A payload release mechanism.

Abstract

This invention consists of at least one payload (B) positioned on the aircraft by the user and / or manufacturer, at least one fuselage (2) which enables the payload (B) to be carried over the aircraft, at least one hook (3) mounted on the fuselage (2) which enables the payload (B) to be carried over and / or thrown over the fuselage (2), a first rotating element (4) which is connected to the hook (3) and mounted on the fuselage (2) and which, when triggered, can be rotated around the axis on which it is mounted, thus enabling the hook (3) to be moved, and at least one trigger rod (5) which is connected at one end to the hook (3) and at the other end to the first rotating element (4) which enables the movement to be transferred to the hook (3) by triggering the first rotating element (4) and thus enables the hook (3) to be rotated.It is related to at least one shaft (6) positioned inside the body (2) to be actuated by the first rotating element (4) and which can be rotated by the user to move the first rotating element (4) and rotate it around the axis along which it extends.

Description

1 TARIFF A PAYLOAD RELEASE MECHANISM This invention makes it possible to eject payloads from aircraft. It relates to the payload release mechanism that provides this. The type of ammunition released from aircraft is the payload, 5 from the aircraft. Their separation is achieved with release equipment. On the release mechanisms There are hooks that will allow the ammunition to be carried. Located on the rafts The area hooks are opened by being triggered via pyrotechnic or pneumatic systems, and these This allows the munitions to be dropped from the aircraft. The hooks are closed on the launch pad. or rod mechanisms for positioning in open, locked or free states 10 It is used. Multi-element rod mechanisms are used to transfer the payload inside the hooks. The hooks are positioned in the open / release position when they are to be placed. Additional in other words, the payloads carried by the hooks are released or thrown off the swing. In these situations, the rod mechanisms are triggered and set in motion, and the hooks... The rod mechanisms are rotated and the payloads are released. The payload is 15 in cases where no command is given by the user during movement on the platform It is positioned in a way that will not trigger. United States origin, number US3056623, included in the known state of the art. The patent document describes a load release system. The mechanism is a an inverted T 20 which has a cross arm and can swing on an axle supported by plates. It is mentioned that it includes a lever in this form. In addition, the patent document mentions a spring. The device is positioned to tilt the cross arm in one direction. The document states that it has a fixed stopper. a bar that can move correctly and is adjustable from each end of the aforementioned crossarm It is mentioned that it is extended and attached in a way that allows it to rotate at the ends. In addition, Since the axis of the rods attached to the stopped end of the cross arm passes through the shaft axis, the shaft is 25 with an over-center relationship, the axis of the other bar passes through it. This is mentioned. In this way, axial application is made to the bars in the direction the shaft extends. Resistance to any force is being shown. Thanks to a payload release mechanism developed with this invention, the release systems safely attaching payloads on the aircraft by the user and / or manufacturer 30 It is ensured that it is stored for a predetermined period of time. Another objective of this invention is to launch payloads of different sizes through the same release system in the air. It enables transportation on the vehicle. 2 Another purpose of this invention is to trigger the mechanisms located on the release system. The goal is to ensure efficient motion transmission. Another objective of this invention is to trigger the mechanisms located on the release system. The purpose is to provide redundancy in order to ensure safety. The first claim made to achieve the purpose of the invention and the claims dependent on this claim are 5 a defined payload release mechanism, by the user and / or manufacturer, air It contains a payload, preferably ammunition, mounted on the vehicle. The payload release mechanism enables payloads to be carried on the aircraft. and preferably includes a fuselage with an ejector unit. The payload is carried on the fuselage. It is moved by means of hooks. The hooks are mounted on the body at point 10 It is attached in such a way that it rotates around it. The payload release mechanism is on the body. mounted and connected to the body when triggered by the user and / or manufacturer It includes a primary rotating element that can rotate around a point. The rotating element is mounted on the housing. It is mounted in such a way as to be connected to the hook. In this way, the first rotating element When triggered, the hook can be rotated around the point where it is attached to the body. 15 The trigger rod causes the hook to rotate as a result of triggering the first rotating element. This is provided by a trigger rod that connects to the first rotating element at one end and to the hook at the other end. It is mounted on top. The trigger rod can rotate on the first rotating element and the hook. It is mounted in this way. This ensures that the rotating element is positioned around the point where it is attached to the housing. By rotating it, the trigger rod is also moved, causing the hook to move 20 degrees onto the body. It allows it to rotate around the point where it is supported. The payload release mechanism... located inside the housing in connection with the first rotating element, user and / or The first rotating element is triggered mechanically or autonomously by the manufacturer. The first rotating element rotates around the axis along which it extends, triggered simultaneously. It contains at least one shaft located inside the body that allows it to be rotated. 25 The subject of the invention is a payload release mechanism, consisting of a shaft to which the primary rotating element is attached at one end. a second rotating element is attached to the other end, opposite the first rotating element. It includes. The second rotating element is mounted on the shaft simultaneously and concurrently with the first rotating element. It is mounted to rotate in different directions. The payload release mechanism is located at one end. The second rotating element is mounted on the body in such a way that it can rotate from the other end to the hook and has 30 Multiple backup triggers positioned opposite the trigger bar It includes a rod. This allows the shaft to be triggered by the user or autonomously. As a result of its rotation, the backup trigger bar is synchronized and matched with the trigger element. by moving it, it rotates around the point where the hook is mounted to the body. It provides redundancy to the trigger bar thanks to the spare trigger bar. 35 3 This is ensured. In addition, the trigger bar and the spare trigger bar will remain opposite each other. In the diagram, one end is connected to a hook, and the other end to the first rotating element and the second rotating element respectively. Thanks to its attachment to the element, the payload is carried on the fuselage during transport. The transferred load can be distributed. In one application of the invention, the payload release mechanism consists of a shaft on which the shaft is mounted and the shaft is 5 a first axis (F) which is the direction along which the body lies or parallel to the direction It includes a payload release mechanism, connecting a trigger rod at one end to the other. mounted at one end to the spare trigger rod and almost entirely to the first axis It includes at least one connecting rod positioned in parallel. Connecting rod Thanks to this, the first rotating element and / or the second rotating element is activated, resulting in 10 The trigger bar and the backup trigger bar will move simultaneously and in a synchronized manner. It is ensured that the movement is synchronized. In one application of the invention, the payload release mechanism passes through the first axis. and a first axis that divides the body into two parts that are almost completely symmetrical with respect to the first axis. The plane of symmetry is approximately perpendicular to the first axis, in the direction the body extends. It includes a second axis that is parallel. This axis passes through the fuselage and... the body divided into two almost completely symmetrical parts, perpendicular to the first plane of symmetry A second plane of symmetry is located. The payload release mechanism is mounted on the fuselage. Mounted in such a way that it is connected to a hook and can rotate around the point where it is mounted. It includes at least one narrow-mouth hook. Trigger bar and / or spare trigger 20 the bar, different from the point where the hook is mounted on the body so that it rotates onto the hook. A hook transmission is a point that allows the pushing or pulling force to be transmitted to the hook. It is supported on points. Multiple, preferably two, hook transmission points. They will be positioned opposite each other and symmetrical with respect to the second plane of symmetry. It receives. The payload release mechanism, the narrow mouth hook, and the hook together simultaneously 25 It allows it to be rotated by being triggered, with a hook transmission point at one end and another at the other. It includes at least one main transmission rod attached to a narrow-mouth hook at one end. On the body, at least one such that it remains symmetrical with respect to the second plane of symmetry of the main transmission bar A spare main transmission rod is included. The spare main transmission rod is located at