Molded fixing tool and method for a launch tube with a guide rail

Abstract

The application discloses a forming tool for integrally forming and fixing a launching cylinder with a guide rail, which comprises a first half-circular structure and a second half-circular structure that can be fixed to each other, wherein the first half-circular structure and the second half-circular structure are combined to have a circular inner cavity, the size of the circular inner cavity is matched with the shape of a columnar winding core mold, a groove is formed on the outer surface of the columnar winding core mold, a guide rail mounting groove is arranged at the groove in the inner cavity of the first half-circular structure and / or the second half-circular structure, and a locking structure is further arranged on the first half-circular structure and / or the second half-circular structure and used for fixing the guide rail in the groove. The application further provides a forming method of the launching cylinder with the guide rail. The forming tool and the forming method solve the positioning and locking problems of the guide rail on the columnar winding core mold, and have the effects of high efficiency, high positioning precision, good product quality, excellent performance and the like.

Description

TECHNICAL FIELD

[0001] The present application belongs to the field of missile launching device, and particularly relates to a forming tool for a launching barrel and a forming method of the launching barrel. BACKGROUND

[0002] Composite material launching barrels are widely used due to their excellent performance of light weight and high strength. There are two main forming methods for the composite material launching barrel with guide rails: the first method is to form the guide rail and the barrel body respectively, and then to install the guide rail on the inner wall of the barrel body by mechanical connection; the second method is to integrally form the guide rail and the barrel body. For a launching barrel with a very long length and a small diameter, the installation and positioning of the guide rail are very difficult when the first method is used, and the production efficiency is low. In addition, screw holes need to be opened on the composite material barrel, which will reduce the strength and sealing performance of the barrel. In comparison, the method of integrally forming the guide rail and the barrel body does not need to open holes on the barrel, does not affect the performance of the barrel, and can reduce the weight of the barrel due to the absence of bolt connection, and can reduce the processing procedures and the operation difficulty, and is a high-efficiency forming method.

[0003] Although the integrally forming method of the composite material launching barrel has obvious advantages, there are still some problems in the forming process, such as the initial fixation of the guide rail and the core mold when the barrel is wound. The common solution to this problem is to manually lay up a layer on the first guide rail, fix the guide rail on the core mold by curing the layer (or paste the pre-impregnated material guide rail on the core mold), and then fix each guide rail in turn. After all the guide rails are fixed, the core mold is wound on the machine to form the barrel. In this method, the curing (or pre-impregnated material pasting) of each guide rail needs to be carried out in turn, and cannot be completed at the same time. The curing of each guide rail takes several hours, and the total curing time of this process is equal to the number of guide rails multiplied by the curing time. Therefore, this manual lay-up (or pre-impregnated material pasting) solution is not only complicated, but also low in forming efficiency of the barrel. Moreover, due to the characteristics of the manual lay-up process, it is difficult to ensure the process quality, and manual lay-up of the guide rail may also need to extend the layer to the outer surface of the core mold to ensure that the cured guide rail does not fall off the core mold. This operation will result in defects or joints (joints between adjacent extended layers) on the wall surface of the formed barrel. The pre-impregnated material pasting process also has quality problems, such as porosity.

[0004] Therefore, it is necessary to provide an efficient forming tool and forming method for the initial fixation of the guide rail and the core mold when the barrel is wound and the forming quality of the launching barrel. SUMMARY

[0005] The technical problems to be solved by the present application are to overcome the deficiencies and defects mentioned in the above background art, and to provide a molding tool for integrally molding and fixing a launch tube with guide rails, which has high molding efficiency and good quality of the launch tube, and a molding method for molding the launch tube with guide rails by using the molding tool.

