Rotary latching mechanism simulation test device

Abstract

The application discloses a rotary locking mechanism simulation test device, which comprises a base, wherein a first sensor, a sensor support and a locking mechanism assembly are arranged on the base. The sensor support and the locking mechanism assembly are fixedly installed on the base, and the first sensor is fixedly connected to the sensor support and connected with the locking mechanism assembly through a coupling. The test process of the application does not need live ammunition, the key components are arranged outside, and the structural parameters are easy to adjust, so that the motion characteristics of the rotary locking mechanism can be monitored and recorded, and the shortcomings of the traditional method, such as poor economic benefit, low test efficiency, unadjustable component structural parameters and difficult observation of the action process, are solved.

Description

Technical Field

[0001] The invention belongs to the field of automatic weapon simulation test, and in particular relates to a rotary locking mechanism simulation test device. Background Art

[0002] Automatic weapons require a closed chamber and a secure hold on the cartridge case during firing to prevent it from breaking and preventing the release of gunpowder gases. After firing, the cartridge case must be promptly withdrawn to ensure the next round enters the chamber, ensuring effective and safe firing. The locking mechanism in automatic weapons fulfills this function. The reliability of its operation significantly impacts the reliability and safety of the entire automatic weapon system, making it a crucial factor to consider during the design process.

[0003] Locking mechanisms operate in two main categories: inertial locking and rigid locking. Among rigid locking mechanisms, rotary locking mechanisms are widely used in gas-operated and barrel-recoil automatic weapons due to their uniform force distribution, smooth operation, flexibility, reliability, and strong environmental adaptability. To ensure a smooth and stable opening and closing process, a guiding helical surface is essential. The rationality of the helical surface design directly determines the stability and reliability of the rotary locking mechanism. Relying on design experience and trial and error through repeated live-fire exercises is the current common approach to rotary locking mechanism design. However, this method is costly and inefficient, and test results are easily affected by ammunition variations and test conditions. Furthermore, because rotary locking mechanisms are often located within the automatic weapon's automaton, their motion parameters are often difficult to observe and measure, further complicating the design of rotary locking mechanisms. Summary of the Invention

[0004] The purpose of the present invention is to provide a rotary locking mechanism simulation test device, which does not require live ammunition during the test process, has key components placed outside and structural parameters that are easy to adjust, and is convenient for monitoring and recording the motion characteristics of the rotary locking mechanism, thereby solving the shortcomings of traditional methods such as poor economic benefits, low test efficiency, inability to adjust component structural parameters, and difficulty in observing the movement process.

[0005] The technical solutions for achieving the purpose of the present invention are:

[0006] A rotary locking mechanism simulation test device comprises a base and a machine head rotatably supported on the base;

[0007] A first guide rail piece and a second guide rail piece are symmetrically arranged on the base;

[0008] A machine head is provided between the first guide rail piece and the second guide rail piece;

[0009] The first guide rail piece and the second guide rail piece are clamped with an organic body, and the organic body is coaxial with the axis of the machine head, and can move forward and backward along the axis of the machine head;

[0010] The machine body is provided with a spiral groove; the guide protrusion of the machine head is arranged at the spiral groove of the machine body and can rotate under the drive of the spiral groove;

[0011] A recoil spring is provided on the nose of the machine to provide energy for the recoil process of the machine body;

[0012] The machine body is provided with a push rod for receiving external force and driving the machine head to move, completing the simulation of the opening and locking process;

[0013] The machine head and the machine body are respectively provided with a first sensor and a second sensor for monitoring parameters of the motion process of the test device.

[0014] Compared with the prior art, the present invention has the following significant advantages:

[0015] 1) No need to consume live ammunition or repeatedly produce prototypes, which reduces test costs and improves test efficiency;

[0016] 2) The structural parameters of key components are easy to adjust, and the motion process of the rotary locking mechanism under different structural parameters can be simulated;

[0017] 3) Key components are located outside to facilitate monitoring and recording of their motion characteristics. BRIEF DESCRIPTION OF THE DRAWINGS

[0018] Figure 1 It is a schematic diagram of the overall structure of the rotary locking mechanism simulation test device of the present invention.

[0019] Figure 2 It is a schematic structural diagram of the locking mechanism components of the rotary locking mechanism simulation test device of the present invention.

[0020] Figure 3 It is a schematic diagram of the machine head structure of the rotary locking mechanism simulation test device of the present invention.

[0021] Figure 4 It is a schematic diagram of the body structure of the rotary locking mechanism simulation test device of the present invention. DETAILED DESCRIPTION

[0022] The present invention will be further described below with reference to the accompanying drawings and specific embodiments.

[0023] Combine Figure 1A rotary locking mechanism simulation test device includes a base 1, on which are mounted a first sensor 2, a sensor bracket 3, and a locking mechanism assembly 4. The sensor bracket 3 and the locking mechanism assembly are fixedly mounted on the base 1. The first sensor 2 is fixedly connected to the sensor bracket 3 and connected to the locking mechanism assembly 4 via a coupling. The first sensor 2 is an angle sensor or a rotary encoder used to monitor and record rotational motion parameters.