the rear at one end. The hook can be rotated from the other end to the narrow mouth of the hook, to the rear surface of the hook at the transmission point 30 It is mounted in this way. This ensures that when the shaft is triggered, it is synchronized with the main transmission rod. triggered in a timed manner, around the point where the narrow mouth hook is attached to the body. It is rotated. The spare main transmission rod is located at the narrow end of the main transmission rod. It is located on the body, behind the hook. 4 In one application of the invention, the payload release mechanism is connected to a narrow-mouth hook. It can rotate on the body in such a way that it will be triggered together with the narrow mouth hook. It includes at least one wide-mouth hook that is mounted. Main transmission rod and spare main transmission. The rod is mounted to the narrow mouth hook via the narrow mouth hook transmission point. Narrow mouth The hook transmission point will be located below the point where the narrow-mouth hook is attached to the body. 5 The narrow mouth hook is located on the front and rear surfaces as shown in the figure. The main transmission rod is located at the front. The narrow mouth hook on the surface is attached to the transmission point, while the spare main transmission rod remains on the rear surface. The narrow mouth hook is mounted to the transmission point. The narrow mouth hook is mounted via the transmission point. The pushing or pulling force generated by the movement of the hook is transmitted to the narrow mouth hook. Useful. Load release mechanism, with a narrow mouth hook at one end and a wide mouth hook at the other end. 10 Thanks to this connection, the shaft is moved, resulting in the wide-mouth hook turning into a narrow-mouth hook. It includes at least one support transmission bar that allows it to be rotated. The payload release mechanism consists of a narrow-mouth hook at one end and a wide-mouth hook at the other. Thanks to this connection to the hook, the shaft is moved, resulting in the wide mouth of the hook narrowing. the mouth hook allows it to be rotated together with the second 15 of the support transmission rod. The auxiliary support transmission rod is positioned symmetrically with respect to the plane of symmetry. It includes this. In this way, as a result of the shaft being triggered, the backup main transmission rod is simultaneously activated. or the backup support transmission rod is also triggered in succession, opening the wide-mouth hook. It allows the body to rotate around the point where it is attached. In one application of the invention, the payload release mechanism consists of a support transmission 20 at one end. support transmission bar, which is mounted to the support transmission bar at one end and to the spare support transmission bar at the other end. It will be positioned between the auxiliary support transmission bar and will be approximately parallel to the first axis. It includes a connecting rod positioned on the body as shown in the diagram. Connecting rod thanks to this, the first rotary element and / or the second rotary element can be adjusted by the user or The main transmission rod and / or backup main transmission 25 are activated by autonomous triggering. triggering of the support transmission bar and / or backup support transmission bar is provided. In addition, a support bar and / or a spare support bar connection bar is available. Thanks to this, they are triggered simultaneously and synchronously, and they have redundancy for each other. It provides. In one application of the invention, the payload release mechanism consists of a trigger rod and / or 30 via a spare trigger rod, with the first rotary element and / or the second rotary element It includes hooks that are connected to each other. The hooks are located on the body in the first symmetry. They are positioned so that they are symmetrical to each other or mirror-symmetrical with respect to the plane. The hooks are positioned on the body, one on the right and one on the left of the shaft, each almost touching the shaft. They are positioned at equal distances from each other. This ensures that the 35 carried on the fuselage... 5 The load created on the fuselage by the payloads is distributed by multiple hooks. They are met. On the body, the narrow mouth hooks are aligned with each other in the first plane of symmetry. It is positioned to be symmetrical or mirror-symmetrical. The shaft is positioned in the housing. Narrow mouth hooks located on its right and left sides, hooks and main transmission rods. and / or are connected via auxiliary main transmission rods. Wide mouth hooks are also attached to the body 5 on which they are mirror symmetric with respect to each other's first plane of symmetry They are positioned on the body, to the right and left of the shaft. Wide mouth hooks, narrow mouth hooks with support transmission rod and / or spare support transmission It is connected by a rod. There are two rods on the body, one to the right and one to the left of the shaft. multiple main transmission rods, spare main transmission rods, support transmission rods and spare support transmission rods 10 It contains a rod. This allows them to be positioned in mirror symmetry with respect to each other's first axis of symmetry. Area hooks, narrow mouth hooks, and wide mouth hooks can be used simultaneously or sequentially. It is triggered in such a way that the payloads carried on the fuselage are transferred to the fuselage. The loads it creates are due to multiple hooks located on the right and left of the shaft, and a narrow opening. It can be carried by hook and / or wide-mouth hook. 15 In one application of the invention, the payload release mechanism consists of a load located on the shaft and released from the shaft. It includes at least one bracket that extends into the housing. The bracket connects to the shaft. Equipment assembly is provided that will allow the user to trigger the spindle. The body has a bracket mounted at one end that can be detached from the body, and another end that can be detached from the body. It contains at least one balance shaft mounted inside. Balance shaft 20 There is at least one spring located in such a way as to partially encircle its surface. balance shaft housing At the end that extends inwards, the compression rod is rotated on the balance shaft. It is positioned in such a way that the compression bar can be moved by the user. The amount of compression of the spring on the balance shaft by moving it along the balance shaft. The compression ratio is changed. The compression ratio depends on the type of payload to be carried on the fuselage. It varies depending on the user and is determined by the compressed spring and the rotating element. and / or the amount of force required to keep the first rotating element in the locked position. This can be increased. In this way, the spring is compressed further using a compression rod. the opposing force that allows the rotating element to move from the locked to the unlocked state The amount of force generated in one direction is increased, and the first rotating element and / or the second rotating element 30 The element can be prevented from being triggered without a command being passed by the user. In one application of the invention, the payload release mechanism is located at the position of the first rotating element of the shaft. Located at the end of the field and in the form of an indentation, the user controls the shaft and simultaneously enabling the rotation of the first and / or second rotating element It includes at least one adjustment hole in the form of an indentation. The user can insert a 35mm hole into this adjustment hole. 6 with Allen-type equipment installed on the first rotating element and / or second rotating element shaft. by rotating together between locked state (I) or free state (II) It can be activated. The payload release mechanism is located on the payload. and useful by being placed inside hooks, narrow mouth hooks and / or wide mouth hooks. It includes at least one eye bolt that allows the load to be carried on the fuselage. Locked 5 In case (I) hooks, wide mouth hooks and / or narrow mouth hooks inside the shackles It is positioned in such a way as to be placed. In addition, in the locked state (I) spring compression It is positioned by being clamped onto the balance shaft via a bar. In this way, hooks, narrow mouth hooks and / or wide mouth hooks coming out of the eye Locked position (I) 10 by applying force in the opposite direction against forces that may cause is protected. In a preferred application of the invention, hooks, narrow mouth hooks and / or wide The mouth hooks will be locked even when no payload is mounted on the body (I). This allows them to be positioned in a certain way and is controlled by the user using the compression bar. compressed by a predetermined amount into the first rotating element and / or the second rotating element. There is a spring that applies force in the opposite direction. Thanks to this, the hooks on the body are positioned 15 degrees. Their transition from the locked state (I) to the free state (II) can be prevented. Useful The load release mechanism allows the user to position the rotating equipment in the adjustment hole. as a result of being rotated by the first rotary element and / or the second rotary element It includes a free state (II) in which the shaft rotating together compresses the spring via the bracket. By rotating the first rotating element and / or the second rotating element, the hooks, narrow mouth 20 hooks and / or wide-mouth hooks around the point where they are attached to the body It is rotated and brought to the free position (II). While the broadcast is brought to the free position, extra Due to being compressed, the first rotation occurs the moment the adjustment hole is released by the user. hooks, narrow mouth hooks and / or wide mouth hooks together with the first element and / or second rotating element The hooks return from the free position (II) to the locked position. 