CN206494126U - A kind of pallet - Google Patents
A kind of pallet Download PDFInfo
- Publication number
- CN206494126U CN206494126U CN201720167837.4U CN201720167837U CN206494126U CN 206494126 U CN206494126 U CN 206494126U CN 201720167837 U CN201720167837 U CN 201720167837U CN 206494126 U CN206494126 U CN 206494126U
- Authority
- CN
- China
- Prior art keywords
- wing aircraft
- plate
- convex portion
- stopper slot
- aircraft plate
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Landscapes
- Pallets (AREA)
Abstract
The utility model discloses a kind of pallet, a kind of pallet includes substrate and all-wing aircraft plate, the substrate includes upper convex portion and shoulder, the first horizontal stopper slot is provided with the side of the upper convex portion, the second stopper slot is provided with the shoulder, the all-wing aircraft plate includes being used to stop the stop part that goods is moved to both sides, the side of the all-wing aircraft plate is abutted with the side of upper convex portion, and the side of the all-wing aircraft plate is provided with the positioning joint coordinated with the first stopper slot grafting, the bottom of the all-wing aircraft plate is provided with the telescopic resilient key coordinated with the second stopper slot grafting, protrude or collapse to both sides with packaging goods is prevented, effectively prevent packaging goods from producing in transportation to structure for conveying such as rollers to block up, ensure the stable advantage of transport.
Description
Technical field
The utility model is related to a kind of container shipping field, more particularly to a kind of pallet.
Background technology
Pallet is by a kind of air transport facility of bulk goods container shipping, it is adaptable to which raceway is conveyed, and is that hydraulic lifting is put down
The conveying of platform roller, raceway convey small trailer, the auxiliary products of automobile rollway conveyor, are the indispensable dresses of one kind of army's air transport
It is standby, it can also be used to the bulk goods shipment of civil aviaton.
Authorization Notice No. discloses a kind of new pallet for CN2498087 Chinese patent, is in composite panel (8)
It is interior to be provided with metallic framework (7), aluminum alloy edge-wrapped (5) is surrounded by periphery, sets be tethered at hole (4), annex pair (3) in position,
The material of composite panel (8) is FRP composite.The utility model is the raceway conveying of aircraft, hydraulic elevating platform rolling
Son conveying, raceway conveying trailer, the auxiliary products of automobile rollway conveyor.
It is more convenient when it is used to load the regular bulk goods for being beneficial to stacking;But bulk goods is often difficult to stack
For regular cube, even if being wrapped up with net or oilcloth, it can still spread, overstock to both sides in the horizontal direction, it is defeated to roller, raceway etc.
Send structure to cause to block up, then by the vibrations in course of conveying, be likely to result in the situation that goods caves in or is scattered.
Utility model content
The purpose of this utility model is to provide a kind of pallet, which solves existing pallet and is loading bulk goods
When the problem of lack Horizontal limiting.
Above-mentioned technical purpose of the present utility model technical scheme is that:
A kind of pallet, including substrate and all-wing aircraft plate, the substrate include upper convex portion and shoulder, the side of the upper convex portion
On be provided with the first horizontal stopper slot, the shoulder and be provided with the second stopper slot, the all-wing aircraft plate includes being used to stop goods
The stop part that thing is moved to both sides, the side of the all-wing aircraft plate is abutted with the side of upper convex portion, and the side of the all-wing aircraft plate is set
The positioning joint coordinated with the first stopper slot grafting is equipped with, the bottom of the all-wing aircraft plate is provided with to be coordinated with the second stopper slot grafting
Telescopic resilient key.
Using such scheme, it is necessary to which when loading goods progress container shipping, all-wing aircraft plate is placed on shoulder, due to
In the effect of itself of all-wing aircraft plate, the all-wing aircraft plate of resilient key retraction, all-wing aircraft plate to positioning joint and the first stopper slot is promoted to coordinate, bullet
Property pin automatic spring and the second stopper slot coordinate, so that all-wing aircraft plate is stably fixed on substrate;All-wing aircraft plate and substrate are formed
Concave shape structure, forms in the both sides of substrate and stops, so as to prevent delivery goods from protruding or topple over to both sides well.
More preferably:It is provided with the all-wing aircraft plate on the flush end concordant with the upper surface of upper convex portion, the substrate
It is provided with the loading plate being pressed on the flush end of all-wing aircraft plate.
