A deformation-preventing pretreatment fixing structure before cold drawing of titanium edge material

Abstract

The utility model discloses a kind of titanium edge material before cold drawing of deformation-preventing pretreatment fixing structure, it is related to titanium edge material cold drawing processing technical field, including first fixed plate component and combination column component, the top surface of first fixed plate component is equipped with equidistance arrangement installation and is equipped with stable frame component, the combination column component is vertically installed in four diagonal places of first fixed plate component and second fixed plate component.The titanium edge material before cold drawing of deformation-preventing pretreatment fixing structure, by setting up installation and being equipped with combination column component in four diagonal places of first fixed plate component, structure setting of simultaneously cooperation second fixed plate component can be flexibly combined according to use needs, and intercalation is carried out between each other, while using the structure setting of stable frame component, to this can cooperate with the length specification of material and carry out adaptive adjustment, and good structural stability and firmness are guaranteed, to reduce unnecessary structural deformation of material in pretreatment process as far as possible.

Description

Technical Field

[0001] This utility model relates to the field of cold drawing processing technology for titanium edge materials, specifically a deformation-pre-treatment fixing structure for titanium edge materials before cold drawing. Background Technology

[0002] Cold drawing of titanium scrap is a metalworking process that uses tensile force to force titanium material through a die orifice, primarily used for producing titanium alloy bars and wires. This process is characterized by dimensional precision and a smooth surface finish, and is widely used in aerospace, energy, and other fields.

[0003] Conventional pretreatment fixing structures are limited by structural constraints, which restrict the amount of material that can be fixed and make it difficult to achieve structural expansion and combination. Utility Model Content

[0004] The purpose of this invention is to provide a deformation-prevention and fixing structure for titanium edge material before cold drawing, so as to solve the problems mentioned in the background art.

[0005] To achieve the above objectives, this utility model provides the following technical solution: a deformation-prevention fixing structure for titanium edge material before cold drawing, comprising a first fixing plate component and a combined column component. The top surface of the first fixing plate component is equipped with equidistantly arranged stable structural members, and a second fixing plate component is provided directly below the first fixing plate component. The combined column component is vertically installed at the four opposite corners of the first fixing plate component and the second fixing plate component. The combined column component includes a combined base, a first splicing rod, and a second splicing rod. The upper end of the combined base is vertically connected to the first splicing rod, and the bottom of the combined base is vertically connected to the second splicing rod.

[0006] Furthermore, the first fixing plate component includes a support plate body, a combination hole, and an assembly hole. The support plate body has a combination hole at each of its four opposite corners, and an assembly hole is provided on the middle surface of the support plate body.

[0007] Furthermore, the assembly holes are arranged in an equidistant array on the middle surface of the support plate body, and the second fixing plate component and the first fixing plate component adopt the same structural arrangement.

[0008] Furthermore, the stabilizing structure includes a stabilizing sleeve, a support rod, a fixing sleeve, and a connecting sleeve. The stabilizing sleeve is vertically connected to both sides, and the lower end of the support rod is connected to the fixing sleeve. The bottom of the fixing sleeve is provided with a connecting sleeve.

[0009] Furthermore, the connecting sleeve and the assembly hole are threaded together, and the connecting sleeve and the fixing sleeve are integrally formed.

[0010] Furthermore, the stabilizing sleeve, the fixing sleeve, and the connecting sleeve are all located on the same vertical central axis, and the stabilizing sleeve, the support rod, and the fixing sleeve are welded together.

[0011] Furthermore, the lower end of the combined hole and the combined seat are threaded together, and the first splicing rod and the second splicing rod adopt the same structural configuration.

[0012] Furthermore, the upper and lower ends of the first splicing rod are connected by a threaded structure, and the upper end of the first splicing rod is threadedly connected to the lower end of the combination seat, and the lower end of the first splicing rod is threadedly connected to the upper end of the combination seat.

[0013] This utility model provides a deformation-pre-treatment and fixing structure for titanium edge material before cold drawing, which has the following beneficial effects:

[0014] 1. This utility model, by setting up a first fixed plate component and a second fixed plate component with identical structures, and using them in conjunction with a combined column component, wherein the first splicing rod and the second splicing rod have identical structures, and the two can be spliced ​​together end to end by structural screwing, and can also be combined with a combined base by screwing. The combined base itself can be structurally screwed using the lower structure and the combined hole, thereby realizing the rapid splicing and combination of the first fixed plate component, the second fixed plate component and the combined column component. Using the above structure, an appropriate number of combined column components can be structurally spliced ​​and combined according to the length of the material, and the first fixed plate component and the second fixed plate component are connected to the two ends of the combined column component after assembly, so as to facilitate the vertical placement of the material between the first fixed plate component and the second fixed plate component, thereby ensuring the stability and structural safety of the material itself, and minimizing unnecessary structural deformation problems of the material itself during the pre-processing process.

