Safety Valve Test System

Abstract

The invention relates to a safety valve test system (E) that enables the testing of safety valves controlling aircraft cabin pressure. Safety valves controlling aircraft cabin pressure are critical to flight safety. The invention relates to a system that enables the safe, precise and efficient testing of various safety valves used in different aircraft models within the same test system.

Description

1 TARIFF Safety Valve Test System TECHNICAL FIELD The invention enables the testing of safety valves that control cabin pressure in aircraft. This relates to the safety valve testing system. This system makes testing processes safer, 5 It was developed with the aim of making it efficient and standardized. STATE OF THE ART Safety valves that control cabin pressure in aircraft are critical for flight safety. These are the components. In the known state of the art, testing safety valves is generally performed. This is done manually. Existing systems require a pressure of 10 during testing. ensuring that the conditions are met, evaluating whether the valve is working correctly, and This makes it difficult to obtain reliable test results. One of the biggest problems encountered in the known state of the art is during the testing process. The problem is the lack of standardization. Testing processes largely depend on operator experience. This is changing and causing inconsistencies in test results. 15 Different operators applying different procedures affects the accuracy and repeatability of the tests. This can negatively affect its availability. Another problem encountered in the known state of the art is the limited number of tests performed during testing. The valve is being tested. Another significant problem arises due to manual operations. These are occupational safety risks. Since safety valves are tested under high pressure, an incorrect 20 Incorrect assembly or faulty pressure control can lead to serious accidents. Especially manual... During the connections and testing procedures carried out, compressed air leaks or sudden bursts may occur. Pressure fluctuations pose a danger to operators. Tests performed under the known state of the art are generally time-consuming and require maintenance. This prolongs the processes. Long testing periods disrupt aircraft maintenance plans and 25 This reduces operational efficiency. Furthermore, lengthy testing increases maintenance costs. This increases the burden on airlines and maintenance centers. 2 The unreliability of test results under the known state of the art is also a significant issue. This is the problem. Current test systems provide accurate pressure measurements and valve performance. Their analyses are inadequate, and this leads to erroneous assessments. This is causing some valves to open unnecessarily due to false positive or negative test results. Failure to detect faulty valves during replacement poses a flight safety risk. It constitutes. Consequently, systems that have these shortcomings in the known state of the art, testing processes for safety valves used in aircraft in a safe and efficient manner. This prevents the accurate evaluation of the valves being tested. This complicates, prolongs maintenance processes, and increases occupational safety risks. 10 Furthermore, the reliance of current systems on manual intervention is reflected in the test results. This leads to inconsistencies and reduces operational efficiency. Therefore, this Testing processes of safety valves considering the problems innovative test systems that standardize, enhance safety and shorten maintenance times The need is steadily increasing. 15 The invention aims to eliminate the aforementioned disadvantages and create a new field in the relevant technical area. It was developed to bring advantages. THE PURPOSE OF THE INVENTION The main purpose of the invention is to enable safety valves that control aircraft cabin pressure to operate at specified pressures. The goal is to test whether it functions according to the test criteria. 20 Another purpose of the invention is to detect faulty or malfunctioning safety valves. The aim is to ensure these changes are made, thereby maximizing flight safety. Another aim of the invention is to standardize the assembly and testing procedures for safety valves. The goal is to shorten maintenance times and make workflows more efficient. Another aim of the invention is to increase safety in tests conducted under high pressure. 25 The goal is to minimize the health risks that operators may face. The purpose of the invention is to perform valve tests in a controlled manner and according to specific standards. The aim is to ensure measurement accuracy by performing this procedure. 3 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. A BRIEF DESCRIPTION OF THE INVENTION The invention functions as a closed pressure chamber in the aforementioned safety valve test system. The test tank, which enables the testing of safety valves, is the safety valve to be tested. the valves to be mounted on the clamp connection point on the aforementioned test tank The clamps provide the predetermined pressure and airflow during testing. by ensuring that the valve operates within the specified pressure limits within the specified time interval. It contains an air intake valve that allows measurement of whether it is working or not. 10 devices that control the cabin pressure of aircraft during flight to be characterized It relates to a safety valve testing system that enables the testing of safety valves. Another preferred configuration of the invention is the system that enables pressure measurement. It includes a pressure gauge connected to the aforementioned test tank. Another preferred design of the invention provides safety in case of overpressure. It includes a pressure reducer connected to the aforementioned test tank. 15 Another preferred design of the invention is the generation of oscillations during testing. It includes a torispherical dome connected to the aforementioned test tank that provides blocking. Another preferred configuration of the invention involves integrating the safety valves to be tested into the system. tank cap that allows connection and shutting off the pressurized environment during testing. It includes. 20 Another preferred configuration of the invention is the locking of the aforementioned tank lid. It includes clamps that connect to the aforementioned tank cap. Another preferred configuration of the invention is the aforementioned safety valves to be tested. Linear rail guide that allows alignment for securing to clamps. It includes the mechanism. 25 Another preferred design feature of the invention is the aforementioned test, which facilitates maintenance. It includes a drain valve connected to the tank. Another preferred configuration of the invention is the aforementioned safety valve test system. It is made of stainless steel. 4 BRIEF DESCRIPTION OF THE FIGURES The best way to utilize the advantages of the existing invention, together with its structure and additional elements. For understanding, it should be evaluated together with the figures explained below. is necessary. Figure 1. Representative view of the components of the safety valve test system, which is the subject of the invention. 