Portable anti-aircraft missile training device and method

Abstract

The application provides a portable anti-air missile training device and a use method, which comprises: a sighting training cartridge (1), a launching mechanism (2), a ground power supply and gas supply switching device (3), a ground energy source (4), a gas supply cylinder (5), and a matched pipeline (6) and wire (7). The sighting training cartridge can simulate the interception, unlocking and launching functions of a real portable anti-air missile under the action of the ground energy source power supply and the gas supply cylinder gas supply, so as to achieve the purpose of training marksmen and commanders. The application can train the whole process of the marksmen's sighting, interception, unlocking and launching under the condition of keeping the same quality and rotational inertia as the real missile, and the sighting training cartridge can truly respond to the actions of the marksmen. Compared with the existing training equipment, the application can truly show the missile instantaneous field of view, tracking field of view, electric lock and unlocking state.

Description

TECHNICAL FIELD

[0001] The present application relates to the technical field of missiles, in particular to a portable air defense missile training device and a use method. BACKGROUND

[0002] A missile is a weapon that relies on its own power device to propel, guided by a guidance system to control its flight trajectory, guide the warhead to the target and destroy it.

[0003] Before shooting a portable air defense missile with a real bullet, the shooter needs to undergo a lot of training to master the shooting essentials and the ability to handle special situations. However, the training devices currently used by the shooter are as follows: (1) a weight training bullet filled with an empty cartridge after launching; (2) an operation training bullet with only structure and electrical interface but no electrical function; (3) a sighting training bullet without a real seeker. The above three training devices either differ from the mass and moment of inertia of the real cartridge bullet, or cannot truly reflect the target detection capability of the missile, cannot realize the interaction between the cartridge bullet and the shooter, and cannot truly simulate the target interception, seeker unlocking and precession of the missile, affecting the training experience of the shooter training. SUMMARY

[0004] In view of the defects in the prior art, the purpose of the present application is to provide a portable air defense missile training device and a use method.

[0005] According to the portable air defense missile training device provided by the present application, it comprises: a sighting training cartridge bullet 1, a launching mechanism 2, a ground power and gas supply adapter 3, a ground energy source 4, a gas supply cylinder 5, a matching conduit 6 and a wire 7;

[0006] The sighting training cartridge bullet 1 is connected with the launching mechanism 2 through the socket and the pin;

[0007] The sighting training cartridge bullet 1 is connected with the gas supply cylinder 5 through the ground power and gas supply adapter 3 and the matching conduit 6; the gas supply cylinder 5 cools the sighting training cartridge bullet 1;

[0008] The sighting training cartridge bullet 1 is connected with the ground energy source 4 through the ground power and gas supply adapter 3 and the wire 7; the ground energy source 4 supplies power to the sighting training cartridge bullet 1.

[0009] Preferably, the sighting training cartridge bullet 1 comprises a guidance cabin 101, a weight warhead cabin 102 and a weight engine cabin 103 connected in sequence;

[0010] The guidance cabin 101 is connected with the weight warhead cabin 102 through threads, and the weight warhead cabin 102 is connected with the weight engine cabin 103 through threads;

[0011] The guidance cabin 101 comprises a seeker and a control cabin;

[0012] The counterweight warhead compartment 102 has the same mass and moment of inertia as the real missile's warhead compartment;

[0013] The counterweight engine compartment 103 has the same mass and moment of inertia as the real missile's engine compartment.

[0014] Preferably, the seeker of the training cartridge 1 is an infrared detector, the guidance compartment 101 modulates the continuous infrared radiation emitted by the target into pulse signals, and calculates the relative position of the target through the calculation of the on-board computer, and sends a missile capture signal to the launching mechanism 2, after the launching mechanism 2 receives the signal, it supplies power to the LED indicator light and the buzzer on the training cartridge 1, at this time, the LED light is on and the buzzer is ringing, prompting the shooter that the missile has captured the target, and the seeker is in an electrically locked state, after the first gear of the launching mechanism 2 is pressed, the seeker is unlocked and enters the tracking state, at this time, as long as the target does not leave the tracking field of view of the seeker, the missile will not lose the target, after waiting, the second gear of the launching mechanism 2 is pressed, and the on-board computer detects the second gear pressing signal, delays for a period of time, and then immediately executes the ignition program to simulate the missile launch.

