CN112978192B - Three-dimensional storage rack for aircraft tires - Google Patents
Three-dimensional storage rack for aircraft tires Download PDFInfo
- Publication number
- CN112978192B CN112978192B CN202110354673.7A CN202110354673A CN112978192B CN 112978192 B CN112978192 B CN 112978192B CN 202110354673 A CN202110354673 A CN 202110354673A CN 112978192 B CN112978192 B CN 112978192B
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- tire
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- 230000006835 compression Effects 0.000 claims description 71
- 238000007906 compression Methods 0.000 claims description 71
- 238000005056 compaction Methods 0.000 claims description 12
- 238000005096 rolling process Methods 0.000 claims description 8
- 230000000712 assembly Effects 0.000 claims description 7
- 238000000429 assembly Methods 0.000 claims description 7
- 239000007787 solid Substances 0.000 claims description 5
- 230000008676 import Effects 0.000 claims description 4
- 230000005540 biological transmission Effects 0.000 description 5
- 238000010586 diagram Methods 0.000 description 2
- 230000004308 accommodation Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65G—TRANSPORT OR STORAGE DEVICES, e.g. CONVEYORS FOR LOADING OR TIPPING, SHOP CONVEYOR SYSTEMS OR PNEUMATIC TUBE CONVEYORS
- B65G1/00—Storing articles, individually or in orderly arrangement, in warehouses or magazines
- B65G1/02—Storage devices
- B65G1/04—Storage devices mechanical
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65G—TRANSPORT OR STORAGE DEVICES, e.g. CONVEYORS FOR LOADING OR TIPPING, SHOP CONVEYOR SYSTEMS OR PNEUMATIC TUBE CONVEYORS
- B65G1/00—Storing articles, individually or in orderly arrangement, in warehouses or magazines
- B65G1/02—Storage devices
- B65G1/04—Storage devices mechanical
- B65G1/0492—Storage devices mechanical with cars adapted to travel in storage aisles
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Transmission Devices (AREA)
- Toys (AREA)
Abstract
The invention relates to a three-dimensional storage rack for aircraft tires, which comprises an outer frame, wherein a left regular hexagon inner frame and a right regular hexagon inner frame are oppositely arranged in the outer frame, a main shaft is arranged in the middle of the left regular hexagon inner frame and the right regular hexagon inner frame, and a left inner bracket disc and a right inner bracket disc are arranged on the main shaft; the left inner bracket plate and the right inner bracket plate are fixedly connected with the left regular hexagon inner frame through brackets respectively; six rotation gears are uniformly distributed on the rotation gear II by the center of the left inner bracket disc, and the gear III is synchronously meshed with the rotation gear II; the left side of the outer frame is provided with a left labor-saving gear set, the inner side of the left labor-saving gear set is provided with a gear five, the outer side of the left labor-saving gear set is provided with a gear four, the gear four is externally connected with a left handle, the gear five is connected with a gear three, and the gear five is connected with a gear four; the gear IV slides inwards to be separated from the gear V, and the gear IV slides outwards to be meshed with the gear V; the invention has simple structure and convenient use.
Description
Technical Field
The invention relates to storage of special tires, in particular to a three-dimensional storage rack for aircraft tires.
Background
Aircraft are of many types, and aircraft tires are wearing parts, and each aircraft use unit has a tire store, which necessarily has a tire frame for accommodating the tires. The stock of aircraft tires has high requirements: 1. the accommodation space cannot be large; 2. to prevent deformation, the tire is turned 90 degrees every quarter; 3. the tires are not allowed to stack; 4. the individual tires are heavy and the loading and unloading height cannot exceed the normal range of manual operation (less than 1.4 meters). The existing general tire frames have the following defects: 1. the top layer is assembled and disassembled beyond the normal range of operation due to the multi-storage and the storage, so that the assembly and disassembly are difficult, and the safety cannot be ensured; 2. double-sided loading and unloading wastes the usable floor area of the warehouse; 3. the tire is easy to deform, so that the rotation of the tire is unstable, the requirement of autorotation in each quarter cannot be met, and the tire is deformed and wasted. 4. The tire frame with various specifications is required, and one tire frame cannot be suitable for tires with all specifications, so that the specifications of the tire frame cannot be matched with the specifications of the tire in a warehouse, and the tire warehouse cannot effectively operate.
