Portable quick pin retreating mechanism for launch canister
Through the integrated mechanical structure of the safety cover and the bullet-blocking pin, the complexity and high cost of the portable launcher cancellation mechanism are solved, and the reliable locking and unlocking of the missile is achieved, simplifying operation and reducing production costs.
Patent Information
- Application Number
- CN202421860004.2
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-08-02
- Publication Date
- 2025-07-08
- Estimated Expiration
- 2034-08-02
AI Technical Summary
The existing portable launcher retraction mechanism has problems such as complex structure, many parts, and high assembly accuracy requirements, and the electronic retraction cost is high and the operability is low.
The mechanical structure of the safety cover and the bullet-blocking pin is adopted to lock and unlock the missile through the rotation of the safety cover, and the limit bumps and sealing rings ensure airtightness, simplify operation and reduce costs.
It realizes reliable locking and unlocking of missiles, is easy to operate, reduces production costs, and supports large-scale equipment of portable launchers.
Smart Images
Figure CN223077535U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of launch tubes, and in particular, to a quick pin-removing mechanism for a portable launch tube. Background Art
[0002] A launch tube is a special cylindrical device for holding and launching missiles. It mainly consists of a framework, a cylinder body, a firing control mechanism, and a docking mechanism, and has functions such as supporting, sealing, storing, and launching missiles. Some can also impart an initial rotational speed to the missile and serve as a director for missile launch. When using the launch tube, a pin-removing mechanism is required to control the launch of the missile.
[0003] However, the existing pin-removing mechanisms for portable launch tubes are usually divided into two types: mechanical pin-removing and electronic pin-removing. The traditional mechanical pin-removing structure is complex, involves many parts, and has high requirements for assembly accuracy; electronic pin-removing requires the use of electric detonators, which are costly, and electric detonators belong to pyrotechnic devices and are controlled devices, with low operability. Summary of the Utility Model
[0004] The purpose of the utility model is to provide a quick pin-removing mechanism for a portable launch tube to solve the above problems.
[0005] To achieve the above purpose, an embodiment of the utility model provides a quick pin-removing mechanism for a portable launch tube, including: a launch tube cylinder body, an assembly housing installed on the launch tube cylinder body, a grip fixed to the bottom of the assembly housing, an ignition button installed on the grip, a safety cover provided on the assembly housing, a connecting member installed in the safety cover, a bullet-blocking pin member provided on the connecting member, and a bullet-blocking pin channel opened in the launch tube cylinder body and the assembly housing;
[0006] A first pin is fixedly connected to the assembly housing, and the safety cover is rotatably connected to the assembly housing through the first pin;
[0007] A second pin is fixedly connected to the connecting member, and the bullet-blocking pin is rotatably connected to the connecting member through the second pin.
[0008] Further, assembly grooves are opened on both sides of the assembly housing, a plurality of limiting circular grooves are symmetrically opened on the assembly housing, and the plurality of limiting circular grooves are respectively arranged in the two assembly grooves. Two limiting convex blocks respectively adapted to the plurality of limiting circular grooves are symmetrically and fixedly connected to the inner wall of the safety cover;
[0009] The safety cover is in interference fit with the two assembly grooves.
[0010] Further, the head of the bullet-blocking pin member is provided with a rounded shape, and a blocking block is fixedly connected to the lower end of the bullet-blocking pin member;
[0011] The stopper is frustum-shaped, and the lower end of the bullet-blocking pin channel is conical.
[0012] Furthermore, two limiting rings are fixedly sleeved on the outer wall of the bullet-blocking pin member. A first sealing ring and a second sealing ring are movably sleeved outside the bullet-blocking pin member. The first sealing ring is arranged between the two limiting rings, and the second sealing ring is located between the stopper and one of the limiting rings.
[0013] Furthermore, control grooves are symmetrically formed in the outer wall of the safety cover.
[0014] Furthermore, a plurality of fixed clamps are sleeved on the launch tube cylinder body, and both ends of the plurality of fixed clamps are fixedly connected to the assembly housing.