[0006] The molding tool for integrally molding and fixing a launch tube with guide rails comprises a first half-circular structure and a second half-circular structure that can be fixed to each other, wherein the first half-circular structure and the second half-circular structure have a circular inner cavity after being combined, the size of the circular inner cavity matches the shape of a cylindrical winding core mold used for molding the launch tube (so that the circular inner cavity can closely fit the circular surface of the cylindrical winding core mold), the outer surface of the cylindrical winding core mold is provided with a groove for installing the guide rail, and the inner cavity of the first half-circular structure and / or the second half-circular structure is correspondingly provided with an inwardly recessed guide rail installation groove at the groove, which facilitates the installation of the guide rail into the groove, and the first half-circular structure and / or the second half-circular structure is further provided with a locking structure for fixing the guide rail in the groove.

[0007] In the present application, the installation and adjustment of the guide rail are facilitated by providing the guide rail installation groove. If the guide rail installation groove is not provided, when the molding tool is sleeved on the outer surface of the cylindrical winding core mold, the molding tool closely fits the outer surface of the cylindrical winding core mold, and since the size of the guide rail matches the size of the groove on the outer surface of the cylindrical winding core mold, and there may be a manufacturing tolerance of the guide rail, it may be difficult to directly install the guide rail, and the guide rail cannot be adjusted. By providing the guide rail installation groove, a larger space is left for the installation of the guide rail, which facilitates the installation and position adjustment of the guide rail. Then, by using the locking structure, the guide rail can be fixed. The locking structure of the present application tightly presses the guide rail, has strong pressing force on the guide rail, can adjust the position of the guide rail, and more stably fixes the guide rail, so that the position adjustment of the guide rail is more convenient.

[0008] The main materials of the launch tube and the guide rail in the present application are resin-based composite materials, and the number of guide rails is determined according to actual needs. Correspondingly, the number and shape of the grooves provided on the outer surface of the cylindrical winding core mold correspond to the number and shape of the guide rails, respectively.

[0009] In the above molding tool, preferably, the locking structure comprises a fixing bolt, the first half-circular structure and / or the second half-circular structure for providing the locking structure is provided with a through hole at the guide rail installation groove, which matches the fixing bolt, and the fixing bolt can move up and down in the through hole so that the end portion thereof abuts against the surface of the guide rail to achieve the fixation of the guide rail. By moving the fixing bolt up and down in the through hole, the locking mechanism can be in a locked or unlocked state.

[0010] Preferably, the fixing bolt is provided with a protective sleeve near the end of the guide rail to prevent the fixing bolt from damaging the surface of the guide rail. The protective sleeve can be a plastic sleeve, and a hole can be formed in the end of the fixing bolt. The plastic sleeve is provided with a hole, and the plastic sleeve is installed on the end of the fixing bolt by a pin to protect the surface of the guide rail and prevent the fixing bolt from directly contacting the guide rail to affect the surface of the guide rail.

[0011] Preferably, the width of the guide rail installation groove is greater than the width of the guide rail. The width of the guide rail installation groove is greater than the width of the guide rail, which can more conveniently realize the installation and position adjustment of the guide rail.

[0012] Preferably, the number of the guide rail installation grooves and the locking structures on each forming tool corresponds to the number of the guide rails on the columnar winding core mold, and the setting positions of the guide rail installation grooves and the locking structures on each forming tool correspond to the setting positions of the guide rails on the columnar winding core mold. The above setting can ensure the fixing effect of the locking structures of the forming tool on the guide rails. Preferably, the guide rails are provided with four guide rails, and the first semicircular structure and the second semicircular structure are respectively provided with two locking structures and guide rail installation grooves.

[0013] Preferably, one end of the first semicircular structure and the second semicircular structure is hingedly connected to each other, and the other end is connected through a buckle structure. The first semicircular structure and the second semicircular structure at the hinge can rotate relative to each other, and the buckle structure at the other end can realize the buckling and opening of the first semicircular structure and the second semicircular structure.

[0014] Preferably, the buckle structure comprises a first clamping pin, a second clamping pin, a buckle, and a clamping shaft. One end of the clamping shaft is movably arranged on the first semicircular structure through the first clamping pin, the other end of the clamping shaft is movably arranged on the buckle through the second clamping pin, and the buckle is movably arranged on the second semicircular structure.