Disclosure of Invention
The technical problem to be solved by the invention is to provide the aircraft tire goods shelf which is simple in structure and convenient to use.
In order to solve the technical problems, the invention provides an aircraft tire three-dimensional storage frame, which comprises an outer frame, wherein a left regular hexagon inner frame and a right regular hexagon inner frame are oppositely arranged in the outer frame, a main shaft is arranged in the middle of the left regular hexagon inner frame, and a left inner bracket disc and a right inner bracket disc are arranged on the main shaft; the left inner bracket plate and the right inner bracket plate are fixedly connected with the left regular hexagon inner bracket plate and the right regular hexagon inner bracket plate respectively through brackets;
the left end of the main shaft extends out of the left inner bracket disc and is provided with a second rotation gear and a third rotation gear on the outer side of the main shaft, six rotation gears are uniformly distributed on the second rotation gear by the center of the left inner bracket disc, and the third rotation gear is synchronously meshed with the second rotation gear; the left side of the outer frame is provided with a left labor-saving gear set, the inner side of the left labor-saving gear set is provided with a gear five, the outer side of the left labor-saving gear set is provided with a gear four, the gear four is externally connected with a left handle, the gear five is connected with a gear three, and the gear five is connected with a gear four; the gear IV slides inwards to be separated from the gear V, and the gear IV slides outwards to be meshed with the gear V;
The right end of the main shaft extends out of the right inner bracket disc and is provided with a first gear; the right side of the outer frame is provided with a right labor-saving gear set and a self-locking mechanism, the inner side of the right labor-saving gear set is connected with a first gear, and the outer side of the right labor-saving gear set is provided with a right handle;
The circumference between the left inner bracket disc and the right inner bracket disc is uniformly provided with active rollers, six active rollers are arranged, the left end of each active roller is connected with a corresponding second rotation gear, and the right end of each active roller is movably connected with the right inner bracket disc;
Bearing seats II are respectively arranged on two sides of the outer frame, and the two ends of the main shaft are respectively fixed with the bearing seats II and are connected through the corresponding bearing seats II;
The periphery of the left and right regular hexagon inner frames are provided with adjustable compression roller assemblies and fixed compression roller assemblies; the adjustable compression roller assembly and the fixed compression roller assembly are respectively provided with six groups; the adjustable compression roller assembly comprises an adjustable compression roller bracket, an adjustable compression roller, a pre-tightening bolt and a loading and unloading booster spring, a long slot hole is formed in the joint of the pre-tightening bolt and the adjustable compression roller bracket, a pre-tightening force adjusting bolt is arranged on the adjustable compression roller bracket, and a plurality of limiting holes corresponding to the long slot hole are formed in the left regular hexagon inner frame; the fixed compression roller assembly comprises fixed compression roller legs and fixed compression rollers; the adjustable compression roller support is provided with a bearing seat III, and the two ends of the adjustable compression roller are provided with a bearing III and are connected through the bearing seat III; the fixed compression roller support is provided with a first bearing seat which can be adjusted and fixed back and forth along the fixed compression roller support, and two ends of the fixed compression roller are provided with bearings which are connected with the first bearing seat; the adjustable compression roller assembly is provided with a stress application rod;
the adjustable compression roller, the fixed compression roller and the driving roller are positioned to form an airplane tire accommodating groove, the inner side of a bracket corresponding to the airplane tire accommodating groove is respectively provided with a belt wheel core fixing disc and an inner core disc, and a screw is arranged between the belt wheel core fixing disc and the inner core disc; the outside of the bracket is movably provided with a fixed core disc sliding block, and the fixed core disc sliding block is connected with a screw rod.
Preferably, the left side of the outer frame is provided with a four-season signboard and a four-season pointer; the first outer side of the gear is provided with a digital mark corresponding to the airplane tire accommodating groove.
