A method for winding fiber cloth into carbon fiber tubes

Abstract

This invention provides a method for winding fiber cloth into carbon fiber tubes. The method includes: arranging the fiber cloth into 4-6 groups according to the winding sequence; pre-laminating each group of fiber cloth to obtain a fiber composite layer; and then sequentially winding the 4-6 groups of fiber composite layers onto a carbon fiber tube mold core; the included angle between the winding start lines of adjacent groups of fiber composite layers is 30-90 degrees. This winding method ensures that the thickness of the fiber cloth obtained from winding is uniform throughout, resulting in carbon fiber tubes with satisfactory roundness, uniform thickness, and stable quality. It also improves work efficiency and is suitable for industrial production.

Description

Technical Field

[0001] This invention belongs to the technical field of carbon fiber tubes, and particularly relates to a method for winding carbon fiber tubes with fiber cloth. Background Technology

[0002] Carbon fiber refers to high-strength, high-modulus fibers with a carbon content of over 90%, possessing excellent high-temperature resistance. It is produced from acrylic and viscose fibers through high-temperature oxidation and carbonization, making it an excellent material for manufacturing high-tech equipment in aerospace and other applications. The main uses of carbon fiber are in the manufacture of advanced composite materials and in enhancing the properties of composites with resins, metals, ceramics, and carbon.

[0003] Carbon fiber robotic arms are the most widely used automated mechanical devices in the field of robotics. Although they vary in form, they all share a common characteristic: by receiving commands, they can precisely position themselves at a point in three-dimensional (or two-dimensional) space to perform tasks. Robotic arms generally have three types of movements: extension, rotation, and lifting. Rotation and lifting are accomplished by the horizontal arm and the column. The basic function of the arm is to move the gripper to the required position and to bear the maximum weight of the workpiece being grasped, as well as the weight of the arm itself. In addition, piping, cooling devices, stroke positioning devices, and automatic detection devices are generally also mounted on the arm. Therefore, the arm's structure, working range, load-bearing capacity, and motion accuracy directly affect the overall performance of the machine. Meanwhile, support arms made of carbon fiber have several advantages: lightweight, flexible and accurate operation, high strength, good temperature resistance, and cost-effectiveness.

[0004] Carbon fiber tubes are mainly used in carbon fiber robotic arms. CN113085217A discloses a method for preparing carbon fiber tubes, which includes the following steps: (1) pre-treating a carbon fiber pultruded plate; (2) sequentially laying a first prepreg and a carbon fiber pultruded plate on a mandrel, bonding the first prepreg and the carbon fiber pultruded plate together, and then sequentially laying a second prepreg and a release film; (3) then sequentially undergoing hot pressing, tube winding, mandrel removal, surface treatment, machining, and cleaning to obtain a carbon fiber tube. Tube winding involves sequentially winding carbon fiber cloth onto the surface of the mandrel after hot pressing in a predetermined order.

[0005] However, the above-mentioned tube winding method is mainly applicable to carbon fiber tubes with a single structure, and is not applicable to carbon fiber tubes with a composite structure. It is easy to cause the roundness and thickness of the carbon fiber tubes with a composite structure to be substandard, and the quality to be unstable.

[0006] Therefore, there is an urgent need to develop a method for winding fiber cloth into a composite structure carbon fiber tube. Summary of the Invention

[0007] The purpose of this invention is to provide a method for winding fiber cloth into carbon fiber tubes. The method optimizes the combination sequence of the fiber cloth and the angle relationship of the starting line of the winding process, effectively ensuring the uniformity of the fiber cloth thickness at all parts of the winding tube, and producing carbon fiber tubes with compliant roundness and uniform thickness.

[0008] To achieve this objective, the present invention employs the following technical solution:

[0009] This invention provides a method for winding fiber cloth into a carbon fiber tube. The method includes: arranging the fiber cloth in the order of winding and dividing it into 4-6 groups; pre-lamination of each group of fiber cloth to obtain a fiber composite layer; and then sequentially winding the 4-6 groups of fiber composite layers onto the carbon fiber tube mold core.

