CN108423311A - A kind of unmanned plane logistics transport cargo device - Google Patents

A kind of unmanned plane logistics transport cargo device Download PDF

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Publication number
CN108423311A
CN108423311A CN201810196811.1A CN201810196811A CN108423311A CN 108423311 A CN108423311 A CN 108423311A CN 201810196811 A CN201810196811 A CN 201810196811A CN 108423311 A CN108423311 A CN 108423311A
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CN
China
Prior art keywords
bolted
shell
unmanned plane
transverse slat
transported
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
CN201810196811.1A
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Chinese (zh)
Inventor
不公告发明人
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Wenzhou Jiegao Technology Co Ltd
Original Assignee
Wenzhou Jiegao Technology Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Wenzhou Jiegao Technology Co Ltd filed Critical Wenzhou Jiegao Technology Co Ltd
Priority to CN201810196811.1A priority Critical patent/CN108423311A/en
Publication of CN108423311A publication Critical patent/CN108423311A/en
Withdrawn legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B65CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65DCONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
    • B65D25/00Details of other kinds or types of rigid or semi-rigid containers
    • B65D25/02Internal fittings
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B65CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65DCONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
    • B65D81/00Containers, packaging elements, or packages, for contents presenting particular transport or storage problems, or adapted to be used for non-packaging purposes after removal of contents
    • B65D81/02Containers, packaging elements, or packages, for contents presenting particular transport or storage problems, or adapted to be used for non-packaging purposes after removal of contents specially adapted to protect contents from mechanical damage
    • B65D81/05Containers, packaging elements, or packages, for contents presenting particular transport or storage problems, or adapted to be used for non-packaging purposes after removal of contents specially adapted to protect contents from mechanical damage maintaining contents at spaced relation from package walls, or from other contents
    • B65D81/07Containers, packaging elements, or packages, for contents presenting particular transport or storage problems, or adapted to be used for non-packaging purposes after removal of contents specially adapted to protect contents from mechanical damage maintaining contents at spaced relation from package walls, or from other contents using resilient suspension means

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Handcart (AREA)

Abstract

The invention discloses a kind of unmanned plane logistics to transport cargo device, including transverse slat, shell and bottom plate;It has been bolted hydraulic cylinder at left and right sides of the transverse slat lower surface, and link block is welded at left and right sides of its upper surface;There are two the link block settings, and the upper end has been bolted clip;The clip movable end has been threadably secured lead screw;The lead screw passes through clip movable end and No.1 bevel gear;The No.1 bevel gear engages with No. two bevel gears;No. two bevel gears are fixed on motor output shaft upper end;The hydraulic cylinder is equipped with hydraulic stem;The shell lower surface is bolted on rubber slab upper surface, and its inner wall is equipped with seal closure by buffer spring;The seal closure front end is equipped with slide fastener, and rear end is equipped with exhaust tube;The exhaust tube is bolted on air pump inlet end;Multigroup damping spring and buffer spring is arranged in inside of the invention, can need freight with effective protection.

