FULLY AUTOMATIC LANE-FEEDED CLOSE-RANGE AIR DEFENSE SYSTEM
Patent Information
- Application Number
- TR202615181U
- Authority / Receiving Office
- TR · TR
- Patent Type
- Utility models
- Current Assignee / Owner
- Filing Date
- 2026-09-04
- Publication Date
- 2026-09-21
- Estimated Expiration
- 2036-09-04
Smart Images
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Abstract
Description
1 TARIFF FULLY AUTOMATIC LANE-FEEDED CLOSE-RANGE AIR DEFENSE SYSTEM TECHNICAL AREA 5 The invention is in the field of defense industry; it is a fully automated belt-fed, close-range system. fully automated strip that can be used to neutralize aerial threats (drones, etc.) It relates to powered close-range air defense systems. STATE OF THE ART Today, close-range aerial threats such as unmanned aerial vehicles are ineffective. Defense systems with different operating principles, with the aim of making them available. is used. In this context, fully automatic weapon systems with magazine or belt feed are used with 15 Smoothbore rifle-based systems are among the known applications. Belt-fed systems, magazine-fed systems. Higher ammunition capacity and longer continuous firing capability compared to other systems. It can provide. The amount of ammunition that can be used in current magazine-fed systems is limited to the physical capacity of the magazine and is 20. It is limited. Especially for vehicles moving quickly at close range or those that need to move multiple objects in a short period of time. In situations where an air threat emerges, the ammunition is quickly depleted, the magazine... This requires changing or reloading the system. This interrupts the firing. This led to the failure and the inability to maintain uninterrupted fire intensity in the face of the threat. It is possible. Indeed, in automatic weapons, box and drum type magazines have a capacity of 25. It has physical limitations, and lane feeding can be done more easily with lanes that can be joined together. It is known to enable high ammunition capacity. Another current application is for smoothbore rifles capable of using particulate ammunition at close range. It is used against air threats. The large number of fragments scattered by this type of ammunition is 30 While it can increase the area where the target can be hit, the tube-type automatic rifles used in current smoothbore shotguns... or the capacity of magazine-based ammunition feeding systems may be limited. For example, tube-based In systems with a magazine, the magazine length directly determines the amount of ammunition that can be carried. This limits the range; when the ammunition runs out, the need for reloading arises. 35 In addition, a significant portion of existing automated systems contain moving mechanisms. Friction between them leads to heating and expansion during prolonged and intense operation. 2 This can lead to operational problems. In moving systems, during long operating hours... to reduce seizing that may occur due to heating and expansion. the need arises. In belt-fed systems, providing a high ammunition capacity is sufficient on its own. 5 not, but the importance of guiding the ammunition in an orderly fashion along the feed line. It involves the bending or twisting of flexible strips under the effect of movement and rebound. This can cause feeding problems. Therefore, especially at high rates of fire. holding the ammunition belt in a specific position, towards the ammunition feeding mechanism transferred in this manner and brought to a ready position synchronized with the next ammunition firing cycle 10 It needs to be brought. In the known technology; high ammunition capacity, uninterrupted belt feeding, and particulate matter. ammunition usage, controlled guidance of ammunition, and low friction a structure that can provide an automated operating mechanism within the same system 15 There is a need for capacity limitations in current applications, and refilling is necessary. Due to the resulting interruptions in firing, feeding and guidance problems, and intense mechanical problems that may arise during the operation, against close-range air threats. This highlights the need to develop a more effective system. "Remote-controlled weapon" with application number US201314406077, in the known state of the art. "A munitions feeder located at the station, loaded by a belt / metallic link chain" invention The patent application titled "Remotely Operated Weapon Station (RCWS)" Ammunition feeder loaded with belt / metallic link chain. The feeder is chained. a 25 to guide the ammunition from the ammunition magazine to the bullet entry point of the weapon It includes a feeding mechanism. The feeding mechanism feeds the chained ammunition into the ammunition. a first one to direct from its reservoir towards the RCWS's raising / lowering axis area from the chute assembly and the weapon's raising / lowering axis area for chained ammunition It has a second groove assembly to continue guiding the projectile toward the entry port. The chained ammunition passes from the first chute assembly to the second chute assembly 30 It traverses the raising / lowering axis region. While the first chute assembly remains fixed, the