[0010] The included angle between the wrapping start lines of two adjacent fiber composite layers is 30-90 degrees, such as 30 degrees, 40 degrees, 50 degrees, 60 degrees, 70 degrees, 80 degrees or 90 degrees, but is not limited to the listed values. Other unlisted values ​​within this range are also applicable.

[0011] The fiber cloth winding method of the present invention first prepares the fiber cloth by laminating it to obtain 4-6 sets of fiber combination layers, and then controls the included angle between the winding start lines of two adjacent sets of fiber combination layers to be 30-90 degrees, which can ensure that the thickness of the fiber cloth obtained by winding is uniform and consistent, so that the roundness of the carbon fiber tube formed later meets the standard, the thickness is uniform, the quality is stable, and the work efficiency is also improved.

[0012] As a preferred technical solution of the present invention, the fiber cloth winding method is preferably as follows: the fiber cloth is sorted according to the winding sequence and divided into 5 groups, each group of fiber cloth is pre-stacked to obtain a fiber combination layer, and then the 5 groups of fiber combination layers are sequentially rolled onto the carbon fiber tube mold core.

[0013] Preferably, the included angles between the wrapping start lines of two adjacent sets of fiber composite layers are 40 degrees, 50 degrees, 90 degrees, 90 degrees, and 90 degrees, respectively.

[0014] The present invention preferably uses a 10-layer fiber cloth.

[0015] As a preferred embodiment of the present invention, the fiber cloth includes glass fiber cloth and / or carbon fiber cloth.

[0016] Preferably, the carbon fiber cloth includes PAN-based carbon fiber cloth and / or pitch-based carbon fiber cloth.

[0017] Preferably, the PAN-based carbon fiber cloth includes any one or a combination of at least two of PAN125, PAN250 or PAN0200. Typical but not limited examples of such combinations include: a combination of PAN125 and PAN250, a combination of PAN250 and PAN0200, or a combination of PAN125, PAN250 and PAN0200, etc.

[0018] Preferably, the pitch-based carbon fiber cloth includes model Pitch3.

[0019] Preferably, the fiberglass cloth is of type GF100.

[0020] As a preferred technical solution of the present invention, the thickness of the PAN-based carbon fiber cloth is 0.02-0.25mm, for example, it can be 0.02mm, 0.05mm, 0.07mm, 0.1mm, 0.15mm, 0.2mm or 0.25mm, etc., but it is not limited to the listed values. Other unlisted values ​​within the above range are also applicable.

[0021] Preferably, the thickness of the pitch-based carbon fiber cloth is 0.29-0.3 mm, for example, it can be 0.29 mm, 0.292 mm, 0.294 mm, 0.296 mm, 0.298 mm or 0.3 mm, but it is not limited to the listed values. Other unlisted values ​​within the above range are also applicable, with 0.292 mm being the preferred value.

[0022] Preferably, the pitch-based carbon fiber cloth is pentagonal, with one end having a width of 18-21mm, such as 18mm, 18.5mm, 19mm, 19.5mm, 20mm, 20.5mm or 21mm, and the other end having a width of 34-37mm, such as 34mm, 34.5mm, 35mm, 35.5mm, 36mm, 36.5mm or 37mm, and a length of 890-900mm, such as 890mm, 892mm, 894mm, 896mm, 898mm or 900mm, but is not limited to the listed values. Other unlisted values ​​within the above range are also applicable.

[0023] In this invention, the pentagon is formed by the three straight sides and the hypotenuse of a right trapezoid corresponding to two sides.

[0024] Preferably, the thickness of the GF100 is 0.05-0.15mm, for example, it can be 0.05mm, 0.07mm, 0.09mm, 0.1mm, 0.13mm or 0.15mm, etc., but it is not limited to the listed values. Other unlisted values ​​within the above range are also applicable, and 0.1mm is preferred.