Using such scheme, the gravity of goods is largely acted on the load bearing member, and bearing part is pressed on all-wing aircraft plate, so that
Using bearing part as transfer, so as to provide the torque for preventing goods from being offset to both sides with the gravity of goods itself, reduce by two limits
More stablize after the stress of bit architecture, loading.
More preferably:It is convex that the lower surface of the loading plate is provided with cunning, is provided with and convex matches somebody with somebody with cunning in the upper convex portion
The chute of conjunction.
Using such scheme, it can be given and be oriented to when loading plate is placed with chute and sliding convex cooperation, make it all the time
Shaft alignment state is kept, prevents it from being offset to both sides.
More preferably:It is provided with the chute on positioning hole, the loading plate and is provided through loading plate with determining
The countersunk head alignment pin that position hole grafting coordinates.
Using such scheme, loading plate is prevented after being placed on correct position by the positioning of countersunk head alignment pin and chute
Loading plate is moved, and is loaded and be also prevent coming off for countersunk head alignment pin after goods, so as to keep loading plate with substrate in packaging
Can fully it be kept relative stability in transportation.
More preferably:Mounting hole is provided with the bottom of the all-wing aircraft plate, the resilient key includes shank and precompressed
Spring, shank coordinates with mounting hole grafting, and the pre-compressed spring is arranged between mounting hole and shank.
Using such scheme, provide the pin joint state of precompression holding shank using spring and assign the energy that shank resets
Power.
More preferably:End of the shank in mounting hole is provided with wire drawing, and the wire drawing passes through mounting hole
Bottom hole and lateral surface from all-wing aircraft plate is passed.
Using such scheme, pull wire drawing can by shank retraction mounting hole, so that all-wing aircraft plate be taken out, relieving when
Shank is waited because the effect of spring automatically resets.
More preferably:The end of the wire drawing is provided with draw ring.
Using such scheme, use more facilitates, and also avoids in wire drawing retraction seal.
More preferably:The shank is set into multi-diameter shaft, and the aperture of the mounting hole is provided with prevention multi-diameter shaft and slided
The baffle ring gone out, the baffle ring is threadedly coupled with mounting hole, and the small shaft portion of the multi-diameter shaft of the shank passes through baffle ring.
Using such scheme, baffle ring can prevent shank from coming off, and the baffle ring of threaded connection also causes the installation and more of shank
Change and more facilitate.
In summary, the utility model has the advantages that:
1st, stopped by loading all-wing aircraft plate and being formed in the both sides of pallet, prevent packaging goods from protruding or collapse to both sides,
Effectively prevent packaging goods from producing in transportation to structure for conveying such as rollers to block up, ensure that transport is stable;
2nd, easy dress is easily taken by the spacing guarantee all-wing aircraft plate of steady pin and resilient key, and loads stable, and by loading
Plate transfer, the weight for loading goods is acted on the L-type space of a whole page of all-wing aircraft plate completely, increases its stability, and reduce by two limits
The stress of bit architecture.
Brief description of the drawings
Fig. 1 is the structural representation of the pallet of embodiment 1;
Fig. 2 is the structural representation of the substrate of embodiment 1;
Fig. 3 is partial enlarged drawings of the Fig. 1 of embodiment 1 at A.
In figure, 1, substrate;2nd, all-wing aircraft plate;3rd, loading plate;4th, wire drawing;5th, baffle ring;6th, resilient key;11st, the first stopper slot;
12nd, the second stopper slot;13rd, chute;14th, positioning hole;15th, upper convex portion;16th, shoulder;21st, positioning joint;22nd, mounting hole;23rd, put down
End;24th, stop part;31st, cunning is convex;41st, draw ring;61st, shank;62nd, pre-compressed spring;7th, countersunk head alignment pin.
Embodiment
The utility model is described in further detail below in conjunction with accompanying drawing.
This specific embodiment is only to explain of the present utility model, and it is not to limitation of the present utility model, ability
Field technique personnel can make the modification without creative contribution to the present embodiment as needed after this specification is read, but
As long as all being protected in protection domain of the present utility model by Patent Law.
Embodiment 1:A kind of pallet, as shown in figure 1, including substrate 1, all-wing aircraft plate 2 and loading plate 3.
Referring to Figures 1 and 2, substrate 1 includes upper convex portion 15 and shoulder 16, and horizontal the is provided with the side of upper convex portion 15
The second stopper slot 12 is provided with one stopper slot 11, shoulder 16.
