CN202880263U - Combined type aviation tyre storage and transportation rack - Google Patents
Combined type aviation tyre storage and transportation rack Download PDFInfo
- Publication number
- CN202880263U CN202880263U CN201220471619.7U CN201220471619U CN202880263U CN 202880263 U CN202880263 U CN 202880263U CN 201220471619 U CN201220471619 U CN 201220471619U CN 202880263 U CN202880263 U CN 202880263U
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- frame
- screw assembly
- aircraft tyre
- leading screw
- accumulating
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Abstract
The utility model relates to aviation tyre storage and transportation devices, in particular to a combined type aviation tyre storage and transportation rack. The combined type aviation tyre storage and transportation rack comprises a rack body assembly, a transmission mechanism, a speed reducer and a lead screw assembly, wherein the lead screw assembly is installed on the bottom of the rack body assembly in a rotating mode, the speed reducer which is driven by manual operation or power operation is installed on one side of the rack body assembly, and the speed reducer is connected with the lead screw assembly through the transmission mechanism to drive the lead screw assembly to rotate. Aviation tyres are sequentially placed on the lead screw assembly along the axial direction of the lead screw assembly and are rotated synchronously along with the lead screw assembly. The combined type aviation tyre storage and transportation rack is simple in structure, convenient to install and capable of enabling the aviation tyres to rotate synchronously. According to the combined type aviation tyre storage and transportation rack, an upper rack body can turn relative to a lower rack body, and during transportation, the upper rack body turns inwards until the upper rack body is parallel to the lower rack body, and thus transportation space is saved significantly. When two storage and transportation racks are stacked, the two storage and transportation racks can be lifted upwards as a whole through a forklift. An upper guide connecting plug-in unit and a lower guide connecting plug-in unit connected in guiding and butting modes, and thus loading efficiency, stability and safety are improved significantly.
Description
Technical field
The utility model relates to the storage and transportation apparatus of aircraft tyre, specifically a kind of compound type aircraft tyre accumulating frame.
Background technology
Existing air unit war warehouse storehouse adopts fixed type two to three-ply tire frame to deposit aircraft tyre.The used tire dolly volume of army is large, and the time of installation is also long, and four individual demands just can be finished installation in more than six hour; Tire dolly is high four layers, needs ascend operation during installation, has larger potential safety hazard.Existing tire dolly also can't fold, and is very difficult in war instruction transportation.In the tire of war warehouse library storage, the 80kg that weighs that has when putting on the tire dolly, requires great effort, takes a lot of work.Aircraft tyre is in storing process, and in order to prevent squeegee action, every three months must rotate 90 °, each is equipped with 6～7 aircraft tyres on the existing tire dolly, must rotate singly, and work capacity is large, operation is extremely inconvenient, and each tyre rotation is asynchronous, and easy generation leakage turns, mistake turns.
The utility model content
It is a kind of easy for installation that the purpose of this utility model is to provide, the compound type aircraft tyre accumulating frame that aircraft tyre is rotated synchronously.
Another purpose of the present utility model is to provide a kind of saving transport space, and easily compound type aircraft tyre accumulating frame saves time.
The purpose of this utility model is achieved through the following technical solutions:
The utility model comprises support body assembly, transmission device, retarder and leading screw assembly, wherein the leading screw assembly is rotatably installed in the bottom of support body assembly, be installed in a side of support body assembly by the retarder of manual or motorized motions, and be connected, drive the rotation of leading screw assembly by transmission device and described leading screw assembly; Aircraft tyre axially is placed on the leading screw assembly successively along the leading screw assembly, rotates synchronously with the leading screw assembly.
