JP7364274B2 - Fiber woven composite material structural member, automobile frame manufactured therefrom, and manufacturing method - Google Patents

Description

TECHNICAL FIELD The present invention relates to the technical field of application of fiber fabric composite materials, and more particularly to a fiber fabric composite material structural member, an automobile frame manufactured using the same, and a manufacturing method.

With the rapid development of technology in modern times, high demands are placed on materials, and carbon fiber has high strength, heat resistance, corrosion resistance, fatigue resistance, light weight, and can withstand very large tensile forces, making it better than steel and aluminum. It also has extremely high properties, belongs to a typical high-performance fiber, and has overwhelming advantages compared to conventional metal materials. In addition to being used alone as a heat insulating material, carbon fiber is generally added as a supplementary material into materials such as resin, metal, ceramic, and concrete to form carbon fiber composite materials. Materials are beginning to be used in numerous fields.

In an environment of energy conservation and carbon dioxide emission reduction around the world, the weight of automobiles is gradually becoming lighter, and the use of plastics, composite materials, etc. in automobiles is becoming more widespread, and fiber composite materials are replacing existing metal structures. is an effective means of reducing air pollution caused by vehicle exhaust gas and realizing energy savings. Carbon fiber is a fibrous carbon material with a carbon content of more than 90%, which has high strength and high elasticity, and carbon fiber composite materials are manufactured through the optimization design of matrix, fiber selection, carbon fiber content and distribution. It can be manufactured into various high-performance structural members that can meet the demands of various fields.

In a conventional car, only 1% of the gasoline is used to transport passengers, the rest is used for the movement of the car itself, and by replacing steel with fiber composite materials, the weight of the car can be reduced by more than half. The weight reduction effect is 50% lighter than metal materials and 30% lighter than aluminum materials, and fiber composite materials are lightweight and have high strength as automobile parts, are integrated into parts, and have good design, impact resistance, and corrosion resistance. It has the advantage of being excellent and easy to mold. Currently, fiber composite materials are actually applied to parts such as automobile brake pads and wheels, and their application to automobile frames is still relatively rare. The frames of automobiles and buses are three-dimensional frames, and the role of the frame is to withstand loads including the weight of the vehicle's own parts as well as collisions, distortions, and inertial forces received during driving. In the prior art, the frame structure of an automobile is roughly divided into a separate frame and an unseparated frame.The separate frame is made of steel by welding or riveting thick steel pipes, and the engine, suspension, body, etc. are mounted on this steel frame. Because the parts are attached, the steel tubes of the separate frame are heavy, and the frame weight accounts for most of the total vehicle weight; the separate frame is made of pressed and welded steel (the advanced version is aluminum). The requirements for design and manufacturing technology are very high, the quality of the product is difficult to control, the manufacturing process is complicated, and the overall frame structure lacks rigidity and strength.

Energy saving and environmental protection have gradually become important issues that the automobile industry is concerned about, and people have begun to consider ways to make automobiles lighter. Reducing the weight of automobiles not only reduces the empty weight of automobiles and saves raw materials, but also reduces automobile production costs and fuel consumption, which contributes to energy conservation and environmental conservation. This has led people to try to replace traditional frame construction materials with lighter weight, stronger composite materials.

In carbon fiber composite materials, the greatest feature of carbon fibers is that they can withstand extremely large tensile forces, and the resin can withstand pressure. In this case, because the plate thickness is too small, the generated torque is small and the advantage that carbon fiber can withstand very large tensile forces is not fully utilized. Therefore, it is necessary to research ways to fully utilize the advantage that carbon fibers can withstand tensile forces. For this reason, it has become an extremely important issue to manufacture carbon fiber composite materials as structural members with light density so that they can withstand extremely large tensile forces. Next, the fact that carbon fiber composite materials are not suitable for rapid production is also an important cause of inhibiting the development of carbon fiber composite materials.

In order to solve the above problems, the present invention provides a carbon fiber woven composite material structural member, an automobile frame manufactured using the same, and a manufacturing method.

The present invention consists of the following technical solutions.
A textile composite material structural member, wherein a tubular shape is formed on the outside of the structural member, the tubular structural member is a textile textile composite material honeycomb pipe supported by a textile textile composite material, and the textile textile composite material therein is a textile composite material structural member. There are plain weave and twill weave.

The honeycomb holes of the composite honeycomb pipe are filled with a sandwich structure material or a fiber composite pipe or a hollow support. The sandwich structure material filled in the honeycomb holes of the composite honeycomb pipe is a core material in which the honeycomb holes of the composite honeycomb pipe are filled with the sandwich structure material.

The fiber fabric composite material honeycomb pipe includes at least two single helical winding assembly members closely attached to form a helical winding assembly member bundle, and the single helical winding assembly members cover the surface of the core material of the sandwich structure material with the fiber fabric composite material tape. The helically wound fiber woven composite tape is helically wound by tightening the previously wrapped part of the fiber woven composite tape with the later wrapped fiber woven composite tape. Construct a composite material honeycomb pipe.

The fiber fabric composite material honeycomb pipe supported by the fiber fabric composite material is a star-shaped support structure in which the laminated fiber fabric composite material sewn with suture threads is formed so as to radially support the suture threads as supporting members. be. A fiber fabric composite honeycomb pipe is formed between the fiber fabric composites of the star-shaped supports.

The fiber fabric composite material support constitutes a tube part support in which a part of the laminated fiber fabric composite material sewn with a suture thread is wound around as a tube part, and connected radially using the suture thread as a support member. However, the other part constitutes a composite support body of the radial part and the winding tube part so that the laminated fiber fabric composite material sewn with the suture thread supports the suture thread radially as a support member.

The fiber fabric composite material honeycomb pipe supported by the fiber fabric composite material is a pipe in which laminated fiber fabric composite materials sewn together with suture threads are each wound as a winding tube section, and are radially connected using the suture threads as supporting members. This constitutes a winding tube support body.

The fiber fabric composite material honeycomb pipe supported by the fiber fabric composite material is defined as one set of laminations for every N layers of the laminated fiber fabric composite material stitched with sutures, where N≧2, and each set of After the laminates in each set are partially extended radially, each set of laminates is branched and extended in N directions to form N branches, each branching part being a part of the laminates in the other set. The branched portions are overlapped and extended in pairs to form a honeycomb support with radial edges; or the fiber fabric composite honeycomb pipe supported by the fiber fabric composite material is sutured with a suture thread. A set of laminations is formed for every N layers of the laminated fiber fabric composite material, where N≧2, the center layer of each set of laminations is wound as a winding tube, and the other layers are partially extended radially. After being taken out, it is branched to form a plurality of branch parts, and each branch part is overlapped and extended in pairs with the branch parts of other sets of laminated layers, and the edges constitute a honeycomb support body. be.

The outer surface of the helically wound fiber fabric composite material honeycomb pipe is again helically wound with a fiber fabric composite material tape, and a part of the fiber fabric composite material previously wrapped with a later wrapped fiber fabric composite material tape. Tighten the tape.

