Rotatable Reverse Propulsion System Transport Trolley

Abstract

The invention presents a reverse thrust maintenance system (B) developed to perform maintenance of reverse thrust elements (RI) in aircraft engines safely and efficiently. The system includes components such as support arm (1), crane linkage (2), gearbox (3), chassis (4), jack (5), wheel (6) and indicator (7).

Description

1 TARIFF Rotatable Reverse Propulsion System Transport Trolley TECHNICAL FIELD The invention reverses the thrust force generated in aircraft engines during flight. 5. Facilitating the maintenance of the counter-thrust elements that slow down the aircraft It relates to a reverse thrust maintenance system that provides this. STATE OF THE ART In the current state of the art, the counter-thrust elements found in aircraft engines The systems used in maintenance are generally fixed and have limited mobility. Current systems have some disadvantages. These systems have 10 components. It is inadequate for lifting, transporting and positioning, maintenance This makes the processes more difficult. In the current state of the art, mostly manual lifting and handling systems. Using manual rotation of the components to reach the area to be maintained, or It needs to be moved. This situation causes both a loss of time and 15 This increases the risk of damage to parts during maintenance, especially large and heavy ones. The inability to make precise angle and height adjustments on the components makes maintenance procedures difficult. This jeopardizes its accuracy and reliability. Current systems require components to be secured and moved in a controlled manner during maintenance. Because it cannot ensure proper adjustment, precise settings cannot be made, and the occupational safety risk is 20. The number of workers required is increasing. Current systems involve manual processes, resulting in excessive labor. It is used and excessive labor leads to erroneous interventions, thus improving the maintenance process. It prolongs the process. In addition, the handling of heavy components during manual operation requires the workers to... This poses a risk of injury and safety. In conclusion, systems with these shortcomings in the known state of the art; aircraft 25 safely and efficiently perform maintenance operations on the reverse thrust element located in their engines. It has shortcomings such as its inability to perform. This situation causes damage to the reverse thrust element. This increases the risk of vision loss, complicates care processes, and reduces the need for labor. 2 This increases the risk. Furthermore, existing systems are dependent on manual intervention. This leads to longer maintenance periods and increased occupational safety risks. Therefore, the reverse thrust element facilitates maintenance procedures and improves occupational safety. The need for innovative maintenance systems that improve performance is steadily increasing. The invention aims to eliminate the aforementioned disadvantages and introduce new technologies to the relevant technical field. It was developed to bring advantages. THE PURPOSE OF THE INVENTION The main purpose of the invention is to improve the maintenance of the thrust reversers found in aircraft engines. The goal is to carry it out safely, quickly, and efficiently. Another objective of the invention is to enable the controlled lifting of the counter thrust element, 10 Its purpose is to allow it to be moved and rotated at the desired angle. Another objective of the invention is to enable the reverse thrust element to be easily transported to the maintenance area and The goal is to ensure it remains fixed during the process. Another purpose of the invention is to enable precise angle and height adjustment during maintenance operations. The goal is to ensure the component is held in the correct position. 15 The aim of the invention is to reduce the need for labor in the maintenance process and to eliminate manual intervention. The goal is to minimize the existing dependency. Another purpose of the invention is to prevent damage to the reverse thrust element during maintenance operations. The goal is to minimize the risk of damage by preventing the person from seeing it. Another aim of the invention is to improve occupational safety through the maintenance system and provide 20 benefits for employees. The goal is to provide a safe working environment. The aim of the invention is to overcome the limited mobility in existing systems by achieving reverse thrust. The aim is to enable the element to be positioned in a more flexible and controlled manner. In conclusion, alternative solutions have been developed for all the problems mentioned above. It has been determined that innovation in the relevant technical field is appropriate. 25 3 A BRIEF DESCRIPTION OF THE INVENTION The invention is the framework of the aforementioned reverse thrust maintenance system, and the reverse thrust element. The chassis, which enables it to carry its weight and support its structure, is pushed back during maintenance. A gearbox that allows an element to rotate at an angle within a predetermined range. 5. During maintenance, raise the reverse thrust element to a predetermined height. Flight jacks found in aircraft engines are characterized by containing a jack that provides flight. reverse thrust, which causes the aircraft to slow down. with a reverse thrust maintenance system that facilitates the maintenance of the thrust element. It is related. Another preferred configuration of the invention is to place the aforementioned reverse thrust element on the outside. 10 The support connected to the aforementioned chassis provides a secure grip by wrapping around the section. It includes the arm. Another preferred configuration of the invention is the elimination of the reverse thrust element and crane connection attached to the aforementioned support arm to enable its transportation. It includes. 