[0015] Preferably, after the training cartridge 1 captures the target, the LED light on the training cartridge 1 is on and the buzzer is ringing at this time, the missile is in an electrically locked state, the shooter deviates from the infrared source through the front and rear sights on the training cartridge 1, when the LED light on the training cartridge 1 is off and the buzzer is not ringing, the angle of the training cartridge 1 is the instantaneous field of view of the seeker; the instantaneous field of view represents the field of view of the guidance compartment 101 at any instant.

[0016] Preferably, after the training cartridge 1 captures the target, the buzzer on the training cartridge 1 is ringing and the LED light is on, the shooter presses the first gear of the launching mechanism at this time, the guidance compartment 101 is in an unlocked state, the buzzer and the LED light on the training cartridge 1 remain bright, the shooter deviates from the infrared source through the front and rear sights on the training cartridge 1, until the LED light is off and the buzzer is not ringing, at this time, the angle of the training cartridge 1 is the tracking field of view, and the tracking field of view represents the range of the guidance compartment 101 tracking the target.

[0017] Preferably, the target is a 200W incandescent bulb placed 50 meters in front of the training cartridge 1.

[0018] Preferably, the gas supply cylinder and the ground energy source can be reused.

[0019] The application provides a use method of the portable anti-air missile training device.

[0020] Preferably, the launching mechanism 2 is connected with the aiming training cartridge missile 1, the ground energy source 4 is connected with the aiming training cartridge missile 1 through the ground power and gas supply adapter 3 and the wire 7, the gas supply cylinder 5 is connected with the aiming training cartridge missile 1 through the ground power and gas supply adapter 3 and the matched pipeline, the incandescent bulbs are placed in front of the aiming training cartridge missile 1, the incandescent bulbs are lightened in sequence, the valve of the gas supply cylinder 5 is opened, the power switch of the ground energy source 4 is opened, the aiming training cartridge missile 1 aims at the incandescent bulbs, when the buzzer of the aiming training cartridge missile 1 rings and the LED light is bright, the shooter presses the first gear of the launching mechanism 2, then waits, and presses the second gear of the launching mechanism 2, and the missile launching is implemented.

[0021] Preferably, the launching mechanism 2 is connected with the aiming training cartridge missile 1, the ground energy source 4 is connected with the aiming training cartridge missile 1 through the ground power and gas supply adapter 3 and the wire 7, the gas supply cylinder 5 is connected with the aiming training cartridge missile 1 through the ground power and gas supply adapter 3 and the matched pipeline, the incandescent bulbs are placed in front of the aiming training cartridge missile 1, the incandescent bulbs are lightened in sequence, the valve of the gas supply cylinder 5 is opened, the power switch of the ground energy source 4 is opened, the aiming training cartridge missile 1 aims at the incandescent bulbs, when the buzzer of the aiming training cartridge missile 1 rings and the LED light is bright, the shooter presses the first gear of the launching mechanism 2, then waits, and presses the second gear of the launching mechanism 2, and the missile launching is implemented.

[0022] Compared with the prior art, the application has the beneficial effects as follows:

[0023] 1. The aiming training cartridge of the present application can simulate the interception, unlocking and launching functions of a real portable air defense missile under the action of ground energy supply and gas cylinder gas supply, so as to train the shooter and commander.

[0024] 2. The present application can train the whole process of aiming, interception, unlocking and launching of the shooter while keeping the same mass and rotational inertia as the real missile, and the aiming training cartridge can truly respond to the actions of the shooter.

[0025] 3. Compared with the operation of the real missile, the gas cylinder and ground energy supply of the training device can be reused, avoiding the shortcomings that the real ground energy and gas source can only be used once.

[0026] 4. Compared with the existing training equipment, the present application can truly show the instantaneous field of view, tracking field of view, electric lock and unlocking state of the missile. BRIEF DESCRIPTION OF DRAWINGS

[0027] Other features, objects and advantages of the present application will become more apparent from the following detailed description of non-limiting embodiments, made with reference to the accompanying drawings:

[0028] Figure 1 The portable air defense missile training device structure schematic diagram provided by the present application.