The cross section of the honeycomb pipe forms a multilayer honeycomb hole outwardly about the axis, and the outermost layer is the pipe wall.

The fiber fabric composite material extends from the support shaft to the outside of the pipe wall, is bent along the pipe wall, and is combined with the pipe wall to form a part of the pipe wall, and covers the entire pipe wall and the supporting material inside thereof. It is integrally connected through the fiber fabric composite material bent along the pipe wall.

The fiber fabric composite material extends from the support shaft to the outside of the tube wall, is bent along the tube wall, and is combined with the tube wall, and the tube wall is a helically wound fiber fabric composite material tape, and the fiber fabric composite material is bent along the tube wall. The helically wound fiber woven composite material and the helically wound fiber woven composite tape are bonded together.

After the fiber fabric composite material is stretched from the support shaft to the pipe wall location, it can be subsequently extended from the pipe wall to serve as an external bonding member of the structural member, and to transmit the force experienced by the external bonding member to the support material. .

The fiber fabric composite material extends from the support shaft out of the pipe wall, is bent along the pipe wall, forms part of the pipe wall, and after being bent to the support material extending from the pipe wall, further It can extend from the tube wall together with the support material to transmit forces experienced by the external coupling member to the tube wall and the support material therein.

The number of support shafts in the pipe wall is at least two, and the support shafts are connected and supported by a fiber fabric composite material.

The cross-sectional contours of different parts of the structural member along the axis of the tube are different, or the contours are the same but different in size.

The tubular structural member has a branched shape (e.g., a “Y” branched shape, a “T” branched shape, or a “cross” branched shape), and the main pipe and branch pipes of the tubular structural member are connected to the pipe wall. Not only are they joined, but the support shaft inside the pipe is also joined.

The structural member is an integral three-dimensional frame structure.

The integral three-dimensional frame structure is a star-shaped support in a honeycomb hole, a single helical winding assembly member or a ring sandwich structure material or a ring fiber composite material pipe or a ring hollow support, and the fiber fabric is made of carbon fiber. It is a woven fabric and constitutes an integrated carbon fiber woven composite material skeleton.

The number of support shafts in the same cross section of the carbon fiber fabric composite material integrated frame is at least two, and the support shafts are connected and supported by the fiber fabric composite material.

The carbon fiber woven composite material frame is used as a frame of an automobile, a frame of an aircraft, a frame of a train, and a frame of a container.

A power transmission shaft or strut made of the fiber fabric composite material structural member.

A method for manufacturing a fiber woven composite material structural member, comprising:
Step 1) of creating three-dimensional drawings of the required structural members;
A mold drawing for the structural member core is created based on the three-dimensional drawing, and the structural member core is manufactured (the core is provided with core pins corresponding to the honeycomb holes, and the core is made of sandwich structural material or fiber composite material). (Material pipe or hollow support) Step 2);
step 3) of creating a mold drawing of the structural member main mold based on the three-dimensional drawing and also creating the structural member main mold;
Step 4) of separately determining the planar shape of each fiber-woven composite material used for support within the three-dimensional drawing structural member, based on its spatial shape;
Step 5) of cutting the fiber fabric composite material prepreg based on the planar shape of Step 4) (Similarly determining and cutting the pipe wall prepreg by Step 4) and Step 5);
step 6) of determining sutures of the prepreg based on the three-dimensional drawing;
Step 7) of laminating the prepregs that require each layer according to the determined suture position;
Step 8) suturing the laminated prepregs according to the position of the suture thread (hand suturing or sewing machine suturing can be used);
Step 9: Spread the sewn laminated prepreg sheet, align the honeycomb holes formed in the prepreg sheet with the core pins of the core based on the three-dimensional drawing, insert the core pins into the matching honeycomb holes, and cover the outside of the core pins with the outer prepreg. )and,
Step 10) of forming a tube wall by covering the core with tube wall prepreg;
Step 11) of inserting the core covered with tube wall prepreg into the main mold;
step 12) in which the core is heated and hardened, the main mold is heated and hardened, or the core and the main mold are simultaneously heated and hardened, and then the core and the main mold are taken out to obtain the required structural member;
including.

Among the outer prepreg sheets in step 9), the prepreg sheet extending from the pipe wall and serving as a connecting member is reserved without covering the outside of the core pin, and the remaining prepreg sheet covers the outside of the core pin.

The pipe wall prepreg sheet serving as the connection member and the supporting prepreg sheet extending from the pipe wall are overlapped and extended together from the pipe wall.

The superimposed prepreg sheets, which extend together from the tube wall, are sewn into a master mold to be fitted together and proceed to other steps.

The core in step 2) is manufactured by foam-molding the foam in a mold.

A method for manufacturing an integrated three-dimensional frame structure using a carbon fiber woven composite material structural member, the method comprising:
Step (1) of creating a three-dimensional drawing of the integrated three-dimensional frame structure;
Step (2) of disassembling the annular framework based on the framework in the three-dimensional drawing (including the monocyclic framework, and optionally the monocyclic framework subsequently included in the solid polycyclic framework, the hollow The monocyclic frame contained in the polycyclic frame, the monocyclic frame contained in the partially hollow polycyclic frame are collectively referred to as the "monocyclic frame," and
Step (3) of manufacturing a monocyclic rigid foam core frame based on the shape of each monocyclic frame (including a monocyclic rigid foam core frame if necessary, a solid polycyclic core frame if necessary) Monocyclic rigid foam core included in a hollow polycyclic rigid foam core, monocyclic rigid foam core included in a hollow polycyclic rigid foam core, partially hollow polycyclic rigid foam core further manufacturing a monocyclic rigid foam core frame included in the core frame);
Step (4) of wrapping the outer surface of each annular rigid foam core with continuous carbon fiber woven prepreg to form a composite structural member of monocyclic carbon fiber woven prepreg (if necessary, solid polycyclic carbon Composite material structural members of monocyclic carbon fiber fabric prepreg included in fiber fabric composite material structural members, composite material structural members and parts of monocyclic carbon fiber fabric prepreg included in hollow polycyclic carbon fiber fabric composite material structural members. a monocyclic carbon fiber woven prepreg composite structural member included in a hollow polycyclic carbon fiber woven composite structural member);
step (5) of creating a mold drawing of the main mold of the integrated three-dimensional frame structure based on the three-dimensional drawing and also creating the main mold;
a step (6) of separately determining the planar shape of each fiber fabric composite material used for support within the three-dimensional drawing structural member, based on the spatial shape thereof;
Step 7) of cutting the fiber woven composite material prepreg based on the planar shape of step (4) (similarly determining and cutting the pipe wall prepreg according to step (4) and step (5));
(8) determining sutures of the prepreg based on the three-dimensional drawing;
a step (9) of laminating prepregs requiring each layer according to the determined suture position;
a step (10) of suturing the laminated prepregs according to the position of the suture thread (hand suturing or sewing machine suturing can be used);
Spread the sewn laminated prepreg sheets, align the honeycomb holes formed in the prepreg sheet based on the three-dimensional drawing with the monocyclic frame of the core, insert the monocyclic frame into the matching honeycomb holes, and then remove the outer prepreg. (11) covering the outside of the core pin;
forming a tube wall by covering the core with tube wall prepreg (12);
a step (13) of inserting a core coated with tube wall prepreg into the main mold;
A step (14) of heating and hardening the core, heating and hardening the main mold, or heating and hardening the core and the main mold at the same time, and then taking out the core and the main mold to obtain the required structural member;
including.

