A cutting mechanism.

Abstract

This invention comprises a fuselage (2), which is an aircraft, at least one blade (3) located on the fuselage (2) that allows control of the airflow to move the fuselage (2), at least one control rod (4) located inside the fuselage (2) that enables the user to generate a cyclical motion input, thereby controlling the movement of the blade (3), at least one cutter (5) located on the fuselage (2) that cuts a cable (K) that comes into contact with the fuselage (2) during its movement, thus preventing damage to the fuselage (2) and / or the blades (3), at least one primary apparatus (6) located on the fuselage (2) that contains the cutter (5) and directs the cable (K) towards the cutter (5), and a device located on the primary apparatus (6) that almost completely surrounds the primary apparatus (6).It is related to at least one second apparatus (7) which extends outwards from the body (2) and thus directs the cable (K) to the first apparatus (6) for cutting the cable (K) so that the cable (K) can be cut by the cutter (5).

Description

1 TARIFF A CUTTING MECHANISM This invention relates to a variable-range cable cutter mechanism found in aircraft. 5 The cable cutters found on helicopters are generally designed for use in emergency situations. It is a safety device. This device poses a danger to the helicopter's rotors or other critical parts. the circuit is activated when encountering obstacles such as electrical wires or cables that could create a fire. The device activates quickly if the helicopter gets caught on a cable, sending a 10-degree shock to the rotor. It ensures the threat is safely neutralized without causing harm. Usually hydraulic or... It operates with a mechanical system. The cable cutter cuts cables quickly and efficiently. It preserves the helicopter's maneuverability. It's also safe for pilots and flight crew. This is important because the presence of a cable cutter reduces the helicopter's chances of landing safely. These devices increase the safety of helicopters and prevent potential accidents. It plays a critical role in this regard. Patent GB2514090 originating from the United Kingdom, which is included in the prior art. The document mentions the cable cutting mechanism found in aircraft. The document describes a cable cutter 20 that is mounted on the aircraft and also functions as an antenna. It is defined as follows: The device consists of an electrically conductive main body and electrical components connected to this body. It consists of an isolated auxiliary part. The main body and the auxiliary part, It is designed to form a VHF / UHF dipole communications antenna. It also functions as a coaxial antenna. The connector ends are connected to the main body and the auxiliary part. The device performs the cable cutting process. It also includes blades. This device has both a cable cutting function and is used for communication on the plane. 25 It acts as an antenna to provide this. Thanks to a cutting mechanism developed with this invention, the effective area of ​​the cutter can be changed. An adjustable cutting mechanism is provided, depending on the cable's position. Another purpose of this invention is to create a cable cutter 30 that can be adjusted depending on the change in the blade angle. to provide. The initial demands and the demands dependent on this demand, which are implemented to achieve the purpose of the invention. The defined cutting mechanism, the fuselage which is the main structure of the aircraft, controls the movement of the fuselage. It has at least one blade that directs the airflow to provide guidance. This blade directs the fuselage. 35 and plays a critical role in its movement. The user controls it via a control located inside the body. 2 The rod controls the movement of the blade. This control rod allows the user to perform cyclical movements. It allows the blade position to be changed by providing input motion. Body The cutter on it cuts a cable (K) that comes into contact with the body during movement, thus both It protects both the housing and the blade. This cutter prevents damage to the cable in the event of a potential hazard. It enhances safety by preventing visibility. In the operation of the cutting mechanism, the cable's 5 There is a first device for guiding the cutter. This first device guides the cutter. While housing it, it helps to route the cable (K) correctly. The first device The second device surrounding and connected to it will allow the cable (K) to be cut. It is designed in this way. The second device is necessary for routing the cable and reaching the cutter. This mechanism forms the structure that allows any 10 during the movement of the aircraft. When a problem is encountered, ensuring the cable is cut safely will protect both the vehicle and... It also aims to protect the security of users. The cutting mechanism that is the subject of the invention is a structure that moves on the first apparatus, the second. The apparatus is being designed and at least one motion mechanism is being used to provide this movement. 