Preferably, the three-dimensional storage rack for the aircraft tires is also matched with a small electric lifting vehicle, and the small electric lifting vehicle is provided with a tire loading and unloading platform. The small electric lift truck and the tire loading and unloading platform facilitate the rapid loading and unloading of the aircraft tires, and save manpower.
Preferably, the outer frame is also provided with a model signboard, an import and export sign, the model signboard is arranged, and the import and export sign is convenient to operate and can rapidly identify the model of the aircraft tire.
Preferably, the periphery of the driving roller is uniformly distributed with toothed friction surfaces so as to increase the friction force with the tire.
The adjustable compression roller, the fixed compression roller and the driving roller are positioned to form six groups of aircraft tire accommodating grooves; the active rolling rotation drives the aircraft tire to rotate in the aircraft tire accommodating groove through friction, and the adjustable compression rolling and the fixed compression rolling support the aircraft tire and simultaneously maintain flexible rotation of the aircraft tire; the pressure of the adjustable compression roller to the tread of the aircraft tire is adjusted by the cooperation of the pre-tightening bolt and the loading and unloading booster spring, so that the optimal friction force required by the rotation of the aircraft tire in the aircraft tire accommodating groove is met.
The outer frame supports the right and left regular hexagon inner frames through the main shaft, the right handle drives the first gear to work through the right labor-saving gear set when rotating, and the first gear drives the right inner bracket plate to integrally rotate, so that the loading and unloading of the aircraft tires in the aircraft tire accommodating grooves are realized.
The gear IV can stretch back and forth along with the left handle, and the working modes of the driving roll and the left and right regular hexagon inner frame are switched through the adjustment of the disconnection state of the gear IV and the gear V. After the left handle rotates, six driving rollers are driven to synchronously rotate through a gear IV, a gear V and a gear III, and each aircraft tire is driven to rotate in the corresponding aircraft tire accommodating groove through friction force by the rotating driving rollers, so that the quarterly placement angle adjustment of the aircraft tire is completed.
The outer side of the gear I is provided with a digital mark corresponding to the airplane tire accommodating groove, the digital mark corresponding to the airplane tire accommodating groove corresponds to the airplane tire accommodating groove, the outer frame on one side face of the gear I is provided with a self-locking mechanism, and an elastic pin roll in the self-locking mechanism can be manually pulled out to rotate 90 degrees to separate from and automatically spring into a gear tooth slot at any angle to lock the inner frame to rotate, so that fixed point, orientation, height fixing and safe loading and unloading are realized.
The first bearing seat on the fixed rolling component can be adjusted and fixed along the fixed pressing rolling support leg, so that the placing requirements of different types of aircraft tires are met.
The loading and unloading booster spring arranged below the adjustable compaction roller supports the adjustable compaction roller assembly to rotate around the rotary pin shaft, so that the adjustable compaction roller is lifted up, and the required entering and exiting space for loading and unloading the tire is met.
After the stressing rod manually presses down the adjustable compaction roller to compact the tire, a pre-tightening bolt is inserted into the corresponding limiting hole for fixation, and the pre-tightening adjusting bolt can adjust the pressure of the adjustable compaction roller to the tire, namely, the pressure of three equal parts of contact points of the adjustable compaction roller, the driving roller and the fixed roller around the aircraft tire can be adjusted, so that the friction force between the driving roller and the tire is adjusted, and the autorotation effectiveness of the tire is ensured.
The two sides of the airplane tire accommodating groove are provided with centering pressing disc assemblies, and each centering pressing disc assembly consists of a centering pressing disc, a bearing, a manual rotating disc with nuts, a trapezoidal screw shaft, a centering pressing disc sliding block and two bolts. The center bearing of the centering compaction disc is fixed on the rotating disc with the nut, and the manual rotating disc with the nut rotates along the screw rod of the trapezoidal screw shaft, so that the centering compaction disc has a compaction function. The centering compaction disc sliding block can slide to a positioning clamping point along the sliding groove, corresponds to the center point of various types of tires, and ensures that the tires are not inclined to the side while ensuring the concentricity of the tires in the groove.