The carbon fiber woven composite material structural member is annular in shape, the core is an annular rigid foam material, and the outer surface of the annular rigid foam material is wrapped with the carbon fiber woven composite material. Rotate to form a monocyclic carbon fiber woven composite structural member.

In the carbon fiber woven composite material structural member, the monocyclic carbon fiber woven composite material structural member is in the form of a bundle, and the number of monocyclic carbon fiber woven composite material structural members in the bundle is at least two, and one bundle The outer surface of the monocyclic carbon fiber woven composite material structural member is wound with a carbon fiber woven composite material to form a polycyclic carbon fiber woven composite material structural member.

In the carbon fiber woven composite material structural member, a monocyclic carbon fiber woven composite material structural member is filled and compacted inside the carbon fiber woven composite material that is wound around the outer surface of the polycyclic carbon fiber woven composite material structural member. A solid polycyclic carbon fiber woven composite structural member is constructed.

In the carbon fiber woven composite material structural member, a carbon fiber woven composite material is wound around the outer surface of the polycyclic carbon fiber woven composite material structural member from the outside to the inside, a monocyclic carbon fiber woven composite material structural member, and a cavity. The hollow polycyclic carbon fiber woven composite material structural member is constructed by the section.

In the carbon fiber woven composite material structural member, since the portion along the axis of the polycyclic carbon fiber woven composite material structural member is a hollow portion, the polycyclic carbon fiber woven composite material structural member is partially hollow. Configure.

In the carbon fiber woven composite material frame manufactured by the carbon fiber woven composite material structural member, the monocyclic carbon fiber woven composite material structural member, the solid polycyclic carbon fiber woven composite material structural member, the hollow polycyclic carbon fiber woven composite material structural member The carbon fiber woven composite structural member and the partially hollow polycyclic carbon fiber woven composite structural member are collectively referred to as a carbon fiber woven composite structural member ring, and the carbon fiber woven composite structural member ring is used as a frame. The outer surface of the carbon fiber woven composite structural member ring constituting the bundle portion adjacently within the frame is wound with the carbon fiber woven composite material.

The carbon fiber woven composite material frame is a non-closed structure.

A method of manufacturing a frame using a carbon fiber woven composite material structural member, the method comprising:
Step (1) of creating a three-dimensional drawing of the frame;
Step (2) of disassembling the annular framework based on the framework in the three-dimensional drawing (including the monocyclic framework, and optionally the monocyclic framework subsequently included in the solid polycyclic framework, the hollow The monocyclic frame contained in the polycyclic frame, the monocyclic frame contained in the partially hollow polycyclic frame are collectively referred to as the "monocyclic frame," and
Step (3) of manufacturing a monocyclic rigid foam core frame based on the shape of each monocyclic frame (including a monocyclic rigid foam core frame if necessary, a solid polycyclic core frame if necessary) Monocyclic rigid foam core included in a hollow polycyclic rigid foam core, monocyclic rigid foam core included in a hollow polycyclic rigid foam core, partially hollow polycyclic rigid foam core further manufacturing a monocyclic rigid foam core frame included in the core frame);
Step (4) of wrapping the outer surface of each annular rigid foam core with continuous carbon fiber woven prepreg to form a composite structural member of monocyclic carbon fiber woven prepreg (if necessary, solid polycyclic carbon Composite material structural members of monocyclic carbon fiber fabric prepreg included in fiber fabric composite material structural members, composite material structural members and parts of monocyclic carbon fiber fabric prepreg included in hollow polycyclic carbon fiber fabric composite material structural members. a monocyclic carbon fiber woven prepreg composite structural member included in a hollow polycyclic carbon fiber woven composite structural member);
If necessary, the monocyclic carbon fiber woven prepreg composite structural member included in the solid polycyclic carbon fiber woven composite material structural member may be converted into a composite material structural member bundle of bare solid polycyclic carbon fiber woven prepreg. assembling and winding the outer surface of the bare solid polycyclic carbon fiber fabric prepreg composite material structural member bundle with continuous carbon fiber fabric prepreg to constitute a solid polycyclic carbon fiber fabric prepreg composite material structural member;
The composite material structural member of the monocyclic carbon fiber fabric prepreg included in the hollow polycyclic carbon fiber fabric composite structural member is assembled as a composite material structural member bundle of the bare solid polycyclic carbon fiber fabric prepreg, and the Wrapping the outer surface of the composite material structural member bundle of cyclic carbon fiber woven prepreg with continuous carbon fiber woven prepreg to constitute a composite material structural member of hollow polycyclic carbon fiber woven prepreg;
Bare composite structural member of monocyclic carbon fiber woven prepreg included in partially hollow polycyclic carbon fiber woven composite structural member Bundle of partially hollow polycyclic carbon fiber woven prepreg composite material structural member The outer surface of a composite structural member bundle of bare partially hollow polycyclic carbon fiber fabric prepreg is wrapped with continuous carbon fiber fabric prepreg to form a partially hollow hollow polycyclic carbon fiber fabric prepreg. Step (5) of configuring a composite material structural member;
Composite structural members of monocyclic carbon fiber woven prepreg, composite structural members of solid polycyclic carbon fiber woven prepreg, composite structural members of hollow polycyclic carbon fiber woven prepreg, partially hollow polycyclic The carbon fiber fabric prepreg is produced by assembling one or more of the composite material structural members of the carbon fiber fabric prepreg as a frame, and winding the outer surface of the frame adjacent to each other to form a bundled part. a step (6) of configuring a composite material frame of woven prepreg;
A step (7) in which a carbon fiber woven prepreg composite material frame is placed in a mold, heated and cured, and when released from the mold, becomes a carbon fiber woven composite material frame;
including.

In the method for manufacturing a frame using a carbon fiber woven composite material structural member, the carbon fiber woven composite material frame is a frame of an automobile, an aircraft, a train, and a container.

An automobile frame made of carbon fiber fabric composite material, wherein the chassis of the automobile frame includes a star-shaped support structure formed such that the laminated fiber fabric composite material sewn with suture threads supports the suture threads radially as supporting members. and a fiber fabric composite honeycomb pipe is formed between the fiber fabric composite materials of the star-shaped support; the carbon fiber fabric composite honeycomb pipe is covered with a single helical winding assembly member, and the single helical winding assembly member has a sandwich structure. The surface of the core material of the material is spirally wrapped with a fiber fabric composite tape, and the previously wrapped fiber fabric composite tape is tightly tightened with the later wrapped fiber fabric composite tape; , the textile composite material honeycomb pipe has at least two single helical wound assembly members in close contact with each other to form a helical wound assembly member bundle, and the helically wound textile composite material tape in the helical wound assembly member bundle is a helically wound textile composite material tape. The chassis is a chassis frame, and the vehicle body frame is placed on the chassis frame and connected by elastic members to constitute a separate frame made of a carbon fiber woven composite material; Two unitary carbon fiber woven composite frames with separate frames. The technical features in the above technical solution can also be applied to the present technical solution if necessary.