Wherein: described support body assembly comprises that upper frame, lower frame, upper guiding connect plug-in unit, lower guiding connects plug-in unit and L shaped folding, and wherein lower frame is parallel with the leading screw assembly, and the two ends of lower frame all are connected with lower guiding and connect plug-in unit; The two ends of described lower frame are all hinged by an end of the first bolt and L shaped folding, and the other end of each L shaped folding all connects a upper frame, are equipped with guiding on the top of each upper frame and connect plug-in unit; Two described accumulating framves connect plug-in unit by upper guiding connection plug-in unit and lower guiding and mutually peg graft;
On the described upper frame that is positioned at the lower frame two ends rotating block plate is installed, upper frame is provided with column, and this column inboard has notch along short transverse, and described block plate is connected with notch by the second bolt, and block plate is adjustable in the position of column short transverse; The outer surface of described block plate is equally divided into four zones, in each zone all with the symbol that represents the time;
The described spacing cross bar of detouchable that between the upper frame at lower frame two ends, is provided with, aircraft tyre is between leading screw assembly and spacing cross bar, and the upper limb of aircraft tyre is connected on the spacing cross bar; The two ends of described lower frame all are equipped with the limiting block wheel assembly, comprise spacing gear wheel and gear wheel frame, and wherein spacing gear wheel is installed on the lower frame by the gear wheel frame, and the longitudinal center line of described spacing gear wheel and the longitudinal center line of aircraft tyre are perpendicular; Described lower frame is provided with hanger;
Described leading screw assembly comprises two leading screws that parallel, the two ends of lower frame are respectively equipped with two bearing brackets, the two ends of every rhizoid thick stick all are installed on the bearing bracket by bearing, the two ends of two rhizoid thick sticks all link to each other by transmission device, and wherein arbitrary rhizoid thick stick is connected with the mouth of described retarder; Described transmission device is sprocket wheel, chain structure, and the two ends of two rhizoid thick sticks all are equipped with sprocket wheel, links to each other by chain between two sprocket wheels of every end.
Advantage of the present utility model and good effect are:
1. the utility model is simple in structure, easy for installation, and aircraft tyre is rotated synchronously.
2. relatively lower frame upset of upper frame of the present utility model, during transportation, upper frame inwardly is turned to parallel with lower frame, has greatly saved transport space.
3. can lift on the whole with fork truck when two accumulating framves are stacked, connect plug-in unit by upper and lower guiding and guide to docking, greatly improve efficiency of loading, stability and safety.
4. the utility model is provided with block plate and limiting block wheel assembly, and the aircraft tyre of having avoided support body to carry contacts with support body or sprocket wheel and rubs, and affects tyre rotation.
5. block plate of the present utility model and aircraft tyre rotate synchronously, and rotation situation can be by observing with symbol on the block plate outer surface.
6. the utility model is provided with the spacing cross bar of detouchable between the upper frame at two ends, avoids the contingent tire disengaging of beating in the transportation.
Description of drawings
Fig. 1 is structural front view of the present utility model;
Fig. 2 is the birds-eye view of Fig. 1;
Fig. 3 is the left view of Fig. 1;
Wherein: 1 is suspension ring, and 2 is eyenut, and 3 is handle, and 4 is the first bolt, 5 is the support body assembly, and 6 is lower frame, and 7 is upper frame, 8 is block plate, and 9 is spacing gear wheel assembly, and 10 is transmission device, 11 is retarder, and 12 is the leading screw assembly, and 13 is that upper guiding connects plug-in unit, 14 is that lower guiding connects plug-in unit, and 15 is spacing cross bar, and 16 is the bearing bracket, 17 is column, and 18 is spacing gear wheel, and 19 is L shaped folding.
The specific embodiment
The utility model is described in further detail below in conjunction with accompanying drawing.
