Composite material launch canister formed by winding

Abstract

The utility model discloses a composite material launch canister formed by winding in the technical field of launch canisters, which comprises a canister body, a guide rail is arranged on the inner wall of the canister body, flange plates are arranged at the two ends of the canister body, two bearing sleeves are embedded between the inner wall and the outer wall of the canister body, the number of the bearing sleeves is two, and the number of the bearing sleeves is two. A first supporting lug and a second supporting lug are arranged on the outer surfaces of the two bearing sleeves correspondingly. Through the arrangement of the bearing sleeve, the first support lug and the second support lug, in the production process of the barrel, after the barrel is wound to produce a certain diameter size, a worker can sleeve the bearing sleeve on the outer surface of the barrel, and then the winding work is continued, so that the bearing sleeve is wrapped and embedded between the inner wall and the outer wall of the barrel; and the bearing sleeve is arranged, and the first supporting lug and the second supporting lug are arranged on the outer surface of the bearing sleeve, so that after production is completed, the overall structural strength of the barrel can be improved through the bearing sleeve, the first supporting lug and the second supporting lug, and then the bearing performance of the barrel is improved.

Description

Technical Field

[0001] The utility model relates to the technical field of launch tubes, in particular to a launch tube made of a winding-molded composite material. Background Art

[0002] Composite launch tubes are widely used due to their lightweight and high-quality properties. They are usually solidified and formed using large autoclaves. The existing launch tube winding molding method adopts a process scheme in which mold grooving and the guide rail and the cylinder structure layer are integrally formed. The mold is used to ensure the dimensional accuracy of the guide rail, and the winding line shape is adjusted during production to ensure product quality. The launch tube uses fiber-reinforced composite materials, which can effectively solve the problems of heavy weight, welding deformation, and easy rust of metal structure cylinders.

[0003] However, there are some problems with the existing technology: although the existing winding-molded composite launch tube has the characteristics of lightweight and structural integration, in actual use, since the launch tube needs to withstand large loads and impact forces, and the existing composite launch tube has no load-bearing structure inside the integration, it is difficult to withstand large loads for a long time. Therefore, we propose a winding-molded composite launch tube. Utility Model Content

[0004] In view of the deficiencies in the prior art, the utility model provides a composite material launching tube formed by winding.

[0005] The purpose of the present utility model is achieved as follows: a winding-molded composite material launch tube, comprising a tube body, the inner wall of the tube body is provided with a guide rail, both ends of the tube body are provided with flanges, a bearing sleeve is buried between the inner and outer walls of the tube body, the number of the bearing sleeves is two, and the outer surfaces of the two bearing sleeves are respectively provided with a first support ear and a second support ear.

[0006] Optionally, both ends of the cylinder are fixedly sleeved with connecting sleeves, and the flange is fixedly mounted on the connecting sleeves.

[0007] Optionally, a guide bar is fixedly mounted on the outer surface of the bearing sleeve on the right side, and a through hole is opened on the guide bar.

[0008] Optionally, the inner wall of the cylinder is fixedly mounted with reinforcing ribs located on both sides of the guide rail, and the outer surfaces of the reinforcing ribs are fixedly fitted on the guide rail.

[0009] Optionally, the number of the first supporting ears is four, and the four first supporting ears are evenly and circumferentially mounted on the outer surface of the bearing sleeve.

[0010] Optionally, there are four guide rails, and the cross-section of the guide rails is trapezoidal.

[0011] Compared with the prior art, the beneficial effects of the present invention are:

[0012] The utility model provides a bearing sleeve, a first support ear and a second support ear. During the production process of the cylinder, after the cylinder is wound to produce a certain diameter, the worker can sleeve the bearing sleeve on the outer surface of the cylinder and continue the winding work, so that the bearing sleeve is wrapped and buried between the inner and outer walls of the cylinder, and the first support ear and the second support ear are provided on the outer surface of the bearing sleeve. Therefore, after the production is completed, the bearing sleeve, the first support ear and the second support ear can improve the overall structural strength of the cylinder, thereby increasing the bearing capacity of the cylinder. BRIEF DESCRIPTION OF THE DRAWINGS

[0013] In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the following briefly introduces the drawings required for use in the embodiments or the description of the prior art. Obviously, the drawings described below are merely embodiments of the present invention. For ordinary technicians in this field, other drawings can be obtained based on the provided drawings without paying any creative work.

[0014] Figure 1 It is a structural diagram provided by the utility model;

[0015] Figure 2 This is a front structural diagram provided by the utility model;

[0016] Figure 3 This is a schematic diagram of the installation structure of the second lug provided by the utility model;

[0017] Figure 4 This is a schematic diagram of the installation structure of the first lug provided by the utility model;

[0018] Figure 5 This is a structural diagram of the bearing sleeve provided by the utility model;

[0019] Figure 6 yes Figure 2 Schematic diagram of the locally enlarged structure at point A in the middle.

[0020] In the figure: 1. Cylinder; 2. Guide rail; 3. Flange; 4. Bearing sleeve; 5. First lug; 6. Second lug; 7. Connecting sleeve; 8. Guide strip; 9. Reinforcing rib. DETAILED DESCRIPTION

[0021] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the embodiments described are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without making creative efforts are within the scope of protection of the present invention.