Compared with the prior art, the invention has the following beneficial effects:
(1) The invention saves space by three-dimensional space multi-groove storage.
(2) The invention realizes fixed point, directional and fixed height loading and unloading through the rotation of the inner frame in the outer frame and the locking at any angle. The loading and unloading height does not exceed the normal range of manual operation, thereby achieving the effects of saving space, safety and stability;
(3) The invention realizes revolution and rotation easily through the transmission of the labor-saving gear set. The two groups of revolution labor-saving gear sets are separated from the rotation labor-saving gear sets, so that the revolution transmission and the rotation transmission are not interfered with each other, and the operation is efficient.
(4) According to the invention, the adjustable compression roller, the driving roller and the fixed roller are adjusted through the pretightening force adjusting bolt, so that the friction force between the driving roller and the tire is adjusted, and the effectiveness and stability of the rotation of the tire are ensured.
Drawings
FIG. 1 is a schematic perspective view of the present invention;
FIG. 2 is a schematic view of a left side partial structure of the present invention;
FIG. 3 is a schematic view of a partial structure of an aircraft tire receiving slot according to the present invention;
FIG. 4 is a schematic view of a left side drive structure of the present invention;
FIG. 5 is a schematic diagram of a left side drive mechanism of the present invention;
fig. 6 is a schematic diagram of a gear-driving of the present invention.
Detailed Description
The invention is further described below with reference to the accompanying drawings:
As shown in fig. 1 to 6, the three-dimensional storage rack for aircraft tires of the present invention comprises an outer frame 1, wherein right and left regular hexagonal inner frames 2,2' are relatively arranged in the outer frame 1, a main shaft 28 is centrally arranged in the right and left regular hexagonal inner frames 2,2', and the main shaft 28 is provided with right and left inner bracket plates 9,9'; the left and right inner bracket plates 9,9 'are fixedly connected with the left and right regular hexagon inner frames 2,2' through brackets 36 respectively;
Six rotation gears II 18 and three gears 19 are arranged on the outer side of the left end of the main shaft 28, which extends out of the left inner support disc 9, six rotation gears II 18 are uniformly distributed around the center of the left inner support disc 9, side gears are integrally arranged on the inner side of the three gears 19, and the side gears of the three gears 19 are synchronously meshed with the rotation gears II 18; the left side of the outer frame 1 is provided with a left labor-saving gear set 22, the inner side of the left labor-saving gear set 22 is provided with a gear five 35, the outer side of the left labor-saving gear set 22 is provided with a gear four 34, the gear four 34 is externally connected with a left handle 10, the gear five 35 is connected with a gear three 19, and the gear five 35 is connected with a gear four 34; the fourth gear 34 slides inwards to be separated from the fifth gear 35, and the fourth gear 34 slides outwards to be meshed with the fifth gear 35;
The right end of the main shaft 28 extends out of the right inner bracket disc 9' and is provided with a first gear 12; the right side of the outer frame 1 is provided with a right labor-saving gear set 22 'and a self-locking mechanism 13, the inner side of the right labor-saving gear set 22' is connected with a first gear 12, and the outer side of the right labor-saving gear set 22 'is provided with a right handle 10';
a driving roller 8 is uniformly distributed between the left inner bracket disc 9 and the right inner bracket disc 9', six driving rollers 8 are arranged, the left end of each driving roller 8 is connected with a corresponding rotation gear II 18, and the right end of each driving roller 8 is movably connected with the right inner bracket disc 9';
Two sides of the outer frame 1 are respectively provided with a second bearing seat 27, and two ends of the main shaft 28 are respectively fixed with the second bearing seat and are connected by the corresponding second bearing seat 27;