second chute... The assembly is dynamic and, together with the mounting bracket assembly, moves around the raising / lowering axis. This document describes the lane as being moved while the turret is in motion. It focuses on RCSW architecture related to ammunition storage and delivery to the weapon. However, the guide body, rail, tension cover, and controlled 35mm ammunition in our invention guidance and sliding assembly, sliding plate, pin, roller bearing, through the claw 3 The synchronous and continuous power supply mechanism implemented is described in document US201314406077. It is not explained. In another known instance of the art, reference number EP15151086, “For machine guns The patent application titled "Combat vehicle with ammunition loading system" is a patent application for an invention called "A 5 ammunition loading system, ammunition is loaded from an ammunition platform to a fuselage area. To be transported between them, a round of ammunition (20) from the body area (18) ammunition It includes a lifting mechanism (24) to lift it into compartment (16). Ammunition magazine (20), a machine gun (12) consisting of ammunition cartridges (36) connected to each other It includes an ammunition belt (34); the magazine is attached to the machine gun at the front end of the ammunition belt. accessible for feeding and connection to the rear end of another ammunition belt. a front opening (26') that allows the rear end of the ammunition belt to be another a rear opening that allows access for attachment to the front end of the ammunition belt (26'') includes. An arrangement of successive and adjacent ammunition magazines (20a, 20b), working. During this time, the ammunition belt was moved from the far magazine (20b) to the near magazine (20a) of the machine gun. (12) by enabling the ammunition belts to move continuously to the machine gun It is stated as "it makes it possible to feed them." The invention that is the subject of this document is essentially... Replacement of ammunition magazines and uninterrupted ammunition belts of the gun on the turret It provides a solution to the problem of delivering weapons in this way. However, in our invention... ammunition's movement within the weapon, alignment, prevention of twisting, barrel 20 transfer to the line, mechanism developed for realizing the gas-driven automatic cycle This is not explained in document EP15151086. In conclusion, the existence of the above problems and the inadequacy of the current solutions are related to the technical aspects. This has made it necessary to make improvements in the field. 25 THE PURPOSE OF THE INVENTION The present invention meets the aforementioned requirements while eliminating all disadvantages. Fully automated belt-fed close-range aerial 30 that lifts and offers some additional advantages. It is related to the defense system. The aim of the invention is to achieve high fire density, especially against close-range aerial threats. fully automatic belt adaptable to different calibers of ammunition, ensuring its sustainability. The goal is to develop a self-supporting air defense system. 35 4 Within the scope of the invention, ammunition with a magazine is regulated by means of a magazine, rail and guide body. and by ensuring an uninterrupted supply to the system, resulting in ammunition capacity The aim is to reduce interruptions in firing and increase the continuity of burst firing. Also, tension... By securing the ammunition with a cover and bearing under a certain force, high-speed Preventing the ammunition from twisting around its own axis during operation 5 is the goal. The invention enables synchronized operation between the sliding assembly, sliding plate, bearing, and claw. This ensures that the next round of ammunition is fed into the feed position in a regular manner during each firing cycle. The aim is to introduce and ensure fully automated operation continuity. 10 The invention involves using a low-friction bearing within the lower housing to enable movement. Reducing friction in systems, which can occur during long-term operation. to reduce seizing due to heating and expansion and to improve the operational stability of the system. The aim is to increase it. Also, the movement of the gas piston group and the slide group and 15 By means of the recoil spring, the bolt assembly is returned to its starting position. ignition, discharge and re-feeding processes in successive cycles This is the goal. The invention allows for the creation of a system with high ammunition capacity, increased supply continuity, and 20 different types of ammunition. It is adaptable to ammunition of various calibers and provides intense protection against close-range air threats. The aim is to develop a system capable of rapid firing. The structural and characteristic features and all the advantages of the invention are given in the figures below. Thanks to the detailed explanation written with references to the figures, it is clearer than ever. 25 This will be understood, and therefore the evaluation will also take these forms and detailed explanations into account. It must be done by taking it. BRIEF DESCRIPTION OF THE FIGURES The best way to utilize the advantages of the existing invention, together with its structure and additional elements. For understanding, it should be evaluated together with the figures explained below. is required. Figure 1; Perspective view of the air defense system that is the subject of the invention. 