedly provided with an upper connecting spring, and the lower end of the upper connecting spring is fixedly provided with an upper clamping block.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010426133.0A CN111559505A (en) | 2020-05-19 | 2020-05-19 | Intelligent express logistics device for flying and transporting |
| GBGB2014064.6A GB202014064D0 (en) | 2020-05-19 | 2020-09-08 | An intelligent flight transportation express logisitics device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010426133.0A CN111559505A (en) | 2020-05-19 | 2020-05-19 | Intelligent express logistics device for flying and transporting |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN111559505A true CN111559505A (en) | 2020-08-21 |
Family
ID=72069499
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202010426133.0A Withdrawn CN111559505A (en) | 2020-05-19 | 2020-05-19 | Intelligent express logistics device for flying and transporting |
Country Status (2)
| Country | Link |
|---|---|
| CN (1) | CN111559505A (en) |
| GB (1) | GB202014064D0 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112531397A (en) * | 2021-01-08 | 2021-03-19 | 南京启琳天通讯科技有限公司 | Electrical engineering antidetonation waterproof wiring protective housing |
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- 2020-05-19 CN CN202010426133.0A patent/CN111559505A/en not_active Withdrawn
- 2020-09-08 GB GBGB2014064.6A patent/GB202014064D0/en not_active Ceased
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105539824A (en) * | 2015-12-31 | 2016-05-04 | 东莞市吉飞机器人有限公司 | Intelligent unmanned aerial vehicle system capable of continuously working in wide range |
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| CN207257979U (en) * | 2017-09-07 | 2018-04-20 | 杭州双弯月电子科技有限公司 | A kind of transport formula unmanned plane |
| CN108082519A (en) * | 2018-01-29 | 2018-05-29 | 成都市煜沣科技有限公司 | One kind is suitable for small drone landing positioning charging platform |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112531397A (en) * | 2021-01-08 | 2021-03-19 | 南京启琳天通讯科技有限公司 | Electrical engineering antidetonation waterproof wiring protective housing |
| CN112531397B (en) * | 2021-01-08 | 2022-04-26 | 深圳风云信息技术有限公司 | Electrical engineering antidetonation waterproof wiring protective housing |
Also Published As
| Publication number | Publication date |
|---|---|
| GB202014064D0 (en) | 2020-10-21 |
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| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20200821 |
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