The peripheries of the left and right regular hexagon inner frames 2,2' are respectively provided with an adjustable compression roller assembly 3 and a fixed compression roller assembly 5; six groups of adjustable compression roller assemblies 3 and six groups of fixed compression roller assemblies 5 are respectively arranged; the adjustable compression roller assembly 3 comprises an adjustable compression roller bracket 30, an adjustable compression roller 29, a pre-tightening bolt 23 and a loading and unloading assisting spring 11, a long slot hole is formed in the joint of the pre-tightening bolt 23 and the adjustable compression roller bracket 30, a pre-tightening force adjusting bolt 24 is arranged on the adjustable compression roller bracket 30, and a plurality of limiting holes corresponding to the long slot holes are formed in the left regular hexagon inner frame 2; the fixed compression roller assembly 5 comprises fixed compression roller legs 32 and fixed compression rollers 5a; the adjustable compression roller bracket 30 is provided with a bearing seat III 31, and the two ends of the adjustable compression roller 29 are provided with bearings III and are connected by the bearing seat III 31; the fixed compression roller support 32 is provided with a first bearing seat 26, the first bearing seat 26 can be adjusted and retained along the fixed compression roller support 32, and two ends of the fixed compression roller 5a are provided with bearings which are connected with the first bearing seat 26; the adjustable compression roller assembly 3 is provided with a force-applying rod 33;
The adjustable compression roller 29, the fixed compression roller 5a and the driving roller 8 are positioned to form an aircraft tire accommodating groove, the inner side of a bracket 36 corresponding to the aircraft tire accommodating groove is respectively provided with a belt wheel core fixing disc 6 and an inner core disc 4, and a screw is arranged between the belt wheel core fixing disc 6 and the inner core disc 4; the outer side of the bracket 36 is movably provided with a fixed core disc sliding block 7, and the fixed core disc sliding block 7 is connected with a screw rod.
The left side of the outer frame 1 is provided with a four-season signboard 21 and a four-season pointer 20; the outer side of the first gear 12 is provided with a digital mark corresponding to the airplane tire accommodating groove.
The aircraft tire solid storage rack is also matched with a small electric lift car 16.
The outer frame 1 is also provided with a model sign board 14 and an import and export sign 15.
Toothed friction surfaces are uniformly distributed on the periphery of the driving roller 8.
As can be seen from fig. 3, the adjustable compression roller assembly 3 is pressed down by the force-applying rod 33 to rotate until the adjustable compression roller 29 is pressed against the aircraft tire 17, then a larger precompression is applied, and the pretightening bolt 23 is inserted, so that the friction states of the aircraft tire and the adjustable compression roller 29, the fixed compression roller 5a and the driving roller 8 are consistent, and the stable and reliable rotation is achieved.
As can be seen from fig. 5, the left labor-saving gear set 22 and the third gear 19 are rotated by the left handle 10; the gear III 19 drives the rotation gear II 18 in six directions to rotate, the rotation gear II 18 drives the six driving rollers 8 to rotate, and the driving rollers 8 drive the tires 17 to rotate in the airplane tire accommodating grooves.
As can be seen from fig. 6, the right handle 10' rotates the right side labor saving gear set 22', the first transmission gear 12, and the left and right regular hexagonal inner frames 2,2' are integrally rotated along the main shaft 28. The side face of the gear I12 is provided with a self-locking mechanism 13, an elastic self-locking pin in the manual self-locking mechanism 13 pops out to be aligned with the digital mark on the surface of the gear I12, the left and right regular hexagon inner frames 2 and 2' stop, and the position of the airplane tire storage groove is indicated to correspond to the position of the inlet and outlet, so that fixed-point and fixed-height loading and unloading are realized.
As can be seen from fig. 3, the invention can realize the storage of multi-model tires, the fixed compression rollers 5 can be adjusted to corresponding positions on the fixed compression roller legs 32 of the left and right regular hexagon inner frames 2,2', and the long slot holes corresponding to the corresponding bolt holes are added, so that the storage function of multi-model tires can be realized.
In order to realize safe, stable and quick assembly and disassembly, the invention can be provided with a small-sized electric lifting platform car 16 and a tire loading and unloading platform 25, thereby realizing easier, safer, stable and quick assembly and disassembly.