Reference picture 1, all-wing aircraft plate 2 is L-type, and the upturned portion of L-type is stop part 24, and stop part is used to stop goods to both sides
It is mobile;The face of horizontal ends 23 of all-wing aircraft plate 2 is abutted with the side of upper convex portion 15, and is provided with the horizontal end face of all-wing aircraft plate 2 and the
The positioning joint 21 that the grafting of one stopper slot 11 coordinates, the bottom of all-wing aircraft plate 2 be provided with the grafting of the second stopper slot 12 coordinate can
Flexible resilient key 6;Steady pin and resilient key 6 provide positioning, by the stable limitation of all-wing aircraft plate 2 on substrate 1;Reference picture 3, bullet
Property pin 6 include shank 61 and pre-compressed spring 62, mounting hole 22 is provided with the bottom of all-wing aircraft plate 2, shank 61 is inserted with mounting hole 22
Cooperation is connect, shank 61 is set into multi-diameter shaft, the aperture of mounting hole 22 is provided with the baffle ring 5 for preventing multi-diameter shaft from skidding off, baffle ring 5 and peace
Dress hole 22 is threadedly coupled, and the small shaft portion of the multi-diameter shaft of shank 61 passes through baffle ring 5;Pre-compressed spring 62 is arranged on mounting hole 22 and pin
Between body 61, end of the shank 61 in mounting hole 22 is provided with wire drawing 4, wire drawing 4 through mounting hole 22 bottom hole and from all-wing aircraft
The lateral surface of plate 2 is passed, and the end of wire drawing 4 is provided with draw ring 41, when dismounting all-wing aircraft plate 2 are needed, pulls wire drawing 4 by pin
In the all-wing aircraft plate 2 of the retraction of body 61, while moving horizontally all-wing aircraft plate 2 can laterally pull out.
Referring to Figures 1 and 2, the flush end 23 concordant with the upper surface of upper convex portion 15 is provided with all-wing aircraft plate 2, loading plate 3 is supported
The upper surface of flush end 23 and upper convex portion 15 is connected on, is concentrated on the weight of whole goods on loading plate 3 with this, and with loading plate 3
Acted on as transfer on all-wing aircraft plate 2;The lower surface of loading plate 3, which is provided with sliding convex 31, upper convex portion 15, to be provided with and sliding convex 31
The chute 13 of cooperation, provides sliding with this and is oriented to and spacing;It is provided with to be provided with positioning hole 14, loading plate 3 in chute 13 and passes through
The countersunk head alignment pin 7 that loading plate 3 coordinates with the grafting of positioning hole 14 is worn, loading plate 3 and base during container shipping are ensured with this
Stablizing relatively between plate 1.
When assembling, all-wing aircraft plate 2 is placed on shoulder 16, due to the weight of itself of all-wing aircraft plate 2, resilient key 6
In retraction all-wing aircraft plate 2, promote all-wing aircraft plate 2 to the grafting of 21 and first stopper slot of positioning joint 11 cooperation, at the same resilient key 6 it is automatic
Fall into the second stopper slot 12, limit all frees degree;Then loading plate 3 is placed in upper convex portion 15, convex 31 and chute is slided
13 coordinate, and place countersunk head alignment pin 7 in the corresponding hole position of loading plate 3, promote loading plate 3, slide to after specified location, sink
Head alignment pin 7 and the grafting of positioning hole 14 are spacing;At the same time, loading plate 3 is also pressed on the flush end 23 of all-wing aircraft plate 2.
Claims (8)
1. a kind of pallet, it is characterized in that:Including substrate (1) and all-wing aircraft plate (2), the substrate (1) include upper convex portion (15) and
It is provided with horizontal the first stopper slot (11), the shoulder (16) and sets on shoulder (16), the side of the upper convex portion (15)
There is the second stopper slot (12), the all-wing aircraft plate (2) includes being used to stop the stop part that goods is moved to both sides(24), the all-wing aircraft
The side of plate (2) is abutted with the side of upper convex portion (15), and the side of the all-wing aircraft plate (2) is provided with and the first stopper slot (11)
The positioning joint (21) that grafting coordinates, the bottom of the all-wing aircraft plate (2) be provided with the second stopper slot (12) grafting coordinate can
Flexible resilient key (6).
2. a kind of pallet according to claim 1, it is characterized in that:It is provided with and upper convex portion on the all-wing aircraft plate (2)
(15) carrying being pressed on the flush end of all-wing aircraft plate (2) (23) is provided with the concordant flush end (23) in upper surface, the substrate (1)
Plate (3).