[0015] As a general technical concept, the application also provides a forming method for forming a launch tube with guide rails by using the above forming tool, which comprises the following steps:

[0016] S1: According to the internal structure of the launch tube, a columnar winding core mold with a groove on the surface is made, and the shape of the columnar winding core mold matches the shape of the inner cavity of the launch tube with guide rails. A release agent is applied to the surface of the columnar winding core mold.

[0017] S2: Preparing a guide rail;

[0018] S3: uniformly segmenting the plurality of forming tools on the surface of the columnar winding core mold, and mutually fixing and closing the first half-circle structure and the second half-circle structure, so that the locking structure is in an unlocked state;

[0019] S4: inserting the guide rail from the end of the columnar winding core mold, and adjusting the locking mechanism to fix the guide rail in the groove on the outer surface of the columnar winding core mold, i.e. realizing the fixation of the guide rail and the columnar winding core mold;

[0020] S5: loading the columnar winding core mold to a winding device, winding resin-impregnated fiber yarn, curing, demolding, i.e. completing the forming of the launch can with the guide rail.

[0021] In the forming method, preferably, the winding starts from the end surface of the columnar winding core mold, when winding approaches the forming tool, the forming tool is removed and the winding continues backward until the winding on the surface of the columnar winding core mold is completed.

[0022] In the forming method, preferably, the guide rail is prepared by a pultrusion forming process, and the main material of the guide rail is a fiber reinforced resin-based composite material (such as fiber reinforced epoxy resin); and the main material of the launch can is a fiber reinforced resin-based composite material.

[0023] In the present application, the guide rail and the main material of the launch can are the same, by winding the resin-impregnated fiber yarn (which has adhesion to the guide rail) on the surface of the guide rail, the obtained can body is bonded to the guide rail as a whole after the resin is cured, and the gluing operation is not needed.

[0024] The guide rail and the composite material launch barrel body are separately formed in the prior art, and the guide rail is installed by mechanical connection and needs to be opened on the barrel body, which seriously affects the strength and performance of the barrel body, and the installation of the guide rail is difficult, the guide rail and the barrel body are integrally formed by the process of the application, the synchronous bonding of the guide rail is realized when the launch barrel body is formed, the guide rail is formed by the pultrusion process, the barrel body is formed by the winding process, and the two are bonded by the resin of the barrel body without damaging the composite material barrel body, the guide rail and the barrel body are not connected by bolts, the interface performance is good, the integrity is good, and the product performance is good.

[0025] Compared with the prior art, the application has the advantages that:

[0026] 1、The forming tool and the forming method of the application solve the positioning and locking of the guide rail on the columnar winding core mold through the cooperation of the guide rail installation groove and the locking structure, and the scheme has the effects of high efficiency, high positioning accuracy, good product quality and excellent performance compared with the traditional curing positioning scheme.

[0027] 2、The forming tool and the forming method of the application have high fixing accuracy, good stability and convenient disassembly for the guide rail, and obviously reduce the time and difficulty of fixing the guide rail.

[0028] 3、The launch barrel with the guide rail obtained by the forming tool and the forming method of the application is integrally formed with the guide rail and the launch barrel body, is not connected by bolts, has good integrity, and reduces the weight of the launch barrel. BRIEF DESCRIPTION OF DRAWINGS

[0029] In order to more clearly illustrate the technical solutions in the embodiments of the application or the prior art, the following will briefly introduce the drawings needed to be used in the embodiments or the prior art description. Obviously, the drawings in the following description are some embodiments of the application, and those skilled in the art can obtain other drawings according to these drawings without creative labor.

[0030] Figure 1Structure diagram of the columnar winding core mold in the embodiment.

[0031] Figure 2 Structure diagram of the guide rail in the embodiment.

[0032] Figure 3 Structure diagram of the combination of the guide rail and the columnar winding core mold in the embodiment.