[0024] Combine Figures 2 to 4 The locking mechanism assembly 4 includes a first bearing seat 401, a first bracket 402, a first guide rail piece 403, a return spring 404, a machine head 405, a second guide rail piece 406, a guide rail seat 407, a machine body 408, a second sensor 409, a push rod 410, a second bearing seat 411 and a second bracket 412. The first bracket 402 and the second bracket 412 are respectively fixed to the two ends of the guide rail seat 407; the guide rail seat 407 is fixed on the base 1, the first bearing seat 401 and the second bearing seat 411 are respectively fixed to the first bracket 402 and the second bracket 412, and bearings are provided in the first bearing seat 401 and the second bearing seat 411 for supporting the machine head 405; the first guide rail piece 403 and the second guide rail piece 406 Symmetrically arranged on both sides of the top of the guide rail seat 407, the guide rail gap can be adjusted by changing the thickness of the first guide rail piece 403 and the second guide rail piece 406, thereby realizing the simulation of the opening and closing locking process under different guide rail gaps; the machine head 405 is arranged between the first guide rail piece 403 and the second guide rail piece 406, and one end is arranged at the second bearing seat 411, and the other end passes through the first bearing seat 401 and is connected to the first sensor 2 through a coupling, and a guide protrusion 40501 is provided on the machine head 405; the machine body 408 is clamped on the first guide rail piece 403 and the second guide rail piece 406, and is coaxial with the axis of the machine head 405, and can move forward and backward along the axis direction of the machine head 405, and a spiral groove 40801 is provided on the machine body 408; the guide protrusion of the machine head 405 40501 is arranged at the spiral groove 40801 of the body 408, and can rotate driven by the spiral groove 40801. The head is detachable, and the simulation of the opening and closing process under different spiral structures can be achieved by adjusting the width and spiral parameters of the spiral groove 40801; the recoil spring 404 is coaxial with the axis of the head 405 and is placed between the body 408 and the first bracket 402, for supplying energy to the recoil process; the push rod 410 is fixedly installed on the body 408, for receiving external force and driving the entire simulation device to move; the second sensor 409 is arranged on the body 408 and moves with the body 408. The second sensor 409 is a posture sensor or an acceleration sensor, which is used to detect and record the translational motion parameters of the body 408.

[0025] The working process of the rotary locking mechanism simulation test device of the present invention is as follows:

[0026] Under the action of external force, the push rod 410 of the locking mechanism assembly 4 drives the body 408 to move backward and compress the return spring 404. The spiral groove 40801 of the body 408 guides the guide protrusion 40501 of the machine head 405 and drives the machine head 405 to rotate, so as to simulate the unlocking rotation process; due to the energy storage effect of the return spring 404, the speed of the body 408 gradually decreases and returns to its original position under the action of the return spring 404, while driving the machine head 405 to rotate in the opposite direction, completing the simulation of the locking rotation process; during the entire action process, the first sensor 2 monitors and records the rotational motion parameters of the machine head 405, and the second sensor 409 monitors and records the translational motion parameters of the body 408; at the same time, by adjusting the structural parameters of the first guide rail piece 403, the second guide rail piece 406, and the spiral groove 40801 of the body 408, the simulation of the unlocking and closing process under different structural parameter conditions can be completed.

[0027] The present invention provides a firearm automatic mechanism simulation test device, wherein the test process does not require live ammunition, key components are located externally, and structural parameters are easily adjustable, thereby facilitating monitoring and recording of the motion characteristics of a rotary locking mechanism. This device overcomes the shortcomings of the prior art, such as poor economic benefits, low test efficiency, inability to adjust component structural parameters, and difficulty in observing the motion process.

Claims

1. A rotary locking mechanism simulation test device, characterized in that: It includes a base, a machine head rotatably supported on the base; A first guide rail piece and a second guide rail piece are symmetrically arranged on the base; A machine head is provided between the first guide rail piece and the second guide rail piece; The first guide rail piece and the second guide rail piece are clamped with an organic body, and the organic body is coaxial with the axis of the machine head, and can move forward and backward along the axis of the machine head; The machine body is provided with a spiral groove; the guide protrusion of the machine head is arranged at the spiral groove of the machine body and can rotate under the drive of the spiral groove; A recoil spring is provided on the nose of the machine to provide energy for the recoil process of the machine body; The machine body is provided with a push rod for receiving external force and driving the machine head to move, completing the simulation of the opening and locking process; The head and the body are respectively provided with a first sensor and a second sensor for monitoring the parameters of the motion process of the test device; A guide rail seat is provided on the base, and a first bracket and a second bracket are fixed at both ends of the guide rail seat respectively; a first bearing seat and a second bearing seat are fixed to the first bracket and the second bracket respectively; the first guide rail piece and the second guide rail piece are symmetrically arranged on both sides of the top of the guide rail seat; one end of the machine head is arranged at the second bearing seat, and the other end passes through the first bearing seat and is connected to the first sensor through a coupling.

2. The rotary locking mechanism simulation test device according to claim 1, characterized in that: The thickness of the first guide rail piece and the second guide rail piece is adjustable.

3. The rotary locking mechanism simulation test device according to claim 1, characterized in that: The body is detachable, and the simulation of the opening and closing processes under different spiral structures can be achieved by adjusting the width of the spiral groove and the spiral parameters.

4. The rotary locking mechanism simulation test device according to claim 1, characterized in that: The first sensor is an angle sensor or a rotary encoder.

5. The rotary locking mechanism simulation test device according to claim 1, characterized in that: The second sensor is a posture sensor or an acceleration sensor.

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