25 In one application of the invention, the payload release mechanism is in the locked position (I) with an Allen key-type device inserted into the adjustment hole by the user via the adjustment hole It includes a rotating shaft. By rotating the shaft, a structure is formed on the shaft that is integral to the shaft. It is rotated in the bracket and the balance shaft is attached to the bracket in a rotatable manner. The spring on it is compressed. As a result of rotating the shaft around the first axis, the first 30 The first rotating element and / or the second rotating element also preferably rotates clockwise. rotary element and / or trigger rod and / or spare by rotation of the second rotary element The trigger rods are pulled so that they approach the first axis. This allows the trigger to be activated. rod and / or spare trigger rods from hook transmission points to rods on the first axis By pulling correctly, the rods are rotated around the point where they are mounted to the body and 35 It enables the main transmission rod to become free (II). By rotating the hooks 7 And the spare main transmission rod is also pulled so that it approaches the first axis. In this way, Narrow mouth hooks are mounted to the body by pulling them from the narrow mouth hook transmission point. It is brought to the free position (II) by turning it around. Turning of the narrow mouth hooks with the support transmission rod and the support transmission rod will also approach the first axis They are pulled. In this way, the wide-mouth hooks are pulled and mounted to the body at point 5. It is brought to a free position (II) by being rotated around it. The first rotating element and / or the second Hooks, narrow mouth hooks and / or wide mouth hooks are formed by rotating the rotating element. trigger rod and / or backup trigger rod, main transmission rod and / or backup, respectively main transmission rod, support transmission rod and / or backup support transmission rod via the body They are brought to a free position (II) by being rotated around the point to which they are attached. 10 By releasing the adjustment hole, the user pushes the compressed spring bracket. It causes the shaft to rotate in the opposite direction and to come into the locked position (I). In this way, the first The rotating element and / or secondary rotating element rotate clockwise, triggering the rod and / or spare part. trigger rod, main transmission rod, backup main transmission rod, support transmission rod and spare By pushing the support transmission rods away from the first axis, the hooks, narrow mouth 15 The hooks and wide mouth hooks are made to return to the locked position (I). In an application of the invention, the payload release mechanism consists of the first rotating element and / or the trigger rod and / or backup trigger rod located on the second rotating element the point where the first rotating element and / or the second rotating element is mounted in a rotatable manner It contains multiple trigger points. In the locked state (I), the adjustment hole and trigger point are 20. a first line passing through their centers, adjustment hole and hook transmission points in the locked state A second line runs through their centers. The first and second lines are locked together. There is a difference in centering (overcentering) between them relative to each other. The trigger point is locked. In this case, the centering differs according to the hook transmission point and the adjustment hole centers. It is located on the body in such a way as to form. In this way, the first rotating element and / or 25 By applying a counter-moment force on the second rotating element, the hooks, narrow mouth hooks and / or wide mouth hooks are locked unless there is intervention by the user. They are positioned on the fuselage in such a way as to maintain their (I) positions. In one application of the invention, the payload release mechanism operates after the shaft is triggered. 30 wide mouth hook that will allow the hook to be rotated around the point where it is mounted to the body. The first with a wide mouth hook support transmission rod and / or spare support transmission rod at least one wide-mouth hook transmission point that allows it to be pulled towards the axis Includes: Support transmission rod and / or spare support transmission rod wide mouth hook. It is mounted on wide-mouth hook transmission points that can rotate. Hook transmission The transmission point, the narrow mouth hook transmission point and the wide mouth hook transmission point are each part of the body 35 8 It is positioned at different distances from the second axis. This allows for... The hooks, narrow mouth hooks and wide mouth hooks each result from the rotation of the shaft. By creating an almost equal angle of rotation, the body moves from the locked position (I) to the free position (II) Hooks are categorized into two types according to their size: narrow-mouth hooks and wide-mouth hooks. The distances to the axis are determined by the user. 5 In one application of the invention, the payload release mechanism is connected to the body of the balance shaft. a fixed end with one end attached, a balance shaft with one end connected to the bracket and opposite to the fixed end It includes a movable end. A balance shaft passes through the centers of the fixed end and the movable end. a third line will run along it and pass through the centers of the fixed end and the adjustment hole. A fourth line extending from it is located. The payload release mechanism, the first rotary 10 Third line and fourth line while element and / or second rotating element is locked The angle of opposite moment, which is the angle between them, is determined by the user based on the type and / or weight of the payload. The movable part attached to the bracket will create a predetermined angle of counter-moment according to the diagram. It includes a tip. This allows the first rotating element and / or the second rotating element to rotate when the spring is locked. By applying a counter-moment force to the element through the bracket, the first rotating element and / or the second 15 on the body in such a way as to maintain the locked (I) positions of the rotating element They are kept in balance. In one application of the invention, the payload release mechanism involves mounting the balance shaft onto the balance shaft. at least one adjustable shim mounted to almost completely surround the perimeter. It includes an adjustable shim that contacts the pedestrian at one end and the fixed end at the other. mounted on the balance shaft in a quantity predetermined by the user. This allows the spring to be locked in position (I) depending on the type or weight of the payload. It can be compressed in such a way as to create the amount of opposing moment force required to maintain its position. In one application of the invention, the payload release mechanism is located on the fuselage and At least one cartridge that explodes either triggered by a user-submitted command or autonomously. 25 It contains. When the cartridges are detonated, a high-pressure fluid is released. It is exiting. The fluid is designed to allow the payload to be discharged through the shell, and It allows the hooks to be triggered to release. Cartridges The explosion takes place inside the combustion chamber located on the body of the cartridge. The fluid, which is a high-pressure gas released as a result of the explosion, exits the combustion chamber at 30°. It is transmitted outwards via a transmission channel. At the other end of the transmission channel, approximately... It includes at least one piston mounted in a movable manner. This enables combustion. High-pressure fluid entering the transmission channel from the chamber exits at the other end of the transmission channel. This moves the piston upwards. The piston moves upwards, causing the first rotation. This allows the element or the second rotating element to rotate together with the shaft. In this way, 35 9 hooks, narrow mouth hooks and wide mouth hooks switch from the locked position (I) to the free position (II) It exits the axes and enables the release of the payload. The piston As a result of the triggering fluid losing pressure, the spring's first rotating element and / or second The piston moves downwards in response to the force applied to the rotating element. This Thus, hooks, narrow mouth hooks and / or wide mouth hooks are in the first case (I) 5 It is turning. In one application of the invention, the payload release mechanism consists of two parts, each with a different diameter than the other. The hooks include narrow-mouth hooks and wide-mouth hooks, available in various sizes. Body The type of hook mounted on it is determined by the user according to the type of payload. While the payload is not yet positioned on the aircraft, the first rotating element, the second 10 Rotating element, hooks, narrow mouth hooks and / or wide mouth hooks locked on the body. The situation is (I). The payloads are placed on the fuselage by the user while the aircraft is on the ground. It is mounted on top of it. Therefore, the first rotating element located on the body is the second. Rotating element, hooks, narrow mouth hooks and / or wide mouth hooks via adjustment hole. It is rotated to the free position (II) and the payload is placed on the fuselage. 