[0015] 2. This utility model features a stabilizing frame component installed on the surface of either the first or second fixed plate component. The entire stabilizing frame component can be structurally connected to the assembly hole by screwing the connecting sleeve at the bottom of the fixed sleeve. This structural arrangement provides a certain degree of structural support for the material between the first and second fixed plate components, thereby ensuring the structural stability of the material and ensuring effective pre-processing. At the same time, the structural arrangement between the first fixed plate component, the stabilizing frame component, and the second fixed plate component allows multiple materials to be arranged as needed to achieve good space utilization. Attached Figure Description

[0016] Figure 1 This is a schematic diagram of the main body of the anti-deformation pretreatment fixing structure for titanium edge material before cold drawing according to this utility model.

[0017] Figure 2 This is a schematic diagram of the first fixing plate component of the anti-deformation pretreatment fixing structure for titanium edge material before cold drawing according to this utility model.

[0018] Figure 3 This is a three-dimensional structural diagram of a stabilizing frame component for the anti-deformation pretreatment fixing structure before cold drawing of titanium edge material according to this utility model.

[0019] Figure 4 This is a three-dimensional structural diagram of a combined column component for a pre-treatment and fixing structure to prevent deformation of titanium edge material before cold drawing, according to this utility model.

[0020] In the figure: 1. First fixed plate component; 101. Support plate body; 102. Combination hole; 103. Assembly hole; 2. Stabilizing frame component; 201. Stabilizing sleeve; 202. Support rod; 203. Fixed sleeve; 204. Connecting sleeve; 3. Second fixed plate component; 4. Combination column component; 401. Combination seat; 402. First splicing rod; 403. Second splicing rod. Detailed Implementation

[0021] The embodiments of this utility model will be described in further detail below with reference to the accompanying drawings and examples. The following examples are for illustrative purposes only and should not be construed as limiting the scope of this utility model.

[0022] like Figures 1 to 4As shown, a deformation-prevention fixing structure for titanium edge material before cold drawing includes a first fixing plate component 1 and a combined column component 4. The top surface of the first fixing plate component 1 is equipped with equidistantly arranged stabilizing frame components 2, and a second fixing plate component 3 is positioned directly below the first fixing plate component 1. The combined column component 4 is vertically installed at the four diagonal points of the first fixing plate component 1 and the second fixing plate component 3. The combined column component 4 includes a combined base 401, a first splicing rod 402, and a second splicing rod 403. The upper end of the combined base 401 is vertically connected to the first splicing rod 402, and the bottom end of the combined base 401 is vertically connected to the second splicing rod 403. A threaded connection is formed between the combined hole 102 and the lower end of the combined base 401. The first splicing rod 402... 2. The first splicing rod 402 and the second splicing rod 403 adopt the same structural setting. The upper and lower ends of the first splicing rod 402 are connected by mutual threads. The upper end of the first splicing rod 402 is threadedly connected to the lower end of the combination seat 401, and the lower end of the first splicing rod 402 is threadedly connected to the upper end of the combination seat 401. The first splicing rod 402 and the second splicing rod 403 have the same structure. They can be spliced ​​together end to end by twisting the structure. They can also be combined with the combination seat 401 by twisting. The combination seat 401 itself can be twisted with the combination hole 102 by using the lower end structure, so as to realize the rapid splicing and combination of the first fixed plate component 1, the second fixed plate component 3 and the combination column component 4.

[0023] like Figures 1 to 4 As shown, the first fixing plate component 1 includes a support plate body 101, a combination hole 102, and an assembly hole 103. The support plate body 101 has combination holes 102 at each of its four diagonal corners, and an assembly hole 103 is provided on the middle surface of the support plate body 101. The assembly holes 103 are arranged in an equidistant array on the middle surface of the support plate body 101. The second fixing plate component 3 adopts the same structural arrangement as the first fixing plate component 1. The stabilizing frame component 2 includes a stabilizing sleeve 201, a support rod 202, a fixing sleeve 203, and a connecting sleeve 204. Support rods 202 are vertically connected to both sides of the stabilizing sleeve 201, and the lower end of the support rod 202 is connected to the fixing sleeve 203. The bottom of the fixed sleeve 203 is provided with a connecting sleeve 204. The connecting sleeve 204 and the assembly hole 103 are connected by threads, and the connecting sleeve 204 and the fixed sleeve 203 are integrated. The stabilizing sleeve 201, the fixed sleeve 203 and the connecting sleeve 204 are all on the same vertical central axis, and the stabilizing sleeve 201, the support rod 202 and the fixed sleeve 203 are connected by welding. The entire stabilizing structure 2 can be structurally connected to the assembly hole 103 by screwing the connecting sleeve 204 at the bottom of the fixed sleeve 203. With this structure, a certain degree of structural support can be provided for the material between the first fixed plate component 1 and the second fixed plate component 3.