[0025] Preferably, the GF100 is pentagonal, with one end having a width of 10-23mm, such as 10mm, 12mm, 14mm, 16mm, 18mm, 20mm, 21mm or 23mm, and the other end having a width of 27-38mm, such as 27mm, 30mm, 32mm, 34mm, 36mm or 38mm, and a length of 890-900mm, such as 890mm, 892mm, 894mm, 896mm, 898mm or 900mm, but is not limited to the listed values. Other unlisted values ​​within the above range are also applicable.

[0026] As a preferred embodiment of the present invention, the fiber composite layer comprises 1-3 layers of fiber cloth, preferably 2 layers.

[0027] As a preferred technical solution of the present invention, the pre-layering includes: firstly, stacking each group of the fiber cloth, and then ironing to obtain the fiber combination layer.

[0028] As a preferred technical solution of the present invention, the overlapping process involves reserving a gap between the corresponding long side positions of two adjacent fiber cloths in each group.

[0029] Preferably, the width of the interval is 4-6mm, for example, it can be 4mm, 4.4mm, 4.8mm, 5mm, 5.4mm, 5.8mm or 6mm, but it is not limited to the listed values. Other unlisted values ​​within the above range are also applicable, preferably 5mm.

[0030] Preferably, the ironing temperature is 50-60℃, such as 50℃, 52℃, 54℃, 56℃, 58℃ or 60℃, but it is not limited to the listed values. Other unlisted values ​​within the above range are also applicable.

[0031] As a preferred technical solution of the present invention, the structure of the carbon fiber tube core is that the two ends are straight tubes and the middle is a frustum-shaped tube.

[0032] As a preferred technical solution of the present invention, the diameter of one end of the straight tube is 3-4mm, for example, it can be 3mm, 3.2mm, 3.4mm, 3.6mm, 3.8mm or 4mm, etc., and the length is 4-8mm, for example, 4mm, 4.5mm, 5mm, 5.5mm, 6mm, 6.5mm, 7mm, 7.5mm or 8mm, etc., but it is not limited to the listed values. Other unlisted values ​​within the above range are also applicable.

[0033] Preferably, the diameter of the straight tube at the other end is 8-9 mm, for example, 8 mm, 8.2 mm, 8.4 mm, 8.6 mm, 8.8 mm or 9 mm, and the length is 200-240 mm, for example, 200 mm, 205 mm, 210 mm, 215 mm, 220 mm, 225 mm, 230 mm, 235 mm or 240 mm, but it is not limited to the listed values. Other unlisted values ​​within the above range are also applicable.

[0034] Preferably, the length of the frustum-shaped tube is 640-650mm, such as 640mm, 642mm, 644mm, 646mm, 648mm or 650mm, but it is not limited to the listed values. Other unlisted values ​​within the above range are also applicable.

[0035] As a preferred technical solution of the present invention, the rolling process includes: ironing the interval and the corresponding rolling start line with an iron.

[0036] In this invention, the mold core after the tube is rolled is cured and molded in sequence according to the existing technology, and then the mold core is removed to obtain a carbon fiber tube for semiconductors with satisfactory roundness and uniform thickness.

[0037] In this invention, the thickness of the fiber tube after removing the mold core is 1.4-1.5 mm.

[0038] The numerical range described in this invention includes not only the point values ​​listed above, but also any point values ​​within the numerical ranges not listed above. Due to space limitations and for the sake of brevity, this invention will not exhaustively list all the specific point values ​​included in the range.