15 After the payload is placed on the fuselage, the adjustment hole is released to activate the first rotating element, secondary rotating element, hooks, narrow mouth hooks and / or wide mouth hooks It returns to the locked position (I). The payload is on the aircraft while the fuselage is locked. It is transmitted via a command given by the user or via a command generated autonomously. The cartridges located on the body are detonated by means of this device, releasing 20 high-pressure gases. The fluid triggers the piston. As a result of the piston being triggered, the aircraft flies during flight. first rotating element, second rotating element, hooks, narrow mouth hooks and / or wide mouth hooks The hooks are released (II), allowing the payload to be ejected from the aircraft. The countermoment created by the spring after the payload is ejected from the aircraft. thanks to its force, the first rotating element, the second rotating element, hooks, narrow mouth hooks 25 and / or the wide-mouth hooks return to the locking position. A payload release mechanism is attached to achieve the purpose of this invention. These are shown in the figures, and from these figures; Figure 1 - Side view of the fuselage and payload in the locked position (I). Figure 2 – First rotating element, second rotating element, hooks, narrow mouth hooks, wide mouth 30 (I) is the perspective view with the hooks locked. Figure 3 – Backup trigger bar, backup main trigger bar and backup support trigger. It is a perspective view of the bar. 10 Figure 4 - Perspective of the first rotating element, second rotating element, spring, adjustment hole, bracket, and shaft. It is the appearance. Figure 5 – Top view of the balance shaft, shim, and compression rod. Figure 6 – Top view of the first axis, second axis, and shaft. Figure 7 - Front view of the first axis of symmetry. 5 Figure 8 – Side view of the second axis of symmetry. Figure 9 – Side view of the piston and combustion chamber. Figure 10 – Different centering, the first line and the second line are side views. Figure 11 – Angle of reciprocal moment. The third and fourth lines are side views. Figure 12 – Perspective view of the combustion chamber, conduction channel, and piston. 10 Figure 13 - Wide mouth hook transmission point, support transmission rod, wide mouth hook, narrow mouth The hook, hook and first rotating element are shown in the free position (II) side view. The parts in the figures are individually numbered, and their corresponding numbers are shown below. It has been given. 1. Payload Release Mechanism 15 2. Body 3. Hook 301. Narrow Mouth Hook 302. Wide Mouth Hook 4. First Rotating Element 20 5. Trigger Bar 501. Replacement Trigger Bar 502. Main Transmission Rod 503. Spare Main Transmission Rod 504. Support Transmission Bar 25 505. Backup Support Transmission Bar 11 5001. Connecting Bar 6 miles 7. Second Rotating Element 8. Hook Transmission Point 9. Narrow Mouth Transmission Turning Point 5 10. Bracket 11. Balance shaft 1101. Fixed Tip 1102. Movable Tip 12. Spring 10 13. Compression Bar 14. Adjustment Hole 15. Map 16. Trigger Point 17. Wide Mouth Hook Transmission Point 15 18. Now Cartridge 19 20. Combustion Chamber 21st Transmission Channel 22. Piston 20 (B) Payload (F) First Axis (S) Second Axis (FS) First Symmetry Plane (SS) Second Symmetry Plane 25 (I) Locked State 12 (II) Free State (FL) First Line (SL) Second Line (OC) Differential Centering (TL) Third Line 5 (ZL) Fourth Line (G) Fluid A payload release mechanism (1) developed with the invention can be released by the user and / or manufacturer At least one payload (B) positioned on the aircraft, the payload (B) on the aircraft at least one body (2) that allows it to be carried over, the body (2) can be rotated on 10 mounted and the payload (B) is carried on the fuselage (2) and / or over the fuselage (2) at least one hook (3) which allows it to be thrown, the body which will be connected with hook (3). (2) supported on and triggered around the axis on which it is supported. a first rotary that can be rotated and thus allows the hook (3) to be moved element (4) is connected in such a way that one end is attached to the hook (3) and the other end is attached to the first rotating element (4). In this way, the movement is transferred to the hook (3) by triggering the first rotary element (4). At least one trigger bar (5) which provides and enables the turning of the hook (3), first rotary positioned inside the body (2) to be moved by element (4) and user by being rotated by the first rotating element (4) and moving it along its length It includes at least one shaft (6) that allows it to be rotated around the axis on which it lies (Figure 20). (Figure 1, Figure 2, Figure 3, Figure 4). The subject of the invention is a payload release mechanism (1), with the first rotating element (4) and mutually The first rotary position is positioned on the shaft (6) and rotated by turning the shaft (6). A second rotating element (7) is triggered simultaneously with element (4), with the second rotating element (7) connected and connected at one end to the second rotating element (7) and at the other end to the hook (3), 25 It can rotate from the points where it is connected and is mounted so that it remains opposite the trigger bar (5). In this way, the shaft (6) is triggered by the user, resulting in the trigger bar (5) By moving in a simultaneous and congruent manner, the hook provides redundancy (3) to the hook. (3) Multiple backup triggers that allow it to rotate around the point on which it is supported It includes the bar (501) (Figure 2). 30 13 The payload release mechanism (1) is mounted on the body (2) and can be used by the user and / or The first one can rotate around the point where it is attached to the body (2) when triggered by the manufacturer. It includes a rotating element (4). The first rotating element (4) is attached to the body (2) with a hook (3). It is mounted in such a way as to be connected. In this way, the first rotating element (4) When triggered, the hook (3) moves around the point where it is attached to the body (2) 5 It can be rotated. As a result of triggering the first rotating element (4), the hook (3) The rotation is provided by the trigger bar (5). The trigger bar (5) has one end The first rotating element (4) is mounted on the hook (3) at the other end. Trigger rod (5) The first rotating element (4) and the hook (3) are mounted in such a way that they can rotate. The trigger is activated by rotating the rotating element (4) around the point where it is attached to the body (2). The point where the hook (3) is attached to the body (2) by moving the rod (5) It enables it to rotate around. The payload release mechanism (1), body (2) at least one shaft (6) located in such a way as to be connected to the first rotating element (4) It includes. In this way, the shaft (6) can be mechanically or autonomously controlled by the user and / or manufacturer. As a result of being triggered in this way, the shaft (6) is triggered simultaneously with the first rotating element (4) and the length 15 It allows the first rotating element (4) to be rotated around the axis along which it extends. It provides. The second rotating element (7) is placed on the shaft (6) simultaneously and congruently with the first rotating element (4). It is mounted to rotate in the directions. The payload release mechanism (1) is a 20 mounted on the second rotating element (7) at one end and on the hook (3) at the other end so that it can rotate. and positioned opposite the trigger bar (5) on the body (2) It contains multiple trigger bars (501). In this way, the spindle (6) can be operated by the user or autonomously. As a result of being rotated by being triggered in this way, the trigger bar (501) trigger element by moving simultaneously and congruently around the point where the hook is mounted to the body (2) It enables rotation. 25 In one application of the invention, the payload release mechanism (1) is located on the shaft (6). and a first axis (F) which is the direction in which the shaft (6) lies on the body (2), trigger rod (5) and the spare trigger bar (501) are located between one end of the trigger bar (5) connected to the spare trigger bar (501) at the other end, with the trigger bar (5) and the spare The body (2) 30 will remain between the trigger bar (501) and the first axis (F) and will be parallel to it. By means of the shaft (6) positioned on it, the first rotating element (4) and / or the second As a result of activating the rotary element (7), the trigger rod (5) and the backup trigger At least one connecting rod (5001) that enables the simultaneous movement of the rod (501) It includes. Thanks to the connecting rod (5001), the first rotary element (4) and / or the second rotary element As a result of activating element (7), the trigger bar (5) and the trigger bar 35 14 (501) It is ensured that it moves synchronously in a simultaneous and congruent manner. (Figure 2). In one application of the invention, the payload release mechanism (1) passes through the first axis (F). and a first plane of symmetry (FS) that divides the body (2) into two almost completely symmetrical parts, The shaft (6) is located on the body and is almost perpendicular to the first axis (F) 5 (2) a second axis (S) parallel to the direction it extends along, from the second axis (S) a second plane of symmetry that passes through and divides the body (2) into two almost completely symmetrical parts (SS) is mounted on the body (2) in such a way that it can rotate in connection with the hook (3). at least one narrow mouth hook (301), trigger bar (5) and / or spare trigger bar (501) hook (3) is supported on multiple hook transmission points (8), hook transmission from one end 10 The shaft (6) is connected to the narrow mouth hook (301) at the other end of the point (8). As a result of its movement, the narrow mouth hook (301) together with the hook (3) and in the same direction at least one main transmission rod (502) that is moved in such a way as to allow it to be rotated, so that the main transmission bar (502) is symmetrical with respect to the second plane of symmetry (SS). positioned and from one end to the hook transmission point (8) and