35 Figure 2 shows the front view of the air defense system that is the subject of this invention. Figure 3 shows a cross-sectional view of the power supply structure of the air defense system that is the subject of this invention. Figure 4 shows a side view of the air defense system that is the subject of this invention. Figure 5 shows a top view of the air defense system that is the subject of this invention. REFERENCE NUMBERS 1. Lower body 2. Munitions 3. Sliding group 4. Guide housing 5. Upper body 10 6. Sliding plate 7. Back cover assembly 8. Nails 9. Ray 10. Tension cover 15 11. Mayon vargel 12. Pin 13. Upper body cover 14. Winding handle May 15, 20 16th Barrel 17. Barrel guard 18. Irca spring 19. Router 20. Gas piston assembly 25 21st Turret Group 22. Ammunition 23. Low friction bearing The drawings do not necessarily need to be scaled and are sufficient to understand the existing invention. Details that are not present may have been omitted. Furthermore, at least to a large extent, they are identical. Elements that have, or at least substantially identical, functions are numbered the same. It is shown. 6 DETAILED DESCRIPTION OF THE INVENTION This detailed description explains that the invention is a fully automated belt-fed close-range air defense system. The preferred structures of the system are solely aimed at a better understanding of the subject. and is explained in a way that will not create any limiting effects. 5 Figure 1 shows a perspective view of the air defense system that is the subject of the invention. The invention is specifically designed for neutralizing close-range aerial threats. developed for feeding ammunition into the system in a belt pattern and sequential firing. It is a defense system that enables the fully automated execution of its cycles. 10 The invention consists mainly of the lower body (1), ammunition magazine (2), bolt assembly (3), guide body (4), upper body (5), slide plate (6), rear cover assembly (7), claw (8), rail (9), tension cover (10), swimsuit vargel (11), pin (12), upper body cover (13), cocking lever (14), magazine (15), barrel (16), barrel protection (17), recoil spring (18), steering (19), gas piston group (20), turret group (21), ammunition (22) and low friction bearing (23) consisting of fully automatic strip feed close 15 It includes a range air defense system. Figure 2 shows a frontal view of the air defense system that is the subject of the invention. This lower body (1), ammunition magazine (2), upper body (5), rail (9), tension cover (10), Details of the turret assembly (21) parts are shown. Lower fuselage (1), whole system 20 It is the supporting structure on which the components are assembled. Friction systems are used in conventional systems. The lower housing is a more advantageous low-friction bearing system (23) with ball bearings instead of the bearing system. (1) is used in. The ammunition with a magazine (2), brass casing and multi-part Many ammunitions with shrapnel structure (22) are combined with flexible structure magazines (15) It is being created. Preferably 12 GA (12 gauge) ammunition (22) is used. Top 25 The body (5) is connected to the lower body (1) preferably by a hinged system and can be opened and closed at 90°. It is structured. It works synchronously with the movement of the slide group (3). Upper body (5), swimsuit It contains the crossbar (11) and the slide plate (6). The rail (9) contains the ammunition with a magazine (2) The part in which it travels in a specific order is connected to the guide body (4). Tension cover (10), the ammunition with a magazine positioned on the rail (9) (2) with a certain force 30 by bearing the ammunition (2) around its own axis during high-speed firing. It prevents twisting. The turret group (21) is the vehicle and / or tower of the air defense system. It enables mounting on it. The turret group (21) is controlled by a ball bearing system. This design allows the air defense system to have extensive mobility in two axes. 35 The lower body (1), which forms the load-bearing structure of the system, is where the system components work together. It ensures that it is held in position. The mechanical parts that move inside the lower body (1) 7 By using low friction bearings (23) in the bearing of the components, during movement This ensures that the friction generated is reduced. In this way, long-term operation is possible. reducing heating and expansion that may occur due to friction during operation and related to prevent malfunctions that may occur in moving mechanisms It is ensured that the low friction bearing (23) is removable and replaceable. by replacing low friction bearings (23) that have completed their mechanical life It is possible. The upper body (5) is preferably hinged to the lower body (1) and can be opened approximately 90° It is configured to be able to close. By ensuring that the upper body (5) can be opened, 10 Access to