CN114134633A

CN114134633A - Braiding machine runway module and novel braiding machine runway plate

Info

Publication number: CN114134633A
Application number: CN202111498477.3A
Authority: CN
Inventors: 于增伟
Original assignee: Jiangsu Xiangdao Precision Machinery Co ltd
Current assignee: Jiangsu Xiangdao Precision Machinery Co ltd
Priority date: 2021-12-09
Filing date: 2021-12-09
Publication date: 2022-03-04
Anticipated expiration: 2041-12-09
Also published as: CN114134633B

Abstract

The invention discloses a braiding machine runway module, which comprises an inner ring, wherein fan-shaped notches are formed in two symmetrical sides of the inner ring, groove blocks are clamped in the notches on the two sides, X-shaped grooves are formed in the groove blocks, first outer ring bodies are clamped at two ends of each groove block, a second outer ring body is clamped between the first outer ring bodies on one side, a third outer ring body is clamped between the first outer ring bodies on the other side, the length of the third outer ring body is smaller than that of the second outer ring body, outer runway grooves are formed between the second outer ring body and the first outer ring bodies and the inner ring on the two sides of the second outer ring body, inner runway grooves are formed between the third outer ring body and the first outer ring bodies and the inner ring on the two sides of the second outer ring body, and the outer runway grooves are communicated with the inner runway grooves through the X-shaped grooves on the groove blocks. The maintenance is convenient and efficient, if part of accessories are abraded in the long-term use process, only corresponding modules need to be replaced, and the maintenance is simple and convenient.

Description

Braiding machine runway module and novel braiding machine runway plate

Technical Field

The invention relates to the technical field of braiding machines, in particular to a braiding machine runway module and a novel braiding machine runway plate.

Background

The traditional braiding machine runway panel has long production process period, complex manufacturing process and short service life, only a whole runway plate can be replaced during maintenance, the runway plate cannot be repaired, and the cost is increased. And the traditional casting molding process of the ductile cast iron model is adopted for the runway panel of the traditional braiding machine, so that the energy consumption is large, the deformation quantity of the product is large, the qualification rate is low, and the product can generate dust in the machining process and has influence on the environment and the health of operators.

Disclosure of Invention

Aiming at the defects of the prior art, the invention provides a braiding machine runway module and a novel braiding machine runway plate, which aim to solve the problem that only a whole runway plate can be replaced when the prior runway panel is maintained.

In order to solve the technical problems, the invention provides the following technical scheme:

the utility model provides a braider runway module, including the inner ring, the symmetrical both sides of inner ring have been seted up and have been fan-shaped breach, equal joint has the groove piece in the breach of both sides, seted up X type groove on the groove piece, the both ends joint of groove piece has outer ring body one, the joint has outer ring body two between two outer ring body one of one side, the joint has outer ring body three between two outer ring body one of opposite side, the length of outer ring body three is less than the length of outer ring body two, form outer runway groove between outer ring body two and the outer ring body one and the inner ring of its both sides, form interior runway groove between outer ring body three and the outer ring body one and the inner ring of its both sides, outer runway groove is through X type groove and interior runway groove intercommunication on the groove piece.

Preferably, the groove block is in a cake shape, and first clamping grooves (31) are formed in the two ends, located on the X-shaped groove, of the groove block; the first outer ring body is Y-shaped, a first clamping block is arranged at one end, spliced with the groove block, of the first outer ring body, the first clamping block is clamped in the first clamping groove, and a second clamping block and a second clamping groove are respectively arranged at the other two ends of the first outer ring body; the outer ring body II is arc-shaped, one end of the outer ring body II is provided with a third clamping block matched with the second clamping groove, and the other end of the outer ring body II is provided with a third clamping groove matched with the second clamping block; and a fourth clamping block matched with the second clamping groove is arranged at one end of the outer ring body III, and a fourth clamping groove matched with the second clamping block is arranged at the other end of the outer ring body III.

Above-mentioned technical scheme adopts the butt joint mode of fixture block and draw-in groove between every accessory, reaches seamless butt joint, and whole precision can reach within 0.05 mm.

Preferably, the center of the inner ring is connected with an oil cup for preventing oil from splashing.

According to the technical scheme, the splash-proof oil cup can block gear splash lubricating oil which runs at a high speed in the original gear box, and the problem of oil injection of the original gear which runs at a high speed is solved.

Preferably, the inner ring, the groove block, the first outer ring body, the second outer ring body and the third outer ring body are all provided with screw holes.

Above-mentioned technical scheme, above-mentioned each accessory accessible bolted connection has improved stability when being convenient for install on the panel.

Preferably, the material is formed by pressing and sintering through a powder metallurgy die.