Shown in Fig. 1～3, the utility model comprises support body assembly 5, block plate 8, limiting block wheel assembly 9, transmission device 10, retarder 11, leading screw assembly 12 and spacing cross bar 15, wherein support body assembly 5 comprises that upper frame 7, lower frame 6, upper guiding connect plug-in unit 13, lower guiding connects plug-in unit 14 and L shaped folding 19, lower frame 6 is two, the parallel both sides that are positioned at leading screw assembly 12, two lower guiding that the two ends of every lower frame 6 all are connected with 14, two lower frame 6 every ends of lower guiding connection plug-in unit of inner hollow connect between the plug-in units 14 continuous by crossbeam; The two ends of every lower frame 6 are all hinged with an end of L shaped folding 19 by the first bolt 4, the other end of each L shaped folding all connects a upper frame 7, be equipped with guiding on the top of each upper frame 7 and connect plug-in unit 13, be that upper frame 7 is four, between two upper frames 7 of same end, link to each other by crossbeam.Two accumulating framves connect plug-in unit 14 by upper guiding connection plug-in unit 13 and lower guiding can peg graft mutually, has realized the normalisation that tire accumulating frame is put.Every lower frame 6 is equipped with hanger 1 near the place, two ends, and is fixing with lower frame 6 with eyenut 2, is convenient to lifting.
Under two ends connect, be provided with altogether four bearing brackets 16 on the crossbeam of guiding connection plug-in unit 14, wherein also be fixed with retarder 11 on the crossbeam of arbitrary end; Leading screw assembly 12 comprises two leading screws that parallel, and the two ends of every rhizoid thick stick all are rotatably installed on the bearing bracket 16 by bearing, and the two ends of two rhizoid thick sticks all link to each other by transmission device 10, and wherein arbitrary rhizoid thick stick is connected with the mouth of retarder 11.Transmission device 10 of the present utility model is sprocket wheel, chain structure, and the two ends of two rhizoid thick sticks all are equipped with sprocket wheel, links to each other by chain between two sprocket wheels of every end.Retarder 11 adopts worm type of reduction gearings, changes the side into positive the rotation, rotates than being 30:1 rapid operation, simple and easy, the portable charged electric drill of available 20Nm driving torque or manually to utilize handle 3 that retarder 11 is worked.
By the retarder 11 of manual or motorized motions, and then drive a leading screw rotation, this leading screw drives another screw synchronous rotation by transmission device 10 again; Aircraft tyre axially is placed on the two rhizoid thick sticks successively along leading screw, rotates with screw synchronous.For preventing the contingent aircraft tyre disengaging of beating in the transportation, between the upper frame 7 at lower frame 6 two ends, be provided with the spacing cross bar 15 of detouchable, aircraft tyre is between leading screw assembly 12 and spacing cross bar 15; This spacing cross bar 15 is provided with height adjustable spacing hole, make spacing cross bar 15 and the upper limb of aircraft tyre be close to, fixing, highly determine rear with lockset that spacing cross bar 15 is fixing.
Rub for preventing that aircraft tyre that support body carries from contacting with support body, affect tyre rotation, the utility model is equipped with rotating block plate 8 at the upper frame 7 that is positioned at lower frame 6 two ends, the centre of two upper frames 7 at lower frame 6 two ends is equipped with column 17, these column 17 inboards have notch along short transverse, block plate 8 is connected with notch by the second bolt, and block plate 8 is adjustable in the position of column 17 short transverses, can make the center superposition of block plate 8 and aircraft tyre; Be that the diameter of block plate 8 is greater than the internal diameter of aircraft tyre, and less than the external diameter of aircraft tyre.For convenient pivot region of observing aircraft tyre, the outer surface of block plate 8 is equally divided into four zones, in each zone all with the symbol that represents the time, represented throughout the year such as symbol A, B, C, D among Fig. 3, aircraft tyre 8 drives block plate 8 by friction force and rotates synchronously, the rotation situation that can clearly observe aircraft tyre by the symbol on observation block plate 8 outer surfaces like this.
Rub for preventing that aircraft tyre that support body carries from contacting with the sprocket wheel of transmission device, affect tyre rotation, also respectively be provided with a limiting block wheel assembly 9 on the crossbeam of the utility model guiding connection plug-in unit 14 under two ends connect, the limiting block wheel assembly 9 of every end is positioned in the middle of two bearing brackets 16 of this end, and is positioned at the below of block plate 8; Limiting block wheel assembly 9 comprises spacing gear wheel 18 and gear wheel frame, and wherein spacing gear wheel 18 is installed on the lower frame 16 by the gear wheel frame, and the longitudinal center line of spacing gear wheel 18 and the longitudinal center line of aircraft tyre are perpendicular, spacing gear wheel 18.