In order to realize the rotation stability of the tire, the invention adds the pretightening force adjusting bolt 24 at the lower part of the long slot hole of the pretightening bolt 23 of the adjustable compression roller bracket, and can adjust the pretightening force of the tire and each roller to ensure that the friction force of the tire and each roller is consistent.
The gear IV 34 can slide inwards to be separated from the gear V35, when the rotation is needed, the gear IV 34 is pulled outwards to be combined with the gear V35, the transmission rotation is finished, the gear IV 34 is pushed inwards to be separated from the gear V35, and the whole rotation switching of the airplane tire rotation and the left and right regular hexagon inner frames 2 and 2' is realized.
The foregoing has shown and described the basic principles and main features of the present invention and the advantages of the present invention. It will be understood by those skilled in the art that the present invention is not limited to the embodiments described above, and that the above embodiments and descriptions are merely illustrative of the principles of the present invention, and various changes and modifications may be made without departing from the spirit and scope of the invention, which is defined in the appended claims. The scope of the invention is defined by the appended claims and equivalents thereof.
Claims (5)
1. The utility model provides a three-dimensional storage frame of aircraft tire, includes outer frame (1), its characterized in that: the outer frame (1) is internally provided with left and right regular hexagon inner frames (2, 2 '), the left and right regular hexagon inner frames (2, 2 ') are centrally provided with a main shaft (28), and the main shaft (28) is provided with left and right inner bracket plates (9, 9 '); the left inner bracket plates (9, 9 ') and the right inner bracket plates (2, 2') are respectively and fixedly connected with the left regular hexagon inner frame plates (36);
The left end of the main shaft (28) extends out of the left inner support disc (9), a second rotation gear (18) and a third rotation gear (19) are arranged on the outer side of the left inner support disc (9), six rotation gears are uniformly distributed on the second rotation gear (18) by the circle center of the left inner support disc (9), and the third rotation gear (19) is synchronously meshed with the second rotation gear (18); the left side of the outer frame (1) is provided with a left labor-saving gear set (22), the inner side of the left labor-saving gear set (22) is provided with a gear five (35), the outer side of the left labor-saving gear set (22) is provided with a gear four (34), the gear four (34) is externally connected with a left handle (10), the gear five (35) is connected with a gear three (19), and the gear five (35) is connected with the gear four (34); the fourth gear (34) slides inwards to be separated from the fifth gear (35), and the fourth gear (34) slides outwards to be meshed with the fifth gear (35);
The right end of the main shaft (28) extends out of the right inner bracket disc (9'), and a gear I (12) is arranged behind the right inner bracket disc; the right side of the outer frame (1) is provided with a right labor-saving gear set (22 ') and a self-locking mechanism (13), the inner side of the right labor-saving gear set (22') is connected with a first gear (12), and the outer side of the right labor-saving gear set (22 ') is provided with a right handle (10');
Active rollers (8) are uniformly distributed on the circumference between the left inner bracket disc (9) and the right inner bracket disc (9 '), the active rollers (8) are provided with six branches, the left end of each active roller (8) is connected with a corresponding rotation gear II (18), and the right end of each active roller (8) is movably connected with the right inner bracket disc (9');
two sides of the outer frame (1) are respectively provided with a second bearing seat (27), and two ends of the main shaft (28) are respectively fixed with a second bearing and are connected by the corresponding second bearing seats (27);
The peripheries of the left and right regular hexagon inner frames (2, 2') are respectively provided with an adjustable compression roller assembly (3) and a fixed compression roller assembly (5); six groups of adjustable compression roller assemblies (3) and six groups of fixed compression roller assemblies (5) are arranged; the adjustable compression roller assembly (3) comprises an adjustable compression roller support (30), an adjustable compression roller (29), a pre-tightening bolt (23) and a loading and unloading assisting spring (11), a long slot hole is formed in the joint of the pre-tightening bolt (23) and the adjustable compression roller support (30), a pre-tightening force adjusting bolt (24) is arranged on the adjustable compression roller support (30), and a plurality of limiting holes corresponding to the long slot hole are formed in the left regular hexagon inner frame (2); the fixed compression roller assembly (5) comprises fixed compression roller legs (32) and fixed compression rollers (5 a); the adjustable compression roller support (30) is provided with a bearing seat III (31), and the two ends of the adjustable compression roller (29) are provided with a bearing III and are connected by the bearing seat III (31); the fixed compression rolling support leg (32) is provided with a first bearing seat (26), the first bearing seat (26) can be adjusted and fixed back and forth along the fixed compression rolling support leg (32), and two ends of the fixed compression rolling (5 a) are provided with bearings which are connected with the first bearing seat (26); the adjustable compression roller assembly (3) is provided with a stress application rod (33);
The adjustable compaction roller (29), the fixed compaction roller (5 a) and the driving roller (8) form an airplane tire storage groove after being fixed, a belt wheel fixed core disc (6) and an inner fixed core disc (4) are respectively arranged on the inner side of a bracket (36) corresponding to the airplane tire storage groove, a fixed core disc sliding block (7) is arranged on the outer side of the bracket (36), and the fixed position of the fixed core disc sliding block (7) can be adjusted along the bracket (36).