the mechanism by placing the mine-loaded ammunition (2) into the air defense system It is made easier. Inside the upper body (5) are the slide plate (6), the main body (11) and the pin (12) components involved in carrying out the feeding action of ammunition such as (2) There is also a removable upper body cover (13) on the upper body (5). by positioning them to protect moving mechanisms, and in case of maintenance and / or malfunction, the word 15 Easy access is provided to the relevant mechanisms. Figure 3 shows a cross-sectional view of the power supply structure of the air defense system that is the subject of the invention. This view shows the details of the ammunition parts (2), claw (8), rail (9). It is shown. The ammunition with a magazine (2) is preferably made of brass 20 GA (12 gauge). having a casing and multiple munitions with a multi-particle shrapnel structure (22) by connecting the units to each other via a flexible connection (mayon (15)) structure ammunition (2) is formed by the units of the said ammunition (22) together. It is structured to allow for transportation and sequential feeding. The claw (8) is positioned on the upper body (5), and the movement of the mayo vargel (11) group is 25 during which time, grasping the magazines (15), pull them toward the magazine-loaded ammunition (2) receiving chamber and It is configured to enable the advancement of the ammunition (2) to the relevant location. Ray (9), the launch of ammunition (2) in a controlled and orderly manner along a designated route. It is structured in such a way as to enable its progress. The rail (9) is connected to the guide body (4). positioned and the mine-loaded ammunition (2) within the relevant air defense system 30 It ensures its guidance and progress. Guide for the regular transfer of ammunition with mines (2) to the air defense system The body (4) and the rail (9) connected to it are used. The guide body (4) is fitted with a guide rail. 35 with magazines, configured to include bearings suitable for the geometry of the ammunition (2). The ammunition (2) is made to move along the designated line. The ammunition is made to move along the designated line via the rail (9). The ammunition (2) is allowed to move regularly in the feed direction. 8 By positioning the guide body (4) under the upper body (5), the ammunition with a magazine (2) working area required for alignment and evacuation of empty mines (15) It is formed. There is also a tension cover (10) on the rail (9). Tension cover (10) ammunition with a mine (2) moving on the rail (9) by means of a certain force by being placed on the bed, especially during high-speed operation, the strip of ammunition (2) with the ammunition itself 5 The aim is to prevent twisting around its axis. Thus, the ammunition with a magazine... (2), feed by maintaining its proper position on the guide body (4) and rail (9) It is ensured that it is transferred to the mechanism. The feeding action of the ammunition with the magazine (2) is synchronized with the movement of the bolt group (3) 10 This is done. The movement taken from the sliding group (3) is transferred to the sliding plate (6), The movement of the sliding plate (6) is transmitted to the roller bearing (11) by means of the pin (12). The vargelin (11) moves back and forth on the sliding track and the nail (8) the mayo (15) With its capture, the next ammunition (2) is advanced towards the feeding position. This By synchronizing the movement with the cycle of the slide group (3), the next 15 after one shot ammunition (22) is prepared for the next firing cycle. Figure 4 shows a side view of the air defense system that is the subject of the invention. In this view, the slide assembly (3), guide housing (4), upper housing (5), rear cover assembly (7), barrel (11), pin (12), barrel (15), barrel (16), barrel guard (17), recoil spring (18), 20 guide (19), gas piston assembly (20), ammunition (22), low friction bearing (23) Details of its parts are shown. The slide assembly (3) is located within the lower body (1) at a minimum. Equipped with a bearing system to create friction, it takes the ammunition (2) and the barrel (16) feeds the line, empty ammunition (22) is discharged from under the lower body (1). The guide body (4) is designed to allow the ammunition (2) to advance in a specific pattern. It houses the beds designed according to the geometry of the ammunition (2). Rail (9) The line is mounted on the guide body (4). Alignment of the ammunition (22) and empty The evacuation of the swimsuits (15) is also carried out in this area. The upper body (5), the lower body (1) preferably connected via a hinge mechanism, for maintenance, inspection and intervention It has a structure that can be opened and closed approximately 90° to allow for various operations. Top 30 The body (5) contains the Mayon vargel (11) group and the slide plate (6), the slide It is structured to work in coordination with the movement of the group (3). Back cover group (7) is located on the lower body (1), guiding (19) and reversing beam (18) It fixes it. The swimsuit pulley (11), located inside the upper body (5), is on a sliding track. Moving forward with the movement of the bolt group (3) and the drive of the bolt plate (6), the 35-pin ammunition (2) ensures that the guide body (4) moves up to the stopper on it. Pin (12), on top The body (5) transmits the movement of the sliding plate (6) inside to the turntable (11). 