The present invention manufactures a fiber fabric composite material as a tubular structural member of a honeycomb-like support, and when the manufactured structural member receives force, the applied force is distributed to each branch part of the honeycomb-like structure and the structural member is Common carbon fiber composite materials can withstand very strong tensile forces, but their ability to withstand pressure is relatively poor, and the in-tube support of structural members By using the body with a honeycomb-shaped carbon fiber woven composite material support, the structural member can withstand pressure to a certain extent, and the range and direction in which the structural member is subjected to forces can be expanded. The present invention honeycombs the structural member support, reducing material and weight and cost savings compared to solid structural members, while having the strength to withstand higher forces compared to hollow structural members. Although carbon fiber can withstand very high tensile forces and does not deform, manufacturing it as a solid material not only wastes material and increases weight, but also does not significantly improve performance. Therefore, the present invention realizes the maximum performance of carbon fiber, which can withstand extremely large tensile forces, by filling the honeycomb pipe with a hard foam material; the structure is wound with carbon fiber fabric. The frames of automobiles and the like manufactured using these parts are lightweight and strong, and can be molded using an overwrapping machine, making them suitable for mechanized production.

FIG. 1 is a schematic diagram showing the structure of a radial support. FIG. 2 is a schematic diagram showing the structure of a radial support. FIG. 3 is a schematic diagram showing the structure of a radial support. FIG. 4 is a schematic diagram showing the structure of a radial support. FIG. 1 is a schematic diagram showing the structure of a composite support of a radiating part and a winding tube part. FIG. 2 is a schematic diagram illustrating the structure of a composite support of a radiation part and a winding tube part. It is a schematic diagram which shows the structure of a winding tube part-shaped support body. FIG. 1 is a schematic diagram showing the structure of a radial support with a mold. FIG. 2 is a schematic diagram 2 showing the structure of a radial support with a mold. FIG. 2 is a schematic diagram showing the structure of a composite support of a molded radiating section and a winding tube section. FIG. 2 is a schematic diagram showing the structure of a tube-like support with a mold. FIG. 1 is a schematic diagram showing the structure of a vehicle body frame. FIG. 2 is a schematic diagram showing the structure of the vehicle body frame. FIG. 2 is a schematic diagram showing the structure of a cyclic skeleton support. 14 is an enlarged view of part A in FIG. 13. FIG. FIG. 1 is a schematic diagram showing the structure of a fiber composite material joint. FIG. 2 is a schematic diagram showing the structure of a fiber composite material joint. FIG. 3 is a schematic diagram showing the structure of the vehicle body frame. FIG. 1 is a schematic diagram showing the structure of a hollow stick-like support. FIG. 2 is a schematic diagram 2 showing the structure of a hollow stick-like support. FIG. 2 is a schematic diagram showing the structure of a honeycomb pipe with multilayer honeycomb holes. It is a schematic diagram showing the structure of a honeycomb pipe of two star-shaped supports. It is a schematic diagram showing the structure of a honeycomb pipe of three star-shaped supports. 13 is an enlarged view of the structure of part B in FIG. 12. FIG. FIG. 1 is a schematic diagram showing the structure of an automobile frame. FIG. 3 illustrates some monocyclic carbon fiber woven composite structural members. FIG. 2 illustrates some solid polycyclic carbon fiber woven composite structural members. FIG. 3 is a diagram illustrating some hollow polycyclic carbon fiber woven composite structural members. FIG. 2 is a schematic diagram showing the external structure of an automobile frame. FIG. 2 is a partial structural sectional view of an automobile frame. It is a structural sectional view of a portion where the B pillar is relatively thick. It is a structural cross-sectional view of a portion where the B pillar is relatively thin.

In order to enable those skilled in the art to better understand the present invention, the present invention will be further described in conjunction with specific embodiments below.

Referring to FIGS. 1 to 7, there is provided a fiber fabric composite structural member, wherein a tubular shape is formed on the outside of the structural member, and the tubular structural member is a fiber fabric composite honeycomb pipe supported by the fiber fabric composite material. Yes; the fiber fabric composite material therein includes plain weave and twill weave, and the fiber fabric composite material is carbon fiber or glass fiber.

The honeycomb holes of the composite honeycomb pipe are filled with a sandwich structure material or a fiber composite pipe or a hollow support. The sandwich structure material is mainly a rigid foam material, which can be rigid foamed polystyrene, and the rigid foam material is mainly PVC, PEI, PU, PET, PMI, AIREX, DIAB, 3A, STRUCELL, ROHACELL, rigid foamed material. Examples include metal materials; the fiber composite material pipe is a carbon fiber woven composite material pipe or a carbon fiber wound composite material pipe; the hollow support is a thin hollow plastic support or a thin hollow metal support; The thin walled hollow plastic support can be a blow molded article.

As shown in FIGS. 1 to 4, the fiber fabric composite material honeycomb pipe supported by the fiber fabric composite material means that the laminated fiber fabric composite material sewn with suture threads supports the suture threads radially as supporting members. It is a honeycomb pipe constructed by forming a star-shaped support structure, and covering the outer layer of the star-shaped support structure with one layer of fiber woven composite material as the tube wall, and the holes formed in the star-shaped support structure are honeycomb holes. Naturally, a honeycomb hole can be formed using the star-shaped support structure and the tube wall.

As shown in FIGS. 5 and 6, the fiber fabric composite material support is a part of the laminated fiber fabric composite material sewn with a suture thread, which is wound as a winding tube part, and is radially wound with the suture thread as a supporting member. The composite supports of the radial part and the winding tube part are connected so that the other part constitutes the connected winding tube part support body, and the other part is a laminated fiber fabric composite material sewn with suture threads to support the suture threads radially as supporting members. It consists of A radial support or a composite support consisting of a radial part and a winding pipe part, when a structural member receives a force, transmits the received force to the entire support body through the radial laminated branch part connected to the pipe wall, and receives the force. It can evenly distribute the force to the structural members and prevent deformation or breakage due to unbalanced forces applied to the structural members; the supports are made in a radial shape and have higher load-bearing strength than hollow tubes; At the same time it saves material and cost compared to solid tubing.

As shown in FIG. 7, the fiber fabric composite material honeycomb pipe supported by the fiber fabric composite material is a structure in which the laminated fiber fabric composite materials sewn with suture threads are each wound as a winding tube part, so that the suture threads are It is a honeycomb pipe, which has a radially connected tube support 107 as a support member, and a tube wall 207 which is made by covering the outer layer of a star-shaped support structure with a layer of fiber fabric composite material; When a tube supported by a tube member is used as a transmission shaft or support, the strength to withstand the force of the transmission shaft or support is greatly increased, making it difficult to bend, deform, or break.

