Simulated emission comprehensive test equipment

Abstract

The invention relates to the technical field of reliability detection of guide rail launching devices, and discloses simulated launching comprehensive test equipment which comprises a numerical control suspension and tool assembly, a power assembly is arranged on the side face of the numerical control suspension and tool assembly, and a guide rail assembly is fixedly assembled on the side face of the power assembly. A buffering and resetting assembly is fixedly assembled at the end, away from the power assembly, of the guide rail assembly. By using a universal suspension tool and a gas storage bag as a power source and a numerical control suspension system, the reliability detection requirements of guide rail launching devices of various models and different mounting modes can be met, a specially designed guide rail structure is used, bounce in the simulation bullet launching process can be effectively prevented, the safety during system testing is improved, and the test efficiency is improved. And the size of the mounting tool for the guide rail launching device is redesigned, so that the mounting test requirements of more types of launching devices can be expanded to meet, and the acceleration requirements of simulation bullets with smaller or larger mass can be expanded to meet by changing the pressure of high-pressure gas of a power system.

Description

Technical Field

[0001] The present invention relates to the technical field of reliability detection of rail launch devices, and specifically to a simulation launch comprehensive test equipment. Background Art

[0002] The simulation launch comprehensive test equipment is an important test equipment for ground simulation launch tests of rail launch devices with different models of missiles mounted. It provides necessary detection means for the reliability detection of rail launch devices. The simulation launch comprehensive test equipment can provide the launch environment required for the test, safety assurance after launch, and data processing functions. It can dynamically simulate the separation process between the rail launch device and the missile under the set launch conditions, test and verify the launch function of the launch device product, complete missile positioning, installation, locking, centering and alignment, launch, simulation of the deceleration of the dummy missile, collection, and return, and realize the test function of the reliability test of the launch device.

[0003] Currently, under the existing conditions, the testing of rail launch devices lacks special equipment and detection means; at the same time, the missile launch thrust and speed of different models of launch devices are not the same, and the versatility and economy of the testing devices are poor, which is not conducive to the testing and inspection of rail launch devices. Summary of the Invention

[0004] The present invention provides a simulation launch comprehensive test equipment to solve the problems raised in the above background art.

[0005] The present invention provides the following technical solution: A simulation launch comprehensive test equipment, including a numerical control suspension and tooling assembly. A power assembly is arranged on the side of the numerical control suspension and tooling assembly. A rail assembly is fixedly assembled on the side of the power assembly. A buffer and reset assembly is fixedly assembled at one end of the rail assembly away from the power assembly. A control assembly is arranged at one end of the rail assembly away from the numerical control suspension and tooling assembly. A rail launch device is arranged on the side of the numerical control suspension and tooling assembly. A dummy missile is slidably connected to the bottom of the rail launch device, and the outer edge of the dummy missile is connected to the inner wall of the rail assembly.

[0006] As a preferred technical solution of the present invention, the numerical control suspension and tooling assembly includes a machine tool body. A slide rail is fixedly assembled on the top of the machine tool body. A saddle is slidably connected to the side of the slide rail. A fixed frame is slidably connected to the side of the saddle. A horizontal crossbeam is slidably connected to the side of the fixed frame. A suspension tooling is fixedly assembled at the bottom of the horizontal crossbeam. The inner wall of the suspension tooling is fixedly connected to the top of the rail launch device.

[0007] As a preferred technical solution of the present invention, a motor one is fixedly assembled on the side of the slide rail. The output shaft of the motor one is fixedly sleeved with a ball screw, and the outer wall of the ball screw is threadedly connected to the inner wall of the saddle.

[0008] As a preferred technical solution of the present invention, a second motor is fixedly assembled on the side of the sliding saddle. The output shaft of the second motor is fixedly sleeved with a ball screw, and the outer edge of the ball screw is threadedly connected to the inner wall of the fixed frame.

[0009] As a preferred technical solution of the present invention, a third motor is fixedly assembled on the top of the fixed frame. The output shaft of the third motor is fixedly sleeved with a ball screw, and the outer edge of the ball screw is threadedly connected to the inner wall of the horizontal cross beam.

[0010] As a preferred technical solution of the present invention, the power assembly includes a base body. A gas storage bag is fixedly assembled on the side of the base body. An intake valve is fixedly assembled on the inner wall of the base body. A cylinder body is fixedly assembled on the side of the intake valve, and the inner cavity of the cylinder body passes through the inner cavity of the intake valve and is connected to the inner cavity of the gas storage bag. One end of the cylinder body away from the intake valve is fixedly assembled with a reset valve, and the inner cavity of the reset valve is connected to the inner cavity of the cylinder body.