[0015] Compared with the prior art, the embodiment of the present utility model has the following beneficial effects:
[0016] The quick pin-removing mechanism of the portable launch tube has a simple and ingenious structural design. By adopting the integrated linkage method of the safety cover and the bullet-blocking pin, when the safety cover is closed, double locking of the missile in the launch tube and the ignition button can be achieved. When the safety cover is opened, it can ensure that the launch tube is disarmed and the bullet-blocking pin member can be reliably removed. When the launch is cancelled, the missile and the ignition button can be re-locked. The operation is reversible, and the functions of the bullet-blocking pin member and the launch insurance are integrated into one with the simplest and most intuitive mechanical structure, which is very reliable and convenient to use.
[0017] The quick pin-removing mechanism of the portable launch tube uses fewer parts as a whole, is easy to produce and assemble, greatly reduces costs, and at the same time has a simple operation and can achieve fool-proof operation, which is beneficial to the low-cost mass equipment of the portable launch tube. BRIEF DESCRIPTION OF THE DRAWINGS
[0018] The present utility model will be further described below with reference to the drawings and embodiments.
[0019] Figure 1 The perspective view of the present utility model is shown;
[0020] Figure 2 The perspective view of the present utility model in another state is shown;
[0021] Figure 3 The partial disassembly of the present utility model is shown Figure 1 ;
[0022] Figure 4 The partial disassembly of the present utility model is shown Figure 2 ;
[0023] Figure 5 The partial sectional view of the present utility model is shown;
[0024] Figure 6 Shows the present utility model Figure 3 An enlarged view of part A of
[0025] In the figure
[0026] 1. Launch tube body; 2. Assembly housing; 3. Grip; 4. Ignition button; 5. Safety cover; 6. Connecting piece; 7. Bullet blocking pin part; 8. Bullet blocking pin channel; 9. First pin; 10. Second pin; 11. Assembly groove; 12. Limiting circular groove; 13. Limiting convex block; 14. Block; 15. Limiting ring; 16. First sealing ring; 17. Second sealing ring; 18. Control groove; 19. Fixed clamp. Detailed implementation manners
[0027] Now, the present utility model will be further described in detail with reference to the accompanying drawings. These drawings are all simplified schematic diagrams, only showing the basic structure of the present utility model in a schematic way, so they only show the components related to the present utility model.
[0028] Please refer to Figure 1 , Figure 1 which shows a perspective view of the present utility model; please refer to Figure 2 , Figure 2 which shows a perspective view of the present utility model in another state; please refer to Figure 3 , Figure 3 which shows a partial disassembly of the present utility model Figure 1 ; please refer to Figure 4 , Figure 4 which shows a partial disassembly of the present utility model Figure 2 ; please refer to Figure 5 , Figure 5 which shows a partial sectional view of the present utility model; please refer to Figure 6 , Figure 6 which shows the present utility model Figure 3 An enlarged view of part A of; as Figures 1 - 6 shown, a portable launch tube quick pin-removing mechanism includes: a launch tube body 1, an assembly housing 2 installed on the launch tube body 1, a grip 3 fixed to the bottom of the assembly housing 2, an ignition button 4 installed on the grip 3, a safety cover 5 provided on the assembly housing 2, a connecting piece 6 installed in the safety cover 5, a bullet blocking pin part 7 provided on the connecting piece 6, and a bullet blocking pin channel 8 opened in the launch tube body 1 and the assembly housing 2;
[0029] A first pin 9 is fixedly connected to the assembly housing 2, and the safety cover 5 is rotatably connected to the assembly housing 2 through the first pin 9;