[0022] like Figures 1 to 6 As shown, an embodiment of the present invention provides a wound composite material launch tube, comprising a tube body 1, an inner wall of the tube body 1 is provided with a guide rail 2, flanges 3 are provided at both ends of the tube body 1, a bearing sleeve 4 is buried between the inner and outer walls of the tube body 1, and the number of the bearing sleeves 4 is two, and the outer surfaces of the two bearing sleeves 4 are respectively provided with a first support ear 5 and a second support ear 6.

[0023] Furthermore, both ends of the cylinder 1 are fixedly sleeved with connecting sleeves 7 , and the flange 3 is fixedly installed on the connecting sleeves 7 .

[0024] The flange 3 serves as a connecting piece to firmly connect the two ends of the cylinder 1 with other components, thereby enhancing the overall structural stability.

[0025] Furthermore, a guide bar 8 is fixedly mounted on the outer surface of the right bearing sleeve 4 , and a through hole is formed on the guide bar 8 .

[0026] The design of the guide strip 8 can facilitate the stable positioning of the barrel 1 on the launch stand through the connecting piece, preventing the barrel 1 from deflecting during the launch process.

[0027] Furthermore, reinforcing ribs 9 located on both sides of the guide rail 2 are fixedly mounted on the inner wall of the cylinder 1 , and the outer surfaces of the reinforcing ribs 9 are fixedly attached to the guide rail 2 .

[0028] By designing the reinforcing ribs 9, the structural strength of the guide rail 2 can be improved, so that it can withstand greater loads and impact forces during missile launch, thereby increasing its service life.

[0029] Furthermore, the number of the first ears 5 is four, and the four first ears 5 are evenly mounted around the outer surface of the bearing sleeve 4 .

[0030] Furthermore, there are four guide rails 2 , and the cross section of the guide rails 2 is trapezoidal.

[0031] The guide rail 2 with a trapezoidal cross-section can more evenly disperse the load generated by the missile during the launch process. This design helps to reduce stress concentration and prevent structural damage caused by local overload. By distributing the load over a larger area, the guide rail 2 with a trapezoidal cross-section can significantly improve the structural stability and durability of the cylinder 1. In addition, this design can also extend the service life of the cylinder 1 and reduce the frequency of maintenance and replacement.

[0032] The working principle and use process of this utility model:

[0033] During the production process of the cylinder 1, after the cylinder 1 is wound to produce a certain diameter size, the staff can sleeve the bearing sleeve 4 on the outer surface of the cylinder 1 and continue the winding work so that the bearing sleeve 4 is wrapped and buried between the inner and outer walls of the cylinder 1, and set the first support ear 5 and the second support ear 6 on the outer surface of the bearing sleeve 4. Therefore, after the production is completed, the overall structural strength of the cylinder 1 can be improved by the bearing sleeve 4, the first support ear 5 and the second support ear 6, thereby increasing the bearing capacity of the cylinder 1. The first support ear 5 and the second support ear 6 serve as support points of the cylinder 1, which can effectively disperse the external force applied to the cylinder 1 and enhance the stability of the entire launch system. At the same time, when the cylinder 1 is subjected to impact or vibration, the first support ear 5 and the second support ear 6 can provide necessary support, reduce the deformation of the cylinder 1, and protect the missile inside from damage.

[0034] The above embodiments are only intended to help understand the method and core concept of the present invention. It should be noted that those skilled in the art can make various improvements and modifications to the present invention without departing from the principles of the present invention, and such improvements and modifications also fall within the scope of protection of the claims of the present invention.

Claims

1. A composite material launch tube formed by winding, comprising a tube body (1), the inner wall of the tube body (1) is provided with a guide rail (2), and both ends of the tube body (1) are provided with flanges (3), characterized in that: A bearing sleeve (4) is embedded between the inner and outer walls of the cylinder (1), and the number of the bearing sleeves (4) is two. The outer surfaces of the two bearing sleeves (4) are respectively provided with a first support ear (5) and a second support ear (6).

2. The composite material launch tube of winding molding according to claim 1, characterized in that: Both ends of the cylinder (1) are fixedly sleeved with connecting sleeves (7), and the flange (3) is fixedly mounted on the connecting sleeves (7).

3. The composite material launch tube of winding molding according to claim 1, characterized in that: A guide bar (8) is fixedly mounted on the outer surface of the bearing sleeve (4) on the right side, and a through hole is provided on the guide bar (8).

4. The composite material launch tube of winding molding according to claim 1, characterized in that: The inner wall of the cylinder (1) is fixedly mounted with reinforcing ribs (9) located on both sides of the guide rail (2), and the outer surface of the reinforcing ribs (9) is fixedly attached to the guide rail (2).

5. The composite material launch tube formed by winding according to claim 1, characterized in that: The number of the first lugs (5) is four, and the four first lugs (5) are evenly mounted around the outer surface of the bearing sleeve (4).

6. The composite material launch tube formed by winding according to claim 1, characterized in that: The number of the guide rails (2) is four, and the cross-section of the guide rails (2) is trapezoidal.

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