Description

A kind of unmanned plane logistics transport cargo device
Technical field
The present invention relates to unmanned plane logistics field, cargo device is transported in specifically a kind of unmanned plane logistics.
Background technology
With reaching its maturity for the Internet model, Logistics Developing is swift and violent.Users from networks in all parts of the country places an order, largely Cargo transported to from the place of production in user hand in all parts of the country.The development of logistics not only promotes the development of transport service, also makes storehouse Storing flow management welcomes no small challenge.
How a large amount of commodity reasonably to be managed, is sent in time in client's hand.How the profit of storage space is improved With rate.How warehousing management cost is reduced.A series of problem is all that logistics network operator needs the technology faced and management to ask Topic.
Invention content
The purpose of the present invention is to provide a kind of unmanned plane logistics to transport cargo device, to solve to carry in above-mentioned background technology The problem of going out.
To achieve the above object, the present invention provides the following technical solutions:
A kind of unmanned plane logistics transport cargo device, including transverse slat, shell and bottom plate;At left and right sides of the transverse slat lower surface It has been bolted hydraulic cylinder, and link block is welded at left and right sides of its upper surface;There are two the link block settings, and its Upper end has been bolted clip;The clip is rounded, and its movable end has been threadably secured lead screw;The lead screw is worn Clip movable end and No.1 bevel gear are crossed, and the welding of its both ends has been bolted limited block;On the inside of the No.1 bevel gear Surface is equipped with connecting rod, and it is engaged with No. two bevel gears;No. two bevel gears are bolted on motor output shaft Upper end, and inside protective shell;There are two the protective shell settings, is bolted on respectively in transverse slat upper and lower surface Portion;The hydraulic cylinder upper end is bolted at left and right sides of transverse slat lower surface, and inside is equipped with hydraulic stem, and it is by leading Line and control device are electrically connected;The hydraulic stem lower end of the bolt is fixed on fixed block upper surface middle part;The fixed block setting There are two, and it is fixed on the left and right sides in the middle part of upper surface of outer cover by fixing bolt;Shell lower surface is bolted on Rubber slab upper surface, and its inner wall is equipped with seal closure by buffer spring;The seal closure front end is equipped with slide fastener, rear end peace Equipped with exhaust tube;The exhaust tube is in Y types, two branch pipes in left and right pass through shell and with seal closure unicom, and be equipped with inside it Control valve, lower branch line are bolted on air pump inlet end.
As a further solution of the present invention:The connecting rod is provided with two groups, and one end is slidably connected at No.1 cone Gear inner surface, the other end are mounted on clip movable end inner surface.
As a further solution of the present invention:The motor output shaft passes through transverse slat by bearing, and is bolted In the middle part of protective shell bottom surface, and it is electrically connected by conducting wire and control device;The control device is embedded in transverse slat upper table Face right end, and its surface is equipped with control button.
As a further solution of the present invention:The buffer spring is provided with several groups, and one end is outer by being mounted on Shell inner wall, the other end are mounted on seal closure outer wall surface.
As a further solution of the present invention:The air pump is bolted on plate upper surface rear end, and it passes through Conducting wire and control device are electrically connected.
As a further solution of the present invention:The rubber slab upper end is bolted on shell lower surface, and lower end is logical It crosses bolt and is fixed on plate upper surface, and the upper end inner wall offers damping trough;The damping trough is provided with several groups, uniformly divides Cloth is equipped with supporting rod in rubber slab upper end inner wall inside it.
As further scheme of the invention:It is twined outside the supporting rod and is full of damping spring, and its lower end passes through spiral shell Bolt is fixed on plate upper surface;Four end of the bottom plate is equipped with fixing bolt.
Compared with prior art, the beneficial effects of the invention are as follows:
The configuration of the present invention is simple, easy to use, damping spring and buffer spring is arranged in device, can be effectively in unmanned plane Appearance protects cargo not to be damaged in the case of jolting;Air pump and exhaust tube are set simultaneously, the volume of cargo can be compressed, so as to In a large amount of cargo of transport;Clip, bevel gear and lead screw are set on device, whole device can be fixed on to the nothing of different size On man-machine, in order to improve the universality of device;Hydraulic cylinder and hydraulic stem are set simultaneously, can with the height of controling shell, so as to In the height for adapting to different operating personnel;Air pump and seal closure is arranged in device, can by the volume for effectively reducing cargo, with Convenient for transporting significantly more efficient protection cargo in cargo.
Description of the drawings
Fig. 1 is the structural schematic diagram that cargo device is transported in a kind of unmanned plane logistics.
Fig. 2 is the structural schematic diagram that left view in cargo device is transported in a kind of unmanned plane logistics.
Fig. 3 is the structural schematic diagram that clip in cargo device is transported in a kind of unmanned plane logistics.