3. a kind of pallet according to claim 2, it is characterized in that:It is convex that the lower surface of the loading plate (3) is provided with cunning
(31) chute (13) coordinated with sliding convex (31), is provided with the upper convex portion (15).
4. a kind of pallet according to claim 3, it is characterized in that:Positioning hole (14) is provided with the chute (13),
The countersunk head alignment pin (7) that loading plate (3) coordinates with positioning hole (14) grafting is provided through on the loading plate (3).
5. a kind of pallet according to claim 1, it is characterized in that:Installation is provided with the bottom of the all-wing aircraft plate (2)
Hole (22), the resilient key (6) includes shank (61) and pre-compressed spring (62), and shank (61) coordinates with mounting hole (22) grafting,
The pre-compressed spring (62) is arranged between mounting hole (22) and shank (61).
6. a kind of pallet according to claim 5, it is characterized in that:End of the shank (61) in mounting hole (22)
Wire drawing (4) is provided with, the wire drawing (4) passes through the bottom hole of mounting hole (22) and passed from the lateral surface of all-wing aircraft plate (2).
7. a kind of pallet according to claim 6, it is characterized in that:The end of the wire drawing (4) is provided with draw ring (41).
8. a kind of pallet according to claim 5, it is characterized in that:The aperture of the mounting hole (22) is provided with prevention rank
The baffle ring (5) that terraced axle is skidded off, the baffle ring (5) is threadedly coupled with mounting hole (22), and the shank (61) partially passes through baffle ring
(5)。
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201720167837.4U CN206494126U (en) | 2017-02-24 | 2017-02-24 | A kind of pallet |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201720167837.4U CN206494126U (en) | 2017-02-24 | 2017-02-24 | A kind of pallet |
Publications (1)
Publication Number | Publication Date |
---|---|
CN206494126U true CN206494126U (en) | 2017-09-15 |
Family
ID=59805674
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201720167837.4U Active CN206494126U (en) | 2017-02-24 | 2017-02-24 | A kind of pallet |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN206494126U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108393657A (en) * | 2018-03-02 | 2018-08-14 | 辽宁忠旺铝合金精深加工有限公司 | A kind of production method and products thereof of aviation lightweight pallet |
-
2017
- 2017-02-24 CN CN201720167837.4U patent/CN206494126U/en active Active
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108393657A (en) * | 2018-03-02 | 2018-08-14 | 辽宁忠旺铝合金精深加工有限公司 | A kind of production method and products thereof of aviation lightweight pallet |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN205366661U (en) | Guide rail system is loaded in protractile of back pullout (BPO) special type container | |
CN206624126U (en) | Transfer car(buggy) | |
CN206203683U (en) | Low platform container handling device | |
CN206126384U (en) | Convenient loading and unloading frame | |
CN206494126U (en) | A kind of pallet | |
CN108747632A (en) | A kind of fork truck castings production grinding device | |
CN206475908U (en) | A kind of conveying arrangement for being easy to transport material barrel | |
CN112758149A (en) | Prevent impaired for commodity circulation transport platform protection mechanism of platform | |
CN203111862U (en) | Container | |
KR20110112060A (en) | The transferring apparatus for packages | |
CN207712183U (en) | A kind of AGV trolleies | |
CN207061347U (en) | A kind of convertible article conveying drum | |
CN203047670U (en) | Multifunctional logistics tray | |
CN204871914U (en) | Fork truck tray | |
CN205837745U (en) | The warehouse of loading go-cart is set in a kind of | |
CN107813939A (en) | It is a kind of that there is anticollision and be conveniently adjusted the unmanned plane pallet of storage area | |
CN207579708U (en) | A kind of great logistic car in storage space | |
CN207192695U (en) | A kind of fork truck | |
CN206782610U (en) | A kind of new logistic storage shelf | |
CN201553454U (en) | Material limiting device of round pipe type belt conveyor | |
CN104709472A (en) | Device suitable for entry and exit of freighted airship bags through front cabin door | |
CN205418512U (en) | T type channel -section steel pipe fixed baseplate | |
CN206188049U (en) | Loading attachment of container | |
CN205059373U (en) | Freight train convenient to transport goods | |
CN205708221U (en) | Steel pipe support fixing device in a kind of container |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
GR01 | Patent grant | ||
GR01 | Patent grant |