5 Figure 2. Side view of the components of the safety valve test system, which is the subject of the invention. Figure 3. Representative view of the safety valve test system that is the subject of the invention. EXPLANATION OF REFERENCES IN THE FIGURES E. Safety valve test system 1. Test tank 10 2. Torispheric bomb 3. Tank bed 4. Tank bottom bearing plate 5. Tank bed intermediate supports 6. Tank manhole 15 7. Clamps 8. Linear rail slide mechanism 11. Pressure gauge 12. Pressure breaker 13. Air inlet valve 20 14. Drainage valve 15. Tank fixing plate 16. Grounding 17. Clamp connection point 18. Primary valve mechanism 19. Secondary valve mechanism 20. Primary sleeve inlet 21. Secondary sleeve inlet 5 22. Pneumatic sleeve connection unit 25. Tank cap 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. 10 The invention described in detail below controls the cabin pressure of aircraft. It relates to a safety valve test system (E) which enables the testing of safety valves. The invention describes the testing of safety valves under specified pressure and airflow conditions. It is designed to verify its operation and determine whether it is faulty. The invention involves installing safety valves in a closed test tank (1) at specified pressure levels 15 It includes various components for testing. In this context, the content of the invention includes: Each of the elements mentioned ensures that the testing process is reliable and efficient. They work together in harmony to ensure its realization. The test tank (1) included in the invention is a closed pressure chamber in which safety valves are tested. It functions as follows: Test tank (1), at the pressure levels determined during the test 20 It has a robust structure to provide a safe environment. Clamps (7) will be tested. by securing the safety valves to the clamp connection point (17) on the test tank (1) It ensures a secure mounting. The clamps (7) ensure that the valve remains fixed during testing and By ensuring it is held in the correct position, it increases measurement accuracy. Test During this time, the specified pressure and air flow are provided through the air inlet valve (13) 25 The response of the safety valve is measured. The air inlet valve (13) responds to the valve at a specified time interval. It measures whether it is operating within the specified pressure limits. This 6 This allows us to test whether the valve is functioning correctly under the specified pressure conditions. is being done. During the test procedure, the pressure inside the test tank (1) must be measured precisely and It needs to be checked. For this purpose, the pressure gauge integrated into the test tank (1) (11) is used. During the test, to prevent excessive pressure build-up and 5 A pressure breaker (12) is used to ensure the safety of the system. Pressure breaker (12), When the specified pressure level is exceeded, it activates the test tank (1) It prevents damage. The test tank (1) is designed to withstand pressure. Torspherical dome (2), By preventing oscillations (pressure fluctuations) that may occur during testing, it is even better. It provides a stable test environment. Thanks to this component, the test tank (1) during the test This ensures an even pressure distribution and increases the system's durability. The safety valves to be tested must be connected to the test environment and pressurized during testing. The tank lid (25) is used to ensure the environment is closed. The tank lid (25) is used for testing. the tank (1) should be closed safely and the test should be completed without pressure loss 15 It makes it happen. Clamps (7) are used to ensure the tank lid (25) is locked. Clamps (7), By securing the tank lid (25), any leakage problems during the test can be avoided. It ensures the test can be carried out properly without opening the container. 20 for fixing the safety valves to be tested to the aforementioned clamps (7). A linear rail slide mechanism (8) is used to ensure its alignment. The mechanism is to fix the valves in the specified position in the test tank (1) and It helps ensure the test is carried out according to standards. Linear rail slide The registration mechanism (8) prevents test errors caused by misalignment. After the test process is completed, the remaining compressed air or other 25 in the test tank (1) The test fluids must be drained. For this purpose, a drain valve (14) is used. The drain valve (14) facilitates maintenance and cleaning of the test system for subsequent testing. It allows for quick preparation. The invention enables the safe and accurate operation of safety valves that control aircraft cabin pressure. It functions as a safety valve test system (E) which enables testing. 30 of the invention In terms of operating principle, the testing process begins with the installation of the safety valve into the system. 7 The safety valve to be tested is connected to the test tank (1) using the clamp connection point (17). It is connected and the desired test is performed with the help of the linear rail slide registration mechanism (8). It is brought to the position. After the safety valve assembly is complete, the pressurized medium To ensure this, the tank lid (25) is closed and locked with clamp (7). The test is performed by introducing air into the system at a specified pressure. Air inlet 5 Air or gas is supplied to the test tank (1) via valve (13) and the safety valve operating within the specified pressure values ​​within the specified time interval It is measured whether it is working. In case of excessive pressure that may occur inside the tank during the test. safety pressure is provided by the breaker (12). After the test procedure is completed, the pressure relief valve (14) inside the system 10 It is drained through this mechanism, and the tested valve is safely removed from the system. This procedure... Thanks to this principle, safety valves reduce the pressure that is critical for flight safety. They are checked and it is determined whether the safety valves are functioning correctly. The components of the safety valve test system (E) subject to the invention are shown in Figures 1, 2 and 3. Representative images are given. 15 Because the safety valve test system (E) material is stainless steel, it is suitable for long-term use. deterioration resulting from adverse environmental impacts that occur after use It provides high resistance to corrosion. Therefore, the tested safety valves were resistant to corrosion. The materials are unaffected by rust and other harmful elements. Thus, the system is safe. By maintaining the accuracy and reliability of the valves for a long time, the testing processes are carried out in a healthy manner. It allows it to be carried out in this way. Safety valve test system (E) of safety valves that control aircraft cabin pressure It ensures that testing is carried out safely and precisely, improves workplace safety and operational efficiency. It increases efficiency. The safety valve test system (E) ensures that the safety valves comply with standards. It enables testing in this way, reduces the workload of operators, and streamlines testing processes. This makes it safer and more practical. The invention provides precise pressure control during testing. Safety valve test system. (E) makes it possible to carry out tests in a more systematic, safe and error-free manner. This innovative system ensures that aircraft safety valves operate correctly and efficiently. It enables testing. 30 8 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