According to the technical scheme, the friction reducing performance of the powder metallurgy material is utilized, oil-free self-lubrication of the runway is achieved, the wear resistance is multiple times that of the original ductile iron panel, the original panel is kept for five years, and the original panel is kept for ten years.

The invention also provides a novel runway plate of the braiding machine, which comprises a panel, wherein a plurality of runway modules are connected with the panel end to form a runway.

Compared with the prior art, the invention has the following beneficial effects:

1. the raw materials are saved by more than 40 percent compared with the traditional panel.

2. The use performance is improved, the standardized powder metallurgy die press forming process is adopted for production, the friction reducing performance of the powder metallurgy material is utilized, the panel track is free of oil and self-lubricating, the wear resistance is multiple times of that of the original ductile iron panel, the original panel is kept for five years, and the existing panel is kept for ten years.

3. The precision is high, and the full accessory adopts the insert to assemble, connects through the mode of joint between every accessory, reaches seamless butt joint, and whole precision can reach within 0.05.

4. The maintenance is convenient and efficient, if part of accessories are abraded in the long-term use process, only corresponding modules need to be replaced, and the maintenance is simple and convenient.

5. The running noise is reduced, and the friction coefficient is reduced due to the adoption of the powder metallurgy material, so that the whole load of the machine is reduced, and the noise can be controlled to the advanced level of the same domestic company.

6. The anti-splashing oil cup is arranged, so that gear splashing lubricating oil which runs at a high speed in the original gear box can be blocked, and the problem of oil spraying of the original gear which runs at a high speed is solved.

Drawings

FIG. 1 is a schematic structural view of the present invention;

FIG. 2 is a schematic structural view of an inner ring;

FIG. 3 is a schematic structural view of a slot block;

FIG. 4 is a schematic structural diagram of the outer ring body I;

FIG. 5 is a schematic structural view of the outer ring body II;

FIG. 6 is a schematic structural view of the outer ring body III;

FIG. 7 is a schematic structural view of an anti-splash oil cup;

fig. 8 is a schematic structural view of a first embodiment of a runway panel of a knitting machine;

fig. 9 is a schematic structural view of a second embodiment of a runway panel for a knitting machine;

in the figure: 1-inner ring, 2-notch, 3-groove block, 31-first groove, 4-first outer ring body, 41-first block, 42-second block, 43-second groove, 5-second outer ring body, 51-third block, 52-third groove, 6-third outer ring body, 61-fourth block, 62-fourth groove, 7-anti-splash oil cup and 8-panel.

Detailed Description

The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.

Referring to fig. 1, a braiding machine runway module is pressed by a powder metallurgy die and sintered and formed, and includes an inner ring 1, two symmetrical sides of the inner ring 1 are provided with fan-shaped notches 2, notches 2 on two sides are respectively clamped with a groove block 3, the groove block 3 is provided with an X-shaped groove, two ends of the groove block 3 are clamped with outer ring bodies one 4, an outer ring body two 5 is clamped between the two outer ring bodies one 4 on one side, an outer ring body three 6 is clamped between the two outer ring bodies one 4 on the other side, the length of the outer ring body three 6 is smaller than that of the outer ring body two 5, an outer runway groove is formed between the outer ring body two 5 and the outer ring bodies one 4 on two sides thereof and the inner ring 1, an inner runway groove is formed between the outer ring body three 6 and the outer ring bodies one 4 on two sides thereof and the inner ring 1, and the outer runway groove is communicated with the inner runway groove through the X-shaped groove on the groove block 3.

Referring to fig. 2-5, the groove block 3 is shaped like a cake, and first locking grooves 31 are formed at two ends of the X-shaped groove on the groove block 3. The outer ring body I4 is Y-shaped, a first clamping block 41 is arranged at one end, spliced with the groove block 3, of the outer ring body I4, the first clamping block 41 is clamped in the first clamping groove 31, and a second clamping block 42 and a second clamping groove 43 are respectively arranged at the other two ends of the outer ring body I4. The second outer ring body 5 is arc-shaped, one end of the second outer ring body is provided with a third clamping block 51 matched with the second clamping groove 43, and the other end of the second outer ring body is provided with a third clamping groove 52 matched with the second clamping block 42. One end of the outer ring body three 6 is provided with a fourth block 61 matched with the second block 43, and the other end is provided with a fourth block 62 matched with the second block 42. Adopt the butt joint mode of fixture block and draw-in groove between every accessory, reach seamless butt joint, whole precision can reach within 0.05 mm.

Referring to fig. 6, the center of the inner ring 1 is connected with an oil cup 7. The anti-splashing oil cup 7 can block the gear which runs at high speed in the original gear box from splashing lubricating oil, and the problem of oil spraying of the original gear which runs at high speed is solved.