9 (15); preferably brass and soft shell multi-particle ammunition (22) ensuring the system is fed in a smooth and consistent manner; by joining end-to-end It allows for continuous and rapid firing in the desired quantity. Mayon (15) and Ammunition (22) is combined during the production phase to obtain ammunition with a magazine (2). During firing (due to the pressure generated) the ammunition with a magazine (2) will be re-empty with a magazine (15) and 5 Empty ammunition (22) is separated. Barrel (16) with high rate of fire of ammunition (22) It is configured to ensure that the missile is directed and delivered to its target area. The particle ammunition (22) which is preferably used within the scope of the design, under intense firing conditions suitable for reducing wear or damage to the inner wall of the barrel (16) It is manufactured from steel material with mechanical strength properties. Barrel guard (17), 10 possible effects on the external environment around the barrel (16) operating under intense firing conditions limiting and ensuring safe working conditions of the gas piston group (20) It is structured for this purpose. The return spring (18) is located inside the lower body (1) to ensure that the group (3) is returned to its starting position after the shot It is structured. The return spring (18) enables the return movement to be carried out gradually. 15 It has a double-stage structure that provides. The guide (19), slide group (3) swimsuit (15) aligning the ammunition (22) it receives from the line with the barrel (16) axis and the said a structured to ensure that the ammunition (22) is directed towards the barrel (16) axis It is an element. The router (19) is mounted on the rear cover assembly (7), preferably. It is manufactured from steel material with high carbon content. The router (19), 20 in terms of ensuring that the ammunition (22) is positioned towards the barrel (16) axis, It is a functional component in terms of ensuring the reliable and continuous operation of the system. Gas piston group (20), high pressure gas generated during firing inside barrel (16) in a controlled manner This will allow the gas pressure to be directed and actuated on the piston. It is structured in this way. The movement of the piston is caused by the application of gas pressure on the piston. and consequently the working movement of the sliding group (3) Ammunition (22) is provided, preferably in 12 GA (12 gauge) caliber and brass. It is structured to have a body. The said ammunition (22), the magazine (15) It can be mounted on the system and allows for sequential / multiple shots to be fired within the system. It is structured to provide 30 ammunition (22) that will create a particulate effect on the target. It has a structured ammunition (22) that provides a high destructive effect. Low friction bearing (23), movable system elements located inside the lower housing (1) heating and resulting thermal expansion that may occur under prolonged operating conditions to reduce the increase in friction and the formation of sticking that may be caused by its effects It is structured. Low friction bearing (23) has a structure that does not require continuous maintenance. 35 and after the completion of its defined mechanical service life, it is disassembled and replaced with a new one. It is structured in a way that allows it to be modified. The ammunition used in the system (22) follows one another by means of the magazines (15). The structure of the ammunition with a magazine (2) is formed by bringing together the magazines (15). By making it possible to add ammunition to the system in a strip arrangement (22) and ammunition (22) supply continuity is increased. The invention is a preferred one Although 12 gauge ammunition (22) can be used in the application, the air defense system uses this 5 not limited to calibration, but also involving the proper configuration of the dimensions and geometries of the components. It can be applied to ammunition of different calibers. Preferably 12 GA (12 gauge). Brass casings are used, and depending on user preference, smoothbore shotgun cartridges can also be used as ammunition. (22) can be used as high-pressure, particle-effect close-in defense air defense. The system can be obtained. 10 The bolt assembly (3) located inside the lower body (1) is taken from the ammunition with a magazine (2). transfer of ammunition (22) to the barrel (16) line and empty ammunition after firing (22) is involved in evacuation. The low friction movement of the sliding group (3) Mechanical friction is reduced by supporting the bearing (23). The guide (19) is the slide 15 ammunition (22) taken from the supply line by group (3) towards the barrel (16) axis It provides guidance. The router (19) is located on the rear cover assembly (7) It is located. The rear cover assembly (7) also includes the router (19) and the return spring (18). It ensures the stabilization of the related structure. Figure 5 shows a top view of the air defense system that is the subject of the invention. This Slide plate (6), tension cover (10), spring roller (11), pin (12), upper body cover in view Details of parts (13), cocking handle (14), barrel (16), barrel guard (17), turret assembly (21) It is shown. The sliding plate (6) is located inside the upper body (5), and the sliding plate It is structured to transfer the linear motion of the group (3) to the Mayon rev (11) group. 