CN215317329U - Blank warehouse for machining aviation parts - Google Patents
Blank warehouse for machining aviation parts Download PDFInfo
- Publication number
- CN215317329U CN215317329U CN202121275217.5U CN202121275217U CN215317329U CN 215317329 U CN215317329 U CN 215317329U CN 202121275217 U CN202121275217 U CN 202121275217U CN 215317329 U CN215317329 U CN 215317329U
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- storage box
- wall
- blank
- bearing plate
- fixedly installed
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- 238000003754 machining Methods 0.000 title abstract description 9
- 238000003860 storage Methods 0.000 claims abstract description 40
- 238000012545 processing Methods 0.000 claims abstract description 14
- 238000001125 extrusion Methods 0.000 claims description 6
- 238000000034 method Methods 0.000 abstract description 4
- 230000008569 process Effects 0.000 abstract description 4
- 244000309464 bull Species 0.000 description 4
- 238000004519 manufacturing process Methods 0.000 description 3
- 230000001737 promoting effect Effects 0.000 description 3
- 238000011161 development Methods 0.000 description 2
- 230000005484 gravity Effects 0.000 description 2
- 238000003780 insertion Methods 0.000 description 2
- 230000037431 insertion Effects 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000007123 defense Effects 0.000 description 1
- 230000010354 integration Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000008092 positive effect Effects 0.000 description 1
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Abstract
The utility model relates to the technical field of blank libraries for machining aviation parts, in particular to a blank library for machining aviation parts, which comprises a box body, a driving assembly and a storage box, wherein an upper chassis and a lower chassis are symmetrically and fixedly installed on the inner wall of the box body, the storage box is uniformly and fixedly installed on the outer surface of the driving assembly, the driving assembly comprises a driving motor and a rotating rod, the driving motor is fixedly installed on the upper surface of the box body, the rotating rod is fixedly installed on the driving motor, the storage box is fixedly installed on the outer surface of the rotating rod, through holes are symmetrically formed in the bottom surface of the storage box, a lifting rod is inserted into the inner wall of each through hole, a bearing plate is fixedly installed at the upper end of each lifting rod, a disc is fixedly installed at one end, away from the bearing plate, of each lifting rod, and a spring a is sleeved on the outer surface of each lifting rod, which is located between the disc and the storage box. According to the utility model, through mutual matching of all the parts, automatic replacement of the full-load disc and the empty-load disc can be realized, and the working efficiency of the whole processing process is improved.
Description
Technical Field
The utility model relates to the technical field of blank libraries for machining aviation parts, in particular to a blank library for machining aviation parts.
Background
The aviation manufacturing industry belongs to the high-end equipment industry with high system integration, strong industry drive and huge development opportunity, is vital to guarantee the safety of national defense strategy and promote national economic construction, and is also an important means for promoting adjustment and upgrade of industrial structure in China, promoting development of high-end manufacturing industry and promoting comprehensive national strength.
In various aviation manufacturing industries, the processing of aviation parts is an extremely important stage, in the processing process, a substitute processing part is usually stored in a blank material warehouse, most of blank material warehouses are short of a structure for automatically replacing a full-load tray and an empty-load tray in the material taking process of workers, the workers often need to manually replace the blank material warehouses, the operation is complex, and the working efficiency is reduced.
SUMMERY OF THE UTILITY MODEL
The utility model aims to solve the defects in the prior art and provides a blank warehouse for machining aviation parts.
In order to achieve the purpose, the utility model adopts the following technical scheme: the utility model provides a stock storehouse for aviation spare part processing, includes box, drive assembly and storage box, the inner wall symmetry fixed mounting of box has last chassis and lower chassis, the even fixed mounting in surface of drive assembly has the storage box.
Preferably, the driving assembly comprises a driving motor and a rotating rod, the driving motor is fixedly mounted on the upper surface of the box body, the rotating rod is fixedly mounted on the driving motor, and the storage box is fixedly mounted on the outer surface of the rotating rod.
Preferably, the bottom surface symmetry of storage box has seted up the through-hole, and the inner wall of through-hole is pegged graft and is equipped with the lifter, the upper end of lifter is equipped with the bearing plate admittedly.
Preferably, the lifting rod is far away from one end fixed mounting of bearing plate has the disc, is located between disc and the storage box the surface cover of lifting rod is equipped with spring a.
Preferably, the lower fixed surface of storage box installs the sleeve, the connecting hole has been seted up to the one end that the storage box was kept away from to the sleeve, the lower fixed surface of bearing plate installs the down tube, the down tube is inserted and is established in telescopic inside, the inner wall sliding connection of connecting hole has the inserted bar, the inserted bar is close to telescopic one end fixed mounting and has the sloping block.
Preferably, the upper surface of the lower chassis is provided with a ring-shaped groove, the inner wall of the ring-shaped groove is provided with a jack, the inner wall of the jack is connected with an extrusion block in a sliding manner, and a spring b is fixedly arranged between the extrusion block and the inner wall of the jack.