9 REQUESTS 1. The invention relates to a safety device that controls the cabin pressure of aircraft during flight. a safety valve test system (E) that enables the testing of valves, feature;  In the aforementioned safety valve test system (E), a closed pressure chamber 5 This test performs the function of enabling the testing of safety valves. tank (1),  the safety valves to be tested are on the mentioned test tank (1) Clamps (7) that enable mounting to the clamp connection point (17),  During the test, the predetermined pressure and airflow were maintained. 10 the valve's specified pressure limits within the specified time interval air intake valve that allows measurement of whether it is working or not. (13),  with the mentioned test tank (1) which provides safety in case of overpressure connected pressure breaker (12), 15 It is characterized by its inclusion.

2. A safety valve test system (E) conforming to Claim 1, whose characteristic is; the pressure of the system. pressure gauge (11) connected to the mentioned test tank (1) which enables measurement It includes. 20 3. A safety valve test system (E) that complies with any of the above requirements. Its feature is that it prevents the formation of oscillations during testing. It contains a torispheric dome (2) connected to the mentioned test tank (1). 25 4. A safety valve test system (E) that complies with any of the above requirements. Its feature is that it connects the safety valves to be tested to the system and tests them. It includes a tank cover (25) which enables the pressurized environment to be closed during the process.

5. A safety valve test system (E) that complies with any of the above requirements. its feature is that it enables the locking of the mentioned tank lid (25). It includes clamps (7) connected to the mentioned tank cap (25).

6. A safety valve test system (E) that complies with any of the above requirements. The feature is that the safety valves to be tested are attached to the aforementioned clamps (7) linear rail slide mechanism that enables alignment for fixing. (8) includes. 5 7. A safety valve test system (E) that complies with any of the above requirements. its feature is that it is connected to the mentioned test tank (1) which provides ease of maintenance. It includes a drain valve (14).

8. A safety valve test system (E) that complies with any of the above requirements. and its feature is that the mentioned safety valve test system (E) is stainless steel. It is made of a certain material.

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