As shown in FIG. 21, the fiber fabric composite material honeycomb pipe supported by the fiber fabric composite material is a set of laminations for every N layers of the laminated fiber fabric composite material sewn with suture threads, where N ≧2, and after each set of laminated layers partially extends radially, each set of laminated layers is branched and extends in N directions to form N branched parts, and each set of laminated layers are stacked and extended in pairs with branch parts of other sets of laminates to constitute a honeycomb support with radial edges; or a fiber fabric composite honeycomb pipe supported by the fiber fabric composite material; means one set of laminates every N layers of a laminated fiber fabric composite material sewn with sutures, where N≧2, the center layer of each set of laminates is wound as a winding tube, and the other layers are A part of the laminate is extended radially and then branched to form a plurality of branch parts, and each branch part is overlapped with the branch parts of other sets of laminated layers in pairs and extended, and the edge is a radial honeycomb. It constitutes a support body. As shown in FIG. 21, the cross section of the honeycomb pipe constitutes a multilayer honeycomb hole 16 outward from the axis, and the outermost layer is the tube wall 15. The honeycomb pipe containing the multilayer honeycomb holes 16 can be applied as a transmission shaft or a support, and not only has the advantage of being lightweight, but also has the advantage that when the pipe wall 15 receives force, the received force is transmitted through the radial branching part of the edge. , the received force can be distributed uniformly over the entire support, and such a honeycomb-shaped support can relatively reduce the force received by the pipe wall, and compared to the transmission shaft or column of the conventional structure, the same When subjected to force, the tube wall of the carbon fiber fabric composite honeycomb support with radial edges is less likely to bend or deform, which can extend the life of the transmission shaft or support.

As shown in FIG. 1, the fiber fabric composite material extends from the support shaft to the outside of the tube wall 201, is bent along the tube wall, and is combined with the tube wall to form a part of the tube wall. The whole and its internal support material 101 are integrally connected through the fiber fabric composite material bent along the tube wall. When the textile composite material is extended to the pipe wall and bent along the pipe wall, the force experienced by the pipe wall can be transferred to the textile textile composite support within the pipe, increasing the strength of the pipe material to withstand the force. increase

After the fiber fabric composite material is stretched from the support shaft to the pipe wall location, it is subsequently extended from the pipe wall to serve as an external coupling member of the structural member, and the force received by the external coupling member is transmitted to the support material, Increases the mechanical strength of the structural member by receiving forces across the support material. As shown in FIG. 2, the intratubular support shaft 102 is a radial support, and both ends of the intratubular support shaft 102 extend from the tube wall 202, forming two external coupling members 302. As shown in FIG. 6, the intratubular support shaft 106 is a composite support for the radial-winding tube section, with both ends of the intratubular support shaft 106 extending from the tube wall 206 and connecting two external coupling members 306. Configure. As shown in FIG. 3, the structural member configured by extending one end of the pipe support shaft 103 from the pipe wall 203 includes one external coupling member 303; as shown in FIG. is a composite support for the radial-winding tube section, and one end of the tube support shaft 105 extends from the tube wall 205 to constitute one external coupling member 305.

As shown in FIG. 4, the fiber fabric composite material extends from the support shaft 104 to the tube wall 204, is bent along the tube wall 204, forms part of the tube wall, and extends from the tube wall 204. After the support material is bent to the support material, it further extends from the tube wall together with said support material and constitutes an external bonding member 304 of the structural member, transferring the forces experienced by the external bonding member to the tube wall and the support material therein. By transmitting the force and making the force received uniform throughout, the strength of the tube material to withstand the force is increased.

The number of support shafts in the pipe wall is at least two, and the support shafts are connected and supported by a fiber woven composite material, and the plurality of support shafts are structured to further ensure uniformity of received force. Increases the strength of a member to withstand force.

As shown in FIG. 22, two star-shaped supports of the fiber fabric composite structural member may constitute a honeycomb pipe; as shown in FIG. 23, the star-shaped supports of the fiber fabric composite structural member Three supports may constitute a honeycomb pipe. The tube wall 18 of the honeycomb pipe shown in FIG. 22, which is composed of two star-shaped supports 17, is made by stretching and bending the star-shaped supports 17. The tube wall 20 of the honeycomb pipe structural member shown in FIG. 23 is formed by bending the three star-shaped supports 19.

If desired, the structural element can be designed with different cross-sectional contours at different locations of the structural element along the axis of the tube, or with the same contour but different sizes.

As shown in FIG. 15, support members 802 are provided on the cross section by sorting along the support axis direction in the honeycomb holes of the fiber fabric composite honeycomb pipe 801, and the support members on the cross section resist the force in the axial direction. By increasing the withstand strength, the structural member is less likely to deform or bend along the axial direction.

Depending on the needs of the joining member, the tubular structural member has a branched shape (for example, a “Y” branched shape, a “T” branched shape, or a “cross” branched shape), and the tubular structural member The reason why not only the pipe walls of the main pipe and the branch pipe are joined, but also the support shaft inside the pipe is joined is that the fiber fabrics of the support shaft or the pipe wall are integrated or the fiber fabrics are sewn together; sandwich structure If a material or fiber composite pipe is provided, the sandwich construction material is integrally molded or the fiber fabric of the fiber composite pipe is a continuous fiber. By connecting the pipe walls of the main pipe and branch pipes to the star-shaped supports, the pipe walls of the main pipe and branch pipes and the star-shaped supports form an integral structure, which matches the forces received from the inside and outside, allowing the structural members to It is possible to prevent deformation or damage caused by misalignment of external forces.

The structure of the integral three-dimensional frame is formed by connecting the structural members through a "Y" branch, a "T" branch, or a cross-shaped branch, and forming an integrated three-dimensional frame. It means to constitute a body structure, for example, the skeleton of an off-road vehicle, the skeleton of a passenger car, the skeleton of a bus, the skeleton of a helicopter, or the skeleton of an aircraft.

In particular, by circularly connecting the integral three-dimensional frame structural members, a required completed vehicle frame is assembled. As shown in FIG. 12, the star-shaped supports in the ring-shaped supports used during the ring-joint process of the ring-welded complete vehicle frame 7 can be combined, and the support shaft of the star-shaped supports after the combination is made of carbon fibers. Connected through the textile composite material, the tube wall of the star-shaped support after combining also becomes an integral tube wall; the star-shaped support in the annular support used during the welding process of the annularly welded complete vehicle frame 7; can be separated, for example, the corner B part of the complete vehicle frame in FIG. 12, that is, as shown in FIG. A "Y"-shaped branch, a "T"-shaped branch, or a "cross" branch is formed.

The support axes of the star-shaped support within the annular support are separated, thus forming a "Y"-shaped branch, a "T"-shaped branch, or a "cross" branch. Suitable for the frame structure; therefore, the “Y” branch, “T” branch, or cross-shaped branch (the branching or merging portion shown in FIG. 24) is a planar “Y”. In addition to the branched shape of a character, the branched shape of a "T" character, or the branched shape of a "cross" shape, it is also possible to form a three-dimensional shape by bending the planar shape.