from the other end to the narrow mouth hook 15 (301) mounted, triggered by the shaft (6) and synchronous with the main transmission rod (502) The narrow mouth hook (301) is rotated around the point where it is attached to the body (2) It includes at least one spare main transmission bar (503) that enables spare main transmission. The rod (503), from one end to the hook transmission point (8) at the back, from the other end to the narrow mouth The hook (301) is mounted in a rotatable manner on the rear surface. In this way, the shaft 20 (6) is triggered in such a way that it is triggered simultaneously with the main transmission bar (502) rotating the narrow mouth hook (301) around the point where it is attached to the body (2) is provided. The spare main transmission rod (503) is attached to the narrow mouth hook of the main transmission rod (502). (301) is located on the fuselage so that it remains behind it (Figure 6, Figure 7, Figure 8). In one application of the invention, the payload release mechanism (1) is connected to the narrow mouth hook (301) with 25 at least one wide opening mounted on the body (2) in a rotatable manner to be connected hook (302), main transmission rod (502) and spare main transmission rod (503) narrow mouth hook (301) is mounted and after the shaft (6) is triggered, the narrow mouth hook (301) is supported at least one narrow-mouth hook transmission that allows rotation from a point different from the original point. point (9), from one end to narrow mouth hook transmission point (9) to the other end to wide mouth hook 30 (302) connected by this, as a result of the movement of the shaft (6) the wide mouth hook (302) at least one support that allows it to be rotated together with the narrow mouth hook (301) and hook (3). Transmission rod (504), from one end to narrow mouth hook transmission point (9) and from the other end to wide mouth the support transmission rod (504) to the hook (302) with respect to the second plane of symmetry (SS) mounted in such a way that when the shaft (6) is triggered, the spare main transmission rod (503) 35 15 simultaneously around the point where the wide mouth hook (302) is attached to the body (2) It includes at least one spare support transmission rod (505) which allows it to be rotated. Narrow Pushing or pulling is caused by the movement of the hook (3) through the mouth hook (301) transmission point. The force is transmitted to the narrow mouth hook (301). The payload release mechanism (1) is a It is connected at one end to a narrow mouth hook (301) and at the other end to a wide mouth hook (302), thus 5 As a result of the movement of the shaft (6), the wide mouth hook (302) becomes the narrow mouth hook (301) It includes at least one support transmission bar (504) that allows it to be rotated together. The payload release mechanism has a narrow mouth hook (301) at one end and a wide one at the other end. The mouth is connected to the hook (302) and as a result of the movement of the shaft (6), the wide mouth enabling the hook (302) to be rotated together with the narrow mouth hook (301) and support 10 spare part located in symmetry with respect to the second plane of symmetry of the transmission rod (504) It includes a support transmission rod (505). In this way, the spare part is triggered as a result of the shaft (6) being triggered. Backup support transmission rod to be used simultaneously or sequentially with the main transmission rod (503). (505) is triggered around the point where the wide mouth hook (302) is attached to the body (2). It enables rotation. 15 In one application of the invention, the payload release mechanism (1) transmits support from one end. connected to the support transmission bar (505) at the other end of the support transmission bar (504) It will be positioned between the auxiliary support transmission bar (504) and the first axis (F) Positioned on the body (2) so that it is parallel, the main shaft (6) is connected to it. 20 as a result of activating the transmission rod (502) and / or the spare main transmission rod (503). Simultaneous movement of the support transmission rod (504) and the backup support transmission rod (505) It includes a connecting bar (5001) that enables it to be activated. Thanks to the connecting bar (5001), the first rotary element (4) and / or the second rotary element (7) by the user or autonomously The main transmission rod (502) and / or the backup main transmission rod are activated by triggering in this manner. with support transmission bar (504) and / or spare support transmission bar (505) 25 They are triggered together. In one application of the invention, the payload release mechanism (1) is located on the first body (2). The first rotating object is positioned in such a way that it is mirror-symmetric with respect to the plane of symmetry (FS). element (4) connected via trigger bar (5) and / or spare trigger bar (501) The hooks (3) that can be triggered are mirrors of each other with respect to each other’s first plane of symmetry (FS). in symmetry with hooks (3) and main transmission bar (502) and spare main transmission The narrow mouth hooks (301) are located in such a way as to be connected by means of the bar (503), one another In mirror symmetry with respect to the first plane of symmetry (FS) and narrow mouth hooks (301) will be connected via the support transmission bar (504) and the backup support transmission bar (505). It includes wide mouth hooks (302) located on the body (2) in the figure. 35 on the body (2) 16 Multiple main transmission rods (502) to be on the right and left of the shaft (6), spare main Transmission bar (503), support transmission bar (504) and spare support transmission bar (505) are located This allows them to be in mirror symmetry with respect to each other's first axis of symmetry. hooks (3), narrow mouth hooks (301) and wide mouth hooks (302) simultaneously or together They are triggered in a sequential manner. In this way, the payloads carried on the fuselage (2) are 5 (B) The loads created on the body (2) are multiple on the right and left of the shaft (6). It can be carried by hook (3), narrow mouth hook (301) and / or wide mouth hook (302). In one application of the invention, the payload release mechanism (1) is directed outwards from the shaft (6). located on the shaft (6) in such a way as to extend and allow equipment to be mounted on the shaft (6). at least one bracket (10) providing, mounted to the body (2) at one end and to the bracket at the other end 10 (10) at least one balance shaft (11) which is attached in a removable manner, the balance shaft (11) is long At least one spring (12) located along the balance shaft (11) will remain opposite the bracket (10) and mounted in such a way that it can be moved by the user by rotating it around its own axis. In this way, the spring (12) can be tightened or loosened on the balance shaft (11) It includes at least one compression bar (13) that enables the publication (12) compression amount 15 It varies according to the type of payload (B) to be carried on the fuselage (2) and the user It is determined by the compressed spring (12) and the rotating element and / or the first rotating element. The amount of force required to keep the element (4) locked in place can be increased. This In this way, the spring (12) rotates by being compressed further by means of the compression bar (13). 20 in the opposite direction to the force that will allow the element to move from the locked to the free state. The amount of force generated is increased and the first rotating element (4) and / or the second rotating element The element (7) can be prevented from being triggered without a command being passed by the user. In one application of the invention, the payload release mechanism (1) is the first rotating shaft (6). At least one adjustment located on element (4) in the form of an indentation at its end. hole (14) located on the payload (B) into which the hook (3) is placed, thus 25 At least one eye (15) that allows the useful load (B) to be carried on the fuselage (2), the publication (12) will create preload on the first rotating element (4) and / or the second rotating element (7) as shown and hooks (3), narrow mouth hooks (301) and / or wide mouth hooks (302) The first rotating element is in a locked position (I) when attached to the map (15) via the adjustment hole (14). (4) and / or the spring connected to the shaft (6) as a result of the rotation of the second rotating element (7) 30 (12) in the compressed position, hooks (3), narrow mouth hooks (301) and wide mouth trigger rod (5) of hooks (302), spare trigger rod (501), main transmission rod (502), spare main transmission rod (503), support transmission rod (504) and spare support transmission rod (505) a free state (II) which is brought by being turned and taken out of the map (15) It includes. The payload release mechanism is rotated 35 positioned in the adjustment hole (14). 