[0024] In summary, as Figures 1 to 4 As shown, the anti-deformation pretreatment fixing structure for the titanium edge material before cold drawing is used by first selecting an appropriate number of first fixing plate components 1, stabilizing frame components 2, second fixing plate components 3 and combined column components 4 according to the number of bars. The stabilizing frame components 2 are fixed to the assembly hole 103 on the surface of the support plate body 101 by screwing through the connecting sleeve 204 at the bottom of the fixing sleeve 203.

[0025] Then, according to the length of the bar, the lower end of the combination seat 401 is fixed in the combination hole 102 by screwing. In this way, the combination seat 401 is combined and fixed with the first fixing plate component 1 and the second fixing plate component 3 respectively.

[0026] Simultaneously, select an appropriate number of first splicing rods 402 and second splicing rods 403 and assemble them by screwing. Then, screw the assembled first splicing rods 402 and second splicing rods 403 to the four diagonal combination seats 401 of the first fixed plate component 1 and the second fixed plate component 3 respectively, thereby realizing the structural combination between the first fixed plate component 1, the stable frame component 2, the second fixed plate component 3 and the combination column component 4. Then, insert the rod vertically into the interior of the stable frame component 2 to ensure the stability of the material.

[0027] The embodiments of this utility model are given for illustrative and descriptive purposes only, and are not intended to be exhaustive or to limit the utility model to the forms disclosed. Many modifications and variations will be apparent to those skilled in the art. The embodiments were chosen and described in order to better illustrate the principles and practical applications of this utility model, and to enable those skilled in the art to understand this utility model and design various embodiments with various modifications suitable for a particular purpose.

Claims

1. A deformation-prevention fixing structure for titanium edge material before cold drawing, comprising a first fixing plate component (1) and a combined column component (4), characterized in that: The top surface of the first fixed plate component (1) is equipped with equidistantly arranged stable structural components (2), and a second fixed plate component (3) is provided directly below the first fixed plate component (1). The combined column component (4) is vertically installed at the four opposite corners of the first fixed plate component (1) and the second fixed plate component (3). The combined column component (4) includes a combined base (401), a first splicing rod (402) and a second splicing rod (403). The upper end of the combined base (401) is vertically connected to the first splicing rod (402), and the bottom of the combined base (401) is vertically connected to the second splicing rod (403).

2. The anti-deformation pretreatment and fixing structure for titanium edge material before cold drawing according to claim 1, characterized in that, The first fixing plate component (1) includes a support plate body (101), a combination hole (102) and an assembly hole (103). The support plate body (101) has a combination hole (102) at each of the four opposite corners, and an assembly hole (103) is provided on the middle surface of the support plate body (101).

3. The anti-deformation pretreatment and fixing structure for titanium edge material before cold drawing according to claim 2, characterized in that, The assembly holes (103) are arranged in an equidistant array on the middle surface of the support plate body (101), and the second fixing plate component (3) and the first fixing plate component (1) adopt the same structural arrangement.

4. The anti-deformation pretreatment and fixing structure for titanium edge material before cold drawing according to claim 1, characterized in that, The stabilizing structure component (2) includes a stabilizing sleeve (201), a support rod (202), a fixing sleeve (203), and a connecting sleeve (204). The stabilizing sleeve (201) is vertically connected to both sides of the support rod (202), and the lower end of the support rod (202) is connected to the fixing sleeve (203). The bottom of the fixing sleeve (203) is provided with a connecting sleeve (204).

5. The anti-deformation pretreatment and fixing structure for titanium edge material before cold drawing according to claim 4, characterized in that, The connecting sleeve (204) and the assembly hole (103) are connected by threads, and the connecting sleeve (204) and the fixing sleeve (203) are integrally structured.

6. The anti-deformation pretreatment and fixing structure for titanium edge material before cold drawing according to claim 4, characterized in that, The stabilizing sleeve (201), the fixed sleeve (203), and the connecting sleeve (204) are all located on the same vertical central axis, and the stabilizing sleeve (201), the support rod (202), and the fixed sleeve (203) are welded together.

7. The anti-deformation pretreatment and fixing structure for titanium edge material before cold drawing according to claim 2, characterized in that, The lower ends of the combined hole (102) and the combined seat (401) are threaded together, and the first splicing rod (402) and the second splicing rod (403) adopt the same structural configuration.

8. The anti-deformation pretreatment and fixing structure for titanium edge material before cold drawing according to claim 7, characterized in that, The upper and lower ends of the first splicing rod (402) are connected by a threaded structure, and the upper end of the first splicing rod (402) is threaded to the lower end of the combination seat (401), and the lower end of the first splicing rod (402) is threaded to the upper end of the combination seat (401).

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