CN108423311A - A kind of unmanned plane logistics transport cargo device - Google Patents
A kind of unmanned plane logistics transport cargo device Download PDFInfo
- 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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- China
- Prior art keywords
- bolted
- shell
- unmanned plane
- transverse slat
- transported
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- 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.)
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65D—CONTAINERS 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
- B65D25/00—Details of other kinds or types of rigid or semi-rigid containers
- B65D25/02—Internal fittings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65D—CONTAINERS 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
- B65D81/00—Containers, 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
- B65D81/02—Containers, 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
- B65D81/05—Containers, 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
- B65D81/07—Containers, 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
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.
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 |
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CN108423311A true CN108423311A (en) | 2018-08-21 |
Family
ID=63158120
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN201810196811.1A Withdrawn CN108423311A (en) | 2018-03-10 | 2018-03-10 | A kind of unmanned plane logistics transport cargo device |
Country Status (1)
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CN (1) | CN108423311A (en) |
Cited By (3)
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 |
-
2018
- 2018-03-10 CN CN201810196811.1A patent/CN108423311A/en not_active Withdrawn
Cited By (4)
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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Date | Code | Title | Description |
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PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
WW01 | Invention patent application withdrawn after publication |
Application publication date: 20180821 |
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WW01 | Invention patent application withdrawn after publication |