15 This movement mechanism slides the second apparatus along a specific path on the first apparatus. It is working. When the user triggers the control rod, this movement occurs almost simultaneously. This occurs as follows: The movement of the control rod changes the position of the second apparatus. It provides the necessary signal. Thus, to the blade angle predetermined by the user. Accordingly, the effective range of the cutter also changes automatically. This situation makes the cutter's effect even more effective. to make it effective and the cable (K) to be correctly connected during the movement of the aircraft This mechanism ensures that the cutting is done. This mechanism takes input from the user and processes it into the cutting mechanism. It enables integrated projection. The user-defined blade angle, By determining when and how the circuit breaker will be effective, it increases safety and makes the system more efficient. This ensures its efficient operation. Thus, 25% of the problems that can occur while the aircraft is in motion... Dynamic control is ensured to minimize risks. In one application of the invention, the cutting mechanism, the second apparatus, is fixed on the first apparatus. located in a closed position (I) at least partially inside the fuselage, as shown in the figure. It includes a second attachment. In this position, the second attachment is stationary and performs its cutting function. 30 It does not bring it. However, depending on the blade angle, the second attachment contacts the cutter body. The control rod is moved to cause the cable (K) to be cut. The user moves the control rod. When triggered, the movement mechanism is activated. As a result of the movement mechanism, the second The device switches from the closed position (I) to the open position (II). In the open position (II), the second device It extends outwards from the housing, thereby guiding the cable (K) to the circuit breaker. 35 Thus, the environment necessary for cutting the cable (K) is prepared. The cutting mechanism, It optimizes the cutter's effectiveness depending on the blade angle specified by the user. 3 The user's control input directly affects the effectiveness of the cutting mechanism. Second By moving the device in this way, a measure is taken to increase the safety of the aircraft. Thus, in case of any danger, the cable (K) can be safely cut, The aim is to protect the aircraft and its users. 5 In one application of the invention, the cutting mechanism is controlled by a mechanism that enables the movement of the blades. The main rod includes a primary rod that moves when the control rod is triggered by the pilot. The movement of the first rod causes the second rod to move, resulting in a change in the position of the second apparatus. This allows the second rods to move forward or backward around their own axes when triggered. They are doing. 10 In one application of the invention, the cutting mechanism is powered by the forward movement of the second rod. It includes an intermediate element capable of rotational movement. The intermediate element, the connecting element, and the second rod. It is among them. 15 In one application of the invention, the cutting mechanism has one end connected to the intermediate element and the other end to the actuator. It includes a connected linkage element. The intermediate element, which moves in a cyclical manner, is connected to the actuator. The actuator is activated by turning the screw located on the actuator, which is connected to the connecting element. It brings. 20 In one application of the invention, the cutting mechanism consists of a device whose one end is connected to the actuator via gears. a transmission element positioned so that its other end is connected to the transmission element It includes the rotational movement in the actuator, which is transferred to the gears located on the transmission element. After the transmitted motion, the required displacement ratio is transmitted to the second apparatus. 25 In one application of the invention, the cutting mechanism is triggered by the transmission element, which then drives the second The apparatus includes a rod that allows the first apparatus to move on it. The rod is then attached to the second apparatus. Pushing the device forward helps to cut the cable. In one application of the invention, the cutting mechanism is located on the second apparatus, on the second 30 of the rod. a groove that allows the second device to slide upwards when the first device is pushed upwards It includes. The first device is positioned inside the cavity. In one application of the invention, the cutting mechanism incorporates a fuselage that is a helicopter. Hollow The second apparatus, which moves upwards via the first apparatus moving inside, is 35 It includes a stopper that allows it to stop when it reaches a specific position. For cutting the cable. The second device is secured in place by means of a stopper that allows it to reach the required position. 