[0039] Compared with the prior art, the present invention has the following beneficial effects:

[0040] The fiber cloth winding method provided by the present invention obtains 4-6 sets of fiber combination layers by pre-lamination of the fiber cloth, and then controls the included angle between the winding start lines of two adjacent sets of fiber combination layers to be 30-90 degrees, which can ensure that the thickness of the fiber cloth obtained by winding is uniform and consistent, so that the roundness of the subsequently formed carbon fiber tube meets the standard, the thickness dimension is uniform, the quality is stable, and the work efficiency is improved, making it suitable for industrial production. Attached Figure Description

[0041] Figure 1 This is a cross-sectional schematic diagram of the carbon fiber tube mold core used in Embodiment 1 of the present invention;

[0042] Figure 2 This is a schematic diagram showing the shape and dimensions of the first layer of fiber cloth used in Embodiment 1 of the present invention;

[0043] Figure 3This is a schematic diagram showing the shape and dimensions of the second layer of fiber cloth used in Embodiment 1 of the present invention;

[0044] Figure 4 This is a schematic diagram showing the shape and dimensions of the third layer of fiber cloth used in Embodiment 1 of the present invention;

[0045] Figure 5 This is a schematic diagram showing the shape and dimensions of the fourth layer of fiber cloth used in Embodiment 1 of the present invention;

[0046] Figure 6 This is a schematic diagram showing the shape and dimensions of the fifth layer of fiber cloth used in Embodiment 1 of the present invention;

[0047] Figure 7 This is a schematic diagram showing the shape and dimensions of the sixth layer of fiber cloth used in Embodiment 1 of the present invention;

[0048] Figure 8 This is a schematic diagram showing the shape and dimensions of the seventh layer of fiber cloth used in Embodiment 1 of the present invention;

[0049] Figure 9 This is a schematic diagram showing the shape and dimensions of the eighth layer of fiber cloth used in Embodiment 1 of the present invention;

[0050] Figure 10 This is a schematic diagram showing the shape and dimensions of the ninth layer of fiber cloth used in Embodiment 1 of the present invention;

[0051] Figure 11 This is a schematic diagram showing the shape and dimensions of the tenth layer of fiber cloth used in Embodiment 1 of the present invention;

[0052] Figure 12 This is a schematic diagram showing the positions of the wrapping start lines corresponding to the five fiber composite layers described in Embodiment 1 of the present invention;

[0053] Among them, 1-straight pipe; 2-frustum-shaped pipe; 3-straight pipe. Detailed Implementation

[0054] The technical solution of the present invention will be further illustrated below through specific embodiments. Those skilled in the art should understand that the embodiments described are merely illustrative of the present invention and should not be construed as limiting the invention in any way.

[0055] Example 1

[0056] This embodiment provides a method for winding carbon fiber tubes with fiber cloth. The structure of the carbon fiber tube mold core is that the two ends are straight tubes and the middle is a frustum-shaped tube; its structural schematic diagram is shown below. Figure 1 As shown; the carbon fiber tube core is an iron core, the diameter of the straight tube 3 at one end is 8.43mm and the length is 220mm; the diameter of the straight tube 1 at the other end is 3.46mm and the length is 6mm; the length of the frustum-shaped tube 2 is 644mm;

[0057] The fiber cloth has 10 layers, as detailed below:

[0058] The first layer is GF100 fiberglass cloth, 0.1mm thick, with a TAW of 149g / m². 2 The area is 0.0189m² 2 It weighs 2.82g, and its shape and dimensions are shown in the schematic diagram. Figure 2 As shown; the width (b1) at one end is 11.9 mm, the width (c1) at the other end is 27.5 mm, and the length (a) is 895 mm;

[0059] The second layer is PAN-based carbon fiber cloth of type PAN125, with a thickness of 0.125mm and a TAW of 188g / m. 2 The area is 0.0195m² 2 It weighs 3.67g, and its shape and dimensions are shown in the diagram below. Figure 3 As shown; the width (b2) at one end is 12.5mm, the width (c2) at the other end is 28.1mm, and the length (a) is 895mm;