[0011] As a preferred technical solution of the present invention, a piston rod is arranged inside the cylinder body, and a striking head is fixedly assembled on the side of the piston rod. A small cylinder is fixedly assembled on the side of the base body, and the output end of the small cylinder is slidably connected to the inner wall of the piston rod inside the cylinder body.

[0012] As a preferred technical solution of the present invention, the guide rail assembly includes multiple sections of bases and guide rails, and the inner walls of the multiple sections of bases and guide rails are slidably connected to the outer edge of the simulated bullet. A limiting device is fixedly assembled on the top of the multiple sections of bases and guide rails. A speed measurement radar is fixedly assembled on the top of the multiple sections of bases and guide rails. A reset motor is fixedly assembled at the bottom of the inner wall of the multiple sections of bases and guide rails. A pressure sensor array is fixedly assembled at the top of the inner wall of the multiple sections of bases and guide rails.

[0013] As a preferred technical solution of the present invention, the buffering and resetting assembly includes a striking seat. A hydraulic buffer is fixedly assembled on the side of the striking seat. One end of the hydraulic buffer away from the striking seat is fixedly assembled with a mounting seat. The side of the mounting seat is fixedly assembled with the side of the multiple sections of bases and guide rails, and the inner wall of the multiple sections of bases and guide rails is slidably connected to the bottom of the striking seat. A reset trolley is slidably connected to the inner wall of the multiple sections of bases and guide rails. A steel wire rope is fixedly assembled on the side of the reset trolley, and one end of the steel wire rope away from the reset trolley is movably sleeved on the output shaft of the reset motor.

[0014] As a preferred technical solution of the present invention, the control component includes a console, a display panel is fixedly assembled on the inner wall of the console, a control panel is fixedly assembled on the top of the console, and the control panel is electrically connected to the first motor, the second motor, the third motor, the intake valve, the air storage tank, the small cylinder, the reset valve, the reset motor, the limiting device, the speed measuring radar, and the pressure sensor array.

[0015] The present invention has the following beneficial effects:

[0016] 1. This simulation launch comprehensive test equipment, by using a general-purpose suspension tooling, an air storage tank as the power source, and a numerical control suspension system, can meet the reliability detection requirements of rail launch devices with different mounting methods for various models. By using a specially designed rail structure, it can effectively prevent the bounce during the launch of the simulation projectile, improve the safety during system testing, and by redesigning the size of the mounting tooling for the rail launch device, it can be extended to meet the mounting test needs of more models of launch devices. By changing the pressure of the high-pressure gas in the power system, it can be extended to meet the acceleration requirements of simulation projectiles with smaller or larger masses.

[0017] 2. This simulation launch comprehensive test equipment, by using multiple groups of limiting devices, prevents the simulation projectile from rebounding when decelerating and colliding with the rail launch device, causing damage, and uses a hydraulic buffer with a gas-liquid structure to prevent the simulation projectile from rebounding when decelerating.

[0018] 3. This simulation launch comprehensive test equipment can timely monitor the launch speed of the simulation projectile and perform functions such as data recording, analysis, display, and transmission. By using different types of sensors such as a pressure sensor array and a speed measuring radar, higher-precision speed measurement can be achieved and the measurement density can be improved.

[0019] 4. This simulation launch comprehensive test equipment has complete safety monitoring, alarm, and anti-misoperation functions. Description of the Drawings

[0020] Figure 1 It is a three-dimensional structure schematic diagram of the present invention;

[0021] Figure 2 It is a three-dimensional structure schematic diagram of the numerical control suspension and tooling component of the present invention;

[0022] Figure 3 It is a three-dimensional structure schematic diagram of the power component of the present invention;

[0023] Figure 4 It is a three-dimensional structure schematic diagram of the rail component of the present invention;

[0024] Figure 5 It is a three-dimensional structure schematic diagram of the buffer and reset component of the present invention;

[0025] Figure 6 Schematic diagram of the three-dimensional structure of the control component of the present invention

[0026] In the figure:

[0027] 1. Numerical control suspension and tooling component: 101. Machine tool main body; 102. Slide rail; 103. Motor 1; 104. Saddle; 105. Motor 2; 106. Fixed frame; 107. Motor 3; 108. Horizontal crossbeam; 109. Suspension tooling