By configuring the integral three-dimensional frame structure by inserting or circumferentially joining the structural members, a desired integral skeleton can be assembled. Shown in FIGS. 12 and 13 is a complete vehicle frame constructed from carbon fiber woven composite material. FIG. 12 shows a complete vehicle frame 7 manufactured by circular welding, and the annular support 9 used during the circular welding process is as shown in FIG. These are coil pipes or braided tubes manufactured after heating and hardening; FIG. 13 shows a complete vehicle frame 8 manufactured by plug-in joining, and as shown in FIG. 15, structural members used on the complete vehicle frame 8 are shown. If a support member 802 is provided in the axial direction on 801 and a support is provided to the structural member, the mechanical strength of the complete vehicle can be further increased.

A power transmission shaft or strut made of the fiber fabric composite material structural member.

A method for manufacturing a fiber woven composite material structural member, comprising:
Step 1) of creating three-dimensional drawings of the required structural members;
A mold drawing for the structural member core is created based on the three-dimensional drawing, and the structural member core is manufactured (the core is provided with core pins corresponding to the honeycomb holes, and the core is made of sandwich structural material or fiber composite material). (Material pipe or hollow support) Step 2);
step 3) of creating a mold drawing of the structural member main mold based on the three-dimensional drawing and also creating the structural member main mold;
Step 4) of separately determining the planar shape of each fiber-woven composite material used for support within the three-dimensional drawing structural member, based on its spatial shape;
Step 5) of cutting the fiber fabric composite material prepreg based on the planar shape of Step 4) (Similarly determining and cutting the pipe wall prepreg by Step 4) and Step 5);
step 6) of determining sutures of the prepreg based on the three-dimensional drawing;
Step 7) of laminating the prepregs that require each layer according to the determined suture position;
Step 8) suturing the laminated prepregs according to the position of the suture thread (hand suturing or sewing machine suturing can be used);
Step 9: Spread the sewn laminated prepreg sheet, align the honeycomb holes formed in the prepreg sheet with the core pins of the core based on the three-dimensional drawing, insert the core pins into the matching honeycomb holes, and cover the outside of the core pins with the outer prepreg. )and,
Step 10) of forming a tube wall by covering the core with tube wall prepreg;
Step 11) of inserting the core covered with tube wall prepreg into the main mold;
step 12) of heating and hardening the core, heating and hardening the main mold, or heating and hardening the core and the main mold at the same time;
including.

Among the outer prepreg sheets in step 9), the prepreg sheet extending from the pipe wall and serving as a connecting member is reserved without covering the outside of the core pin, and the remaining prepreg sheet covers the outside of the core pin.

The pipe wall prepreg sheet serving as the connection member and the supporting prepreg sheet extending from the pipe wall are overlapped and extended together from the pipe wall.

The superimposed prepreg sheets, which extend together from the tube wall, are sewn into a master mold to be fitted together and proceed to other steps.

The core in step 2) is manufactured by foam-molding the foam in a mold.

Referring to FIGS. 8 to 11, there are schematic diagrams partially showing a structural member including a core and a main mold during the manufacturing process of a tube wall supporting structural member according to the present invention. As shown in FIG. 8, the laminated prepreg sheet 101 serving as a support is inserted into the core 501, the laminated layers protruding from the core are bent, the outer layer is covered with a fiber woven composite material to become the tube wall 201, and then the inner layer is bent. The fiber fabric composite material covering the core is fitted into the main mold 601 and cured by heating; as shown in FIG. 9, the laminated prepreg sheet 102 serving as a support is inserted into the core 502 and protrudes from the core. By bending the laminated portion, the laminated portion protruding from the tube wall 202 extends together with the tube wall to become the connecting member 302, the outer layer is covered with a fiber fabric composite material to become the tube wall 202, and then the fiber fabric covering the core is formed. After the composite material is fitted into the main mold 602, it is heated and cured; as shown in FIG. The laminated portion protruding from the tube wall 205 extends together with the tube wall to become a connecting member 305, the outer layer is covered with a fiber fabric composite material to become the tube wall 205, and the fiber fabric composite material covering the core is then wrapped around the tube wall 205. After the material is fitted into the main mold 605, it is heated and cured; as shown in FIG. 11, the laminated prepreg sheet 107 serving as a support is inserted into the core 507, and the laminated portion protruding from the core 507 is formed into a winding tube section. The tube wall 207 is formed by wrapping the outer layer with a fiber woven composite material, and then the fiber woven composite material covering the core 507 is fitted into a main mold 607 having a structure to match, and then heated and hardened.

As shown in FIG. 18, the complete vehicle frame is assembled by inserting and joining fiber fabric composite structural members and fiber fabric composite joints; as shown in FIGS. 16 and 17, the carbon fiber composite The material joint 10 is provided with a pipe-shaped plug head 11, which is inserted into a plug socket corresponding to its pipe shape. As shown in the figure, a carbon fiber hook 12, which is a hook of a carbon fiber hook , is planted on the entire pipe-shaped side surface of the insertion head 11, and the installation direction of the carbon fiber hook 12 is set on the entire pipe-shaped side surface of the insertion head 11. The insert head shown in FIG. 16 is a plurality of circular tubes having the same outer diameter, and is inclined in the radial direction from the center of the pipe shape and backward with respect to the direction in which the head 11 is inserted into the plug socket; The insertion head shown in is a honeycomb-shaped pipe with a plurality of radial supports provided inside. A carbon fiber surface fastener hook, which is a hook of a carbon fiber surface fastener, is planted on the entire pipe-shaped side surface of the insertion head, and the direction in which the carbon fiber surface fastener hook 12 is installed is such that the insertion head 11 is inserted. By slanting it backwards and radially from the center of the pipe shape relative to the direction of insertion into the socket , it can be smoothly inserted into an insertion socket that has a hook-and-loop loop, which is a loop of carbon fiber hook-and-loop fastener, on the entire inner circumferential surface. When pulled out in the opposite direction, the carbon fiber hook and loop hook can be hooked onto the hook and loop fastener loop, which prevents the plug socket from falling off the plug head, allowing for a strong connection and ensuring a secure connection. No damage to the head or plug socket.

As shown in FIGS. 19 and 20, the support between the insertion heads on which the complete car frame is assembled by the insertion joint is a hollow stick-like support, and the carbon fiber hollow stick-like support shown in FIG. The carbon fiber hollow stick-shaped support shown in FIG. 20 is used to support the straight part, and the carbon fiber hollow stick-shaped support is used to support the curved part, and both ends of the carbon fiber hollow stick-shaped support have a closed structure and the center has a hollow structure; The hollow stick support is made of carbon fiber woven composite material. On the premise of guaranteeing structural strength, there is also material savings and weight reduction, as well as cost savings.

The complete vehicle frame is made up of an annular frame support made of a fiber fabric composite material, and the structural member of the annular frame support is a fiber fabric composite material structural member in which the inner support has a star-shaped support structure. It is. Each ring of the complete vehicle frame formed by surrounding the annular support body is constituted by a honeycomb structural member having a plurality of uniform support structures therein, thereby ensuring the mechanical strength of the complete vehicle frame.