Upper and lower support body of the present utility model all can be by the rectangular tube welding fabrication.
Principle of work of the present utility model is:
The accumulating frame is collapsible stacking at ordinary times, and upper frame 7 is moved into parallel with lower frame 6, and both highly differ five times, and folding putting greatly saved transport space during transportation, saves time conveniently.When arriving the warehouse installation, limited when outwards turning to four upper frames 1 perpendicular to lower frame 6, with nut the first bolt 4 is tightened.Aircraft tyre is placed between two leading screws, in storing process, shakes the handle 3 that links to each other with reductor 11 or electric drill is docked realization leading screw drive aircraft tyre with reductor 11 and overturn, every three months rotates 90 °.After each accumulating frame installs aircraft tyre, pile when high, upwards hold up with fork truck is whole, four lower guiding by upper strata accumulating frame connect plug-in units 14 and are connected four upper guiding with lower floor and connect plug-in units 13 and guide to docking, combine with the accumulating frame grafting of lower one deck, a few minutes just can be made up one group of accumulating frame, save labor, all be mechanized operation, stopped the potential safety hazard that artificial ascend operation exists.And the design size of compound type aircraft tyre accumulating frame meets the loading and unloading requirement of military east wind transport trolley fully, has guaranteed the facility of transportation, has realized the containerization of accumulating frame transportation.The oad of each frame in the compound type aircraft tyre accumulating frame is identical, and the location of pegging graft is consistent, has realized the normalisation that the accumulating frame is put.
Along with air force's war warehouse storehouse employing wireless radio frequency technology, by with the corresponding Warehouse Management System (WMS) software of the input of shelf card image, realize the fine-grained management of storage goods and materials, use containerization, normalisation, informationalized aircraft tyre accumulating frame, convenient transportation is installed, accurate positioning has solved the difficult problem of air unit's war warehouse storehouse goods and materials emergent pulling, carrying and daily attentions, can provide matenal support for the war instruction quickly.
1. normalisation; The utility model uniform specification can be docked mutually, can also be used for the storage of other materials for preparedness against war, such as storage battery, gas cylinder etc., the normalisation of Implementation repository storage shelf.
2. containerization; The utility model design specification is take active service military truck stowing dimensions as benchmark, satisfies long-distance container shipping requirement, for the emergent pulling of air unit's war warehouse storehouse goods and materials, carrying and daily attention bring very big facility, can fast reserve form guarantee power location.
3. information-based; The utility model can adopt wireless radio-frequency and air force boat material management information system to dock application, can realize fine-grained management and Real Time Monitoring to the accumulating goods and materials.
4. universalization; The utility model also can be used as other boat material stock shelfs, can be used as the interim medical rescue platform of field operations, repairing work platform, commander's conference table, open-air camp bed etc. under field environment.
Claims (10)
1. compound type aircraft tyre accumulating frame, it is characterized in that: comprise support body assembly (5), transmission device (10), retarder (11) and leading screw assembly (12), wherein leading screw assembly (12) is rotatably installed in the bottom of support body assembly (5), be installed in a side of support body assembly (5) by the retarder (11) of manual or motorized motions, and be connected, drive leading screw assembly (12) by transmission device (10) and described leading screw assembly (12) and rotate; Aircraft tyre axially is placed on the leading screw assembly (12) successively along leading screw assembly (12), rotates synchronously with leading screw assembly (12).