[0028] 2. Power component: 201. Base body; 202. Air storage bag; 203. Cylinder body; 204. Intake valve; 205. Reset valve; 206. Impact head; 207. Small cylinder

[0029] 3. Guide rail component: 301. Multi-section base and guide rail; 302. Limit device; 303. Speed measurement radar

[0030] 4. Buffer and reset component: 401. Impact seat; 402. Hydraulic buffer; 403. Mounting seat; 404. Reset trolley; 405. Reset motor

[0031] 5. Control component: 501. Console; 502. Control panel; 503. Display panel

[0032] 6. Guide rail launching device

[0033] 7. Simulated projectile Specific implementation manners

[0034] Next, the technical solutions in the embodiments of the present invention will be clearly and completely described in conjunction with the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, rather than all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.

[0035] Please refer to Figure 1-6 , a simulated launch comprehensive test equipment, including a numerical control suspension and tooling component 1, a power component 2 is arranged on the side of the numerical control suspension and tooling component, a guide rail component 3 is fixedly assembled on the side of the power component 2, a buffer and reset component 4 is fixedly assembled at one end of the guide rail component 3 away from the power component 2, a control component 5 is arranged at one end of the guide rail component 3 away from the numerical control suspension and tooling component 1, a guide rail launching device 6 is fixedly assembled on the side of the numerical control suspension and tooling component 1, a simulated projectile 7 is slidably connected to the bottom of the guide rail launching device 6, and the outer edge of the simulated projectile 7 is connected to the inner wall of the guide rail component 3;

[0036] Adjust different toolings through the numerically controlled suspension and tooling component 1 to automatically or semi-automatically mount the rail launch devices 6 and simulated projectiles 7 with different models and mounting methods, and report the signal of successful mounting to the control component 5 after the mounting is completed;

[0037] After the mounting is completed, with the assistance of sensors, the axis of the simulated projectile 7 is automatically or manually aligned to the launch axis position, and it reports to the control component 5 that it has entered the launch position;

[0038] After receiving the launch command issued by the control component 5, the power component 2 intakes air to push the simulated projectile 7 to launch. The simulated projectile 7 moves along the rail launch device 6 at a certain speed. After overcoming the locking force of the rail launch device 6, it separates from the rail launch device 6 and falls into the multi-segment bases and rails 301 of the lower rail component 3 under the action of its own gravity. It is restricted and limited by the multi-segment bases and rails 301 and moves forward without jitter. The limiting devices 302 distributed in sequence on the multi-segment bases and rails 301 are opened in sequence as the simulated projectile 7 advances to prevent the simulated projectile 7 from rebounding and causing backward movement;

[0039] During this process, the speed measurement radar 303 installed on the rail component 3 records and analyzes the running speed and position data of the simulated projectile 7 in real time until the simulated projectile 7 decelerates to a standstill under the action of the buffering and resetting component 4, and the collected data is reported to the control component 5;

[0040] After receiving the reset command from the control component 5, the reset trolley 404 installed on the rail component 3 automatically resets the simulated projectile 7 to stop waiting directly below the rail launch device 6, completing one launch cycle.

[0041] In a preferred embodiment, the numerically controlled suspension and tooling assembly 1 includes a machine tool body 101. A slide rail 102 is fixedly assembled on the top of the machine tool body 101. A saddle 104 is slidably connected to the side of the slide rail 102. A fixing frame 106 is slidably connected to the side of the saddle 104. A horizontal crossbeam 108 is slidably connected to the side of the fixing frame 106. A suspension tooling 109 is fixedly assembled at the bottom of the horizontal crossbeam 108. The inner wall of the suspension tooling 109 is fixedly connected to the top of the guide rail launching device 6. The machine tool body 101 is the stable and load-bearing component of the numerically controlled suspension and tooling assembly 1. It is made of cast iron and is equipped with a three-axis displacement device, which can bear a vertical load of not less than 1 ton and a horizontal impact force of not less than 50 KN. The slide rail 102, motor 1 103, saddle 104, motor 2 105, fixing frame 106, and motor 3 107 form a three-axis displacement device. The three-axis displacement device enables the mounted guide rail launching device 6 to move and position within 3 degrees of freedom and meet the specified movement and positioning accuracy. The three-axis displacement uses the method of the saddle 104 moving on the slide rail 102 (x-axis), the fixing frame 106 moving on the saddle 104 (y-axis), and the horizontal crossbeam 108 moving on the fixing frame 106 (z-axis). The motors 1 103, 2 105, and 3 107 drive the ball screws in their respective directions, respectively driving the saddle 104, fixing frame 106, and horizontal crossbeam 108 to move and position. The Z-axis direction is designed to bear a vertical load of not less than 1 ton, and a hydraulic locking device is added in the x-axis direction so that the system can withstand a horizontal impact of not less than 50 KN after positioning. The suspension tooling 109 is installed on the horizontal crossbeam 108 and mounts the test guide rail launching device 6, which can meet the mounting requirements of the guide rail launching device 6 with multiple models and different mounting methods.