17 As a result of the rotation of the equipment by the user, the first rotating element (4) and / or The rotating shaft (6) together with the second rotating element (7) compresses the spring (12) by means of the bracket (10). It includes a free state (II). The first rotating element (4) and / or the second rotating element (7) hooks by turning (3), narrow mouth hooks (301) and / or wide mouth hooks (302) (II) 5 by rotating around the point to which they are attached on the body (2) is brought into being. While the publication (12) is being released, it is compressed further. As soon as the adjustment hole (14) is released by the user, the first rotary element (4) and / or hooks (3) together with the second rotating element (7), narrow mouth hooks (301) and / or wide mouth The hooks (302) return from the free position (II) to the locked position. In one application of the invention, the payload release mechanism (1) has an adjustment hole 10 in the locked position (I). (14) The shaft (6) rotated by the user, balance shaft by rotating the shaft (6) (10) bracket which allows the spring (12) located on (11) to be compressed, the shaft (6) The first rotary axis (F) rotates around the first axis (F) from the point attached to the body (2) by being rotated. element (4) and / or second rotating element (7), first rotating element (4) and / or second rotating By rotating the element (7), it pulls the hooks (3) and rotates them and releases them (II) 15 trigger bar (5) and / or spare trigger bar (501) which allows it to be brought, triggered by turning the hook (3), the narrow mouth hooks (301) are turned and main transmission rod (502) and / or backup main which allows it to be brought to the free state (II). The transmission rod (503) is triggered by turning the narrow mouth hooks (301) into the wide mouth. Support 20 which allows the hooks (302) to be rotated and released (II). Transmission bar (504) and / or backup support transmission bar (505), user-configured. As a result of releasing the hole (14), the first rotary element (4) and / or the second rotary locking element (7), hooks (3), narrow mouth hooks (301) and wide mouth hooks (302) It contains a spring (12) that allows it to return to its (I) positions in the situation. First By rotating the rotating element (4) and / or the second rotating element (7), the hooks (3), narrow mouth 25 hooks (301) and / or wide mouth hooks (302) respectively trigger bar (5) and / or Trigger bar (501), main transmission bar (502) and / or backup main transmission bar (503), support on the housing (2) via transmission rod (504) and / or spare support transmission rod (505) They are brought to a free state (II) by being rotated around the point where they are connected. User The spring (12) bracket (10) which is compressed by releasing the adjustment hole (14) 30 By pushing, the shaft (6) is rotated in the opposite direction and locked into position (I). In this way, the first rotating element (4) and / or the second rotating element (7) rotate clockwise trigger rod (5), trigger rod (501), main transmission rod (502), spare main transmission the first axis of the support transmission bar (503), support transmission bar (504) and spare support transmission bars. (F) by pushing away the hooks (3), narrow mouth hooks (301) and wide mouth 35 The hooks (302) are made to return to the locked position (I) (Figure 2, Figure 3). 18 In one application of the invention, the payload release mechanism (1), the first rotating element (4) located on the first of the trigger bar (5) and / or spare trigger bar (501) multiple trigger points where the rotary element (4) and / or the second rotary element (7) are mounted (16), a first line passing through the adjustment hole (14) and the trigger point (16) in the locked state (I). (FL), in the locked state, a second 5 passes through the adjustment hole (14) and the hook transmission point (8) (I). line (SL) is formed by the first line (FL) and the second line (SL) relative to each other in the locked state (I). different centering (overcentre) (OC), hook transmission point (8) and adjustment hole (14) depending on In this way, it is locked in place (I) on the body (2) to create centering (OC). The first rotating element (4) will maintain the (I) position of the hooks (3) in the locked state. and / or applying a force that will create a reverse moment on the second rotating element (7) 10 It includes a trigger point (16) that enables. In the locked state, the first line (FL) and the second Different centering (OC) occurs between the two lines (SL) relative to each other. In this way, the first by applying a counter moment force on the rotating element (4) and / or the second rotating element (7) User of hooks (3), narrow mouth hooks (301) and / or wide mouth hooks (302) Unless there is an intervention by them, they will maintain their locked (I) positions. 15 They are positioned on the body (2) (Figure 10). In one application of the invention, the payload release mechanism (1), support transmission rod (504) and / or the spare support transmission rod (505) is mounted on the wide mouth hook (302) and the shaft (6) after being triggered, the wide mouth hook (302) is attached to the body (2) from the point where it is attached to the body. at least one wide-mouth hook transmission point that allows it to be rotated from a different point 20 (17), hook transmission point (8), narrow mouth hook transmission point (9) and wide mouth hook transmission Each of the points (17) will be located at different distances from each other with respect to the second axis (S). In this way, the hooks (3), narrow mouth hooks (301) and wide are mounted on it. by triggering the mouth hooks (302) to form almost equal rotation angles It includes the free position (II) to which it is brought. Hook transmission point (8), narrow mouth hook transmission 25 point (9) and wide mouth hook transmission points (17) each on the body (2) second axis (S) is positioned at different distances from the mile (6). As a result of turning, hooks (3), narrow mouth hooks (301) and wide mouth hooks (302) By creating almost equal angles of rotation, the body (2) is released from the locked position (I). It moves to situation (II) (Figure 2, Figure 13). 30 In one application of the invention, the payload release mechanism (1) attaches the balance shaft (11) to the housing. (2) a fixed end with a connected end (1101), a movable end of the balance shaft (11) with a connected end to the bracket (10) a third line (TL) passing through the centers of the end (1102), fixed end (1101) and movable end (1102), A fourth line (ZL) passing through the centers of the fixed end (1101) and the adjustment hole (14), in the locked position (I) The angle of opposite moment (α), which is the angle between the third line (TL) and the fourth line (ZL), is 35 19 to create the back moment angle (α) predetermined by the user (10) connected by this means the broadcast (12) first rotary element (4) and / or second rotary element (7) reverse moment force on the shaft (6) to keep it in the locked position (I). It includes a movable tip (1102) which enables its application. Movable tip (1102) thanks to this, the first rotary element (4) and / or the second rotary element 5 when the spring (12) is in the locked position (7)a by applying a reverse moment force through bracket (10) to the first rotating element (4) and / or The body (2) will maintain the locked (I) positions of the second rotating element. They are kept in balance on it (Figure 5, Figure 11). In one application of the invention, the payload release mechanism (1) is mounted on the balance shaft (11). 10 mounted on the body (2) to be positioned between the spring (12) and the fixed end (1101). Depending on the type of payload (B), the number and / or thickness of these can be adjusted by the user. In this way, the spring (12) will generate a reverse moment force sufficient for the type of useful load (B) It includes at least one adjustable shim (18) that enables it to be compressed. Thanks to the shims (18), Depending on the type or weight of the payload (B), the spring (12) will keep the locked position (I) It can be compressed in such a way as to create a counter-moment force (Figure 4). 15 In one application of the invention, the payload release mechanism (1) is provided by the user. At least one cartridge (19) located on the body (2) exploded as a result of being triggered, The explosion of the cartridges (19) allows the useful charge (B) to be ejected from the body (2). at least one fluid (G) providing at least one combustion in which the detonation of the cartridges (19) is carried out. chamber (20), conveying the fluid (G) out of the combustion chamber (20) inside the shell (2) 20 at least one transmission channel (21) that enables transmission in such a way as to the other transmission channel (21) located at the end of the first rotating element (4) and connected to it by the user The explosion of the cartridge (19) causes the first rotating element (4) to rotate and thus by rotating the hooks (3), narrow mouth hooks (301) and / or wide mouth hooks (302) It contains at least one piston (22) that allows the payload (B) to be released. Piston 25 (22) thanks to the first rotating element (4) or the second rotating element (7) together with the shaft (6). It is possible to rotate them. In this way, hooks (3), narrow mouth hooks (301) and wide mouth The hooks (302) move from the locked position (I) to the free position (II) and come out of the eyelets (15) and This enables the release of the payload (B) (Figure 1, Figure 12). In one application of the invention, the payload release mechanism (1) consists of 30 different types of payloads. This allows different types of payloads (B) to be carried on the fuselage (2). The hook (3), the narrow-mouthed hook (301) and the wide-mouthed hook (302) are provided by means of the piston (22). The shaft (6) is brought about by being triggered and rotated, as a result of the triggering of the piston (22) the shaft (6) by means of hooks (3), narrow-mouthed hooks (301) and / or wide-mouthed hooks (302) By rotating it, the payloads (B) mounted on the fuselage (2) are brought into the air 35 20 The vehicle includes the free state (II) in which the piston is removed from the fuselage (2) during flight. (22) As a result of its triggering, the first rotating element (4), the second rotating element element (7), hooks (3), narrow mouth hooks (301) and / or wide mouth hooks (302) free By switching to situation (II), it ensures that the payload (B) is ejected from the aircraft. The payload (B) The opposing moment force created by the spring (12) after being ejected from the aircraft is 5 thanks to the first rotating element (4), the second rotating element (7), hooks (3), narrow mouth hooks (301) and / or wide mouth hooks (302) return to the locked position (Figure 9, Figure 12).