Compared with the prior art, the utility model has the advantages and positive effects that:
in the utility model, when a worker uses the blank warehouse and the material storage box is filled with the substitute workpieces, the bearing plate can be acted by the gravity of the substitute workpieces and has a downward movement trend, then the worker opens the driving motor which can drive the rotating rod to rotate, the material storage box can drive the inclined rod to move together, the sleeve can move along the inner wall of the annular groove along with the material storage box, when the sleeve rotates for a certain position, the bearing plate can press the lifting rod and the inclined rod to move downwards, the lifting rod can drive the disc to move downwards while moving downwards, the spring a is stretched, the inclined rod can extrude the inclined block when moving downwards, the inclined block can eject the inserted rod out of the connecting hole and insert the inserted rod into the inserted hole, the whole rotating rod can be clamped and stops rotating, when the inserted rod is inserted into the inserted hole, the extruding block can be acted by the inserted rod, can be to jack internal motion, and compression spring b, when the staff took the machined part of taking the place in with the storage box and got rid of, spring a and spring b can kick-back simultaneously this moment, the bearing plate can be taken back to the normal position, the inserted bar can be withdrawed in the connecting hole, the bull stick can continue to rotate immediately, rotate next full-load storage box to the staff in front, continue to process, must mutually support between each part, can realize the automatic change of full-load dish and empty-load dish, the work efficiency of whole course of working has been improved.
Drawings
FIG. 1 is a schematic perspective view of a blank warehouse for machining aviation parts according to the present invention;
FIG. 2 is an exploded view of a blank library for aerospace part processing according to the present invention;
fig. 3 is an enlarged view of a blank library for machining aviation parts in fig. 2.
Illustration of the drawings:
1. a box body; 2. an upper chassis; 3. a lower chassis; 4. a storage box; 5. a drive motor; 6. a rotating rod; 7. a lifting rod; 8. a pressure bearing plate; 9. a disc; 10. a spring a; 11. a sleeve; 12. connecting holes; 13. a diagonal bar; 14. inserting a rod; 15. a tapered block; 16. an annular groove; 17. a jack; 18. extruding the block; 19. and a spring b.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more apparent, the present invention is described in further detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the utility model and are not intended to limit the utility model.
In the description of the present invention, it is to be understood that the terms "length", "width", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", and the like, indicate orientations or positional relationships based on the orientations or positional relationships illustrated in the drawings, and are used merely for convenience in describing the present invention and for simplicity in description, and do not indicate or imply that the devices or elements referred to must have a particular orientation, be constructed in a particular orientation, and be operated, and thus, are not to be construed as limiting the present invention. Further, in the description of the present invention, "a plurality" means two or more unless specifically defined otherwise.
Referring to fig. 1-3, the present invention provides a technical solution: the utility model provides a stock storehouse for aviation spare part processing, includes box 1, drive assembly and storage box 4, and the inner wall symmetry fixed mounting of box 1 has last chassis 2 and lower chassis 3, and the even fixed mounting in surface of drive assembly has storage box 4.
In this embodiment: the storage box 4 is driven to rotate through the driving assembly, so that automatic replacement between the full-load storage box 4 and the no-load storage box 4 can be realized, and the material taking of workers is facilitated.
Specifically, drive assembly includes driving motor 5 and bull stick 6, and driving motor 5 is equipped with admittedly to the upper surface of box 1, and driving motor 5 fixed mounting has bull stick 6, and storage box 4 fixed mounting is at the surface of bull stick 6.
In this embodiment: the drive assembly can ensure automatic exchange between a full magazine 4 and an empty magazine 4.
Specifically, the bottom surface symmetry of storage box 4 has seted up the through-hole, and the inner wall of through-hole is pegged graft and is equipped with lifter 7, and the upper end of lifter 7 is equipped with bearing plate 8 admittedly.
In this embodiment: the lifting rod 7 and the bearing plate 8 can be mutually matched, so that the bearing plate 8 can stably move in the storage box 4.
Specifically, a disc 9 is fixedly mounted at one end of the lifting rod 7 far away from the bearing plate 8, and a spring a10 is sleeved on the outer surface of the lifting rod 7 between the disc 9 and the storage box 4.
In this embodiment: the outer surface of the lifting rod 7 is sleeved with a spring a10, so that the bearing plate 8 can be automatically lifted.
Specifically, the lower fixed surface of storage box 4 installs sleeve 11, and connecting hole 12 has been seted up to the one end that storage box 4 was kept away from to sleeve 11, and the lower fixed surface of bearing plate 8 installs down tube 13, and down tube 13 inserts and establishes the inside of sleeve 11, and the inner wall sliding connection of connecting hole 12 has inserted bar 14, and inserted bar 14 is close to the one end fixed mounting of sleeve 11 and has oblique piece 15.
In this embodiment: the inclined rod 13 moves downward along with the bearing plate 8 and presses the inclined block 15, and the inclined block 15 carries the insert rod 14 to move in the connecting hole 12 when being pressed.