[0042] In a preferred embodiment, a motor 1 103 is fixedly assembled on the side of the slide rail 102. The output shaft of the motor 1 103 is fixedly sleeved with a ball screw, and the outer edge of the ball screw is threadedly connected to the inner wall of the saddle 104, thereby driving the saddle 104 to move and position horizontally on the top of the slide rail 102, realizing the movement and positioning of the numerically controlled suspension and tooling assembly 1 in the x-axis direction. The outer wall of the slide rail 102 is fixedly connected to the outer wall of the saddle 104 through a hydraulic locking device to assist the positioning of the saddle 104 and bear the horizontal impact.

[0043] In a preferred embodiment, a motor 2 105 is fixedly assembled on the side of the saddle 104, and the output shaft of the motor 2 105 is fixedly sleeved with a ball screw, and the outer edge of the ball screw is threadedly connected to the inner wall of the fixing frame 106. By the combined use of the motor 2 105 and the ball screw, the motor 2 105 drives the ball screw to rotate, thereby driving the fixing frame 106 to move and position horizontally on the top of the saddle 104, realizing the movement and positioning of the numerically controlled suspension and tooling assembly 1 in the Y-axis direction.

[0044] In a preferred embodiment, a third motor 107 is fixedly assembled at the top of the fixing frame 106. The output shaft of the third motor 107 is fixedly sleeved with a ball screw, and the outer edge of the ball screw is threadedly connected to the inner wall of the horizontal crossbeam 108. The third motor 107 is a servo motor with a brake, so as to drive the horizontal crossbeam 108 to move and position in the vertical direction of the fixing frame 106 by means of the ball screw, realizing the movement and positioning of the numerical control suspension and the tooling assembly 1 in the z-axis direction.

[0045] In a preferred embodiment, the power assembly 2 includes a base body 201. An air storage bag 202 is fixedly assembled on the side of the base body 201. An intake valve 204 is fixedly assembled on the inner wall of the base body 201. A cylinder body 203 is fixedly assembled on the side of the intake valve 204, and the inner cavity of the cylinder body 203 passes through the inner cavity of the intake valve 204 and is connected to the inner cavity of the air storage bag 202. One end of the cylinder body 203 away from the intake valve 204 is fixedly assembled with a reset valve 205, and the inner cavity of the reset valve 205 is connected to the inner cavity of the cylinder body 203. The base body 201 is the bearing foundation of the power assembly 2 and can bear a recoil force of no less than 50 KN generated during launch; the air storage bag 202 stores high-pressure gas and provides the high-pressure gas required for the launch of the high-pressure air cannon; the cylinder body 203 is the main body of the high-pressure air cannon in the power assembly 2 and is composed of a cylinder, a piston, a piston rod, a sealing assembly, etc. The intake valve 204 is composed of a three-way solenoid valve and a temperature and pressure sensor. Under the control of the control assembly 5, it controls the high-pressure gas to be filled into the air storage bag 202 and reach the specified pressure. When the cylinder piston resets, it makes the rear chamber of the cylinder and the air storage bag 202 communicate with the atmosphere to release the internal pressure gas, so that the piston can reset smoothly. The reset valve 205 is composed of a three-way solenoid valve and a temperature and pressure sensor. During the launch of the high-pressure air cannon, the front chamber of the cylinder is kept in communication with the atmosphere through the three-way solenoid valve. After the launch is completed, under the control of the control assembly 5, the solenoid valve controls the high-pressure gas to enter the front chamber of the cylinder and push the piston to move backward to complete the reset of the piston.