[0033] Figure 4 Three-dimensional structure diagram of the forming tool in the embodiment.

[0034] Figure 5 Structure diagram of the forming tool in the embodiment when in the locked state.

[0035] Figure 6 Structure diagram of the forming tool in the embodiment when in the unlocked state.

[0036] Figure 7 Structure diagram of the fixing bolt in the embodiment (disassembled state).

[0037] Figure 8 Structure diagram of the forming tool in the embodiment when installed on the columnar winding core mold (without the guide rail, and the locking mechanism is not locked).

[0038] Figure 9 Side view of Figure 8 .

[0039] Figure 10 Structure diagram of the forming tool in the embodiment when installed on the columnar winding core mold and then installed with the guide rail (the locking mechanism is not locked).

[0040] Figure 11 Structure diagram of the forming tool in the embodiment when installed on the columnar winding core mold (with the guide rail, and the locking mechanism is locked).

[0041] Figure 12 Side view of Figure 11 .

[0042] Figure 13 Structure diagram of the winding equipment in the embodiment when winding on the columnar winding core mold.

[0043] Legend:

[0044] 1, first semicircular structure; 2, second semicircular structure; 3, columnar winding core mold; 31, groove; 4, guide rail; 5, guide rail installation groove; 6, fixing bolt; 7, pin; 8, protective sleeve; 9, first latch; 10, second latch; 11, buckle; 12, clamping shaft. DETAILED DESCRIPTION

[0045] To facilitate understanding of the present invention, the present invention will be described more fully and in detail below with reference to the accompanying drawings and preferred embodiments, but the scope of protection of the present invention is not limited to the following specific embodiments.

[0046] Unless otherwise defined, all technical terms used herein have the same meaning as commonly understood by those skilled in the art. The technical terms used herein are for the purpose of describing particular embodiments only and are not intended to limit the scope of the invention.

[0047] Unless otherwise specified, all raw materials, reagents, instruments and equipment used in this invention can be purchased from the market or prepared by existing methods.

[0048] Example:

[0049] like Figures 1-6 As shown, the integral molding fixture for fixing the launch tube with guide rail in this embodiment includes a first semicircular structure 1 and a second semicircular structure 2 that can be fixedly connected to each other. The first semicircular structure 1 and the second semicircular structure 2 have a circular inner cavity after being combined. The size of the circular inner cavity matches the shape of the columnar winding core mold 3 used for molding the launch tube. The outer surface of the columnar winding core mold 3 is provided with a groove 31 for mounting the guide rail 4. The inner cavity of the first semicircular structure 1 and / or the second semicircular structure 2 is provided with an inwardly recessed guide rail mounting groove 5 at the groove 31 to facilitate the mounting of the guide rail 4 into the groove 31. The first semicircular structure 1 and / or the second semicircular structure 2 are also provided with a locking structure for fixing the guide rail 4 in the groove 31.

[0050] In this embodiment, the locking structure includes a fixing bolt 6. The first semicircular structure 1 and / or the second semicircular structure 2 used to set the locking structure have through holes in the guide rail mounting groove 5 for matching the fixing bolt 6. The fixing bolt 6 can move up and down along the through hole so that its end abuts against the surface of the guide rail 4 to fix the guide rail 4.

[0051] like Figure 7 As shown, in this embodiment, a protective sleeve 8 is provided at the end of the fixing bolt 6 near the guide rail 4 to prevent the fixing bolt 6 from damaging the surface of the guide rail 4. Specifically, in this embodiment, the protective sleeve 8 can be made of plastic. A hole can be made in the end of the fixing bolt 6, and a hole can be made in the plastic sleeve. A pin 7 is used to install the plastic sleeve on the end of the fixing bolt 6.

[0052] In this embodiment, the width of the guide rail mounting groove 5 is greater than the width of the guide rail 4.