15 Another preferred configuration of the invention is the reverse thrust element during maintenance. It includes an indicator that ensures alignment at a predetermined position. Another preferred configuration of the invention is the contact of the aforementioned chassis with the ground. It includes at least one leg that provides support. Another preferred configuration of the invention is that the aforementioned chassis is positioned 20 feet above the ground. It includes wheels attached to the foot to enable movement. Another preferred configuration of the invention is the fixation of the aforementioned chassis. To ensure safety, at least one of the wheels includes a locking mechanism. BRIEF DESCRIPTION OF THE FIGURES The advantages of the current invention, along with its structure and additional elements, can be best utilized in 25 years. For understanding, it should be evaluated together with the figures explained below. is necessary. Figure 1. Front view of the reverse thrust maintenance system, which is the subject of the invention. Figure 2. Side view of the reverse thrust maintenance system, which is the subject of the invention. 4 Figure 3. Representative view of the reverse thrust maintenance system that is the subject of the invention. EXPLANATION OF REFERENCES IN THE FIGURES B. Reverse thrust maintenance system 1. Support arm 2. Crane connection 5 3. Gearbox 4. Chassis 5. Jack 6. Wheel 7. Indicator 10 TI. Reverse thrust element. DETAILED DESCRIPTION OF THE INVENTION This detailed explanation is provided solely for the purpose of better understanding the subject and does not contain any It is explained in a way that will not create a limiting effect. The invention described in detail below is a device found in aircraft engines and used in flight 15 Reverse thrust is the process of reversing the thrust force during a flight, thereby slowing down the aircraft. The invention relates to a reverse push maintenance system (B) which facilitates the maintenance of the element (TI). Safe lifting, transportation, and positioning of the reverse thrust element (RT) at the desired angle. The aim is to rotate the vehicle and provide access to the area to be maintained. Reverse thrust maintenance system (B) makes maintenance operations faster while reducing labor requirements 20 and ensures that it is done safely. The chassis (4) included in the invention carries the weight of the reverse thrust element (TI) and supports the structure. It forms the main supporting frame. The chassis (4) securely supports the reverse thrust element (TI). It allows it to be fixed and moved in some way. The chassis (4) contacts the ground. It includes at least 1 foot that provides support. Also, the chassis (4) is 25 on the ground. It includes wheels (6) attached to the foot to enable it to move. The wheels (6) enable the system to be moved easily in the maintenance area and The locking mechanism located on at least one of the wheels (6) of the chassis (4) It ensures that it is fixed in place. The gearbox (3) must be predetermined during maintenance operations of the reverse thrust element (TI). This allows it to rotate at the angle found in the range. This is because the reverse thrust element (TR) has 5 different angles. detailed examination from various angles and easier maintenance procedures. It makes it possible to perform. The gearbox (3) enables precise angle control. By providing this, it increases workplace safety during maintenance. The jack (5) lifts the reverse thrust element (TR) to a predetermined height. The jack (5) ensures that the load is lifted and lowered in a balanced manner. This ensures structural integrity during maintenance operations. The support arm (1) in the system wraps around the reverse thrust element (TR) from the outside and It provides a secure grip. In addition, the crane attached to the support arm (1) The connection (2) facilitates the lifting and transport of the reverse thrust element (TI). The invention also includes the predetermined 15 reverse thrust element (RI) during maintenance. It includes an indicator (7) that enables alignment in position. Indicator (7) provides alignment. It prevents problems. The invention describes a way to perform maintenance operations on a reverse thrust element (RT) in a safe and controlled manner. It is designed to perform maintenance on the working principle of the invention. The reverse thrust element (TI) is first attached to the support arm (1). Then the crane connection 20 Using (2), the reverse thrust element (TI) is lifted together with the support arm (1) and the chassis (4) It is mounted on it. After the assembly process is completed, the reverse thrust element is removed with the help of the jack (5). (TI) is adjusted to the desired height. The gearbox (3) is used for maintenance of the reverse thrust element (TI). It rotates in a way that allows access to the area where the task will be performed. Thanks to indicator (7), the reverse thrust element (TI) is correctly aligned. 25 The system moves thanks to wheels (6) and once it is ready for operation Then the wheels (6) are fixed by engaging the locking mechanism. Then the maintenance process is carried out. This structure reduces the labor requirement during the maintenance process. It reduces costs, increases operational safety, and makes maintenance operations more practical and efficient. It brings. 30 6 Figure 1, Figure 2 and Figure 3 show the representation of the reverse thrust maintenance system (B) which is the subject of the invention. Their appearances are given. The reverse thrust maintenance system (B) safely lifts the reverse thrust element (TI), It rotates at the desired angle, adjusts the height, and can be moved to the maintenance area. These features speed up maintenance operations, increase workplace safety, and 5 It reduces the risk of damage to the parts. This system ensures the safe and reliable operation of the reverse thrust element (TR). It reduces operator workload and maintenance time by ensuring efficient maintenance. It is abbreviated. The invention simplifies the maintenance of the thrust element (TH) found in aircraft engines. It offers an innovative reverse thrust maintenance system (B). The system has 10 reverse thrust elements (TI). safe handling, lifting and rotation at desired angles This ensures that maintenance operations are faster, safer and more efficient. This is happening. The invention reduces labor costs in aircraft engine maintenance processes. increasing operational efficiency and making maintenance procedures more practical and safer. It brings. 15 The scope of protection of the invention is specified in the attached claims, and these details are strictly adhered to. The explanation cannot be limited to what is given for illustrative purposes only. Because a technically expert person The person, without deviating from the main theme of the invention, can do something similar along with what is described above. It is obvious that these structures can emerge.