[0046] In a preferred embodiment, a piston rod is disposed inside the cylinder body 203, and an impact head 206 is fixedly assembled on the side surface of the piston rod. A small cylinder 207 is fixedly assembled on the side surface of the base body 201, and the output end of the small cylinder 207 is slidably connected to the inner wall of the piston rod in the cylinder body 203. The impact head 206 is installed at the head of the cylinder piston rod by a quick connection method and is made of a soft material (such as copper, aluminum or non-metallic composite material), which can be quickly replaced and increase the service life of the simulation bullet 7. Under the control of the control component 5, at the initial position, the piston rod of the cylinder body 203 moves to a position where it cooperates with the small cylinder 207, and the outer edge of the small cylinder 207 is docked with the inner wall of the piston rod to maintain the piston locking state, preparing to fill the cylinder body 203 with high-pressure gas. When it is necessary to launch the simulation bullet 7, under the control of the control component 5, the small cylinder 207 is inflated, the small cylinder 207 is activated, the piston and the impact head 206 of the cylinder body 203 are released, and the simulation bullet 7 is fired. After the firing is completed, the reset valve 205 assists the cylinder body 203 to reset and then completes the docking action between the inner wall of the piston rod and the small cylinder 207, preparing to refill the cylinder body 203 with gas. The inside of the cylinder body 203 is a piston and a piston rod. The impact head 206 is installed at the front of the piston rod. The piston divides the inner cavity of the cylinder body 203 into two front and rear chambers. The front chamber is filled and discharged with gas through the reset valve 205, and the rear chamber is communicated with the air storage bag 202 and can be filled and discharged with gas through the intake valve 204.

[0047] In a preferred embodiment, the rail assembly 3 includes multiple sections of bases and rails 301, and the inner walls of the multiple sections of bases and rails 301 are slidably connected to the outer edge of the simulation bullet 7. A limiting device 302 is fixedly assembled on the top of the multiple sections of bases and rails 301, a speed measuring radar 303 is fixedly assembled on the top of the multiple sections of bases and rails 301, a reset motor 405 is fixedly assembled on the inner wall of the multiple sections of bases and rails 301, and a pressure sensor array is fixedly assembled on the inner wall of the multiple sections of bases and rails 301. The multiple sections of bases and rails 301 are composed of multiple sections to meet the need for the movement and deceleration of the simulation bullet 7. The multiple sections of bases and rails 301 are symmetrically distributed along the movement axis of the simulation bullet 7 to limit the movement of the simulation bullet 7 in a specified direction. The initial section of the rail has a specific structure to prevent the simulation bullet 7 from rebounding when falling, so as to avoid the simulation bullet 7 from hanging and the tail colliding and damaging the rail launching device 6. The limiting devices 302 are sequentially distributed along the rail on the multiple sections of bases and rails 301. After the simulation bullet 7 passes through, it prevents the simulation bullet 7 from rebounding and opens before the reset system works, enabling the simulation bullet 7 to be reset smoothly. The speed measuring radar 303 measures the real-time position and speed information of the simulation bullet 7 and uploads it to the control component 5.

[0048] In a preferred embodiment, the buffer and reset assembly 4 includes an impact seat 401. A hydraulic buffer 402 is fixedly assembled on the side of the impact seat 401. One end of the hydraulic buffer 402 away from the impact seat 401 is fixedly assembled with a mounting seat 403. The side of the mounting seat 403 is fixedly assembled with the side of the multi-section base and guide rail 301. The inner wall of the multi-section base and guide rail 301 is slidably connected to the bottom of the impact seat 401. A reset trolley 404 is slidably connected to the inner wall of the multi-section base and guide rail 301. A steel wire rope is fixedly assembled on the side of the reset trolley 404. One end of the steel wire rope away from the reset trolley 404 is movably sleeved on the output shaft of the reset motor 405. The impact seat 401 is installed on the end base and guide rail and moves under the constraint of the guide rail. When the simulation projectile 7 moves to the end of the base, it impacts the impact seat 401 and finally decelerates and stops under the action of the hydraulic buffer 402. The hydraulic buffer 402 is installed on the mounting seat 403 to buffer the moving impact seat 401. The hydraulic buffer 402 uses a gas-liquid buffer and has the characteristic of preventing rebound after deceleration, avoiding the rebound of the simulation projectile 7 and damaging the guide rail launching device 6. The mounting seat 403 is located behind the end base, on which the hydraulic buffer 402 is installed and can withstand the impact force when the simulation projectile 7 decelerates and buffers. The reset trolley 404 moves on the guide rail, located between the impact seat 401 and the simulation projectile 7, and is pulled by the steel wire rope driven by the reset motor 405. The initial position of the reset trolley 404 ensures that when the simulation projectile 7 moves, it will not collide with the reset trolley 404, avoiding excessive instantaneous impact force from damaging the steel wire rope. During reset, the steel wire rope pulls the reset trolley 404, driving the simulation projectile 7 to move in the reverse direction along the guide rail for reset until it is directly below the guide rail launching device 6. The reset motor 405 is a friction-type two-way motor with a brake, which can drive the reset trolley 404 to move in both directions and stop in time when the trolley moves to the specified position.