2. The aircraft tire solid storage rack of claim 1, wherein: the left side of the outer frame (1) is provided with a four-season signboard (21) and a four-season pointer (20); the outer side of the first gear (12) is provided with a digital mark corresponding to the airplane tire accommodating groove.
3. The aircraft tire solid storage rack of claim 1, wherein: the aircraft tire three-dimensional storage rack is also matched with a small electric lifting vehicle (16), and the small electric lifting vehicle (16) is provided with a tire loading and unloading platform (25).
4. The aircraft tire solid storage rack of claim 1, wherein: the outer frame (1) is also provided with a model signboard (14); and an import and export identifier (15).
5. The aircraft tire solid storage rack of claim 1, wherein: toothed friction surfaces are uniformly distributed on the periphery of the driving roller (8).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110354673.7A CN112978192B (en) | 2021-04-01 | 2021-04-01 | Three-dimensional storage rack for aircraft tires |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110354673.7A CN112978192B (en) | 2021-04-01 | 2021-04-01 | Three-dimensional storage rack for aircraft tires |
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| Publication Number | Publication Date |
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| CN112978192A CN112978192A (en) | 2021-06-18 |
| CN112978192B true CN112978192B (en) | 2024-06-14 |
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| CN202110354673.7A Active CN112978192B (en) | 2021-04-01 | 2021-04-01 | Three-dimensional storage rack for aircraft tires |
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Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114772141B (en) * | 2022-06-17 | 2023-01-17 | 佛山井松智能科技有限公司 | Tire rotating goods shelf |
| CN119059347B (en) * | 2024-11-05 | 2025-02-25 | 双钱集团（江苏）轮胎有限公司 | Tire bead ring storage device |
Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN214568165U (en) * | 2021-04-01 | 2021-11-02 | 安徽宏昌机电装备制造有限公司 | Airplane tire stereoscopic storage rack |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2887364B2 (en) * | 1995-05-24 | 1999-04-26 | 日本クレセント株式会社 | Tire storage method and tire storage warehouse |
| CN202880263U (en) * | 2012-09-14 | 2013-04-17 | 中国人民解放军空军沈阳航空四站装备修理厂 | Combined type aviation tyre storage and transportation rack |
| SK7060Y1 (en) * | 2013-08-28 | 2015-03-03 | Martin Grexa | Method of uniform tire storage and device for thereof |
| CN208915977U (en) * | 2018-07-23 | 2019-05-31 | 青岛高测科技股份有限公司 | A kind of vertical rotary formula tire storage device |
| CN111605955B (en) * | 2020-06-19 | 2024-08-20 | 成都成设航空科技股份公司 | Rotating wheel type tire-navigation three-dimensional storage system and tire-navigation storage method |
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Patent Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN214568165U (en) * | 2021-04-01 | 2021-11-02 | 安徽宏昌机电装备制造有限公司 | Airplane tire stereoscopic storage rack |
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