25 The movement taken from the sliding group (3) is transferred from the sliding plate (6) to the main bearing group (11). By transmitting it, the working movement of the said group of Mayon Vargel (11) was carried out. is provided. The tension cover (10) is positioned on the rail (9) for the ammunition with a magazine (2) It is structured to provide bearing support with a specific compressive force. Tension The cover (10) maintains the bearing of the ammunition (2) for high-speed firing 30 under these conditions the rotation or twisting of the ammunition (2) around its own axis It limits. The Mayon vargel (11) is located inside the upper body (5) and is sliding. It is structured to move along a line. Mayon vargel (11), the sliding group (3) is driven by the sliding plate (6) in synchronization with the movement and the said Moving forward with the propulsion action, the munition with a munition (2) guide body (4) 35 It advances to the stop element located on it. The pin (12) is inside the upper body (5). positioned to transmit the movement of the sliding plate (6) to the mayon vargel (11) group. 11 It is structured. The movement taken from the slide plate (6) by means of the pin (12) is the reciprocating motion (11) It is ensured that it is transmitted to the line. The upper body cover (13) can be removed from the upper body (5). mounted in this way and positioned inside the upper body (5) and at high speeds protecting the moving mechanical system elements from external influences and ensuring their operation. It is structured in such a way as to ensure its safety. Upper body cover (13), maintenance 5 and to provide access to the relevant mechanical system components when troubleshooting is required. It has a detachable structure. This allows for maintenance, inspection and troubleshooting of the system. This facilitates the process. Figure 5 shows how the internal mechanical system elements can be seen. Part of the upper body cover (13) has been removed. The cocking handle (14) is inside the lower body (1). The first movement of the positioned slide group (3) is done manually by the operator 10 It is structured to enable the operation of the cocking lever (14) by the operator. With the slide assembly (3) being pulled backward, the end of the working stroke (movement distance) It is moved back to its position. Between the cocking lever (14) and the bolt group (3) By using a low-friction mechanism in the transmission of motion, the slide group (3) is reversed. This ensures that the force required from the operator for pulling is reduced. 15 After the system is set up, the cocking lever (14) slide group (3) during the firing cycle It is designed to maintain its fixed position regardless of its movement. Barrel (16) guiding and delivering the ammunition to the target area with a high rate of fire (22) It is structured in a way that will provide this. Particle-based systems are preferably used within the scope of the design. ammunition (22), wear or damage to the inner wall of the barrel (16) under intense firing conditions 20 steel material with suitable mechanical strength properties that will reduce its formation is manufactured. Barrel guard (17) protects the barrel (16) which operates under intense firing conditions. limiting possible effects on the surrounding external environment and the gas piston group (20) It is structured to ensure safe working conditions. The turret group (21) is part of the system. Mounting on a vehicle and / or tower and mechanical connection between the system and the carrier platform 25 It is configured to enable the connection. The turret group (21) is the two of the system. by allowing it to be moved along the axis, within a wide range of motion. It enables its positioning. This two-axis movement is supported by ball bearings. This is carried out through the system, and the system has low friction along the relevant axes. It allows for controlled movement and guidance. 30 The system is prepared for the first firing cycle by means of the cocking lever (14). By pulling the cocking lever (14) backward by the operator, the bolt assembly (3) is returned to its original position. The cocking lever (14) is taken and the first working movement of the system is provided. The system will not move during normal firing cycles once it is installed. 35 It is structured. Thus, the winding lever (14) is essentially the first winding movement of the system. It is used in its implementation. 