4 In one application of the invention, the cutting mechanism incorporates a fuselage that is a helicopter. The cutting mechanism implemented to achieve the purpose of this invention is shown in the attached figures. and, from these forms; 5 Figure 1 – Schematic view of the cutting mechanism (1). Figure 2 – Schematic view of the body (2). Figure 3 – Schematic view of the cutting mechanism (1). Figure 4 – Schematic view of the second apparatus (7) in closed position (I). Figure 5 – Schematic view of the second apparatus (7) in the open position (II). 10 The parts in the figures are individually numbered, and their corresponding numbers are shown below. It has been given. 1. Cutting Mechanism 15 2. Body 3. Pal 4. Control Rod 5. Cutter 6. First Apparatus 20 7. Second Apparatus 8. Movement Mechanism 801. Second Rod 802. Support Staff 803. Fastener 25 804. Transfer Element 9. First Rod 10. Actor 11. Stick 12. Hole 30 13. Stopper (K) Cable (I) Closed Position (II) Open Position 35 The cutting mechanism (1) is located on a fuselage (2), which is an aircraft, on the fuselage (2) at least one blade (3) that allows the airflow to be controlled for movement of the fuselage 5 (2) the creation of the circular movement input by the user within at least one control rod (4), body (2) which provides, thereby controlling the movement of the blade (3) a cable (K) located on the body (2) that comes into contact with the body (2) during the movement of the body (2) at least one cutting tool (5) that prevents damage to the body (2) and / or blades (3) by cutting, The cable (K) is located on the housing (2) and inside which is the cutter (5), and the cable (K) is directed towards the cutter (5). At least one first apparatus (6) directing the first apparatus (6) will surround the first apparatus (6) almost completely. In this way, it is located on the first apparatus (6) in the figure and extends outwards from the body (2). To cut the cable (K), direct the cable (K) to the first apparatus (6) and cut the cable (K) with the cutter (5) It includes at least one second apparatus (7) that allows it to be cut by. 10 The cutting mechanism (1) that is the subject of the invention is the movement of the second apparatus (7) on the first apparatus (6). at least one motion mechanism (8) that enables the control rod (4) to be operated by the user The control rod (4) moves simultaneously with the triggering and thus the user Changing the area of ​​effect of the cutter (5) according to the angle of the blade (3) determined in advance by It includes a second apparatus (7) that provides 15 The aircraft controls the airflow by means of at least one vane (3) located on the fuselage (2). It is in motion. The movement of this blade (3) is controlled by the body (2) and the user with at least one control rod (4) controlled by means of the generated cyclical motion input It is provided. While the body (2) is moving, a cutter (5) that comes into contact with the cable (K) 20 It is located; this cutter prevents damage to the housing (2) and / or blades (3). Cutter (5) is located in a first apparatus (6) on the body (2) and this apparatus holds the cable (K) directs towards the cutter (5). The first apparatus (6) is necessary for cutting the cable (K). when making the orientation, with at least one second apparatus (7) extending outwards from the body (2). It is surrounded. This mechanism allows the cable (K) to be cut safely, minimizing damage. 25 It reduces the risk. (Figure – 1) The cutting mechanism enables the movement between the second apparatus (7) and the first apparatus (6). It includes a small movement mechanism (8). This movement mechanism is controlled by the control rod (4) of the user. It acts simultaneously with being triggered by the user. Thus, 30 The area of ​​effect of the cutter (5) is changed according to the predetermined blade (3) angle. This The mechanism increases the efficiency of the cutter (5) and ensures the safety of the aircraft. The aim is... (Figure – 2, Figure – 3) In one application of the invention, the cutting mechanism (1) has 35 on the first apparatus (6) of the second apparatus (7). a closed position (I) in which it is fixed and at least partly located inside the fuselage (2), second Depending on the angle of the blade (3) of the apparatus (7), the cable (K) that contacts the body (2) of the cutter (5) 6 an open position (II) where it extends outwards from the body (2) by being triggered to cut, By triggering the user’s control rod (4), the movement mechanism (8) moves from the closed position. (I) brought to the open position (II) by directing the cable (K) to the cutter (5) the cable (K) cutter (5) It includes a second apparatus (7) that allows it to be cut by. The cutting mechanism (1), the second apparatus (7) is fixed on the first apparatus (6) and at least partially on the body (2) 5 It contains a closed position (I) in which it is located. The second apparatus (7) depends on the angle of the blade (3). by triggering the cutter (5) to cut the cable (K) which is in contact with the housing (2). It is in an open position (II) where the body (2) extends outwards. The user’s control rod (4) triggered by the movement mechanism (8), the second apparatus (7) moves from the closed position (I) to the open position. is brought to position (II) and thus the cable (K) is directed to the cutter (5) 10 This mechanism allows the cable (K) to be cut safely. This is the aim. (Figure – 4, Figure – 5) In one application of the invention, the cutting mechanism (1) is located on the body (2), which is used by the user At least one first rod (9) which moves the blades (3) by triggering the control rod (4), movement 15 This mechanism (8) moves along the direction it extends with the trigger of the first rod (9). It contains at least one second rod (801) which enables the movement of the second apparatus (7). The cutting mechanism (1) is located on the body (2) and the user controls the control rod (4) It contains at least one first rod (9) which enables the movement of the blades (3) by triggering. The mechanism is equipped with a movement device (8); when the first rod (9) is triggered, it extends 20 It is connected by at least one second rod (801) moving in the same direction. Thus, the second apparatus (7) It allows for movement. In one application of the invention, the cutting mechanism (1) has a second rod which is the actuator (8). (801) converts the linear motion it transmits into circular motion, with one end connected to the second rod (801) 25 It contains at least one intermediate element (802). The cutting mechanism (1), the movement mechanism (8) It is equipped with at least one rod which converts the linear motion transmitted by the second rod (801) into circular motion. It contains an intermediate element (802). This intermediate element (802) has one end connected to the second rod (801). It is working and enabling the transformation of movement. Thus, during the operation of the system The necessary circular motion is obtained and the efficiency of the cutting mechanism (1) is increased. 30 In one application of the invention, the cutting mechanism (1) is the second apparatus, which is the actuator (8). (7) At least one actuator (10) that triggers its movement, one end to the intermediate element (802) and the other end The cyclical motion transmitted from the intermediate element (802) to the actuator (10) is connected to the actuator (10). It contains at least one connecting element (803) that enables it to work. Cutting mechanism 35 (1), together with the motion mechanism (8), at least one actuator that triggers the movement of the second apparatus (7). (10) is included. This actuator (10) has one end connected to the intermediate element (802) and the other end connected to the actuator (10). 7 It is equipped with at least one connecting element (803). The cyclical transfer from the intermediate element (802) The movement enables the actuator (10) to work. In one application of the invention, the cutting mechanism (1) triggers the actuator (10) and the second apparatus (7) It contains at least one transmission element (804) that enables its movement. Cutter The mechanism (1) has at least 5 actuators (10) that trigger the actuator (10) and enable the movement of the second apparatus (7). It contains a transfer element (804). This transfer element (804) controls the functionality of the actuator (10). By increasing it, it effectively moves the second apparatus (7). Thus, the integrity of the system This is ensured and contributes to the safe cutting of the cable (K). In one application of the invention, the cutting mechanism (1) has one end connected to the transmission element (804) and the other end to 10 The second apparatus (7) moves linearly on the first apparatus (6), with the end of the second apparatus (7) connected to the second apparatus (7). It contains at least one bar (11) that allows it to do so. The cutting mechanism (1) has one end At least one rod (11) connected to the transmission element (804) and the other end to the second apparatus (7) It includes. This rod (11) makes the second apparatus (7) move linearly on the first apparatus (6). It provides the possibility of doing so. 15 In one application of the invention, the cutting mechanism (1) is the first apparatus (6) of the second apparatus (7) the second apparatus (7) which allows it to move by sliding over the first apparatus (6) It contains at least one groove (12) that allows it to be placed on top. The cutting mechanism (1), second at least one groove that allows the apparatus (7) to slide over the first apparatus (6) 20 (12) is included. This cavity (12) has the function of placing the second apparatus (7) on the first apparatus (6). Thus, the interaction between the first apparatus (6) and the second apparatus (7) is increased. and the effectiveness of the system is ensured. In one application of the invention, the cutting mechanism (1) has 25 on the first apparatus (6) of the second apparatus (7). at least one that ensures it remains stationary when it reaches a user-defined position. It includes a stopper (13). This stopper (13) holds the second apparatus (7) in the desired position, This contributes to the safe and efficient operation of the system. Thus, the cutter The mechanism (1) ensures the safe cutting of the cable (K) and the arrangement It maintains its integrity. 30 In one application of the invention, the cutting mechanism (1) includes the fuselage (2) which is a helicopter. 35