Fig. 4 is the structural schematic diagram that backsight in cargo device is transported in a kind of unmanned plane logistics.
In figure:1- clips, 2- connecting rods, 3- protective shells, 4- No.1 bevel gears, 5- motors, No. bis- bevel gears of 6-, 7- limits Block, 8- transverse slats, 9- hydraulic cylinders, 10- hydraulic stems, 11- shells, 12- seal closures, 13- supporting rods, 14- bottom plates, 15- damping springs, 16- rubber slabs, 17- damping troughs, 18- buffer springs, 19- fixing bolts, 20- fixed blocks, 21- control devices, 22- link blocks, 23- control valves, 24- exhaust tubes, 25- air pumps, 26- lead screws.
Specific implementation mode
The technical solution of this patent is described in more detail With reference to embodiment.
Please refer to Fig.1-4, cargo device, including transverse slat 8, shell 11 and bottom plate 14 are transported in a kind of unmanned plane logistics;It is described It has been bolted hydraulic cylinder 9 at left and right sides of 8 lower surface of transverse slat, and link block 22 is welded at left and right sides of its upper surface;Institute It states there are two the settings of link block 22, and the upper end has been bolted clip 1;The clip 1 is rounded, and its movable end is logical It crosses to be screwed and has lead screw 26;The lead screw 26 passes through 1 movable end of clip and No.1 bevel gear 4, and the welding of its both ends passes through spiral shell Bolt is fixed with limited block 7, in order to prevent lead screw 26 from being fallen from clip 1;4 inner surface of No.1 bevel gear is equipped with company Extension bar 2, in order to the position of fixed No.1 bevel gear 4, and it is engaged with No. two bevel gears 6;The connecting rod 2 is provided with two Group, and one end is slidably connected at 4 inner surface of No.1 bevel gear, the other end is mounted on 1 movable end inner surface of clip;It is described No. two bevel gears 6 are bolted on 5 output shaft upper end of motor, and inside protective shell 3;The protective shell 3 is arranged There are two, it is bolted on respectively in the middle part of 8 upper and lower surface of transverse slat, in order to protect internal mechanical equipment;The motor 5 Output shaft passes through transverse slat 8 by bearing, and is bolted in the middle part of 3 bottom surface of protective shell, and it passes through conducting wire and control Device 21 processed is electrically connected, in order to driving motor 5;The control device 21 is embedded in 8 upper surface right end of transverse slat, and its surface Control button is installed, in order to control whole device;9 upper end of the hydraulic cylinder is bolted on 8 lower surface of a transverse slat left side Right both sides, inside is equipped with hydraulic stem 10, and it is electrically connected by conducting wire and control device 21;10 lower end spiral shell of the hydraulic stem Bolt is fixed on 20 upper surface middle part of fixed block, in order to drive shell 11 to move up and down;There are two the settings of the fixed block 20, and It is fixed on by fixing bolt 19 at left and right sides of 11 upper surface middle part of shell;11 lower surface of shell is bolted on rubber 16 upper surface of plate, and its inner wall is equipped with seal closure 12 by buffer spring 18;The buffer spring 18 is provided with several groups, and One end is by being mounted on 11 inner wall of shell, and the other end is mounted on 12 outer wall surface of seal closure, in order to prevent in transportational process There is the case where cargo collides shell 11;12 front end of seal closure is equipped with slide fastener, and rear end is equipped with exhaust tube 24;The exhaust tube 24 be in Y types, two branch pipes in left and right pass through shell 11 and with 12 unicom of seal closure, and control valve 23, lower branch line are installed inside it It is bolted on 25 inlet end of air pump, for draining only air in seal closure 12, in order to fixed cargo;The air pump 25 are bolted on 14 upper table surface rear end of bottom plate, and it is electrically connected by conducting wire and control device 21;The rubber slab 16 upper ends are bolted on 11 lower surface of shell, and lower end is bolted on 14 upper surface of bottom plate, and the upper end inner wall Offer damping trough 17;The damping trough 17 is provided with several groups, is evenly distributed on 16 upper end inner wall of rubber slab, and its internal peace Equipped with supporting rod 13;It is twined outside the supporting rod 13 and is full of damping spring 15, and its lower end is bolted on bottom plate 14 Surface;14 4 end of bottom plate is equipped with fixing bolt 19, in order to which whole device to be fixed on inside unmanned plane.
The present invention operation principle be:
In use, starting motor 5 by control device 21 first, motor 5 starts to drive No. two bevel gears 6 to rotate, And then No.1 bevel gear 4 is driven to rotate, to drive lead screw 26 to move, clip 1 is firmly stuck on unmanned plane;Pass through control later Device 21 processed starts hydraulic cylinder 9, and hydraulic cylinder 9, which starts, to be driven the elongation of hydraulic stem 10 or shorten, to driving shell 11 upwards or It is to move down, after the height of shell 11 is suitble to the height of staff's goods putting object, closes hydraulic cylinder 9,;Staff need to The cargo to be transported is put into seal closure 12, and slide fastener is drawn, and later by 21 booster air pump 25 of control device, opens control valve 23, air pump 25, which starts, drives air-flow to be flowed to out of seal closure 12 in exhaust tube 24,25 inlet end of air pump is flowed to later, finally from going out In the air of gas end loss.
The better embodiment of this patent is explained in detail above, but this patent is not limited to above-mentioned embodiment party Formula, one skilled in the relevant art within the scope of knowledge, can also be under the premise of not departing from this patent objective It makes a variety of changes.