[0060] The third layer is PAN-based carbon fiber cloth of model PAN0200, with a thickness of 0.02mm and a TAW of 36g / m. 2 The area is 0.0036m² 2 It weighs 0.13g, and its shape and dimensions are shown in the schematic diagram below. Figure 4 As shown; one is 13.3mm wide and 60mm long; the other is 28.9mm wide and 115mm long;

[0061] The fourth layer is PAN-based carbon fiber cloth of type PAN250, with a thickness of 0.25mm and a TAW of 373g / m. 2 The area is 0.0202m² 2 It weighs 7.53g, and its shape and dimensions are shown in the diagram below. Figure 5 As shown; the width (b4) at one end is 13.4 mm, the width (c4) at the other end is 29.0 mm, and the length (a) is 895 mm;

[0062] The fifth layer is PAN250 PAN-based carbon fiber cloth, 0.25mm thick, with a TAW of 373g / m². 2 The area is 0.0216m² 2 It weighs 8.06g, and its shape and dimensions are shown in the schematic diagram below. Figure 6 As shown; the width (b5) at one end is 15.0 mm, the width (c5) at the other end is 30.6 mm, and the length (a) is 895 mm;

[0063] The sixth layer is GF100 fiberglass cloth, 0.1mm thick, with a TAW of 149g / m². 2 The area is 0.023m² 2 It weighs 3.43g, and its shape and dimensions are shown in the diagram below. Figure 7 As shown; the width (b6) at one end is 16.6mm, the width (c6) at the other end is 32.2mm, and the length (a) is 895mm;

[0064] The seventh layer is PAN250 PAN-based carbon fiber cloth, 0.25mm thick, with a TAW of 373g / m². 2 The area is 0.0235m² 2 It weighs 8.77g, and its shape and dimensions are shown in the diagram below. Figure 8 As shown; the width (b7) at one end is 17.2mm, the width (c7) at the other end is 32.8mm, and the length (a) is 895mm;

[0065] The eighth layer is Pitch34 pitch-based carbon fiber cloth, 0.292mm thick, with a TAW of 500g / m. 2 The area is 0.0249m² 2 It weighs 12.45g, and its shape and dimensions are shown in the schematic diagram below. Figure 9 As shown; the width (b8) at one end is 18.8mm, the width (c8) at the other end is 34.4mm, and the length (a) is 895mm;

[0066] The ninth layer is a pitch-based carbon fiber cloth of type Pitch34, with a thickness of 0.292mm and a TAW of 500g / m. 2 The area is 0.0265m² 2 It weighs 13.25g, and its shape and dimensions are shown in the schematic diagram below. Figure 10 As shown; the width (b9) at one end is 20.6 mm, the width (c9) at the other end is 36.2 mm, and the length (a) is 895 mm;

[0067] The tenth layer is GF100 fiberglass cloth, 0.1mm thick, with a TAW of 149g / m². 2 The area is 0.0281m² 2 It weighs 4.19g, and its shape and dimensions are shown in the schematic diagram below. Figure 11 As shown; the width (b10) at one end is 22.4 mm, the width (c10) at the other end is 38.0 mm, and the length (a) is 895 mm;

[0068] The fiber composite layers are divided into groups of two layers according to their order.

[0069] Among them, the first layer and the second layer are the first group. The two layers of fiber cloth are stacked with the first layer on the bottom and the second layer on the top. A 5mm gap is reserved at the long side with a length of 895mm. Then, the fiber combination layer is ironed flat and pressed with an iron at 55℃ to obtain the first group of fiber combination layers.

[0070] The third and fourth layers are the second group. The third layer of fiber cloth is placed at both ends of the fourth layer of fiber cloth, with a 5mm gap reserved at the long side with a length of 1805mm. Then, it is ironed flat and pressed with an iron at 55℃ to obtain the second group of fiber combination layers.