[0029] Figure 2 The structure schematic diagram of the aiming training cartridge in the portable air defense missile training device provided by the present application.

[0030] Figure 3 The working principle schematic diagram of the present application.

[0031] The drawings show:

[0032] DETAILED DESCRIPTION

[0033] The present application will be described in detail below with specific embodiments. The following embodiments will help those skilled in the art to further understand the present application, but do not limit the present application in any form. It should be noted that for those skilled in the art, without departing from the concept of the present application, a number of changes and improvements can be made. These all belong to the protection scope of the present application.

[0034] The purpose of the present application is to make up for the shortcomings of the existing training equipment, realize the ability of real cartridge detection target, and realize the interaction between the real cartridge and the shooter.

[0035] As Figure 1As shown, according to the portable anti-air missile training device provided by the application, it comprises: a sighting training cartridge 1, a launching mechanism 2, a ground power supply and gas supply adapter 3, a ground energy source 4, a gas supply cylinder 5, and a matched conduit 6 and wire 7. The gas supply cylinder 5 is connected to the ground power supply and gas supply adapter 3 through the conduit 6; the gas supply cylinder 5 uses high-pressure high-purity nitrogen to cool the sighting training cartridge 1 through the ground power supply and gas supply adapter 3 and the matched conduit 6. The ground energy source 4 is electrically connected to the ground power supply and gas supply adapter 3 through the wire 7, and the ground energy source 4 uses rechargeable lithium batteries to supply power to the sighting training cartridge through the ground power supply and gas supply adapter 3 and the wire 7; the sighting training cartridge 1 is connected to the launching mechanism 2 through a socket and a pin; the sighting training cartridge 1 is connected to the gas supply cylinder 5 through the ground power supply and gas supply adapter 3 and the matched conduit 6; and the sighting training cartridge 1 is connected to the ground energy source 4 through the ground power supply and gas supply adapter 3 and the wire 7.

[0036] As shown in the figure, Figure 2 As shown, the sighting training cartridge 1 comprises a guidance cabin 101, a counterweight warhead cabin 102, and a counterweight engine cabin 103 connected in sequence. The guidance cabin 101 and the counterweight warhead cabin 102 are connected by threads, and the counterweight warhead cabin 102 and the counterweight engine cabin 103 are connected by threads. The guidance cabin 101 comprises a seeker and a control cabin, and its main functions are to detect and identify target information, resist infrared interference, stably track the target, measure the line-of-sight angular velocity of the target, form a control command, drive the rudder to deflect, and control the missile to fly along the trajectory determined by the guidance law to the target; the counterweight warhead cabin 102 has the same mass and rotational inertia as the real missile warhead cabin; and the counterweight engine cabin 103 has the same mass and rotational inertia as the real missile engine cabin. The sighting training cartridge 1 is connected to the missile through a fixed pin.

[0037] The working process of the application is as follows: the launching mechanism 2 is connected to the sighting training cartridge 1, and the ground energy source 4 and the gas supply cylinder 5 are connected to the sighting training cartridge 1 through the ground power supply and gas supply adapter 3, the matched conduit 6, and the wire 7. An infrared source such as an incandescent bulb is placed at a suitable position from the sighting training cartridge 1. After the sighting training cartridge 1 aims at the target, the missile gives an interception command, which is transmitted to the sighting training cartridge 1 through the launching mechanism 2, and the indicator light on the sighting training cartridge 1 is lit, and the buzzer on the sighting training cartridge 1 is sounded, prompting the shooter that the missile has captured the target. The shooter presses the first gear of the launching mechanism according to the operation process, the seeker is unlocked, the bit marker precesses, and the seeker enters the tracking state. At this time, the indicator light is still on and the buzzer keeps sounding. After 0.5s, the shooter presses the second gear of the launching mechanism, and the missile executes the launch command from the launching mechanism.

[0038] During the launching process, the shooter can truly understand the concept of instantaneous field of view and tracking field of view through the aiming training cartridge 1. Specifically, the aiming training cartridge 1 intercepts the target, and after the LED light on the aiming training cartridge 1 is on and the buzzer rings, the missile is in an electric lock state. The shooter slowly deviates from the infrared source through the front and rear sights on the aiming training cartridge 1. When the LED light on the aiming training cartridge 1 is off and the buzzer does not ring, the angle of deviation of the aiming training cartridge 1 is the instantaneous field of view of the seeker. The instantaneous field of view represents the field of view of the guidance cabin 101 at any instant.