[0053] The number of the guide rail installation grooves 5 and the locking structures on each forming tool corresponds to the number of the guide rails 4 on the columnar winding core mold 3, and the setting positions of the guide rail installation grooves 5 and the locking structures on each forming tool correspond to the setting positions of the guide rails 4 on the columnar winding core mold 3. In the embodiment, the number of the guide rails 4 is not limited, for example, as shown in FIG. 1, the number of the guide rails 4 is 4, and the number of the guide rail installation grooves 5 and the locking structures is also 4. Figure 3

[0054] In the embodiment, one end of the first semicircular structure 1 and the second semicircular structure 2 is hingedly connected to each other, and the other end is connected through a buckle structure. Specifically, as shown in FIG. 2, the buckle structure includes a first clamping pin 9, a second clamping pin 10, a buckle 11, and a clamping shaft 12 (which can be a hexagonal bolt), one end of the clamping shaft 12 is movably arranged on the first semicircular structure 1 through the first clamping pin 9, the other end of the clamping shaft 12 is movably arranged on the buckle 11 through the second clamping pin 10, and the buckle 11 is movably arranged on the second semicircular structure 2. Figures 4-6

[0055] As shown in FIG. 3, the forming method of the launching cylinder with guide rails in the embodiment is formed by using the above forming tool, which includes the following steps: Figures 8-13

[0056] S1: According to the internal structure of the launching cylinder, a columnar winding core mold 3 with a groove 31 on the surface is made, the shape of the columnar winding core mold 3 matches the shape of the inner cavity of the launching cylinder with guide rails, and a release agent is applied to the surface of the columnar winding core mold 3.

[0057] S2: The guide rails 4 are prepared.

[0058] S3: The plurality of forming tools are evenly segmented and sleeved on the surface of the columnar winding core mold 3, and the first semicircular structure 1 and the second semicircular structure 2 are fixedly connected to each other to close, so that the locking structure is in an unlocked state.

[0059] S4: The guide rails 4 are inserted from the end of the columnar winding core mold 3, and the locking mechanism is adjusted to fix the guide rails 4 in the groove 31 on the outer surface of the columnar winding core mold 3, that is, the fixation of the guide rails 4 and the columnar winding core mold 3 is realized.

[0060] S5: The columnar winding core mold 3 is loaded onto a winding device, and then resin-soaked fiber yarns are wound, cured, and demolded, that is, the forming of the launching cylinder with guide rails is completed.

[0061] In the embodiment, the winding starts from the end surface of the columnar winding core mold 3, when the winding approaches the forming tool, the forming tool is removed and the winding continues backward until the winding on the surface of the columnar winding core mold 3 is completed.

[0062] ​​​In this embodiment, the guide rail 4 is prepared by pultrusion process, and the main material of the guide rail 4 is fiber reinforced resin-based composite material; the main material of the launch tube is fiber reinforced resin-based composite material.

[0063] In order to better understand the forming tool and the forming method in this embodiment, a typical forming method is also provided in this embodiment, which includes the following steps:

[0064] First step: according to the internal structure of the launch tube, a cylindrical winding core mold 3 with grooves 31 on the surface is made, the shape of the cylindrical winding core mold 3 matches the shape of the inner cavity of the launch tube with guide rails (as shown in Figure 1 The grooves are uniformly distributed on the circumference.

[0065] Second step: the guide rail 4 is prepared by pultrusion process, a typical guide rail 4 is made of fiber reinforced epoxy resin composite material, and the size of the guide rail 4 is determined according to the size of the groove 31 (as shown in Figure 2 ).

[0066] Third step: the release agent is applied on the surface of the cylindrical winding core mold 3.

[0067] Fourth step: the guide rail 4 is installed into the groove 31 of the cylindrical winding core mold 3, and the assembly relationship between the guide rail 4 and the cylindrical winding core mold 3 is as shown in Figure 3 .