[0071] The fifth and sixth layers are the third group. The two layers of fiber cloth are stacked with the fifth layer on the bottom and the sixth layer on the top. A 5mm gap is reserved at the long side with a length of 895mm. Then, the fiber combination layer is ironed flat and pressed with an iron at 55℃ to obtain the third group of fiber combination layers.

[0072] The seventh and eighth layers are the fourth group. The two layers of fiber cloth are stacked with the seventh layer on the bottom and the eighth layer on the top. A 5mm gap is reserved at the long side with a length of 895mm. Then, the fibers are ironed flat and pressed with an iron at 55℃ to obtain the fourth group of fiber combination layers.

[0073] The ninth and tenth layers are group 5. The two layers of fiber cloth are stacked with the ninth layer on the bottom and the tenth layer on the top. A 5mm gap is reserved at the long side with a length of 895mm. Then, the fiber combination layer is ironed flat and pressed with an iron at 55℃ to obtain the fifth group of fiber combination layers.

[0074] The five fiber composite layers described above are sequentially rolled onto a carbon fiber tube mold core coated with release agent. Taking the first fiber composite layer as an example, an iron is used to flatten and compact the spacing of the first fiber composite layer with the first rolling start line of the carbon fiber tube mold core. A fabric rolling machine is then used to roll the first fiber composite layer onto the carbon fiber tube mold core. Figure 12 As shown, the angle between the first group of fiber composite layers and the second group of fiber composite layers is 40 degrees; the angle between the second group of fiber composite layers and the third group of fiber composite layers is 50 degrees; the angle between the third group of fiber composite layers and the fourth group of fiber composite layers is 90 degrees; and the angle between the fourth group of fiber composite layers and the fifth group of fiber composite layers is 90 degrees. Furthermore, the five groups of fiber composite layers are rolled in the same direction, for example, all clockwise or all counterclockwise.

[0075] Using the fiber cloth winding method described in this embodiment, 10 layers of fiber cloth are completely rolled onto a carbon fiber tube mold core coated with a release agent. Then, the core is cured and molded sequentially according to existing technology, and the semiconductor carbon fiber tube with roundness, uniform thickness and a thickness of 1.4 mm can be obtained.

[0076] Example 2

[0077] This embodiment provides a method for winding a carbon fiber tube with fiber cloth. The fiber cloth has 10 layers. Except for adjusting the 5 sets of fiber combination layers to 4 sets of fiber combination layers, the other conditions are the same as in embodiment 1.

[0078] The adjustments are as follows: The third to fifth layers are grouped into the second group. The three layers of fiber cloth are stacked with the fourth layer at the bottom and the fifth layer at the top, with the third layer located at both ends of the fourth layer. A 5mm gap is reserved on the long side with a length of 895mm. Then, the fiber combination layer is ironed flat and pressed firmly with an iron at 55℃ to obtain the second group of fiber combination layers.

[0079] The sixth to eighth layers are grouped into the third group. The three layers of fiber cloth are stacked with the sixth layer at the bottom, the seventh layer in the middle, and the eighth layer on top. A 5mm gap is reserved on the long side with a length of 895mm. Then, the cloth is ironed flat and pressed with an iron at 55℃ to obtain the third group of fiber combination layers.

[0080] The four fiber composite layers described above are sequentially rolled onto a carbon fiber tube mold core coated with release agent. Taking the first fiber composite layer as an example, an iron is used to iron and press the spacing of the first fiber composite layer and the first rolling start line of the carbon fiber tube mold core. A fabric rolling machine is then used to roll the first fiber composite layer onto the carbon fiber tube mold core. The angle between the first rolling start line of the first fiber composite layer and the second rolling start line of the second fiber composite layer is 180 degrees. The angle between the second rolling start line of the second fiber composite layer and the third rolling start line of the third fiber composite layer is 90 degrees. The angle between the third rolling start line of the third fiber composite layer and the fourth rolling start line of the fourth fiber composite layer is 180 degrees.