12 Before firing, the upper body (5) is opened and the magazine ammunition (2), rail (9) and guide body (4) are opened. It is placed in the created feed line. After the placement process, the upper body (5), lower The system is brought to the working position by closing the housing (1). The crank handle (14) By pulling it back and releasing it, the slide assembly (3) is activated and in the feeding position The ammunition (22) is transferred to the barrel (16) axis via the guide (19). The same movement 5 during which the sliding plate (6) moves the mayon vargeli (11) and the claw (8) moves in the next By catching the magazine (15), the next ammunition (22) is put into feeding position. The ammunition (22) transferred into the barrel (16) with a mechanical or electric trigger system Some of the gas produced by its ignition passes through the gas transfer line 10 on the barrel (16) The gas is transmitted to the piston group (20) via the gas piston group (20). The gas piston group (20) receives the pressure in question. It mechanically moves the slide group (3) back by its effect. The slide group (3) back ammunition (22) fired by the movement is being discharged, at the same time a new feed cycle is being initiated. The energy that the sliding group (3) has during its return movement is transmitted by the return spring (18). The energy stored in the spring (18) is then released. Moving the slide group (3) forward again, the air defense system start It returns to the working position. In this way, feeding, aiming to the barrel (16), firing, The discharge of empty ammunition (22) and the feeding of new ammunition (22) follow each other 20 Fully automated operation is achieved by performing these operations in a series of cycles. Barrel guard (17) protects the components around the barrel (16) and the gas piston during intense firing. It is positioned around the barrel (16) to protect the group (20). The air defense system is connected to the platform via the turret group (21) 25 is being carried out. The turret group (21) can be mounted on a vehicle and / or tower, two With its axially movable structure, the air defense system can move in different directions. Its positioning directs it towards the air threat. The scope of protection for this application is specified in the claims section above, and is explicitly mentioned in point 30. It cannot be limited to what has been described for illustrative purposes. A person skilled in the field must present the findings of the invention. the innovation introduced can be created by using similar structures and / or this structure It is clear that this technique can also be applied to other similar fields. Therefore such structures are based on the criteria of innovation and especially exceeding the known state of the art. It is also obvious that he will be deprived. 35
Claims
13 REQUESTS 1. The invention is for the purpose of detecting close-range aerial threats for use in the defense industry. fully automated belt-fed air defense systems used in neutralization It is related to the system and its feature is; 5 - The carrier structure in which air defense system components are assembled, inside Lower housing (1) with rolling bearing (23), - A strip formed by combining the magazine (15) and ammunition (22) in a flexible structure. ammunition with a magazine created in the form of (2), - Receiving magazine-loaded ammunition (2) inside the lower body (1) and feeding the barrel (16) line, 10 bolt group (3) which enables the discharge of empty ammunition (22), - In order for the projectiles (2) to advance in a specific pattern, the projectiles (2) alignment of ammunition (22) and empty magazines in a form that conforms to its geometry (15) Guide body (4) that enables its evacuation, - Opened during maintenance, inspection and / or intervention operations in connection with the lower body (1) -15 It can be closed, containing the Mayon vargel (11) group and the slide plate (6), The upper body (5) works in coordination with the movement of the sliding group (3), - The linear movement of the slide group (3) located inside the upper body (5) transferring to the Mayon Vargel (11) group, the Mayon Vargel (11) group's work the sliding plate that triggers its movement (6), 20 - Air of the ammunition with a magazine (2) positioned depending on the guide body (4). A rail that enables guidance and / or advancement within a defense system. (9), - Compression force of the ammunition (2) positioned on the rail (9) 25 by doing so, the munition with a magazine (2) on its own axis under high-speed firing conditions tension cover (10) that restricts its rotation and / or twisting around it. - Enabling the positioning of the ammunition (22) toward the barrel (16) axis router (19), - Enables the connection of the air defense system to the vehicle and / or tower, 30 A mechanical connection between the system and the carrier platform, on at least two axes. movable turret group (21), - Long-term use of the movable system elements located inside the lower body (1) heating and thermal expansion effects that may occur in working conditions a low 35 that reduces the increase in friction and / or seizing that it may cause. friction bearing (23), It is characterized by its inclusion. 14 2. It is an air defense system in accordance with Claim 1, and its feature is; lower fuselage (1) and hinge. It includes a 90° openable and closable upper body (5) connected by means of a mechanism It is characterized by...