Claims

8 REQUESTS 1. A fuselage (2) which is an aircraft, located on the fuselage (2), the movement of the fuselage (2). at least one vane (3) that allows the airflow to be controlled in order to be made to work, fuselage (2) includes the creation of a circular movement input by the user. at least one control rod (4) which controls the movement of the blade (3), body (2) located on the body (2) that comes into contact with the body (2) during the movement of the body (2). by cutting the cable (K) prevents damage to the fuselage (2) and / or the blades (3) at least one cutter (5), located on the housing (2) and containing a cutter (5), the cable (K) directing at least one first apparatus (6) towards the cutter (5), first apparatus (6) immediately 10 located on the first apparatus (6) to surround almost completely the body (2) extending outwards, so that the cable (K) can be cut, the cable (K) first By directing the cable (K) to the device (6), it is possible to cut the cable by the cutter (5). containing at least one second apparatus (7) which provides the second apparatus (7) on the first apparatus (6). at least one movement mechanism (8) that enables it to move, control rod (4) user 15 The control rod (4) moves simultaneously with the triggering of this and In this way, the effect of the cutter (5) according to the blade (3) angle determined by the user. a cutter characterized by a second apparatus (7) that enables the change of area mechanism (1). 20 2. The second apparatus (7) is fixed on the first apparatus (6) and at least partially attached to the body. (2) is a closed position (I) in which the second apparatus (7) depends on the blade (3) angle. triggering the cutter (5) to cut the cable (K) which is in contact with the housing (2). with an open position (II) where the body (2) extends outwards, the user’s control rod (4) triggered by the movement mechanism (8) from closed position (I) open position 25 (II) brought in, directing the cable (K) to the cutter (5) and the cable (K) by the cutter (5) as in claim 1 characterized by the second apparatus (7) which allows cutting. a cutting mechanism (1).

3. The blades (3) are set 30° by the user triggering the control rod (4) located on the body (2). at least one first rod (9) which acts as the actuator, the first rod (9) which has a movement mechanism (8) By being triggered, it moves along the direction it extends, thus enabling the second apparatus (7) The above is characterized by having at least one second rod (801) which allows its movement. a cutting mechanism like any of the requests (1). 35 9 4. The linear motion transmitted by the second rod (801), which has a motion mechanism (8), is cyclical. with at least one intermediate element (802) which converts the motion, one end of which is connected to the second rod (801). a cutting mechanism as in claim 3 characterized (1).

5. At least one actuator which is the movement mechanism (8) and triggers the movement of the second apparatus (7). (10), one end of which is connected to the intermediate element (802) and the other end to the actuator (10), from the intermediate element (802) the most effective way to enable the actuator (10) to work with the transmitted cyclical motion. a cutter as in claim 4 characterized by a small connecting element (803) mechanism (1). 10 6. At least one actuator (10) that triggers the second apparatus (7) and enables its movement. A cutting mechanism (1) as in claim 5, characterized by the transmission element (804).

7. The second device, one end of which is connected to the transmission element (804) and the other end to the second device (7). at least 15 that allows the apparatus (7) to move linearly on the first apparatus (6). a cutting mechanism (1) as in claim 6 characterized by a small bar (11).

8. Enable the second apparatus (7) to slide over the first apparatus (6). providing at least the second apparatus (7) which enables the first apparatus (6) to be placed on top of the first apparatus (6). a 20 like any of the above claims characterized by a cavity (12). cutting mechanism (1).

9. The second apparatus (7) is placed on the first apparatus (6) by the user as determined beforehand. It is characterized by having at least one stopper (13) that ensures it stays fixed when it reaches the position. a cutting mechanism as in any of the above requirements (1). 25 10. Any of the above requirements characterized by the fuselage (2) which is a helicopter a cutting mechanism like in one (1). 30

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