[0039] After the aiming training cartridge 1 intercepts the target, the buzzer on the aiming training cartridge 1 rings and the LED light is on. The shooter presses the first gear of the launching mechanism. At this time, the guidance cabin 101 is in an unlocked state. The buzzer and the LED light on the aiming training cartridge 1 remain in a bright state. The shooter slowly deviates from the infrared source through the front and rear sights on the aiming training cartridge 1 until the LED light is off and the buzzer does not ring. At this time, the angle of deviation of the guidance cabin 101 is the tracking field of view. The tracking field of view represents the range of the guidance cabin 101 tracking the target.

[0040] Through the aiming training device, the shooter can truly experience the real response of the cartridge during the launching process of the missile. During the training process, the shooter can experience the concept of the instantaneous field of view and the tracking field of view of the guidance cabin 101 and have a clear understanding of the physical meaning of the electric lock and unlock of the guidance cabin 101.

[0041] More specifically, in more preferred examples, the use method of the present application is as follows:

[0042] In one preferred example, the launching mechanism 2 is connected to the aiming training cartridge 1. The ground energy source 4 is connected to the aiming training cartridge 1 through the ground power and gas supply switching device 3 and the lead wire 7. The gas supply cylinder 5 is connected to the aiming training cartridge 1 through the ground power and gas supply switching device 3 and the matching conduit. A 200W incandescent bulb is placed 50 meters in front of the aiming training cartridge 1. The incandescent bulbs are lit in turn. The valve of the gas supply cylinder 5 is opened. The power switch of the ground energy source 4 is turned on. The aiming training cartridge 1 aims at the incandescent bulb. After the buzzer on the aiming training cartridge 1 rings and the LED light is on, the first gear of the launching mechanism 2 is pressed. After 0.5s, the second gear of the launching mechanism 2 is pressed, and the missile is launched.

[0043] In another preferred embodiment, the launching mechanism 2 is connected with the aiming training cartridge bullet 1, the ground energy source 4 is connected with the aiming training cartridge bullet 1 through the ground power and gas supply adapter 3 and the wire 7, the gas cylinder 5 is connected with the aiming training cartridge bullet 1 through the ground power and gas supply adapter 3 and the matched pipe, a 200W incandescent bulb is placed 50 meters in front of the aiming training cartridge bullet 1, the incandescent bulbs are lightened in turn, the valve of the gas cylinder 5 is opened, the power switch of the ground energy source 4 is turned on, the incandescent bulb is aimed at by the aiming training cartridge bullet 1, when the buzzer and the LED lamp of the aiming training cartridge bullet 1 are on, the guidance cabin 101 is in the electric lock state, the shooter slowly deviates from the infrared source through the front and rear sights of the aiming training cartridge bullet 1, when the indicator light of the aiming training cartridge bullet 1 is off and the buzzer is not on, the angle of the aiming training cartridge bullet 1 deviation is the instantaneous field of view of the seeker. The instantaneous field of view represents the field of view of the missile at any instant.

[0044] In another preferred embodiment, the launching mechanism 2 is connected with the aiming training cartridge bullet 1, the ground energy source 4 is connected with the aiming training cartridge bullet 1 through the ground power and gas supply adapter 3 and the wire 7, the gas cylinder 5 is connected with the aiming training cartridge bullet 1 through the ground power and gas supply adapter 3 and the matched pipe, a 200W incandescent bulb is placed 50 meters in front of the aiming training cartridge bullet 1, the incandescent bulbs are lightened in turn, the valve of the gas cylinder 5 is opened, the power switch of the ground energy source 4 is turned on, the incandescent bulb is aimed at by the aiming training cartridge bullet 1, when the buzzer and the LED lamp of the aiming training cartridge bullet 1 are on, the guidance cabin 101 is in the electric lock state, the shooter slowly deviates from the infrared source through the front and rear sights of the aiming training cartridge bullet 1, when the indicator light of the aiming training cartridge bullet 1 is off and the buzzer is not on, the angle of the aiming training cartridge bullet 1 deviation is the instantaneous field of view of the seeker. The instantaneous field of view represents the field of view of the missile at any instant.