Claims (7)

1. cargo device, including transverse slat (8), shell (11) and bottom plate (14) are transported in a kind of unmanned plane logistics;It is characterized in that, institute It states and has been bolted hydraulic cylinder (9) at left and right sides of transverse slat (8) lower surface, and link block is welded at left and right sides of its upper surface (22);There are two link block (22) settings, and the upper end has been bolted clip (1);The clip (1) is in circle Shape, and its movable end has been threadably secured lead screw (26);The lead screw (26) passes through clip (1) movable end and No.1 bevel gear (4), and the welding of its both ends has been bolted limited block (7);No.1 bevel gear (4) inner surface is equipped with connecting rod (2), and it is engaged with No. two bevel gears (6);No. two bevel gears (6) are bolted on motor (5) output shaft upper end, And it is internal mounted on protective shell (3);There are two protective shell (3) settings, is bolted on following table on transverse slat (8) respectively Middle face;Hydraulic cylinder (9) upper end is bolted at left and right sides of transverse slat (8) lower surface, and inside is equipped with hydraulic stem (10), and it is electrically connected by conducting wire and control device (21);Hydraulic stem (10) lower end of the bolt is fixed on fixed block (20) upper surface middle part;There are two fixed block (20) settings, and it is fixed on by fixing bolt (19) on shell (11) At left and right sides of surface middle part;Shell (11) lower surface is bolted on rubber slab (16) upper surface, and its inner wall pass through it is slow It rushes spring (18) and seal closure (12) is installed;Seal closure (12) front end is equipped with slide fastener, and rear end is equipped with exhaust tube (24); The exhaust tube (24) is in Y types, two branch pipes in left and right pass through shell (11) and with seal closure (12) unicom, and be equipped with inside it Control valve (23), lower branch line are bolted on air pump (25) inlet end.
2. cargo device is transported in a kind of unmanned plane logistics according to claim 1, which is characterized in that the connecting rod (2) Two groups are provided with, and one end is slidably connected at No.1 bevel gear (4) inner surface, the other end is mounted on clip (1) movable end Inner surface.
3. cargo device is transported in a kind of unmanned plane logistics according to claim 1, which is characterized in that the motor (5) is defeated Shaft passes through transverse slat (8) by bearing, and is bolted in the middle part of protective shell (3) bottom surface, and its by conducting wire and Control device (21) electrically connects;The control device (21) is embedded in transverse slat (8) upper surface right end, and its surface is equipped with control Button.
4. cargo device is transported in a kind of unmanned plane logistics according to claim 1, which is characterized in that the buffer spring (18) several groups are provided with, and one end is mounted on seal closure (12) outer wall table by being mounted on shell (11) inner wall, the other end Face.
5. cargo device is transported in a kind of unmanned plane logistics according to claim 1, which is characterized in that the air pump (25) is logical It crosses bolt and is fixed on bottom plate (14) upper table surface rear end, and it is electrically connected by conducting wire and control device (21).
6. cargo device is transported in a kind of unmanned plane logistics according to claim 1, which is characterized in that the rubber slab (16) Upper end is bolted on shell (11) lower surface, and lower end is bolted on bottom plate (14) upper surface, and in the upper end Wall offers damping trough (17);The damping trough (17) is provided with several groups, is evenly distributed on rubber slab (16) upper end inner wall, and Supporting rod (13) is installed inside it.
7. cargo device is transported in a kind of unmanned plane logistics according to claim 6, which is characterized in that the supporting rod (13) Outside, which twines, is full of damping spring (15), and its lower end is bolted on bottom plate (14) upper surface;(14) four end of the bottom plate Fixing bolt (19) is installed.
CN201810196811.1A 2018-03-10 2018-03-10 A kind of unmanned plane logistics transport cargo device Withdrawn CN108423311A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201810196811.1A CN108423311A (en) 2018-03-10 2018-03-10 A kind of unmanned plane logistics transport cargo device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201810196811.1A CN108423311A (en) 2018-03-10 2018-03-10 A kind of unmanned plane logistics transport cargo device

Publications (1)

Publication Number Publication Date
CN108423311A true CN108423311A (en) 2018-08-21

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Application Number Title Priority Date Filing Date
CN201810196811.1A Withdrawn CN108423311A (en) 2018-03-10 2018-03-10 A kind of unmanned plane logistics transport cargo device

Country Status (1)

Country Link
CN (1) CN108423311A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109353658A (en) * 2018-11-15 2019-02-19 钟夏欣 A kind of general storage box of unmanned plane
CN112093060A (en) * 2020-10-10 2020-12-18 宁波拉修智能科技有限公司 Device capable of increasing load capacity by utilizing multiple unmanned aerial vehicles
CN112830087A (en) * 2020-12-30 2021-05-25 义乌工商职业技术学院 Encrypt thing flow box with automatic identification chip

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109353658A (en) * 2018-11-15 2019-02-19 钟夏欣 A kind of general storage box of unmanned plane
CN112093060A (en) * 2020-10-10 2020-12-18 宁波拉修智能科技有限公司 Device capable of increasing load capacity by utilizing multiple unmanned aerial vehicles
CN112093060B (en) * 2020-10-10 2021-07-20 南京棠邑科创服务有限公司 Device capable of increasing load capacity by utilizing multiple unmanned aerial vehicles
CN112830087A (en) * 2020-12-30 2021-05-25 义乌工商职业技术学院 Encrypt thing flow box with automatic identification chip

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WW01 Invention patent application withdrawn after publication

Application publication date: 20180821

WW01 Invention patent application withdrawn after publication