Specifically, the upper surface of the lower chassis 3 is provided with an annular groove 16, the inner wall of the annular groove 16 is provided with a jack 17, the inner wall of the jack 17 is connected with a squeezing block 18 in a sliding manner, and a spring b19 is fixedly arranged between the squeezing block 18 and the inner wall of the jack 17.
In this embodiment: when the sleeve 11 rotates to a certain position, the inserted link 14 can directly extend out of the connecting hole 12 and be inserted into the inserting hole 17, so that the sleeve 11 is clamped, the material taking by workers is facilitated, the extrusion block 18 and the spring b19 can be matched with the lifting rod 7 and the spring a10, and the inserted link 14 and the inclined block 15 are reset.
The working principle is as follows: when the blank warehouse is used by a worker, when the storage box 4 is filled with the substitute workpieces, the bearing plate 8 is subjected to the action of gravity of the substitute workpieces and tends to move downwards, then the worker opens the driving motor 5, the driving motor 5 drives the rotating rod 6 to rotate, the storage box 4 drives the inclined rod 13 to move together, the sleeve 11 moves along the inner wall of the annular groove 16 along with the storage box 4, when the storage box rotates for a certain position, the bearing plate 8 presses the lifting rod 7 and the inclined rod 13 to move downwards, the lifting rod 7 drives the disc 9 to move downwards while moving downwards, the spring a10 is stretched, when the inclined rod 13 moves downwards, the inclined block 15 is extruded, the inserting rod 14 is ejected out of the connecting hole 12 by the inclined block 15 and enters the inserting hole 17, the whole rotating rod 6 is clamped and stops rotating, when the inserted link 14 is inserted into the insertion hole 17, the extrusion block 18 is extruded by the inserted link 14 and moves towards the inside of the insertion hole 17, and compresses the spring b19, when the worker finishes removing the substitute workpiece in the magazine 4, the spring a10 and the spring b19 rebound at the same time, the bearing plate 8 is brought back to the original position, the inserted link 14 is retracted into the connection hole 12, and then the rotating rod 6 continues to rotate, so that the next full-load magazine 4 is rotated to the front of the worker for further processing.
Although the present invention has been described with reference to specific embodiments, it will be understood by those skilled in the art that various changes and modifications may be made without departing from the spirit and scope of the utility model.
Claims (6)
1. The utility model provides a blank storehouse for aviation spare part processing, includes box (1), drive assembly and storage case (4), its characterized in that: the inner wall symmetry fixed mounting of box (1) has last chassis (2) and lower chassis (3), drive assembly's the even fixed mounting in surface has storage box (4).
2. The blank warehouse for the aviation part processing according to claim 1, wherein: the driving assembly comprises a driving motor (5) and a rotating rod (6), the driving motor (5) is fixedly mounted on the upper surface of the box body (1), the rotating rod (6) is fixedly mounted on the driving motor (5), and the storage box (4) is fixedly mounted on the outer surface of the rotating rod (6).
3. The blank warehouse for the aviation part processing according to claim 1, wherein: the bottom surface symmetry of storage box (4) has seted up the through-hole, and the inner wall of through-hole is pegged graft and is equipped with lifter (7), bearing plate (8) are adorned admittedly to the upper end of lifter (7).
4. The blank warehouse for the aviation part processing according to claim 3, wherein: one end fixed mounting that pressure-bearing plate (8) was kept away from in lifter (7) has disc (9), is located between disc (9) and storage box (4) the surface cover of lifter (7) is equipped with spring a (10).
5. The blank warehouse for the aviation part processing according to claim 3, wherein: the lower fixed surface of storage box (4) installs sleeve (11), connecting hole (12) have been seted up to the one end that storage box (4) were kept away from in sleeve (11), the lower fixed surface of bearing plate (8) installs down tube (13), inside at sleeve (11) is inserted in down tube (13), the inner wall sliding connection of connecting hole (12) has inserted bar (14), the one end fixed mounting that inserted bar (14) are close to sleeve (11) has sloping block (15).
6. The blank warehouse for the aviation part processing according to claim 1, wherein: the upper surface of the lower chassis (3) is provided with a ring-shaped groove (16), the inner wall of the ring-shaped groove (16) is provided with a jack (17), the inner wall of the jack (17) is connected with an extrusion block (18) in a sliding mode, and a spring b (19) is fixedly installed between the extrusion block (18) and the inner wall of the jack (17).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202121275217.5U CN215317329U (en) | 2021-06-08 | 2021-06-08 | Blank warehouse for machining aviation parts |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202121275217.5U CN215317329U (en) | 2021-06-08 | 2021-06-08 | Blank warehouse for machining aviation parts |
Publications (1)
Publication Number | Publication Date |
---|---|
CN215317329U true CN215317329U (en) | 2021-12-28 |
Family
ID=79556312
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202121275217.5U Expired - Fee Related CN215317329U (en) | 2021-06-08 | 2021-06-08 | Blank warehouse for machining aviation parts |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN215317329U (en) |
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2021
- 2021-06-08 CN CN202121275217.5U patent/CN215317329U/en not_active Expired - Fee Related
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Legal Events
Date | Code | Title | Description |
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GR01 | Patent grant | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20211228 |