[0049] In a preferred embodiment, the control component 5 includes a console 501. A display panel 503 is fixedly assembled on the inner wall of the console 501. A control panel 502 is fixedly assembled on the top of the console 501. The control panel 502 is electrically connected to the first motor 103, the second motor 105, the third motor 107, the intake valve 204, the air storage bag 202, the small cylinder 207, the reset valve 205, the reset motor 405, the limiting device 302, the speed measuring radar 303, and the pressure sensor array. The hanging tooling 109 is controlled by the control panel 502 to move to a suitable position to hang the rail launching device 6 and the simulation projectile 7. Then, the simulation projectile 7 is moved to the axis position of the impact head 206 of the power component 2, and the distance from the impact head 206 is adjusted to complete the hanging. The intake valve 204 of the power component 2 is controlled to open, and the air storage bag 202 starts to be pressurized. After the pressure reaches the set working pressure and stabilizes, the system issues a launch permission command, the small cylinder 207 is opened, the air cannon launches and impacts and pushes the simulation projectile 7 to start moving. At the same time, a speed measurement command is sent to the speed measuring radar 303. The limiting device 302 and the speed measuring radar 303 feedback the speed and position information of the simulation projectile 7 to the control component 5 in real time. After waiting for the simulation projectile 7 to stop completely, the control component 5 can give the speed curve of the simulation projectile 7 and display it on the display panel 503 and store it.

[0050] Working principle: When the device is in use, the control component 5 controls the numerical control hanging and tooling component 1 to adjust different toolings to automatically or semi-automatically mount the rail launching devices 6 and the simulation projectiles 7 of different models and different hanging methods. After the hanging is completed, a hanging completion signal is reported to the control component 5. Then, with the assistance of sensors, the axis line of the simulation projectile 7 is automatically or manually aligned to the launch axis position, and it is reported to the control component 5 to enter the launch position. After receiving the launch command issued by the control component 5, the power component 2 intakes air and pushes the simulation projectile 7 to launch. The simulation projectile 7 moves along the rail launching device 6 at a certain speed. After overcoming the locking force of the rail launching device 6, it separates from the rail launching device 6 and falls into the multi-section base and rail 301 of the lower rail component 3 under the action of its own gravity. It is restricted and limited by the multi-section base and rail 301 and keeps moving forward without jumping. The limiting devices 302 distributed in sequence on the multi-section base and rail 301 are opened in sequence as the simulation projectile 7 moves forward to prevent the simulation projectile 7 from rebounding and causing backward movement. During this process, the speed measuring radar 303 installed on the rail component 3 records and analyzes the running speed and position data of the simulation projectile 7 in real time until the simulation projectile 7 decelerates until it stops under the action of the buffering and resetting component 4. The collected data is reported to the control component 5. The control component 5 can give the speed curve of the simulation projectile 7 and display it on the display panel 503 and store it. After receiving the reset command of the control component 5, the reset trolley 404 installed on the rail component 3 automatically resets the simulation projectile 7 to stop waiting directly below the rail launching device 6, completing one launch cycle.

[0051] It should be noted that in this text, relational terms such as first and second are only used to distinguish one entity or operation from another entity or operation, and do not necessarily require or imply any actual relationship or order between these entities or operations. Moreover, the terms "include", "comprise" or any other variant thereof are intended to cover non-exclusive inclusion, such that a process, method, article or device comprising a series of elements includes not only those elements but also other elements not expressly listed, or elements inherent to such process, method, article or device.