[0045] As shown in Figure 3 , the working principle of the present application is:

[0046] The detector of the aiming training cartridge 1 is a high-sensitivity infrared detector, and the ground energy 4 supplies power to the aiming training cartridge 1 through the ground power supply and gas switching device 3. The gas cylinder 5 supplies gas to the aiming training cartridge 1 through the ground common-point gas switching device, and the guiding cabin 101 modulates the continuous infrared radiation emitted by the target into a pulse signal under the action of the refrigeration of the aiming training cartridge 1, and calculates the relative position of the target through the on-board computer, and sends a missile capture signal to the launching mechanism 2. After the launching mechanism 2 receives the signal, the LED indicator light and the buzzer on the aiming training cartridge 1 are powered, at this time, the LED light is bright and the buzzer is ringing, prompting the shooter that the missile has captured the target, and the seeker is in an electrically locked state. After the first gear of the launching mechanism 2 is pressed, the seeker is unlocked and enters the tracking state. At this time, as long as the target does not leave the tracking field of view of the seeker, the missile will not lose the target, and after waiting for 0.5s, the second gear of the launching mechanism 2 is pressed, and the on-board computer detects the signal and executes the ignition program after a delay, and the simulated missile is launched.

[0047] In the description of the present application, it should be understood that the terms "upper", "lower", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer" and the like indicate the orientation or positional relationship based on the orientation or positional relationship shown in the drawings, and are only for the convenience of describing the present application and simplifying the description, and do not indicate or imply that the devices or elements referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore cannot be understood as limiting the present application.

[0048] The specific embodiments of the present application are described above. It should be understood that the present application is not limited to the above specific embodiments, and those skilled in the art can make various changes or modifications within the scope of the claims, which does not affect the essential content of the present application. In the case of no conflict, the embodiments of the present application and the features in the embodiments can be arbitrarily combined.

Claims

1. A portable anti-aircraft missile training device, characterized in that, The application relates to a sighting training cartridge bullet (1), a launching mechanism (2), a ground power and gas supply switching device (3), a ground energy source (4), a gas supply cylinder (5) and matched pipes (6) and wires (7). The sighting training cartridge bullet (1) is connected with the launching mechanism (2) through a socket and a pin. The sighting training cartridge bullet (1) is connected with the gas supply cylinder (5) through the ground power and gas supply switching device (3) and the matched pipes (6); the gas supply cylinder (5) supplies refrigeration for the sighting training cartridge bullet (1). The sighting training cartridge bullet (1) is connected with the ground energy source (4) through the ground power and gas supply switching device (3) and the wires (7); the ground energy source (4) supplies power for the sighting training cartridge bullet (1). The sighting training cartridge bullet (1) comprises a guiding cabin (101), a counterweight warhead cabin (102) and a counterweight engine cabin (103) connected in sequence. The guiding cabin (101) and the counterweight warhead cabin (102) are connected through threads, and the counterweight warhead cabin (102) and the counterweight engine cabin (103) are connected through threads. The guiding cabin (101) comprises a seeker and a control cabin. The counterweight warhead cabin (102) has the same mass and rotational inertia as a real missile warhead cabin. The counterweight engine cabin (103) has the same mass and rotational inertia as a real missile engine cabin. The sighting training cartridge bullet 1 detector is an infrared detector; the guiding cabin (101) modulates continuous infrared radiation emitted by a target into pulse signals, calculates the relative position of the target through a bullet computer, and sends a missile capture signal to the launching mechanism (2); after receiving the signal, the launching mechanism (2) supplies power to LED indicator lights and a buzzer on the sighting training cartridge bullet (1); at this time, the LED lights are bright and the buzzer is on, prompting the shooter that the missile has captured the target and the seeker is in an electric lock state; after the first gear of the launching mechanism (2) is pressed, the electric lock of the seeker is released and the seeker enters a tracking state; at this time, as long as the target does not leave the tracking field of view of the seeker, the missile will not lose the target; after the second gear of the launching mechanism (2) is pressed, the bullet computer detects the second gear pressing signal, delays for a period of time and then immediately executes a firing program to simulate missile launching.