Claims

21 REQUESTS 1. At least one utility vehicle positioned on the aircraft by the user and / or manufacturer. The payload (B) has at least one way to enable the payload (B) to be carried over the aircraft. The body (2) is mounted on the body (2) in a rotatable manner and the payload (B) is mounted on the body (2) at least one 5 that allows it to be carried on and / or thrown off the body (2). hook (3) is supported on the body (2) in such a way as to be connected with hook (3) and When triggered, it can be rotated around the axis on which it is mounted, and thus... a first rotary element (4) which enables the hook (3) to be moved, one end of which is The hook (3) is connected to the first rotating element (4) in such a way that the other end can be rotated. Enabling the movement to be transferred to the hook (3) by triggering the first rotary element (4), and 10 At least one trigger rod (5) that enables the hook (3) to rotate, first rotary element (4) positioned inside the body (2) to be moved by the user by being rotated by the first rotating element (4) and moving it along its length the first one which includes at least one shaft (6) that allows it to be rotated around the axis on which it lies. positioned on the shaft (6) and opposite the rotating element (4) and 15 of the shaft (6) is rotated, triggering a second rotary element simultaneously with the first rotary element (4). element (7) is connected to the second rotating element (7) and from one end to the second rotating element (7) connected to the hook (3) at the other end, can rotate from the points where it is connected and trigger The rod (5) is mounted so that it remains opposite the shaft (6) of the user 20 will be synchronous and matched with the trigger bar (5) as a result of being triggered by it. by moving in this way, the point where the hook (3) is supported, providing redundancy to the hook (3). with multiple spare trigger sticks (501) that allow it to rotate around a payload release mechanism characterized (1).

2. A first 25 is the direction on which the shaft (6) is located and the shaft (6) extends on the body (2). an axis (F) located between the trigger bar (5) and the spare trigger bar (501) connected to the trigger bar (5) at one end and to the spare trigger bar (501) at the other end The one that will be located between the trigger bar (5) and the spare trigger bar (501) and the first so that the shaft (6) is positioned on the housing (2) parallel to the axis (F) by means of activating the first rotary element (4) and / or the second rotary element (7) 30 As a result, the trigger bar (5) and the backup trigger bar (501) move simultaneously. In claim 1, characterized by having at least one connecting rod (5001) that enables it to be activated. such a payload release mechanism (1). 35 22 3. Passing through the first axis (F) and dividing the body (2) into two almost completely symmetrical parts. a first plane of symmetry (FS) is located on the shaft (6) and is directly on the first axis (F). a parallel to the direction in which the trunk (2) extends along its length, immediately perpendicular to it The second axis (S) passes through the second axis (S) and makes the body (2) almost completely symmetrical. A second plane of symmetry (SS) dividing the body into two parts will be connected to the hook (3) 5 (2) at least one narrow mouth hook (301) mounted on it in a rotatable manner, trigger bar (5) and / or multiple on which the spare trigger bar (501) is mounted on the hook (3) hook transmission point (8), from one end to hook transmission point (8) and from the other end to narrow mouth The narrow mouth is connected to the hook (301) and as a result of the movement of the shaft (6). 10 which will allow the hook (301) to be rotated together with the hook (3) and in the same direction. At least one main transmission rod (502) that is actuated in this manner, the main transmission rod (502) positioned in such a way that it is symmetrical with respect to the second plane of symmetry (SS) and one mounted from one end to the hook transmission point (8) and from the other end to the narrow mouth hook (301), As a result of the triggering of the shaft (6), the narrow mouth is simultaneously with the main transmission rod (502). 15 allows the hook (301) to be rotated around the point where it is attached to the body (2). Request 1 or characterized by providing at least one spare main transmission rod (503). a payload release mechanism as in claim 2 (1).

4. Rotatable on the body (2) in connection with the narrow mouth hook (301) 20 at least one wide mouth hook (302), main transmission rod (502) and spare main transmission rod are fitted. after the rod (503) is mounted on the narrow mouth hook (301) and the shaft (6) is triggered turning the narrow mouth hook (301) from a point different from the point where it is supported at least one narrow mouth hook transmission point (9) that allows narrow mouth hook from one end The shaft is connected to the transmission point (9) at the other end by a wide mouth hook (302) so that the shaft 25 (6) as a result of the mobilization of the wide mouth hook (302) narrow mouth hook (301) and At least one support transmission rod (504) that allows it to be rotated together with the hook (3), from one end to the narrow mouth hook transmission point (9) and from the other end to the wide mouth hook (302) The support transmission rod (504) will be symmetrical with respect to the second plane of symmetry (SS). 30 with spare main transmission rod (503) as a result of triggering of the mounted shaft (6). simultaneously around the point where the wide mouth hook (302) is attached to the body (2) with at least one spare support transmission bar (505) that allows it to be rotated a payload release mechanism as in claim 3 characterized (1).

5. From one end to the support transmission rod (504) and from the other end to the spare support transmission rod 35 (505) connected between the support transmission rod (504) and the spare support transmission rod (505) will remain positioned on the fuselage (2) and parallel to the first axis (F) In this way, the main transmission rod (502) and / or spare main transmission rod can be connected to the shaft (6) 23 (503) as a result of its activation, the support transmission bar (504) and the backup support transmission with the connecting rod (5001) that enables the simultaneous movement of the rod (505) a payload release mechanism as in claim 4 characterized (1).