[0030] A second pin 10 is fixedly connected to the connecting member 6. The anti-bounce pin is rotatably connected to the connecting member 6 through the second pin 10. When the launch tube body 1 is stored or carried normally, the safety cover 5 is rotated with the first pin shaft as the center to close it. Since the anti-bounce pin member 7 can rotate in the safety cover 5 with the second pin shaft as the center, at this time, the head of the anti-bounce pin member 7 can move along the anti-bounce pin channel 8 of the assembly housing 2, driving the anti-bounce pin member 7 to move into the launch tube body 1 along the anti-bounce pin channel 8 in the assembly housing 2 until it is inserted into the launch tube body 1 to lock the missile in the launch tube body 1. At the same time, two sealing rings on the anti-bounce pin are pressed in the anti-bounce pin channel 8 to ensure the airtightness of the tube body and the housing. At the same time, the ignition button 4 on the grip 3 will be covered by the safety cover 5 at this time, and the user's finger cannot touch it and cannot press it to launch, thus realizing the double locking of the missile and the ignition button 4. During combat, the safety cover 5 is pulled downwards, and the anti-bounce pin moves downwards with the safety cover 5 and exits from the anti-bounce pin channel 8 in the assembly housing 2. The missile is unlocked, and at the same time, the ignition button 4 is exposed and can be pressed to complete the launch. Through the cooperation of the limit bump 13 and the two limit circular grooves 12, the opening degree of the safety cover 5 can be restricted to ensure that the head of the anti-bounce pin is still in the housing anti-bounce pin channel 8 when the safety cover 5 is in the maximum open position. If the launch command is cancelled, the safety cover 5 can be reinstalled. The rounded corner of the head of the anti-bounce pin member 7 contacts the conical inner wall of the anti-bounce pin channel 8 in the assembly housing 2 and can be inserted back into the tube body along the channel, realizing reversible operation. The anti-pin withdrawal mechanism of this launch tube is ingeniously designed, with few parts used, easy production and assembly, greatly reducing costs. At the same time, the operation is simple and can achieve foolproof operation, which is beneficial to the low-cost mass production of portable launch tubes.
[0031] Optionally, assembly grooves 11 are formed on both sides of the assembly housing 2, and a number of limit circular grooves 12 are symmetrically formed on the assembly housing 2. The number of limit circular grooves 12 are respectively arranged in the two assembly grooves 11, and two limit bumps 13 adapted to the number of limit circular grooves 12 are symmetrically and fixedly connected to the inner wall of the safety cover 5.
[0032] The safety cover 5 is in interference fit with the two assembly grooves 11. When the safety cover 5 rotates on the assembly housing 2 with the first pin 9 as the center, one of the limit bumps 13 in the safety cover 5 will alternately snap into the two limit circular grooves 12 in one of the assembly grooves 11, thereby completing the opening and closing of the safety cover 5 and restricting the opening degree of the safety cover 5, so that the head of the anti-bounce pin member 7 is still in the anti-bounce pin channel 8 of the assembly housing 2 when the safety cover 5 is in the maximum open position, and thus the anti-bounce pin member 7 can be smoothly inserted back when the safety cover 5 is closed. Through the two limit grooves provided, when the safety cover 5 is in the closed state, the outer wall of the safety cover 5 can be on the same horizontal plane as the outer wall of the assembly housing 2. At the same time, due to the interference fit between the safety cover 5 and the two assembly grooves 11, the stability of the safety cover 5 after closing can be ensured.
[0033] Optionally, the head of the bullet-blocking pin 7 is rounded, and a block 14 is fixedly connected to the lower end of the bullet-blocking pin 7;
[0034] The block 14 is frustum-shaped, and the lower end of the bullet-blocking pin channel 8 is conical. When the bullet-blocking pin 7 moves in the bullet-blocking pin channel 8, the rounded head of the bullet-blocking pin 7 facilitates movement in the conical bullet-blocking pin channel 8. Furthermore, the head of the bullet-blocking pin 7 can move along the bullet-blocking pin channel 8 of the assembly housing 2, enabling the bullet-blocking pin 7 to exit or insert in an arc direction, so as to realize the withdrawal or insertion of the bullet-blocking pin 7 as the safety cover 5 rotates; and the frustum-shaped block 14 is adapted to the bullet-blocking pin channel 8. After the bullet-blocking pin 7 is inserted into the bullet-blocking pin channel 8, the block 14 abuts against the inner wall of the bullet-blocking pin channel 8, effectively improving the stability of the bullet-blocking pin 7 in the bullet-blocking pin channel 8.
