A simulated load rear section and rear load section connection structure and its assembly method
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- Filing Date
- 2023-10-19
- Publication Date
- 2026-08-14
AI Technical Summary
[0003]为解决上述技术问题,本发明提供一种模拟载荷后段与后排载段连接结构和及其装配方法,连接结构利用模拟载荷后段和后排载段现有的空间和结构,解决助飞鱼雷空中高速开伞冲击下后段壳体楔环连接处断裂的问题
[0020]本发明提供的一种模拟载荷后段与后排载段连接结构和及其装配方法,在模拟载荷后段和后排载段的空间结构内,通过设置拉紧块和螺杆,紧固模拟载荷后段壳体与后排载段壳体之间的连接。当模拟载荷在空中高速开伞时受到强冲击时,采用本发明提供的后段与后排载段连接结构,能够保证后段与后排载段可靠连接。本发明结构简单,成本低廉,充分利用后段和后排载段现有的空间和结构特点,解决了后段壳体楔环连接处断裂导致试验失败的难题。
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Figure CN117404969B_ABST
Abstract
Description
Technical Field
[0001] This invention belongs to the field of underwater weaponry, specifically relating to a connection structure between the rear section of a simulated load and the rear load section, and its assembly method. Background Technology
[0002] In the live-fire tests of the torpedo-assisted flight, to obtain test data similar to that of a live torpedo launch, simulated loads were used to simulate the torpedo's shape, mass, moment of inertia, and other structural and aerodynamic characteristics. This allowed for the testing, recording, and playback of experimental data. To save costs, the design of the simulated loads was required to be as simple and reliable as possible. Because the new lightweight torpedo uses a wedge-ring connection, the connection between the rear section and the rear load section experiences significant stress. The existing simulated loads' rear section and rear load section lack sufficient impact resistance, which could lead to breakage at the wedge-ring connection of the rear section casing. Summary of the Invention
[0003] To solve the above-mentioned technical problems, the present invention provides a connection structure between the rear section of the simulated load and the rear row of load sections and its assembly method. The connection structure utilizes the existing space and structure of the rear section of the simulated load and the rear row of load sections to solve the problem of fracture at the wedge ring connection of the rear section shell under the impact of high-speed parachute opening in the air of a torpedo-assisted flight.
[0004] The objective of this invention is achieved through the following technical solution: a connection structure between the rear section of a simulated load and the rear load section, comprising a tensioning block and a screw.
[0005] The tensioning block is located in the central square hole of the rear load section housing, on the side away from the rear section housing.
[0006] The outer ring of the tensioning block rests on the outer wall of the central square hole of the rear load section housing, while the inner ring is set tightly against the side wall of the central square hole of the rear load section housing.
[0007] The tensioning block has a through hole.
[0008] Two screws pass through the through holes of the tensioning block and are fixed to the connection between the rear housing and the rear load housing by the fixing mechanism.
[0009] Preferably, one end of the screw is fixed to the tensioning block by a nut.
[0010] Preferably, the fixing mechanism includes a fixing plate and a spring-loaded washer, wherein the fixing plate is fixed to the annular rib at the front end of the rear housing, the fixing plate is provided with a screw hole, the other end of the screw passes through the screw hole of the fixing plate, and is fixed to the fixing plate by the spring-loaded washer and nut.
[0011] Preferably, a filler plate, a cover plate, and a wedge ring are provided at the connection between the rear load section housing and the rear section housing. The wedge ring is inserted into the wedge ring groove at the connection between the rear load section housing and the rear section housing. The filler plate is placed at the wedge ring groove, and the cover plate covers the filler plate for sealing.
[0012] Preferably, an O-ring is provided on the rear load section housing.