2. The portable anti-aircraft missile training device according to claim 1, characterized in that After the sighting training cartridge bullet (1) captures the target, the LED lights on the sighting training cartridge bullet (1) are bright and the buzzer is on; at this time, the missile is in an electric lock state; the shooter offsets the infrared source through the front and rear sights on the sighting training cartridge bullet (1); when the LED lights on the sighting training cartridge bullet (1) are off and the buzzer is not on, the angle of the sighting training cartridge bullet (1) offset is the instantaneous field of view of the seeker; the instantaneous field of view represents the field of view of the guiding cabin (101) at any moment.

3. The portable anti-aircraft missile training device according to claim 2, characterized in that ​ 4. The portable anti-aircraft missile training device according to claim 3, characterized in that The target is a 200W incandescent bulb placed 50 meters in front of the aiming training cartridge (1).

5. The portable anti-aircraft missile training device of claim 2, wherein, The gas supply cylinder and the ground energy source can be reused.

6. The portable anti-aircraft missile training device of claim 1, wherein, The launching mechanism (2) is connected with the aiming training cartridge (1), the ground energy source (4) is connected with the aiming training cartridge (1) through the ground power supply and gas supply switching device (3) and the wire (7), the gas supply cylinder (5) is connected with the aiming training cartridge (1) through the ground power supply and gas supply switching device (3) and the matched pipeline, the incandescent bulbs are placed in front of the aiming training cartridge (1), the incandescent bulbs are lightened in turn, the valve of the gas supply cylinder (5) is opened, the power switch of the ground energy source (4) is turned on, the incandescent bulbs are aimed by the aiming training cartridge (1), after the buzzer of the aiming training cartridge (1) rings and the LED light is on, the first gear of the launching mechanism (2) is pressed, then the second gear of the launching mechanism (2) is pressed after waiting, and the missile launching is implemented.

7. A method of using the portable anti-aircraft missile training device according to any one of claims 1 to 6, characterized in that, The launching mechanism (2) is connected with the aiming training cartridge (1), the ground energy source (4) is connected with the aiming training cartridge (1) through the ground power supply and gas supply switching device (3) and the wire (7), the gas supply cylinder (5) is connected with the aiming training cartridge (1) through the ground power supply and gas supply switching device (3) and the matched pipeline, the incandescent bulbs are placed in front of the aiming training cartridge (1), the incandescent bulbs are lightened in turn, the valve of the gas supply cylinder (5) is opened, the power switch of the ground energy source (4) is turned on, the incandescent bulbs are aimed by the aiming training cartridge (1), after the buzzer of the aiming training cartridge (1) rings and the LED light is on, the first gear of the launching mechanism (2) is pressed, then the second gear of the launching mechanism (2) is pressed after waiting, and the missile launching is implemented.

8. The method of using the portable anti-aircraft missile training device of claim 7, wherein, ​ 9. The method of using the portable anti-aircraft missile training device of claim 8, wherein, The launching mechanism (2) is connected with the aiming training cartridge bullet (1), the ground energy (4) is connected with the aiming training cartridge bullet (1) through the ground power supply and gas supply switching device (3) and the wire (7), the gas supply cylinder (5) is connected with the aiming training cartridge bullet (1) through the ground power supply and gas supply switching device (3) and the matched pipeline, the incandescent bulbs are placed in front of the aiming training cartridge bullet (1), the incandescent bulbs are lighted in sequence, the valve of the gas supply cylinder (5) is opened, the power supply switch of the ground energy (4) is turned on, the aiming training cartridge bullet (1) aims at the incandescent bulb, after the buzzer on the aiming training cartridge bullet (1) rings and the LED lamp is lighted, the shooter presses the first gear of the launching mechanism (2), at this time, the guidance cabin (101) is in the unlocked state, the buzzer and the indicator lamp on the aiming training cartridge bullet (1) still keep the loud state, the shooter deviates from the infrared source through the front and rear sights on the aiming training cartridge bullet (1) until the indicator lamp is extinguished and the buzzer does not ring, at this time, the angle of the missile deviation is the tracking field of view, and the tracking field of view represents the range of the missile tracking the target.

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