CN112978192A - Airplane tire stereoscopic storage rack - Google Patents
Airplane tire stereoscopic storage rack Download PDFInfo
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- CN112978192A CN112978192A CN202110354673.7A CN202110354673A CN112978192A CN 112978192 A CN112978192 A CN 112978192A CN 202110354673 A CN202110354673 A CN 202110354673A CN 112978192 A CN112978192 A CN 112978192A
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- 238000000429 assembly Methods 0.000 claims description 7
- 238000005056 compaction Methods 0.000 claims description 6
- 230000008676 import Effects 0.000 claims 1
- 230000005540 biological transmission Effects 0.000 description 9
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
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Classifications
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- 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
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- 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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Abstract
The invention relates to an airplane tire stereoscopic storage rack which comprises an outer frame, wherein left and right regular hexagonal inner frames are oppositely arranged in the outer frame, a main shaft is arranged in the middle of the left and right regular hexagonal inner frames, and a left and right inner support disc is arranged on the main shaft; the left and right inner bracket discs are fixedly connected with the left and right regular hexagonal inner frames through brackets respectively; the left end of the main shaft extends out of the left inner support disc and is provided with a second rotation gear and a third gear on the outer side, six rotation gears are uniformly distributed on the second rotation gear at the center of the circle of the left inner support disc, and the third gear is synchronously meshed with the second rotation gear; a left labor-saving gear set is arranged on the left side of the outer frame, a gear five is arranged on the inner side of the left labor-saving gear set, a gear four is arranged on the outer side of the left labor-saving gear set, 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 the gear four; the gear slides to the inner side in the four directions to be separated from the gear V, and the gear slides to the outer side in the four directions to be meshed with the gear V; the invention has simple structure and convenient use.
Description
Technical Field
The invention relates to special tire storage, in particular to a three-dimensional storage rack for aircraft tires.
Background
The models of the airplanes are various, the airplane tires are wearing parts, each airplane use unit is provided with a tire warehouse, and the tire warehouse is necessarily provided with a tire rack for accommodating the tires. The inventory of aircraft tires has high requirements: 1. the storage space cannot be large; 2. to prevent deformation, the tire must be rotated 90 degrees every season; 3. the tire is not allowed to be laminated; 4. the individual tires are heavy and the loading and unloading height cannot exceed the normal range for manual handling (less than 1.4 meters). The prior universal tyre frame has the following defects: 1. the loading and unloading of the top layer are beyond the normal range of operation due to the multi-storage and storage, so that the loading and unloading are difficult, and the safety cannot be guaranteed; 2. the double-sided loading and unloading wastes the use area of a storehouse; 3. the tire rolls and is easy to deform, so that the rotation of the tire is unstable, the rotation requirement of every quarter cannot be realized, and the tire is deformed and wasted. 4. The tire frames with various specifications are needed, one tire frame cannot be suitable for tires with all specifications, so that the specification of the tire frame cannot be matched with the specification of tires in a warehouse, and the tire warehouse cannot operate effectively.
Disclosure of Invention
The invention aims to provide an aircraft tire shelf which is simple in structure and convenient to use.