[0081] Using the fiber cloth winding method described in this embodiment, 10 layers of fiber cloth are completely rolled onto a carbon fiber tube mold core coated with a release agent. Then, the process is carried out sequentially according to existing technology, followed by curing and molding, and then removing the mold core. The resulting carbon fiber tube for semiconductors has unstable quality and is prone to substandard roundness.

[0082] Example 3

[0083] This embodiment provides a method for winding a carbon fiber tube with fiber cloth. Except that the included angle between the winding start lines of two adjacent sets of fiber combination layers is 72 degrees, all other conditions are the same as in Embodiment 1.

[0084] Using the fiber cloth winding method described in this embodiment, 10 layers of fiber cloth are completely rolled onto a carbon fiber tube mold core coated with a release agent. Then, the process is carried out sequentially according to existing technology, followed by curing and molding, and then removing the mold core. The resulting carbon fiber tube for semiconductors has unstable quality and is prone to substandard roundness.

[0085] Example 4

[0086] This embodiment provides a method for winding a carbon fiber tube with fiber cloth. Except for the third layer, all other layers use PAN-based carbon fiber cloth of type PAN125, and other conditions are the same as in Embodiment 1.

[0087] Using the fiber cloth winding method described in this embodiment, 10 layers of fiber cloth are completely rolled onto a carbon fiber tube mold core coated with a release agent. Then, the process is carried out sequentially according to existing technology, followed by curing and molding, and then removing the mold core. The resulting carbon fiber tube for semiconductors has unstable quality and is prone to substandard roundness.

[0088] Example 5

[0089] This embodiment provides a method for winding a carbon fiber tube with fiber cloth. Except for the third layer, all other layers use GF100 glass fiber cloth, and all other conditions are the same as in Embodiment 1.

[0090] Using the fiber cloth winding method described in this embodiment, 10 layers of fiber cloth are completely rolled onto a carbon fiber tube mold core coated with a release agent. Then, the process is carried out sequentially according to existing technology, followed by curing and molding, and then removing the mold core. The resulting carbon fiber tube for semiconductors has unstable quality and is prone to substandard roundness.

[0091] Comparative Example 1

[0092] This comparative example provides a method for winding a carbon fiber tube with fiber cloth, in which 10 layers of fiber cloth are rolled one by one onto a carbon fiber tube core coated with a release agent.

[0093] Using the fiber cloth winding method described in this comparative example, 10 layers of fiber cloth are completely rolled onto the carbon fiber tube core coated with release agent. Then, the core is cured and molded in sequence according to the existing technology. The resulting carbon fiber tube for semiconductors has unstable quality and problems such as substandard roundness and uneven thickness have appeared.

[0094] The applicant declares that the detailed structural features of the present invention are illustrated through the above embodiments, but the present invention is not limited to the above detailed structural features, that is, it does not mean that the present invention must rely on the above detailed structural features to be implemented. Those skilled in the art should understand that any improvements to the present invention, equivalent substitutions for the components selected in the present invention, additions of auxiliary components, selection of specific methods, etc., all fall within the protection scope and disclosure scope of the present invention.

[0095] The preferred embodiments of the present invention have been described in detail above. However, the present invention is not limited to the specific details of the above embodiments. Within the scope of the technical concept of the present invention, various simple modifications can be made to the technical solution of the present invention, and these simple modifications all fall within the protection scope of the present invention.

[0096] It should also be noted that the various specific technical features described in the above specific embodiments can be combined in any suitable way without contradiction. In order to avoid unnecessary repetition, the present invention will not describe the various possible combinations separately.

[0097] Furthermore, various different embodiments of the present invention can be combined in any way, as long as they do not violate the spirit of the present invention, they should also be regarded as the content disclosed by the present invention.