[0035] Optionally, two limiting rings 15 are fixedly sleeved on the outer wall of the bullet-blocking pin 7. A first sealing ring 16 and a second sealing ring 17 are movably sleeved outside the bullet-blocking pin 7. The first sealing ring 16 is arranged between the two limiting rings 15, and the second sealing ring 17 is located between the block 14 and one of the limiting rings 15. By the cooperation of the first sealing ring 16 and the second sealing ring 17 provided, when the bullet-blocking pin 7 is placed in the bullet-blocking pin channel 8, the two sealing rings are compressed in the bullet-blocking pin channel 8, ensuring the airtightness of the launcher barrel 1 and the assembly housing 2.
[0036] Optionally, control grooves 18 are symmetrically formed on the outer wall of the safety cover 5. When a user needs to control the opening and closing of the safety cover 5, the user can place the index finger and the thumb in the two control grooves 18 respectively, and then rotate the safety cover 5. The provided control grooves 18 can ensure the stability of the contact between the fingers and the safety cover 5.
[0037] Optionally, a plurality of fixed clamps 19 are sleeved on the launcher barrel 1. Both ends of the plurality of fixed clamps 19 are fixedly connected to the assembly housing 2. By the plurality of fixed clamps 19 provided, the assembly housing 2 and the launcher barrel 1 can be strengthened at multiple points, ensuring the stability of the assembly housing 2 installed on the launcher barrel 1.
[0038] The above are only the preferred embodiments of the present invention and are not used to limit the present invention. For those skilled in the art, the present invention can have various modifications and changes. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present invention shall be included within the protection scope of the present invention.
Claims
1. A rapid pin-removing mechanism for a portable launcher tube, characterized in that Comprising: A launch tube barrel (1), a mounting housing (2) mounted on the launch tube barrel (1), a grip (3) fixed to the bottom of the mounting housing (2), a firing button (4) mounted on the grip (3), a safety cover (5) provided on the mounting housing (2), a connecting member (6) mounted in the safety cover (5), a bullet retaining pin member (7) provided on the connecting member (6), and a bullet retaining pin channel (8) opened in the launch tube barrel (1) and the mounting housing (2); A first pin (9) is fixedly connected to the mounting housing (2), and the safety cover (5) is rotatably connected to the mounting housing (2) through the first pin (9); A second pin (10) is fixedly connected to the connecting member (6), and the bullet retaining pin is rotatably connected to the connecting member (6) through the second pin (10).
2. A rapid bullet retaining pin retracting mechanism for a portable launch tube according to claim 1, characterized in that Assembly grooves (11) are opened on both sides of the mounting housing (2), a number of limiting circular grooves (12) are symmetrically opened on the mounting housing (2), and the number of limiting circular grooves (12) are respectively arranged in the two assembly grooves (11), and two limiting protrusions (13) adapted to the number of limiting circular grooves (12) are symmetrically and fixedly connected to the inner wall of the safety cover (5); The safety cover (5) is in interference fit with the two assembly grooves (11).
3. A rapid bullet retaining pin retracting mechanism for a portable launch tube according to claim 2, characterized in that The head of the bullet retaining pin member (7) is provided with a rounded shape, and a blocking block (14) is fixedly connected to the lower end of the bullet retaining pin member (7); The blocking block (14) is provided in a frustum shape, and the lower end of the bullet retaining pin channel (8) is provided in a conical shape.
4. A rapid bullet retaining pin retracting mechanism for a portable launch tube according to claim 3, characterized in that Two limiting rings (15) are fixedly sleeved on the outer wall of the bullet retaining pin member (7), a first sealing ring (16) and a second sealing ring (17) are movably sleeved outside the bullet retaining pin member (7), the first sealing ring (16) is arranged between the two limiting rings (15), and the second sealing ring (17) is located between the blocking block (14) and one of the limiting rings (15).
5. A rapid bullet retaining pin retracting mechanism for a portable launch tube according to claim 4, characterized in that Control grooves (18) are symmetrically opened on the outer wall of the safety cover (5).
6. A rapid bullet retaining pin retracting mechanism for a portable launch tube according to claim 1, characterized in that A number of fixed clamps (19) are sleeved on the launch tube barrel (1), and both ends of the number of fixed clamps (19) are fixedly connected to the mounting housing (2).