2. by compound type aircraft tyre accumulating frame claimed in claim 1, it is characterized in that: described support body assembly (5) comprises that upper frame (7), lower frame (6), upper guiding connect plug-in unit (13), lower guiding connects plug-in unit (14) and L shaped folding (19), wherein lower frame (6) is parallel with leading screw assembly (12), and the two ends of lower frame (6) all are connected with lower guiding and connect plug-in unit (14); The two ends of described lower frame (6) are all hinged with an end of L shaped folding (19) by the first bolt (4), and the other end of each L shaped folding all connects a upper frame (7), are equipped with upper guiding on the top of each upper frame (7) and connect plug-in unit (13).
3. by compound type aircraft tyre accumulating frame claimed in claim 2, it is characterized in that: two described accumulating framves connect plug-in unit (13) and mutually grafting of lower guiding connection plug-in unit (14) by upper guiding.
4. by compound type aircraft tyre accumulating frame claimed in claim 2, it is characterized in that: on the described upper frame (7) that is positioned at lower frame (6) two ends rotating block plate (8) is installed, upper frame (7) is provided with column (17), this column (17) is inboard to have notch along short transverse, described block plate (8) is connected with notch by the second bolt, and block plate (8) is adjustable in the position of column (17) short transverse.
5. by compound type aircraft tyre accumulating frame claimed in claim 4, it is characterized in that: the outer surface of described block plate (8) is equally divided into four zones, in each zone all with the symbol that represents the time.
6. by compound type aircraft tyre accumulating frame claimed in claim 2, it is characterized in that: be provided with the spacing cross bar of detouchable (15) between the described upper frame (7) that is positioned at lower frame (6) two ends, aircraft tyre is positioned between leading screw assembly (12) and the spacing cross bar (15), and the upper limb of aircraft tyre is connected on the spacing cross bar (15).
7. by compound type aircraft tyre accumulating frame claimed in claim 2, it is characterized in that: the two ends of described lower frame (6) all are equipped with limiting block wheel assembly (9), comprise spacing gear wheel (18) and gear wheel frame, wherein spacing gear wheel (18) is installed on the lower frame (16) by the gear wheel frame, and the longitudinal center line of described spacing gear wheel (18) and the longitudinal center line of aircraft tyre are perpendicular.
8. by compound type aircraft tyre accumulating frame claimed in claim 2, it is characterized in that: described lower frame (6) is provided with hanger (1).
9. by compound type aircraft tyre accumulating frame claimed in claim 2, it is characterized in that: described leading screw assembly (12) comprises two leading screws that parallel, the two ends of lower frame (6) are respectively equipped with two bearing brackets (16), the two ends of every rhizoid thick stick all are installed on the bearing bracket (16) by bearing, the two ends of two rhizoid thick sticks all link to each other by transmission device (10), and wherein arbitrary rhizoid thick stick is connected with the mouth of described retarder (11).
10. by compound type aircraft tyre accumulating frame claimed in claim 9, it is characterized in that: described transmission device (10) is sprocket wheel, chain structure, and the two ends of two rhizoid thick sticks all are equipped with sprocket wheel, links to each other by chain between two sprocket wheels of every end.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201220471619.7U CN202880263U (en) | 2012-09-14 | 2012-09-14 | Combined type aviation tyre storage and transportation rack |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201220471619.7U CN202880263U (en) | 2012-09-14 | 2012-09-14 | Combined type aviation tyre storage and transportation rack |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202880263U true CN202880263U (en) | 2013-04-17 |
Family
ID=48071712
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201220471619.7U Expired - Lifetime CN202880263U (en) | 2012-09-14 | 2012-09-14 | Combined type aviation tyre storage and transportation rack |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202880263U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112978192A (en) * | 2021-04-01 | 2021-06-18 | 安徽宏昌机电装备制造有限公司 | Airplane tire stereoscopic storage rack |
-
2012
- 2012-09-14 CN CN201220471619.7U patent/CN202880263U/en not_active Expired - Lifetime
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112978192A (en) * | 2021-04-01 | 2021-06-18 | 安徽宏昌机电装备制造有限公司 | Airplane tire stereoscopic storage rack |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CX01 | Expiry of patent term | ||
| CX01 | Expiry of patent term |
Granted publication date: 20130417 |