Claims

7 REQUESTS 1. The invention relates to a system that reverses the thrust force in aircraft engines during flight. Maintenance of the reverse thrust element (RT) that slows down the aircraft by turning it. It is a reverse push maintenance system (B) which facilitates; its feature is;  The mentioned reverse thrust maintenance system (B) is the skeleton, and reverse thrust 5 enabling the element (TI) to carry its weight and support its structure. chassis (4),  During maintenance, the reverse thrust element (RT) must be within the predetermined range. reducer (3) that enables it to rotate at the angle found,  During maintenance, raise the reverse thrust element (RT) to a predetermined height of 10 jack (5) that enables lifting, It is characterized by its inclusion.

2. A reverse thrust maintenance system (B) that meets any of the above requirements. Its characteristic feature is that it wraps the aforementioned reverse thrust element (TR) around its outer part, 15 Support arm (1) connected to the chassis (4) which provides a secure grip It includes.

3. A reverse thrust maintenance system (B) that meets any of the above requirements. Its feature is to enable the lifting and transportation of the reverse thrust element (RT). 20 It includes a crane connection (2) attached to the aforementioned support arm (1).

4. A reverse thrust maintenance system (B) that meets any of the above requirements. Its feature is that during maintenance, the reverse thrust element (RT) is predetermined. It contains an indicator (7) that enables alignment in position. 25 5. A reverse thrust maintenance system (B) that meets any of the above requirements. and its feature is that it has at least 1 chassis (4) that makes contact with the ground. It includes a foot.

6. A reverse thrust maintenance system (B) that meets any of the above requirements. Its feature is to enable the movement of the mentioned chassis (4) on the ground. It includes wheels (6) that are attached to the foot. 8 7. A reverse thrust maintenance system (B) that meets any of the above requirements. its feature is to ensure the fixing of the aforementioned chassis (4). at least one of the wheels (6) must contain a locking mechanism.