In order to solve the technical problem, the airplane tire three-dimensional storage rack comprises an outer frame, wherein left and right regular hexagonal inner frames are oppositely arranged in the outer frame, a main shaft is arranged in the middle of the left and right regular hexagonal inner frames, and the main shaft is provided with a left inner support plate and a right inner support plate; the left and right inner support plates are fixedly connected with the left and right regular hexagonal inner frames through supports respectively;
a second rotation gear and a third rotation gear are arranged on the outer side of the left inner support disc after the left end of the main shaft extends out of the left inner support disc, six rotation gears are uniformly distributed on the second rotation gear at the center of the left inner support disc, and the third rotation gear is synchronously meshed with the second rotation gear; a left labor-saving gear set is arranged on the left side of the outer frame, a gear five is arranged on the inner side of the left labor-saving gear set, a gear four is arranged on the outer side of the left labor-saving gear set, 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 the gear four; the gear slides to the inner side in the four directions to be separated from the gear five, and the gear slides to the outer side in the four directions to be meshed with the gear five;
a first gear is arranged at the right end of the main shaft after extending out of the right inner support disc; a right labor-saving gear set and a self-locking mechanism are arranged on the right side of the outer frame, the inner side of the right labor-saving gear set is connected with a first gear, and a right handle is arranged on the outer side of the right labor-saving gear set;
the driving rollers are uniformly distributed on the circumference between the left inner support disc and the right inner support disc, six driving rollers are arranged, the left ends of the driving rollers are connected with the corresponding second self-rotating gears, and the right ends of the driving rollers are movably connected with the right inner support disc;
two sides of the outer frame are respectively provided with a second bearing seat, and two ends of the main shaft are respectively fixed with the second bearing and connected by the corresponding second bearing seats;
the periphery of the inner frame of the left regular hexagon is provided with an adjustable compaction roller assembly and a fixed compaction roller assembly; six groups of adjustable compression roller assemblies and six groups of fixed compression roller assemblies are arranged; the adjustable pressing roller assembly comprises an adjustable pressing roller bracket, an adjustable pressing roller, a pre-tightening bolt and a loading and unloading assisting spring, wherein a long slotted hole is formed in the joint of the pre-tightening bolt and the adjustable pressing roller bracket, a pre-tightening force adjusting bolt is arranged on the adjustable pressing roller bracket, and a plurality of limiting holes corresponding to the long slotted hole are formed in the left regular hexagon inner frame; the fixed pressing roller assembly comprises a fixed pressing roller supporting leg and a fixed pressing roller; a third bearing seat is arranged on the adjustable pressing roller bracket, and a third bearing is arranged at two ends of the adjustable pressing roller and connected by the third bearing seat; the fixed pressing roller supporting leg is provided with a first bearing seat, the first bearing seat can be adjusted forwards and backwards along the fixed pressing roller supporting leg for fixing, and two ends of the fixed pressing roller are provided with bearings and are connected with the first bearing seat; the adjustable pressing roller assembly is provided with a force applying rod;
the adjustable pressing roller, the fixed pressing roller and the driving roller are fixed to form an airplane tire accommodating groove, the inner side of a support corresponding to the airplane tire accommodating groove is provided with a belt wheel core fixing disc and an inner core fixing disc respectively, and a screw rod is arranged between the belt wheel core fixing disc and the inner core fixing disc; the outer side of the bracket is movably provided with a core fixing disk sliding block, and the core fixing disk sliding block is connected with the screw rod.
Preferably, a four-season signboard and a four-season pointer are arranged on the left side of the outer frame; and a digital mark corresponding to the airplane tire accommodating groove is arranged on the outer side of the gear.
Preferably, the aircraft tire stereoscopic storage rack is further matched with a small electric lift truck, and the small electric lift truck is provided with a tire loading and unloading platform. The small electric lift truck and the tire loading and unloading platform facilitate the quick loading and unloading of the aircraft tires and save manpower.
Preferably, the outer frame is further provided with a model signboard, an inlet and outlet sign, the model signboard is arranged, the inlet and outlet sign is convenient to operate, and the model of the airplane tire is rapidly recognized.
Preferably, the periphery of the driving roller is uniformly distributed with a toothed friction surface so as to increase the friction force with the tire.
The adjustable pressing roller, the fixed pressing roller and the active roller form six groups of airplane tire accommodating grooves after being fixed; the active roller rotates to drive the airplane tire to rotate in the airplane tire accommodating groove through friction, and the adjustable pressing roller and the fixed pressing roller support the airplane tire and maintain the flexible rotation of the airplane tire; the airplane tire is put into the airplane tire accommodating groove, then the force applying rod is pressed downwards, the pressure of the adjustable pressing roller on the tread of the airplane tire is adjusted through the cooperation of the pre-tightening bolt and the loading and unloading force-applying spring, and the optimal friction force required by the autorotation of the airplane tire in the airplane tire accommodating groove is met.
The outer frame supports the left and right regular hexagonal inner frames through the main shaft, the gear I is driven to work through the right labor-saving gear set when the right handle rotates, the gear I drives the right inner support disc to integrally rotate, and the loading and unloading of the airplane tires in the airplane tire storage grooves are realized.
The gear four can stretch back and forth along with the left hand handle, and the working modes of the active rolling and the left and right regular hexagon inner frame are switched by adjusting the disconnection state of the gear four and the gear five. After the left handle rotates, the six driving rollers are driven by the gear four, the gear five and the gear three to synchronously rotate, and then the rotating driving rollers drive the airplane tires to rotate in the corresponding airplane tire accommodating grooves through friction force, so that the quarterly placement angle adjustment of the airplane tires is completed.