[0068] Fifth step: the forming tool is prepared. According to the positioning relationship between the guide rail 4 and the cylindrical winding core mold 3, a forming tool is designed and made for positioning and clamping the guide rail 4 on the cylindrical winding core mold 3. As shown in Figures 4-6 , the forming tool is composed of two semicircular structures, one side of the two semicircular structures is hinged, and the other side is connected by a buckle, and the loosening and locking of the forming tool are realized by opening and closing the buckle. When the buckle is locked, a complete circular structure is formed, which is in close contact with the circular surface of the cylindrical winding core mold 3. The buckle structure includes a first pin 9, a second pin 10, a buckle 11 and a shaft 12 (which can be an internal hexagonal bolt). One end of the shaft 12 is movably arranged on the first semicircular structure 1 through the first pin 9, and the other end of the shaft 12 is movably arranged on the buckle 11 through the second pin 10. The buckle 11 is movably arranged on the second semicircular structure 2. The first pin 9 is connected with the internal hexagonal bolt, and the second pin 10 is connected with the buckle 11. When the buckle 11 is turned upward, the second pin 10 pushes the internal hexagonal bolt upward, the mechanism is loosened, and the unlocking state is reached. At this time, the forming tool can be removed from the cylindrical winding core mold 3; when the buckle 11 is turned downward, the second pin 10 presses the internal hexagonal bolt downward, and the mechanism is locked. As shown in Figure 7As shown, the forming tool is also provided with a locking mechanism for fixing the guide rail, which is composed of a fixing bolt 6, a plastic sleeve and a pin 7. The plastic sleeve is installed at the bottom of the fixing bolt 6 and connected by the pin 7. The plastic sleeve serves to protect the contact surface of the guide rail 4 from damage. In use, the forming tool is installed on the cylindrical winding core mold 3, and the locking mechanism is aligned with the guide rail 4. The fixing bolt 6 is tightened to fix the guide rail 4.

[0069] Step 6: Fix the guide rail 4 to the cylindrical winding core mold 3 using 3 forming tools. As shown in Figures 8-10 , the guide rail 4 is installed into the groove 31 of the cylindrical winding core mold 3, as shown in Figures 11-12 , the assembled guide rail 4 and the cylindrical winding core mold 3 are locked by the locking mechanism of the forming tool, and the fixing bolt 6 is used to fix the guide rail 4. The specific operation can be as follows: the forming tool is installed on the cylindrical winding core mold 3 according to the relative position relationship between the locking mechanism and the groove 31, and is turned down to buckle and lock the forming tool. The fixing bolt 6 is pushed to the non-locking position. Each time, one guide rail 4 is inserted into the groove from the side. Finally, the fixing bolt 6 is locked until all the guide rails 4 are installed and fixed.

[0070] Step 7: Load the cylindrical winding core mold 3 onto the winding equipment. According to the structural design requirements, the fiber yarn soaked with resin is used to wrap the launch cylinder body (as shown in Figure 13 ), and the winding machine drives the overall mechanism of the cylindrical winding core mold 3 to rotate at an angular velocity ω. When the fiber yarn is about to complete the winding to cover the area A, the forming tool between the area A and the area B is removed, and the winding continues. When the winding is about to complete the coverage of the area B, the forming tool between the area B and the area C is removed, and the winding continues. When the winding is about to complete the coverage of the area C, the last forming tool is removed, and the winding is finally completed.

[0071] Step 8: Curing and demolding, i.e. completing the integrated molding of the launch cylinder with guide rails.

[0072] After comparison, the forming method in the embodiment has the following specific effect compared with the traditional hand lay-up process, as shown in Table 1.