[0013] In addition to providing a connection structure between the rear section of the simulated load and the rear load section, this invention further provides an assembly method for the above-mentioned connection structure, the specific steps of which are as follows:
[0014] Pass the screw through the fixing plate, fix one end of the screw to the fixing plate with the spring washer and nut, and tighten the fixing plate to the ring rib at the front end of the rear housing with screws;
[0015] An O-ring is installed on the rear load section housing, and the other end of the screw is inserted into the hole of the tensioning block;
[0016] Connect the rear load section housing and the rear section housing, insert the wedge ring into the wedge ring groove at the connection between the rear load section housing and the rear section housing, and put in the packing plate and cover plate;
[0017] Secure the other end of the screw to the tensioning block with a nut, and tighten it with an adjustable wrench.
[0018] The present invention further provides a simulated load, wherein the simulated load rear section shell and the rear section shell are fitted with the above-mentioned simulated load rear section and rear section connection structure.
[0019] Compared with the prior art, the present invention has the following advantages:
[0020] This invention provides a connection structure and assembly method for the rear section and rear load section of a simulated load. Within the spatial structure of the rear section and rear load section of the simulated load, tension blocks and screws are used to secure the connection between the rear section shell and the rear load section shell. When the simulated load is subjected to a strong impact during high-speed parachute deployment in the air, the connection structure provided by this invention ensures a reliable connection between the rear section and the rear load section. This invention has a simple structure, low cost, and fully utilizes the existing space and structural features of the rear section and rear load section, solving the problem of test failure caused by breakage at the wedge ring connection of the rear section shell.
[0021] The connection structure between the rear section and the rear load section of the simulated load provided by this invention can ensure a reliable connection between the rear section and the rear load section of the simulated load, with low cost and good military and social benefits. Attached Figure Description
[0022] Figure 1 This is a schematic diagram of the connection structure between the rear section of the simulated load and the rear load section in an embodiment of the present invention.
[0023] In the diagram, 1 is a nut; 2 is a tensioning block; 3 is a screw; 4 is the rear section housing; 5 is a packing plate; 6 is a cover plate; 7 is a screw; 8 is a fixing plate; 9 is the rear section housing; 10 is a spring washer; 11 is an O-ring seal; and 12 is a wedge ring. Detailed Implementation
[0024] The present invention will now be described in further detail with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the invention and not intended to limit it. Furthermore, it should be noted that, for ease of description, the accompanying drawings show only the parts relevant to the present invention, and not all of the structures.
[0025] The technical solution of the present invention provides a connection structure between the rear section of the simulated load and the rear load section, including a tension block 2 and a screw 3.
[0026] The tensioning block 2 is located in the central square hole of the rear load section housing 4, on the side away from the rear section housing 9.
[0027] The outer ring of the tensioning block 2 rests on the outer wall of the central square hole of the rear load section housing 4, and the inner ring is set close to the side wall of the central square hole of the rear load section housing 4.
[0028] The tensioning block 2 is provided with a through hole.
[0029] Two screws 3 pass through the through holes of the tensioning block 2 and are fixed to the connection between the rear housing 9 and the rear load housing 4 by a fixing mechanism.
[0030] like Figure 1 As shown, in one embodiment of the present invention, one end of the screw 3 is fixed to the tensioning block 2 by a nut 1. The fixing mechanism includes a fixing plate 8 and a spring-loaded washer 10, wherein the fixing plate 8 is fixed to the annular rib at the front end of the rear housing 9, and a screw hole is provided on the fixing plate 8. The other end of the screw 3 passes through the screw hole of the fixing plate 8 and is fixed to the fixing plate 8 by the spring-loaded washer 10 and the nut.
[0031] As a further optimization of the above embodiment, a filler plate 5, a cover plate 6, and a wedge ring 12 are provided at the connection between the rear load section housing 4 and the rear section housing 9. The wedge ring 12 is inserted into the wedge ring groove at the connection between the rear load section housing 4 and the rear section housing 9. The filler plate 5 is disposed at the wedge ring groove, and the cover plate 6 covers the filler plate 5 for sealing. An O-ring seal 11 is provided on the rear load section housing 4.
[0032] In addition to providing a connection structure between the rear section of the simulated load and the rear load section, the present invention further provides an assembly method for the above-mentioned connection structure, the specific steps of which are as follows:
[0033] The screw 3 is passed through the fixing plate 8, and one end of the screw 3 is fixed to the fixing plate 8 by the spring washer 10 and the nut. The fixing plate 8 is then tightened to the annular rib at the front end of the rear housing 9 by the screw 7.