The outer side of the first gear is provided with a digital mark corresponding to the airplane tire storage groove, the digital mark corresponding to the airplane tire storage groove corresponds to the airplane tire storage groove, a self-locking mechanism is installed on an outer frame on one side face of the first gear, an elastic pin shaft in the self-locking mechanism can be manually pulled out to rotate for 90 degrees to be separated from the outer frame and automatically bounced into a gear tooth groove at any angle to lock an inner frame to rotate, and fixed point, orientation, height fixing and safe assembly and disassembly are achieved.
The first bearing seat on the fixed roller assembly can be adjusted forwards and backwards along the fixed pressing roller support leg for fixing, so that the placement requirements of airplane tires of different models are met.
The loading and unloading assisting spring arranged below the adjustable pressing roller supports the adjustable pressing roller assembly to rotate around the rotating pin shaft, so that the adjustable pressing roller is lifted, and the requirement of loading and unloading the tire in and out space is met.
After the force applying rod manually presses the adjustable pressing roller to press the tire, the pre-tightening bolt is inserted into the corresponding limiting hole to be fixed, the pre-tightening adjusting bolt can adjust the pressure of the adjustable pressing roller on the tire, namely the pressure of the adjustable pressing roller, the adjustable driving roller and the adjustable fixing roller around the contact point of the airplane tire in three equal parts 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.
And centering hold-down disk assemblies are arranged on two sides of the aircraft tire accommodating groove and each centering hold-down disk assembly consists of a centering hold-down disk, a bearing, a manual rotating disk with a nut, a trapezoidal screw shaft, a centering hold-down disk sliding block and two bolts. The center bearing of the centering pressing 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 pressing function is realized. The centering pressing disc sliding block can slide to a positioning clamping point along the sliding groove and corresponds to the central point of tires of various models, and the concentricity of the tires in the groove is guaranteed while the tires are prevented from being inclined to the side.
Compared with the prior art, the invention has the following beneficial effects:
(1) the invention realizes space saving by three-dimensional space multi-groove storage.
(2) The invention realizes fixed-point, directional, fixed-height loading and unloading by rotating the inner frame in the outer frame and locking at any angle. The loading and unloading height does not exceed the normal range of manual operation, thereby achieving the effects of space saving, safety and stability;
(3) the invention realizes revolution and rotation easily through the transmission of the labor-saving gear set. Through the separation of the two groups of revolution labor-saving gear sets and the rotation labor-saving gear set, the mutual noninterference of revolution transmission and rotation transmission is realized, and the operation is efficient.
(4) The invention adjusts the pressing force of the adjustable pressing roller, the driving roller and the fixed roller and the tire through the pretightening force adjusting bolt, thereby adjusting the friction force of the driving roller and the tire and ensuring the validity and the stability of the autorotation of the tire.
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 a tire receiving groove of an aircraft according to the present invention;
FIG. 4 is a schematic view of the left side transmission structure of the present invention;
FIG. 5 is a schematic transmission diagram of the left transmission structure of the present invention;
fig. 6 is a schematic view of the gear transmission of the present invention.