[0052] Although the embodiments of the present invention have been shown and described, those of ordinary skill in the art can understand that various changes, modifications, substitutions and variations can be made to these embodiments without departing from the principles and spirit of the present invention. The scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. The simulated launch comprehensive test equipment, including a numerically controlled suspension and tooling assembly (1), is characterized in that: On the side of the described (1) numerically controlled suspension and tooling assembly, a power assembly (2) is provided. On the side of the power assembly (2), a guide rail assembly (3) is fixedly assembled. At one end of the guide rail assembly (3) far from the power assembly (2), a buffer and reset assembly (4) is fixedly assembled. At one end of the guide rail assembly (3) far from the numerically controlled suspension and tooling assembly (1), a control assembly (5) is provided. On the side of the numerically controlled suspension and tooling assembly (1), a guide rail launching device (6) is provided. The bottom of the guide rail launching device (6) is slidably connected to a simulated bullet (7), and the outer edge of the simulated bullet (7) is connected to the inner wall of the guide rail assembly (3).

2. The simulated launch comprehensive test equipment according to claim 1, wherein: The described numerically controlled suspension and tooling assembly (1) includes a machine tool body (101). On the top of the machine tool body (101), a three-axis displacement device is fixedly assembled. On the side of the three-axis displacement device, a horizontal crossbeam (108) is fixedly assembled. At the bottom of the horizontal crossbeam (108), a suspended tooling (109) is fixedly assembled. The inner wall of the suspended tooling (109) is fixedly connected to the top of the guide rail launching device (6).

3. The simulated launch comprehensive test equipment according to claim 1, characterized in that: The described power assembly (2) includes a base body (201). On the side of the base body (201), an air storage bag (202) is fixedly assembled. Inside the base body (201), an air inlet valve (204) is fixedly assembled. On the side of the air inlet valve (204), a cylinder body (203) is fixedly assembled. The inner cavity of the cylinder body (203) passes through the inner cavity of the air inlet valve (204) and is connected to the inner cavity of the air storage bag (202). At one end of the cylinder body (203) far from the air inlet valve (204), a reset valve (205) is fixedly assembled, and the inner cavity of the reset valve (205) is connected to the inner cavity of the cylinder body (203).

4. The simulated launch comprehensive test equipment according to claim 3, characterized in that: Inside the cylinder body (203), a piston rod is provided. On the side of the piston rod, an impact head (206) is fixedly assembled. On the side of the base body (201), a small cylinder (207) is fixedly assembled, and the output end of the small cylinder (207) is slidably connected to the inner wall of the piston rod in the cylinder body (203).

5. The simulated launch comprehensive test equipment according to claim 1, characterized in that: The described guide rail assembly (3) includes multiple sections of bases and guide rails (301). The inner wall of the multiple sections of bases and guide rails (301) is slidably connected to the outer edge of the simulated bullet (7). On the top of the multiple sections of bases and guide rails (301), a limiting device (302) is fixedly assembled. On the top of the multiple sections of bases and guide rails (301), a speed measurement radar (303) is fixedly assembled. Inside the inner wall of the multiple sections of bases and guide rails (301), a reset motor (405) is fixedly assembled. Inside the inner wall of the multiple sections of bases and guide rails (301), a pressure sensor array is fixedly assembled.

6. The analog launch comprehensive test equipment according to claim 1, characterized in that: The buffer and reset assembly (4) includes an impact seat (401), a hydraulic buffer (402) is fixedly assembled on the side of the impact seat (401), a mounting seat (403) is fixedly assembled at the end of the hydraulic buffer (402) away from the impact seat (401), the side of the mounting seat (403) is fixedly assembled with the side of the multi-section base and guide rail (301), and the inner wall of the multi-section base and guide rail (301) is slidably connected to the bottom of the impact seat (401). A reset trolley (404) is slidably connected to the inner wall of the multi-section base and guide rail (301), a steel wire rope is fixedly assembled on the side of the reset trolley (404), and one end of the steel wire rope away from the reset trolley (404) is movably sleeved on the output shaft of the reset motor (405).

7. The simulated launch comprehensive test equipment according to claim 1, characterized in that: The control assembly (5) includes a control console (501), a display panel (503) is fixedly assembled on the inner wall of the control console (501), a control panel (502) is fixedly assembled on the top of the control console (501), and the control panel (502) is electrically connected to the first motor (103), the second motor (105), the third motor (107), the intake valve (204), the air storage tank (202), the small cylinder (207), the reset valve (205), the reset motor (405), the limiting device (302), the speed measuring radar (303), and the pressure sensor array.

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