[0034] An O-ring 11 is installed on the rear load section housing 4, and the other end of the screw 3 is inserted into the hole of the tensioning block 2.
[0035] Connect the rear load section housing 4 and the rear section housing 9, insert the wedge ring 12 into the wedge ring groove at the connection between the rear load section housing 4 and the rear section housing 9, and put in the filler plate 5 and the cover plate 6.
[0036] The other end of the screw 3 is fixed to the tension block 2 by nut 1 and tightened with an adjustable wrench, thus achieving a reliable connection between the rear section and the rear load section.
[0037] The present invention also provides a simulated load, wherein the simulated load rear section housing 4 and the rear section housing 9 are fitted with the above-mentioned simulated load rear section and rear section connection structure.
[0038] The above are preferred embodiments of the present invention. It should be noted that, for those skilled in the art, several improvements and modifications can be made without departing from the principle of the present invention, and these improvements and modifications should also be considered within the scope of protection of the present invention.
Claims
1. A connection structure between the rear section of a simulated load and the rear load section, characterized in that: The connecting structure includes a tensioning block (2) and a screw (3); The tensioning block (2) is located in the central square hole of the rear load section housing (4), on the side away from the rear section housing (9); The outer ring of the tensioning block (2) is abutted on the outer wall of the central square hole of the rear load section housing (4), and the inner ring is set close to the side wall of the central square hole of the rear load section housing (4); The tensioning block (2) is provided with a through hole; The two screws (3) pass through the through hole of the tensioning block (2) and are fixed by the fixing mechanism at the connection between the rear section housing (9) and the rear load section housing (4) to realize a reliable connection between the simulated load rear section and the rear load section; One end of the screw (3) is fixed to the tensioning block (2) by a nut (1); The fixing mechanism includes a fixing plate (8) and a spring flat pad (10), wherein the fixing plate (8) is fixed to the ring rib at the front end of the rear housing (9), and a screw hole is provided on the fixing plate (8). The other end of the screw (3) passes through the screw hole of the fixing plate (8) and is fixed on the fixing plate (8) by the spring flat pad (10) and the nut. The rear section housing (4) and the rear section housing (9) are provided with a filler plate (5), a cover plate (6) and a wedge ring (12), wherein the wedge ring (12) is inserted into the wedge ring groove at the connection between the rear section housing (4) and the rear section housing (9), the filler plate (5) is provided at the wedge ring groove, and the cover plate (6) covers the filler plate (5) for sealing.
2. The connection structure between the rear section of the simulated load and the rear load section as described in claim 1, characterized in that: An O-ring (11) is provided on the rear load section housing (4).
3. An assembly method for a simulated load rear section and a rear load section connection structure, characterized in that: The method is used to assemble the connection structure according to any one of claims 1-2, and the specific steps are as follows: The screw (3) is passed through the fixing plate (8), and one end of the screw (3) is fixed on the fixing plate (8) by the spring flat washer (10) and nut. The fixing plate (8) is tightened on the annular rib at the front end of the rear housing (9) by the screw (7). An O-ring (11) is provided on the rear load section housing (4), and the other end of the screw (3) is inserted into the hole of the tensioning block (2); Connect the rear section housing (4) and the rear section housing (9), insert the wedge ring (12) into the wedge ring groove at the connection between the rear section housing (4) and the rear section housing (9), and put in the filler (5) and the cover plate (6). The other end of the screw (3) is fixed to the tension block (2) by the nut (1) and tightened with an adjustable wrench.
4. A simulated load, characterized in that: The rear load section housing (4) and the rear section housing (9) of the simulated load are fitted with a connection structure as described in any one of claims 1-2.
Citation Information
Patent Citations
Aircraft circular-section cabin segment connecting method
CN106247871A
Cabin section rapid pose adjusting and tensioning device based on six-axis platform
CN109696092A