The manufacturing method of a complete car frame manufactured by circular welding is as follows:
Step 1) of creating three-dimensional drawings of the required structural members;
step 2) of creating a support structure diagram of the complete vehicle frame based on the three-dimensional drawing and manufacturing the frame support (the support is used to support the fiber fabric prepreg and is a coil pipe or a braided tube); ,
Step 3) of separately determining the planar shape of each fiber-woven composite material used for support within the three-dimensional drawing structural member, based on its spatial shape;
Step 4) of cutting the fiber fabric composite material prepreg based on the planar shape of Step 3);
step 5) of determining sutures of the prepreg based on the three-dimensional drawing;
Step 6) of laminating the prepregs that require each layer according to the determined suture position;
Step 7) suturing the laminated prepregs according to the position of the suture thread (hand suturing or sewing machine suturing can be used);
Spread the sewn laminated prepreg sheets, align the honeycomb holes formed in the prepreg sheet with the skeleton support based on the three-dimensional drawing, cover the inside of the honeycomb holes with the prepreg sheet, and cover the outside of the skeleton support with the outer prepreg. Step 8) and
step 9) of coating the skeletal support with a tube wall prepreg to form a tube wall;
Step 10) of manufacturing a complete vehicle skeleton by sewing the skeleton support coated with the tube wall.
step 11) of heating and hardening the complete vehicle frame;
including.

In step 8), aligning the honeycomb holes with the skeletal support means inserting the skeletal support into the expanded laminated prepreg sheet according to the cavity position in the three-dimensional drawing structure, and then inserting the skeletal support into the layered prepreg sheet to cover the cavity. The joint is sutured and the skeletal support is covered within the cavity and serves to support the laminated prepreg.

A method for manufacturing a carbon fiber composite material joint provided with a carbon fiber hook-and-loop fastener hook , the method comprising:
Organic fibers are made into flame-retardant fibers through thermal oxidation stability treatment, and the fibers are carbonized at high temperatures, rendered infusible and non-combustible, and continue to maintain their fiber state, and then heated under high temperatures in an inert gas atmosphere. A step (1) of firing and carbonizing the organic fiber to lose some carbon and other non-carbon atoms to form a fibrous material containing carbon as a main component, that is, carbon fiber;
Step (2) of taking one water-soluble plastic tube and opening an oblique hole on the outer periphery of the water-soluble plastic tube;
a step (3) of implanting carbon fibers into the diagonal holes of the water-soluble plastic tube using a tufting machine;
a step (4) of fitting the main mold onto the water-soluble plastic tube;
adding a styrofoam mold between the main mold and the water-soluble plastic tube (5);
a step (6) of dissolving the water-soluble plastic tube in water and inserting the core;
A step (7) in which a cylindrical cavity is formed between the core and the Styrofoam mold, a light alloy is injected into the cylindrical cavity, and thermal decomposition and vaporization occur in the Styrofoam mold under the thermal action of the liquid metal. ,
After the liquid metal is cooled and hardened, the core is removed and a plug head with a carbon fiber hook and loop hook is formed (8);
including.

The honeycomb holes of all the composite honeycomb pipes are filled with sandwich structural material or fiber composite pipes or hollow supports. The sandwich structure material is mainly a rigid foam material, which can be rigid foamed polystyrene, and the rigid foam material is mainly PVC, PEI, PU, PET, PMI, AIREX, DIAB, 3A, STRUCELL, ROHACELL, rigid foamed material. Examples include metal materials; the fiber composite material pipe is a carbon fiber woven composite material pipe or a carbon fiber wound composite material pipe; the hollow support is a thin hollow plastic support or a thin hollow metal support; The thin walled hollow plastic support can be a blow molded article.

The hard foam material can support the walls of the honeycomb holes by being injected into the honeycomb holes and expanding.

Referring to FIGS. 25 to 28, the frame 100 of the carbon fiber composite structural member shown in FIG. 25 is assembled with a carbon fiber composite structural member ring 110. The material structural member ring 110 can be a monocyclic carbon fiber woven composite material structural member 111 as shown in FIG. , the outer surface of the annular rigid foam material 112 is wrapped with a carbon fiber woven composite material 113. The winding is performed by wrapping the outer surface of the rigid foam material 112 with the carbon fiber woven composite material 113 like an overwrapping machine; The annular rigid foam material 112 may be a monolithic structure or a bonded structure; the rigid foam material 112 may be made of rigid foamed polystyrene (e.g. polymethacrylimide (PMI)), rigid foamed metal (e.g. aluminum foam or other materials).

In the carbon fiber woven composite structural member, as shown in FIG. 3, the monocyclic carbon fiber woven composite structural member is in the form of a bundle, and the number of monocyclic carbon fiber woven composite structural members 111 in the bundle is at least With two pieces, the outer surface of one bundle of monocyclic carbon fiber woven composite material 27 structural member is wrapped with carbon fiber woven composite material 113 (not shown to show a bundled structure) to form a polycyclic carbon fiber woven fabric. Compose a composite material structural member. As shown in FIG. 27, a monocyclic carbon fiber fabric composite structural member 111 is filled and compacted into the inside of the carbon fiber fabric composite material wound around the outer surface of the polycyclic carbon fiber fabric composite structural member. A polycyclic carbon fiber woven composite material structural member 120 is constructed. Fill compaction leaves virtually no gaps between the internal monocyclic carbon fiber woven composite structural members. As shown in FIG. 28, a carbon fiber woven composite material 113 (not shown to show a bundle-like structure) wound around the outer surface of the polycyclic carbon fiber woven composite material structural member from the outside to the inside, a single ring The hollow polycyclic carbon fiber woven composite material structural member 113 and the hollow portion 131 constitute a hollow polycyclic carbon fiber woven composite material structural member 130 . The position of the cavity may be located at the axis of the hollow polycyclic carbon fiber fabric composite structural member 130 or may be offset from the axis of the hollow polycyclic carbon fiber fabric composite structural member 130.

In the carbon fiber woven composite material structural member, since the portion along the axis of the polycyclic carbon fiber woven composite material structural member is a hollow portion, the polycyclic carbon fiber woven composite material structural member is partially hollow. Configure. Cavity locations are reserved in the partially hollow polycyclic carbon fiber woven composite structural member to accommodate several components.

In the carbon fiber woven composite material frame manufactured by the carbon fiber woven composite material structural member, the monocyclic carbon fiber woven composite material structural member 111, the solid polycyclic carbon fiber woven composite material structural member 120, and the hollow polycyclic carbon fiber woven composite material structural member 120 are provided. The cyclic carbon fiber woven composite material structural member 130 and the partially hollow polycyclic carbon fiber woven composite material structural member are collectively referred to as the carbon fiber woven composite material structural member ring 110, and the carbon fiber woven composite material structural member The ring 110 is assembled as a frame, and the outer surface of the carbon fiber woven composite material structural member ring adjacently constituting the bundled part in the frame is made of a carbon fiber woven composite material (not shown because it shows a bundled structure). Wind. The monocyclic carbon fiber woven composite material structural member, the solid polycyclic carbon fiber woven composite material structural member, the hollow polycyclic carbon fiber woven composite material structural member, and partially the carbon fiber woven composite material frame body. The hollow polycyclic carbon fiber woven composite material structural member is at least one type, and may be a combination of different types.