Referring to fig. 7, a novel runway plate of a braiding machine comprises a panel 8, wherein a plurality of runway modules are connected with the panel 8 end to end, screw holes are formed in an inner ring 1, a groove block 3, an outer ring body I4, an outer ring body II 5 and an outer ring body III 6, and all accessories are fixed with the panel through bolts to form a runway.

The runway panel shown in fig. 8 is a 32-ingot runway, the runway panel shown in fig. 9 is a 16-ingot runway, and when the number of ingots in the runway module on the panel 8 is different, the diameter of the whole runway changes along with the change of the number of the ingots; but the diameter of each runway module will also vary. Therefore, according to the difference of the number of ingots, the two outer ring bodies 5 or the three outer ring bodies 6 can be abandoned on the basis of the runway module, as shown in fig. 9, the three outer ring bodies 6 are abandoned, the two outer ring bodies 5 are remained, and the runway module is formed by connecting the adjacent one outer ring body 4 on one side. The two parts can be abandoned at the same time, the length of the outer ring bodies one 4 at two sides is prolonged, and the adjacent outer ring bodies one 4 at two sides are connected to form the runway module.

In conclusion, the parts of the invention adopt a novel processing technology of powder metallurgy die pressing and sintering molding, have high dimensional precision and are suitable for mass production. The powder metallurgy material is an alloy material, is wear-resistant and low in noise, and contains a large amount of self-lubricating oil inside after being treated by a special process. The modularized design can adapt to the use of various models, the commonality is strong, and original runway board technology is that a model corresponds a runway board. The special design scheme avoids the problem that the table top is clean and has no oil stain in the high-speed and long-time production process of the machine. The modular design has low requirements on the operation skills of manufacturing staff and obviously reduces the production cost. When the module parts reach the service life, the whole runway panel does not need to be replaced, and the module parts are worn and worn, so that the corresponding modules are replaced, the maintenance period is short, and the maintenance cost is low.

It is to be noted that the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. Without further limitation, an element defined by the phrase "comprising an … …" does not exclude the presence of other identical elements in a process, method, article, or apparatus that comprises the element.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims

1. A braiding machine runway module is characterized by comprising an inner ring (1), wherein two symmetrical sides of the inner ring (1) are provided with fan-shaped notches (2), notches (2) on the two sides are respectively clamped with a groove block (3), the groove block (3) is provided with an X-shaped groove, two ends of the groove block (3) are respectively clamped with an outer ring body I (4), wherein the joint has outer ring body two (5) between two outer ring body one (4) of one side, the joint has outer ring body three (6) between two outer ring body one (4) of opposite side, the length of outer ring body three (6) is less than the length of outer ring body two (5), form outer runway groove between outer ring body two (5) and the outer ring body one (4) and the inner ring (1) of its both sides, form interior runway groove between outer ring body three (6) and the outer ring body one (4) and the inner ring (1) of its both sides, outer runway groove passes through X type groove on groove block (3) and interior runway groove intercommunication.

2. The braiding machine runway module of claim 1, wherein: the groove block (3) is in a cake shape, and first clamping grooves (31) are formed in the two ends, located on the X-shaped groove, of the groove block (3).

3. The braiding machine runway module of claim 2, wherein: the outer ring body I (4) is Y-shaped, a first clamping block (41) is arranged at one end, spliced with the groove block (3), of the outer ring body I (4), the first clamping block (41) is clamped in the first clamping groove (31), and a second clamping block (42) and a second clamping groove (43) are arranged at the other two ends of the outer ring body I (4) respectively.

4. The braiding machine runway module of claim 3, wherein: the second outer ring body (5) is arc-shaped, one end of the second outer ring body is provided with a third clamping block (51) matched with the second clamping groove (43), and the other end of the second outer ring body is provided with a third clamping groove (52) matched with the second clamping block (42).

5. The braiding machine runway module of claim 4, wherein: and one end of the outer ring III (6) is provided with a fourth clamping block (61) matched with the second clamping groove (43), and the other end of the outer ring III is provided with a fourth clamping groove (62) matched with the second clamping block (42).

6. The braiding machine runway module of claim 5, wherein: the center of the inner ring (1) is connected with an anti-splash oil cup (7).

7. The braiding machine runway module of any of claims 1-6, characterized in that: screw holes are formed in the inner ring (1), the groove block (3), the outer ring I (4), the outer ring II (5) and the outer ring III (6).

8. The braiding machine runway module of claim 7, wherein: the material is pressed by a powder metallurgy die and sintered to form the material.

9. The utility model provides a novel braider runway board which characterized in that: comprises a panel (8), and a plurality of runway modules are connected end to end on the panel (8) to form a runway.