6. On the body (2), there will be 5 that are mirror symmetrical to each other with respect to the first plane of symmetry (FS). as shown in the figure, the first rotary element (4) and the trigger rod (5) and / or spare The hooks (3) which can be triggered in connection with the trigger bar (501) are connected to each other. The hooks are such that they are mirror images of each other with respect to the first plane of symmetry (FS). (3) connected via the main transmission rod (502) and the spare main transmission rod (503). The narrow mouth hooks (301) are positioned in such a way that they are 10 to each other's first plane of symmetry (FS). According to the mirror symmetry and with narrow mouth hooks (301) support transmission rod (504) and the body (2) will be connected via the spare support transmission rod (505) Number 4-5, characterized by the wide mouth hooks (302) on it. a payload release mechanism like in any of the requests (1). 15 7. Located on the shaft (6) and extending outwards from the shaft (6) and on the shaft (6) at least one bracket (10) that allows equipment to be mounted, from one end to the body (2) At least one balance attached to the bracket (10) which can be removed from the other end mounted. balance shaft (11), at least one spring (12) located along the length of the balance shaft (11), balance shaft (11) will remain opposite the bracket (10) and rotate 20 degrees around its own axis by the user. The spring (12) balance shaft is mounted in such a way that it can be moved by rotating it. (11) at least one compression that allows it to be compressed or loosened any of the above requests characterized by the bar (13) Useful load release mechanism (1). 25 8. The shaft (6) shall have an indentation at its end located on the first rotating element (4). at least one adjustment hole (14) located on the payload (B) into which the hook is placed (3) is located on the fuselage (2) which allows the useful load (B) to be carried on it. at least one map (15), spring (12) first rotary element (4) and / or second rotary element (7) It is positioned to create a preload on it and hooks (3), narrow mouth hooks 30 (301) and / or a locked position (I) where wide-mouthed hooks (302) are attached to the eyelet (15), adjustment through the hole (14) the first rotating element (4) and / or the second rotating element (7) As a result of its rotation, the spring (12) connected to the shaft (6) is in a compressed position. that, hooks (4), narrow mouth hooks (301) and wide mouth hooks (302) trigger bar (5), spare trigger bar (501), main transmission bar (502), spare main transmission 35 via the bar (503), support transmission bar (504) and spare support transmission bar (505) with a free state (II) which is brought in by turning and taken out of the map (15) a payload release mechanism as in claim 7 characterized (1). 24 9. In the locked position (I), the spindle (6) is rotated by the user via the adjustment hole (14), the spindle (6) allows the spring (12) located on the balance shaft (11) to be compressed by turning it. The bracket (10) that provides the body (2) around the first axis (F) by rotating the shaft (6) The first rotating element (4) and / or the second rotating element (7) returning from the connected point, the first 5 The hooks are pulled by rotating the rotating element (4) and / or the second rotating element (7). (3) trigger bar that allows it to be rotated and (II) released. (5) and / or spare trigger bar (501) is triggered by turning the hook (3) and narrow It allows the mouth hooks (301) to be rotated and brought to the free position (II). Main transmission rod (502) and / or spare main transmission rod (503), narrow mouth 10 triggered by turning the hooks (301) wide mouth hooks (302) Support transmission bar that allows it to be rotated and brought to the free position (II). (504) and / or spare support transmission rod (505), by the user adjustment hole (14) As a result of its release, the first rotating element (4) and / or the second rotating element (7), 15 hooks (3), narrow mouth hooks (301) and wide mouth hooks (302) in the locked position (I) characterized by the spring (12) that allows it to return to its original positions 7-9 a payload release mechanism like in any of the numbered requests (1).

10. The trigger bar (5) and / or backup trigger located on the first rotary element (4). 20 where the rod (501) is mounted to the first rotating element (4) and / or the second rotating element (7) Multiple trigger points (16), locked position (I) adjustment hole (14) and trigger point (16) passing through a first line (FL), in the locked position (I) adjustment hole (14) and hook transmission. a second line (SL) passing through point (8) the first line (FL) and the second line (I) in the locked state The difference in centering (overcentre) (OC) that the lines (SL) create relative to each other, hook transmission 25 locked in such a way as to create different centering (OC) according to point (8) and adjustment hole (14). In this case (I) located on the body (2) so that the hooks (3) are locked (I) first rotating element (4) and / or second rotating element to maintain their positions (7) triggering which allows the application of a force that will create a reverse moment on it. as in any of the claims numbered 8-9 characterized by point (16) Payload release mechanism (1). 30 11. Wide mouth of support transmission rod (504) and / or spare support transmission rod (505) the wide mouth hook is mounted on the hook (302) and after the shaft (6) is triggered (302) allows the body to be rotated from a point different from the point where it is supported (2). providing at least one wide mouth hook transmission point (17), hook transmission point (8), narrow mouth 35 The hook transmission point (9) and the wide mouth hook transmission point (17) are each separate from each other. this is mounted on it at different distances from the second axis (S). 25 thanks to the hooks (3), narrow mouth hooks (301) and wide mouth hooks (302) immediately (II) as in any of the claims numbered 4-10 characterized by having a body (2) a payload release mechanism (1). 5 12. A fixed end (1101) with the end of the balance shaft (11) attached to the body (2), balance shaft (11) a movable end (1102) with an end attached to the bracket (10), a fixed end (1101) and a movable end (1102) a third line passing through their centers (TL), fixed end (1101) and adjustment hole (14) a fourth line (ZL) passing through their centers, a third line (TL) while locked (I) and 10 The angle of inverse moment (α), which is the angle between the fourth line (ZL), is determined by the user beforehand. By attaching it to the bracket (10) in such a way as to create the determined counter-moment angle (α) broadcast (12) first rotary element (4) and / or second rotary element (7) in locked state (I) to apply reverse moment force on the shaft (6) in such a way as to keep it from remaining 15 of the requests numbered 7-11 characterized by the movable end (1102) that enables a payload release mechanism like any of them (1).

13. Mounted on the balance shaft (11) so that it remains between the spring (12) and the fixed end (1101), The number of payloads (B) to be attached to the fuselage (2) is determined by the user according to the type of payload (B). and / or its thickness can be adjusted so that the broadcast (12) will be sufficient for the payload (B) type 20 At least one adjustable element that allows compression to be created in such a way as to generate a counter-moment force. a payload release mechanism as in claim 12 characterized by shim (18) (1).

14. The explosive that detonates when triggered by the user and is located on the body (2) a small cartridge (19), released by the explosion of the cartridges (19) and the useful charge (B) from the body 25 (2) at least one fluid (G) that allows the cartridges (19) to explode At least one combustion chamber (20) where the fluid (G) is expelled from the combustion chamber (20) at least one transmission that ensures transmission within the correct trunk (2) channel (21) will be connected to the first rotating element (4) at the other end of the transmission channel (21). As shown in the figure, the first rotary 30 as a result of the cartridge (19) bursting by the user. the element (4) is rotated and thus the hooks (3) are turned, narrow mouth hooks (301) and / or by rotating the wide-mouth hooks (302) to release the payload (B). from requests 4-13 characterized by having at least one piston (22) that enables a payload release mechanism like any of them (1). 35 15. Each of these has a different diameter, allowing for the carrying of different types of payloads (B) on the fuselage. (2) hook (3) that allows it to be carried on the narrow mouth hook (301) and wide mouth hook The hook (302) is triggered by means of the piston (22) and the shaft (6) is rotated, bringing the piston in 26 (22) triggering of the hooks (3) by means of the shaft (6), narrow mouth hooks (301) and / or wide-mouthed hooks (302) are brought onto the body (2) by turning them the mounted payloads (B) are removed from the fuselage (2) during the aircraft flight releasing a payload as in claim 14 characterized by free state (II). mechanism (1). 5

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