The carbon fiber woven composite frame is a non-closed structure 140. In this case, cantilever structures may occur.

A method of manufacturing a frame using a carbon fiber woven composite material structural member, the method comprising:
Step (1) of creating a three-dimensional drawing of the frame;
Step (2) of disassembling the annular framework based on the framework in the three-dimensional drawing (including the monocyclic framework, and optionally the monocyclic framework subsequently included in the solid polycyclic framework, the hollow The monocyclic frame contained in the polycyclic frame, the monocyclic frame contained in the partially hollow polycyclic frame are collectively referred to as the "monocyclic frame," and
Step (3) of manufacturing a monocyclic rigid foam core frame based on the shape of each monocyclic frame (including a monocyclic rigid foam core frame if necessary, a solid polycyclic core frame if necessary) Monocyclic rigid foam core included in a hollow polycyclic rigid foam core, monocyclic rigid foam core included in a hollow polycyclic rigid foam core, partially hollow polycyclic rigid foam core further manufacturing a monocyclic rigid foam core frame included in the core frame);
Step (4) of wrapping the outer surface of each annular rigid foam core with continuous carbon fiber woven prepreg to form a composite structural member of monocyclic carbon fiber woven prepreg (if necessary, solid polycyclic carbon Composite material structural members of monocyclic carbon fiber fabric prepreg included in fiber fabric composite material structural members, composite material structural members and parts of monocyclic carbon fiber fabric prepreg included in hollow polycyclic carbon fiber fabric composite material structural members. a monocyclic carbon fiber woven prepreg composite structural member included in a hollow polycyclic carbon fiber woven composite structural member);
If necessary, the monocyclic carbon fiber woven prepreg composite structural member included in the solid polycyclic carbon fiber woven composite material structural member may be converted into a composite material structural member bundle of bare solid polycyclic carbon fiber woven prepreg. assembling and winding the outer surface of the bare solid polycyclic carbon fiber fabric prepreg composite material structural member bundle with continuous carbon fiber fabric prepreg to constitute a solid polycyclic carbon fiber fabric prepreg composite material structural member;
The composite material structural member of the monocyclic carbon fiber fabric prepreg included in the hollow polycyclic carbon fiber fabric composite structural member is assembled as a composite material structural member bundle of the bare solid polycyclic carbon fiber fabric prepreg, and the Wrapping the outer surface of the composite material structural member bundle of cyclic carbon fiber woven prepreg with continuous carbon fiber woven prepreg to constitute a composite material structural member of hollow polycyclic carbon fiber woven prepreg;
Bare composite structural member of monocyclic carbon fiber woven prepreg included in partially hollow polycyclic carbon fiber woven composite structural member Bundle of partially hollow polycyclic carbon fiber woven prepreg composite material structural member The outer surface of a composite structural member bundle of bare partially hollow polycyclic carbon fiber fabric prepreg is wrapped with continuous carbon fiber fabric prepreg to form a partially hollow hollow polycyclic carbon fiber fabric prepreg. Step (5) of configuring a composite material structural member;
Composite structural members of monocyclic carbon fiber woven prepreg, composite structural members of solid polycyclic carbon fiber woven prepreg, composite structural members of hollow polycyclic carbon fiber woven prepreg, partially hollow polycyclic The carbon fiber fabric prepreg is produced by assembling one or more of the composite material structural members of the carbon fiber fabric prepreg as a frame, and winding the outer surface of the frame adjacent to each other to form a bundled part. a step (6) of configuring a composite material frame of woven prepreg;
A step (7) in which a carbon fiber woven prepreg composite material frame is placed in a mold, heated and cured, and when released from the mold, becomes a carbon fiber woven composite material frame;
including.

In the method for manufacturing a frame using a carbon fiber woven composite material structural member, the carbon fiber woven composite material frame is a frame of an automobile, an aircraft, a train, and a container.

An automobile frame made of a carbon fiber woven composite material, as shown in FIGS. 29 and 30, the chassis 1001 of the automobile frame has a laminated fiber woven composite material sewn with suture threads that extends radially in a radial direction using the suture threads as supporting members. A star-shaped support structure formed to support a fiber-woven composite honeycomb pipe formed between the fiber-woven composite material of the star-shaped support; a carbon fiber-woven composite honeycomb pipe covered with a single helical-wound assembly member. In the single helical wound assembly member, the surface of the core material of the sandwich structure material is helically wound with a fiber woven composite material tape, and some of the previously wound fibers are wrapped with a later wrapped fiber woven composite material tape. Tightly tighten the textile composite material tape; the vehicle body frame 1002 has a textile composite material honeycomb pipe that closely contacts at least two single helical-wound assembly members to form a helical-wound assembly bundle, and the helical tape in the helical-wound assembly member bundle. The wound fiber fabric composite material tape constitutes a helically wound fiber fabric composite material honeycomb pipe; The vehicle body frame is placed on a chassis frame and connected with an elastic member to form a separate frame made of carbon fiber fabric composite material; the chassis and vehicle body frame become one separate frame made of carbon fiber fabric composite material of a single unit structure. The technical features in the above technical solution can also be applied to the present technical solution if necessary.

Claims (2)

The carbon fiber composite material plug head includes a carbon fiber composite material joint 10 and a pipe-shaped plug head 11 provided on the joint 10 , and the plug head 11 has a corresponding pipe-shaped plug head. The structure is configured to be inserted into a socket containing a
A carbon fiber hook 12, which is a hook of a carbon fiber hook, is planted on the pipe-shaped side surface of the insertion head 11, and the installation direction of the carbon fiber hook 12 is such that the insertion head 11 is A carbon fiber composite material plug-in head that is inclined rearward and radially from the pipe-shaped center with respect to the direction of insertion into the plug-in socket . A carbon fiber surface fastener hook 12, which is a hook of a carbon fiber surface fastener, is planted on the entire pipe-shaped side surface of the insertion head 11, and the installation direction of the carbon fiber surface fastener hook 12 is set in the same direction as that of the insertion head 11. By tilting radially from the pipe-shaped center backward with respect to the direction of insertion into the plug socket, the plug socket has a hook-and-loop fastener loop , which is a loop of carbon fiber hook-and-loop fastener, on the entire inner peripheral surface. When inserting the insertion head 11, the carbon fiber hook and loop fastener does not catch, but when pulling out in the opposite direction, the carbon fiber hook and loop hook hooks on the hook and loop fastener , and the insertion socket is inserted. The carbon fiber composite material plug head according to claim 1, characterized in that it can be firmly joined by preventing it from falling off from the head, and prevents damage to the plug head and the plug socket.

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