Detailed Description
The invention is further described with reference to the accompanying drawings in which:
as shown in fig. 1 to 6, the three-dimensional storage rack for aircraft tires comprises an outer frame 1, wherein left and right regular hexagonal inner frames 2, 2 ' are oppositely arranged in the outer frame 1, a spindle 28 is arranged in the center of the left and right regular hexagonal inner frames 2, 2 ', and the spindle 28 is provided with left and right inner support plates 9, 9 '; the left and right inner support plates 9 and 9 'are fixedly connected with the left and right regular hexagonal inner frames 2 and 2' through supports 36 respectively;
a second rotation gear 18 and a third rotation gear 19 are arranged on the outer side of the left inner support disc 9 after the left end of the main shaft 28 extends out of the left inner support disc 9, six rotation gears 18 are uniformly distributed on the second rotation gear 18 by using the circle center of the left inner support disc 9, side gears are integrally arranged on the inner sides of the third rotation gear 19, and the side gears of the third rotation gear 19 are synchronously meshed with the second rotation gear 18; a left labor-saving gear set 22 is arranged on the left side of the outer frame 1, a gear five 35 is arranged on the inner side of the left labor-saving gear set 22, a gear four 34 is arranged on the outer side of the left labor-saving gear set 22, the gear four 34 is externally connected with the 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 gear four 34 slides inwards to separate from the gear five 35, and the gear four 34 slides outwards to be meshed with the gear five 35;
a first gear 12 is arranged at the right end of the main shaft 28 after extending out of the right inner support plate 9'; a right labor-saving gear set 22 'and a self-locking mechanism 13 are arranged on the right side of the outer frame 1, the inner side of the right labor-saving gear set 22' is connected with a first gear 12, and a right handle 10 'is arranged on the outer side of the right labor-saving gear set 22';
the driving rollers 8 are uniformly distributed on the circumference between the left inner support disc 9 and the right inner support disc 9 ', six driving rollers 8 are arranged, the left end of each driving roller 8 is connected with a corresponding second self-rotating gear 18, and the right end of each driving roller 8 is movably connected with the right inner support 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 and are connected by the corresponding second bearing seats 27;
the periphery of the left and right regular hexagonal inner frames 2, 2' is provided with an adjustable compaction roller component 3 and a fixed compaction roller component 5; six groups of adjustable pressing roller assemblies 3 and six groups of fixed pressing roller assemblies 5 are arranged; the adjustable pressing roller assembly 3 comprises an adjustable pressing roller bracket 30, an adjustable pressing roller 29, a pre-tightening bolt 23 and a loading and unloading power-assisted spring 11, a long slotted hole is formed in the joint of the pre-tightening bolt 23 and the adjustable pressing roller bracket 30, a pre-tightening force adjusting bolt 24 is arranged on the adjustable pressing roller bracket 30, and a plurality of limiting holes corresponding to the long slotted hole are formed in the left regular hexagonal inner frame 2; the fixed pressing roller assembly 5 comprises a fixed pressing roller support leg 32 and a fixed pressing roller 5 a; a third bearing seat 31 is arranged on the adjustable pressing roller bracket 30, and a third bearing is arranged at two ends of the adjustable pressing roller 29 and connected by the third bearing seat 31; the fixed pressing roller support leg 32 is provided with a first bearing seat 26, the first bearing seat 26 can be adjusted forwards and backwards along the fixed pressing roller support leg 32 for fixing, and two ends of the fixed pressing roller 5a are provided with bearings and are connected with the first bearing seat 26; the adjustable pressing roller component 3 is provided with a forcing rod 33;
the adjustable pressing roller 29, the fixed pressing roller 5a and the driving roller 8 are retained to form an airplane tire accommodating groove, the inner sides of the brackets 36 corresponding to the airplane tire accommodating groove are respectively provided with a belt wheel core fixing disc 6 and an inner core fixing disc 4, and a screw rod is arranged between the belt wheel core fixing disc 6 and the inner core fixing disc 4; the outer side of the bracket 36 is movably provided with a core fixing disk sliding block 7, and the core fixing disk sliding block 7 is connected with the screw rod.
A four-season signboard 21 and a four-season pointer 20 are arranged on the left side of the outer frame 1; and a digital mark corresponding to the airplane tire accommodating groove is arranged on the outer side of the first gear 12.
The airplane tire stereoscopic storage rack is also matched with a small electric lift truck 16.
The outer frame 1 is further provided with a model signboard 14 and an inlet and outlet sign 15.
The periphery of the driving roller 8 is uniformly distributed with toothed friction surfaces.
As can be seen from fig. 3, the adjustable pressure roller assembly 3 is pressed down by the force applying rod 33 to rotate until the adjustable pressure roller 29 presses the aircraft tire 17, then a little higher pre-pressure is applied, and the pre-tightening latch 23 is inserted, so that the aircraft tire can be ensured to be consistent with the friction states of the adjustable pressure roller 29, the fixed pressure roller 5a and the active roller 8, and the stable and reliable autorotation is achieved.
As can be seen in fig. 5, the left side labor-saving gear set 22 and the third gear 19 are rotated by the left handle 10; the third gear 19 drives the second autorotation gear 18 in six directions to rotate, the second autorotation gear 18 drives the six driving rollers 8 to rotate, and the driving rollers 8 drive the tires 17 to autorotate in the tire accommodating grooves of the airplane.