[0073] Table 1: Comparison between the traditional hand lay-up process and the integrated molding method of the forming tool in the embodiment

[0074]

Claims

1. An integrated molding tool for molding a fixed band guide of a launching tube, characterized by comprising: The application relates to a forming tool for a cylindrical winding core mold (3) of a launch tube, which comprises a first half-circular structure (1) and a second half-circular structure (2) capable of being fixed to each other, wherein the first half-circular structure (1) and the second half-circular structure (2) are combined to have a circular inner cavity which is matched with the shape of the cylindrical winding core mold (3) for forming the launch tube, a groove (31) for arranging a guide rail (4) is arranged on the outer surface of the cylindrical winding core mold (3), an inwardly recessed guide rail arranging groove (5) which is convenient for arranging the guide rail (4) into the groove (31) is arranged at the groove (31) of the inner cavity of the first half-circular structure (1) and / or the second half-circular structure (2), and a locking structure for fixing the guide rail (4) in the groove (31) is further arranged on the first half-circular structure (1) and / or the second half-circular structure (2). The locking structure comprises a fixing bolt (6), the first half-circular structure (1) and / or the second half-circular structure (2) for arranging the locking structure is provided with a through hole which is matched with the fixing bolt (6) at the guide rail arranging groove (5), and the fixing bolt (6) is moved up and down along the through hole so that the end of the fixing bolt (6) is abutted against the surface of the guide rail (4) to realize the fixation of the guide rail (4).

2. The forming tool of claim 1, wherein The fixing bolt (6) is provided with a protective sleeve (8) which is close to the end of the guide rail (4) and is used for preventing the fixing bolt (6) from damaging the surface of the guide rail (4).

3. A forming tool according to claim 1 or 2, characterised in that The number of the guide rail arranging grooves (5) and the locking structures on each forming tool is corresponding to the number of the guide rails (4) on the cylindrical winding core mold (3), and the arrangement positions of the guide rail arranging grooves (5) and the locking structures on each forming tool are corresponding to the arrangement positions of the guide rails (4) on the cylindrical winding core mold (3).

4. The forming tool of claim 1 or 2, wherein One end of the first half-circular structure (1) and the second half-circular structure (2) is hingedly connected to each other, and the other end is connected through a buckle structure.

5. The forming tool of claim 4, wherein The buckle structure comprises a first clamping pin (9), a second clamping pin (10), a buckle (11) and a clamping shaft (12), one end of the clamping shaft (12) is movably arranged on the first half-circular structure (1) through the first clamping pin (9), the other end of the clamping shaft (12) is movably arranged on the buckle (11) through the second clamping pin (10), and the buckle (11) is movably arranged on the second half-circular structure (2).

6. A molding method for molding a launch can with a rail using the molding tool according to any one of claims 1 to 5, characterized by, The application further discloses a method for manufacturing the cylindrical winding core mold (3) of the launch tube, which comprises the following steps: S1, preparing the cylindrical winding core mold (3) with the groove (31) on the surface according to the internal structure of the launch tube, wherein the shape of the cylindrical winding core mold (3) is matched with the shape of the inner cavity of the launch tube with the guide rail; and coating release agent on the surface of the cylindrical winding core mold (3); S2, preparing the guide rail (4); S3, uniformly segmenting and arranging a plurality of the forming tools on the surface of the cylindrical winding core mold (3), and fixedly connecting the first half-circular structure (1) and the second half-circular structure (2) to each other to be closed, so that the locking structure is in an unlocked state. S4: inserting the guide rail (4) from the end of the columnar winding core mold (3), and adjusting the locking structure to fix the guide rail (4) in the groove (31) on the outer surface of the columnar winding core mold (3), i.e. to realize the fixation of the guide rail (4) and the columnar winding core mold (3); S5: loading the columnar winding core mold (3) to a winding device, winding resin-soaked fiber yarn, curing, demolding, i.e. completing the molding of the guide rail-equipped launch canister.

7. The molding method according to claim 6, characterized by During winding, the winding starts from the end surface of the columnar winding core mold (3), when winding approaches the molding tool, the molding tool is removed and the winding continues backward until the winding on the surface of the columnar winding core mold (3) is completed.

8. The forming method according to claim 6 or 7, characterized in that The guide rail (4) is prepared by using a pultrusion molding process, and the main material of the guide rail (4) is a fiber-reinforced resin-based composite material; the main material of the launch canister is a fiber-reinforced resin-based composite material.

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