3. An air defense system compliant with Claim 1, characterized by its high carbon content 5 It is characterized by containing a steel-made guide (19).
4. An air defense system conforming to claim 1 or claim 3, with the following features: lower fuselage (1) rear cover assembly (7) which fixes the router (19) and the return broadcast (18) It is characterized by its inclusion. 10 5. It is an air defense system in accordance with Claim 1, and its feature is; on the upper fuselage (5) positioned, during the movement of the group of mayon vargel (11) the mayons (15) grasping and taking the magazine-loaded ammunition (2), pulling it towards its bed, magazine-loaded 15 by having a claw (8) that enables the ammunition (2) to advance to the relevant position. It is characterized by...
6. An air defense system conforming to claim 1 or claim 5, and having the following features: upper fuselage (5) a sliding group (3) which is positioned inside and moves along a sliding track Driven by the sliding plate (6) in sync with its movement, the said drive 20 by moving forward, the guide body (4) of the ammunition with the magazine (2) It contains a mayon vargel (11) which moves it up to the stopper element on it. It is characterized by...
7. An air defense system conforming to claim 1 or claim 6, with the characteristic of; upper fuselage (5) 25 The movement of the sliding plate (6) located inside is transferred to the mayon vargel (11) group transmitting the movement taken from the sliding plate (6) to the mayon rev line (11). It is characterized by containing a pin (12) that provides 8. An air defense system conforming to claim 1 or claim 2, with the characteristic of; upper fuselage (5) 30 connected to it, located inside the upper body (5) at high speeds It provides protection for moving mechanical system elements against external influences. the relevant mechanical system when maintenance, repair and / or troubleshooting is required The upper body cover (13) is detachable to provide access to its components. It is characterized by its inclusion. 35 It is an air defense system in accordance with Claim 1, and its feature is that it is located in the lower fuselage (1). The first movement of the positioned slide group (3) is done manually by the operator. the slide during the firing cycle after the system is set up, which enables the operation The cocking lever (14) which maintains its fixed position regardless of the movement of the group (3) It is characterized by containing 5 10. It is an air defense system in accordance with Claim 1, and its feature is that the ammunition (22) has a high rate of fire. It is characterized by having a barrel (16) that enables it to be directed to the target area with its speed. is being done.
11. An air defense system conforming to Claim 1 or Claim 10, characterized by intense fire. possible effects of the external environment around the barrel (16) operating under these conditions limiting, barrel which ensures safe working conditions of the gas piston group (20) It is characterized by having protection (17).
12. An air defense system conforming to claim 1 or claim 4, with the following features: lower fuselage (1) The bolt group (3) located inside returns to its starting position after firing. enabling its reversal, the return movement being gradual It includes a double-stage recoil spring (18) which enables its realization. It is characterized by... 20 13. An air defense system conforming to Claim 1, Claim 10, or Claim 11, and having the following characteristics: The high-pressure gas generated during firing inside the barrel (16) is controlled the piston is moved by applying gas pressure to the piston. 25 It is characterized by containing a gas piston group (20). It is an air defense system in accordance with Claim 14, and its characteristic is that it is 12 caliber / gauge. containing brass casing and / or smoothbore shotgun shell ammunition (22) It is characterized by 30