As shown in fig. 6, the right handle 10 ' rotates the right power saving gear set 22 ' and the first transmission gear 12 to integrally rotate the right and left regular hexagonal inner frames 2, 2 ' along the main shaft 28. The side surface of the first gear 12 is provided with a self-locking mechanism 13, an elastic self-locking pin shaft in the manual self-locking mechanism 13 is popped out to be aligned with the digital marks on the surface of the first gear 12, the left and right regular hexagonal inner frames 2 and 2' are stopped to indicate the position of the tire storage groove of the airplane to correspond to the position of an inlet and an outlet, and therefore fixed-point, fixed-height loading and unloading are achieved.
As can be seen from figure 3, the invention can realize the storage of various types of tires, the fixed pressing rollers 5 can be adjusted and fixed on the fixed pressing roller supporting feet 32 of the left and right regular hexagon inner frames 2, 2' to corresponding position points, and the slotted holes corresponding to the corresponding bolt holes are added, thereby achieving the storage function of various types of tires.
In order to realize safe, stable and quick assembly and disassembly, the small electric lifting platform truck 16 can be equipped, and the tire assembly and disassembly platform 25 can be additionally manufactured, so that easier, safe, stable and quick assembly and disassembly are realized.
In order to realize the stability of the autorotation of the tire, the pretightening force adjusting bolt 24 is added at the lower part of the long slotted hole of the pretightening bolt 23 of the adjustable pressing roller bracket, so that the prepressing force of the tire and each roller can be adjusted, and the friction force of the tire and each roller is consistent.
The gear four 34 of the invention can slide inwards to separate from the gear five 35, when the rotation is needed, the gear four 34 is pulled outwards to be combined with the gear five 35, the transmission rotation is carried out, the rotation is finished, the gear four 34 is pushed inwards to separate from the gear five 35, and the integral rotation switching between the rotation of the airplane tire and the left and right regular hexagon inner frames 2 and 2' is realized.
The foregoing shows and describes the general principles and broad features of the present invention and advantages thereof. It will be understood by those skilled in the art that the present invention is not limited to the embodiments described above, which are described in the specification and illustrated only to illustrate the principle of the present invention, but that various changes and modifications may be made therein without departing from the spirit and scope of the present invention, which fall within the scope of the invention as claimed. 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: a left regular hexagonal inner frame (2) and a right regular hexagonal inner frame (2, 2 ') are oppositely arranged in the outer frame (1), a main shaft (28) is arranged in the middle of the left regular hexagonal inner frame (2, 2 '), and a left inner support plate and a right inner support plate (9, 9 ') are arranged on the main shaft (28); the left and right inner support plates (9, 9 ') are fixedly connected with the left and right regular hexagonal inner frames (2, 2') through supports (36) respectively;
a left inner support disc (9) extends outwards from the left end of the spindle (28), a second rotation gear (18) and a third 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) with the circle center of the left inner support disc (9), and the third gear (19) is synchronously meshed with the second rotation gear (18); a left labor-saving gear set (22) is arranged on the left side of the outer frame (1), a fifth gear (35) is arranged on the inner side of the left labor-saving gear set (22), a fourth gear (34) is arranged on the outer side of the left labor-saving gear set (22), the fourth gear (34) is externally connected with a left handle (10), the fifth gear (35) is connected with a third gear (19), and the fifth gear (35) is connected with the fourth gear (34); the gear four (34) slides inwards to be separated from the gear five (35), and the gear four (34) slides outwards to be meshed with the gear five (35);
a first gear (12) is arranged at the right end of the main shaft (28) after extending out of the right inner support disc (9'); a right labor-saving gear set (22 ') and a self-locking mechanism (13) are arranged on the right side of the outer frame (1), the inner side of the right labor-saving gear set (22') is connected with the first gear (12), and a right handle (10 ') is arranged on the outer side of the right labor-saving gear set (22');
active rollers (8) are uniformly distributed on the circumference between the left inner support disc and the right inner support disc (9, 9 '), six active rollers (8) are arranged, the left end of each active roller (8) is connected with a corresponding second self-rotating gear (18), and the right end of each active roller (8) is movably connected with the right inner support 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 connected by the corresponding second bearing seats (27);