Claims

1. A method for winding fiber cloth into a carbon fiber tube, characterized in that, The fiber cloth winding method includes: arranging 10 layers of fiber cloth in the order of winding and dividing them into 5 groups; each group of fiber cloth is pre-stacked to obtain a fiber combination layer; and then the 5 groups of fiber combination layers are sequentially rolled onto the carbon fiber tube mold core. The structure of the carbon fiber tube mold core is that the two ends are straight tubes and the middle is a frustum-shaped tube; The first layer is GF100 fiberglass cloth with a thickness of 0.1mm; the second layer is PAN125 PAN-based carbon fiber cloth with a thickness of 0.125mm; the third layer is PAN0200 PAN-based carbon fiber cloth with a thickness of 0.02mm; the fourth layer is PAN250 PAN-based carbon fiber cloth with a thickness of 0.25mm; the fifth layer is PAN250 PAN-based carbon fiber cloth with a thickness of 0.25mm; the sixth layer is GF100 fiberglass cloth with a thickness of 0.1mm; the seventh layer is PAN250 PAN-based carbon fiber cloth with a thickness of 0.25mm; the eighth layer is Pitch34 pitch-based carbon fiber cloth with a thickness of 0.292mm; the ninth layer is Pitch34 pitch-based carbon fiber cloth with a thickness of 0.292mm; and the tenth layer is GF100 fiberglass cloth with a thickness of 0.1mm. The first and second layers are the first group of fiber composite layers, with the first layer at the bottom and the second layer at the top; the third and fourth layers are the second group of fiber composite layers, with the third layer of fiber fabric located at both ends of the fourth layer of fiber fabric; the fifth and sixth layers are the third group of fiber composite layers, with the fifth layer at the bottom and the sixth layer at the top; the seventh and eighth layers are the fourth group of fiber composite layers, with the seventh layer at the bottom and the eighth layer at the top; the ninth and tenth layers are the fifth group of fiber composite layers, with the ninth layer at the bottom and the tenth layer at the top. The angle between the first group of fiber composite layers and the second group of fiber composite layers is 40 degrees; the angle between the second group of fiber composite layers and the third group of fiber composite layers is 50 degrees; the angle between the third group of fiber composite layers and the fourth group of fiber composite layers is 90 degrees; and the angle between the fourth group of fiber composite layers and the fifth group of fiber composite layers is 90 degrees. The five groups of fiber composite layers are rolled in the same direction.

2. The fiber cloth winding method according to claim 1, characterized in that, The pitch-based carbon fiber cloth of model Pitch34 is pentagonal, with a width of 18-21mm at one end and 34-37mm at the other end, and a length of 890-900mm.

3. The fiber cloth winding method according to claim 1, characterized in that, The fiberglass cloth of model GF100 is pentagonal, with a width of 10-23mm at one end, a width of 27-38mm at the other end, and a length of 890-900mm.

4. The fiber cloth winding method according to claim 1, characterized in that, The pre-lamination process includes: first, stacking each group of the fiber fabrics, and then ironing them to obtain the fiber composite layer.

5. The fiber cloth winding method according to claim 4, characterized in that, The overlapping process involves reserving a gap between the corresponding long sides of each pair of adjacent fiber cloth pieces.

6. The fiber cloth winding method according to claim 5, characterized in that, The width of the interval is 4-6 mm.

7. The fiber cloth winding method according to claim 4, characterized in that, The ironing temperature is 50-60℃.

8. The fiber cloth winding method according to claim 1, characterized in that, The diameter of the straight tube at one end is 3-4 mm and the length is 4-8 mm.

9. The fiber cloth winding method according to claim 1, characterized in that, The diameter of the straight tube at the other end is 8-9 mm, and the length is 200-240 mm.

10. The fiber cloth winding method according to claim 1, characterized in that, The length of the frustum-shaped tube is 640-650mm.

11. The fiber cloth winding method according to claim 5, characterized in that, The rolling process includes: ironing the intervals and the corresponding rolling start lines with an iron.

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