the periphery of the left and right regular hexagonal inner frames (2, 2') is provided with an adjustable compaction roller assembly (3) and a fixed compaction roller assembly (5); six groups of adjustable pressing roller assemblies (3) and six groups of fixed pressing roller assemblies (5) are arranged; the adjustable pressing roller assembly (3) comprises an adjustable pressing roller support (30), an adjustable pressing roller (29), a pre-tightening bolt (23) and a loading and unloading power-assisted spring (11), a long slotted hole is formed in the joint of the pre-tightening bolt (23) and the adjustable pressing roller support (30), a pre-tightening force adjusting bolt (24) is arranged on the adjustable pressing roller support (30), and a plurality of limiting holes corresponding to the long slotted hole are formed in the left regular hexagonal inner frame (2); the fixed pressing roller assembly (5) comprises a fixed pressing roller supporting leg (32) and a fixed pressing roller (5 a); a third bearing seat (31) is arranged on the adjustable pressing roller bracket (30), and a third bearing is arranged at two ends of the adjustable pressing roller (29) and connected by the third bearing seat (31); the fixed pressing roller support leg (32) is provided with a first bearing seat (26), the first bearing seat (26) can be adjusted forwards and backwards along the fixed pressing roller support leg (32) for fixation, and two ends of the fixed pressing roller (5 a) are provided with bearings and are connected with the first bearing seat (26); the adjustable pressing roller component (3) is provided with a forcing rod (33);
the adjustable pressing roller (29), the fixed pressing roller (5 a) and the driving roller (8) are fixed to form an airplane tire storage groove, the inner side of a support (36) corresponding to the airplane tire storage groove is provided with a belt wheel core fixing disc (6) and an inner core fixing disc (4) respectively, the outer side of the support (36) is provided with a core fixing disc sliding block (7), and the core fixing disc sliding block (7) can be adjusted to be fixed along the support (36).
2. An aircraft tire stereoscopic storage rack as in claim 1, wherein: a four-season signboard (21) and a four-season pointer (20) are arranged on the left side of the outer frame (1); and the outer side of the first gear (12) is provided with a digital mark corresponding to the tire accommodating groove of the airplane.
3. An aircraft tire stereoscopic storage rack as in claim 1, wherein: the airplane tire stereoscopic storage rack is also matched with a small electric lift truck (16), and the small electric lift truck (16) is provided with a tire loading and unloading platform (25).
4. An aircraft tire stereoscopic storage rack as in claim 1, wherein: the outer frame (1) is also provided with a model signboard (14); an import and export identifier (15).
5. An aircraft tire stereoscopic storage rack as in claim 1, wherein: the periphery of the driving roller (8) is uniformly distributed with toothed friction surfaces.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110354673.7A CN112978192A (en) | 2021-04-01 | 2021-04-01 | Airplane tire stereoscopic storage rack |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110354673.7A CN112978192A (en) | 2021-04-01 | 2021-04-01 | Airplane tire stereoscopic storage rack |
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| Publication Number | Publication Date |
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| CN112978192A true CN112978192A (en) | 2021-06-18 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN202110354673.7A Pending CN112978192A (en) | 2021-04-01 | 2021-04-01 | Airplane tire stereoscopic storage rack |
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| CN (1) | CN112978192A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114772141A (en) * | 2022-06-17 | 2022-07-22 | 佛山井松智能科技有限公司 | Tire rotating goods shelf |
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| 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 |
| CN111605955A (en) * | 2020-06-19 | 2020-09-01 | 成都成设航空科技股份公司 | Rotating wheel type air tire three-dimensional storage system and air tire storage method |
| 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 |
-
2021
- 2021-04-01 CN CN202110354673.7A patent/CN112978192A/en active Pending
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH08319006A (en) * | 1995-05-24 | 1996-12-03 | Nippon Kuresento Kk | Method and storage for cubically storing tire |
| 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 |
| DE202014104016U1 (en) * | 2013-08-28 | 2014-10-21 | Martin Grexa | Device for tire storage |
| 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 |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN114772141A (en) * | 2022-06-17 | 2022-07-22 | 佛山井松智能科技有限公司 | Tire rotating goods shelf |
| CN114772141B (en) * | 2022-06-17 | 2023-01-17 | 佛山井松智能科技有限公司 | Tire rotating goods shelf |
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