A liquid filling apparatus.

The integrated piston and piston nut structure with a male and female flange system addresses the inefficiencies and safety issues of current liquid filling methods, providing a rapid, leak-proof, and safe liquid transfer solution for aircraft.

TR202414991YPending Publication Date: 2026-10-21TUSAŞ - TÜRK HAVACILIK & UZAY SANAYİİ ANONİM ŞİRKETİ
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Patent Information

Application Number
TR202414991U
Authority / Receiving Office
TR · TR
Patent Type
Utility models
Current Assignee / Owner
Filing Date
2024-11-01
Publication Date
2026-10-21
Estimated Expiration
2034-11-01

AI Technical Summary

Technical Problem

Current liquid filling methods for aircraft are time-consuming, prone to leakage, pose occupational health risks, and can result in equipment loss due to manual operation and loose connections, especially in high-pressure applications.

Method used

A leak-proof liquid filling apparatus with an integrated piston and piston nut structure, featuring a male and female flange system with sealing elements and a fool-proof clamping mechanism to ensure secure, pressurized filling without leakage.

Benefits of technology

The apparatus ensures rapid, safe, and reliable liquid transfer, reducing operator errors and preventing equipment loss, while maintaining a leak-proof seal and enhancing operational safety.

✦ Generated by Eureka AI based on patent content.
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Abstract

The invention relates to a liquid filling apparatus that enables pressurized filling of a liquid tank located on an aircraft, which fits perfectly to the tank opening and prevents leakage during filling.
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Description

1 TARIFF A LIQUID FILLING APPARATUS The technical field to which the invention relates: The invention enables pressurized filling of a liquid reservoir located on board an aircraft. providing, perfectly matching the reservoir opening and during filling 5 It relates to a liquid filling apparatus that prevents leakage. State of the art: Used to protect operational unmanned aerial vehicles (UAVs) from ice. Liquids are filled manually using a funnel. Pressurized filling. Because it cannot be done this way, refilling an aircraft with fluid takes approximately 5 hours. 10 This manual process, in addition to being a waste of time, causes the liquid to spill onto the operator and Because there is a possibility of it spilling onto the aircraft, it is also a matter of occupational health and safety. This carries a risk. Error or incorrect action by the personnel performing the liquid filling process. There is also a possibility that the equipment may fall into the aircraft's cargo hold as a result of its use. Additionally... The filling devices must have a leak-proof design and fit together perfectly. 15 It is necessary. Furthermore, hydraulics can maintain high pressure even when it is possible to achieve it during liquid filling. Problems with piston loosening in hydraulic transmission systems operating under pressure. It is located there. The nut, which is used to prevent the piston from loosening, is separate from the piston. Because they are included as a component, these two are sufficiently robust in 20 The problem of lack of interconnectedness arises. This situation leads to high pressure and In high-speed fluid transfer operations, the piston or nut may loosen, and this... This can result in a loss of connection power. Connection Unexpected loosening of these components can lead to fluid leaks. The South Korean-made 25 with registration number “KR102057922B1” is in the known state of the art. The invention in question concerns the connection structure of the piston and piston nut. by improving the piston and piston nut to prevent them from loosening. By implementing an integrated structure for the piston nut, we can solve the above problems. It is designed with an improved joint structure between the piston and a piston nut. 2 A hydraulic cylinder device consists of a rod, a piston, and a piston nut. A piston and a piston nut are integrated, thus forming the piston and piston nut. A structure has been developed that prevents the nut from loosening. United States number “US7318327B2” in known state of the art. The invention, which is the subject of the application originating from [origin], is a small-scale liquid oxygen liquefaction device. 5 The device aims to increase safety, efficiency, and costs in liquid oxygen production. The devices and methods developed for lowering the liquid are described. In one application, the liquid a liquid oxygen tank is placed between the cryocooler and the dewar to control oxygen escape. A barrier is added. A boiling tube connected to the dewara prevents the dewara from tipping over. It allows the expanding gas to escape while enabling the liquid to settle safely in the tube. 10 It recognizes a tipping trigger switch that cuts off the power when the device is tipped over. United States number “US8915268B2” in the known state of the art. The invention that is the subject of the application originating from [origin] is a liquefied gas storage / delivery system. and describes the method involving a liquefied gas storage system. Liquefied gas storage systems include the supply of liquefied gases such as liquid oxygen (LOX). It includes a structure containing a suitable storage container. The structure's outer surface is rotatable. A turntable is provided. The most important feature of a portable liquid storage / delivery device. an interface shaped to fit the shape of at least part of the turntable It is provided in or on a portable liquid storage / delivery device. A connector is located on the interface that connects to a corresponding connector. Two 20 connector, insertion of portable liquid storage / delivery device into interface and rotating It is joined by rotating the table. The current state of the technology involves liquid filling devices. However, UAVs are aerial. A fully leak-proof seal for the vehicle's de-icing system fluid filling adapter. Liquid 25, which has this feature and ensures a perfect fit with the male-female structure of the tank flanges. There are some missing filling devices. In conclusion, due to the negative aspects described above and the current solutions, the subject matter... Due to its shortcomings, an improvement in the relevant technical field is necessary. It has been made. 3 The purpose of the invention: The main purpose of the invention is to connect the UAV's ice protection fluid to the tank filling nozzle and the liquid. by aligning the filling apparatus perfectly and fitting together in a form-compatible manner. The sealing process ensures a leak-proof finish. Another objective of the invention is to reduce the liquid used for ice protection in UAVs to 5. for filling by being able to perform pressurized filling without any leakage. The goal is to save time. Another purpose of the invention is the leak-proof clamping mechanism located on the liquid filling apparatus. Its mechanism is to eliminate risks to occupational health and safety. Another aim of the invention is to develop a fool-proof liquid filling apparatus. Even personnel who have no knowledge of the operation can make mistakes. its purpose is to prevent him from doing it. Another purpose of the invention is to separate the parts of the apparatus by tightening them with a leak-proof bolt. This eliminates the possibility of the aircraft falling into the cargo hold due to operator error. The structural and characteristic features and all the advantages of the invention are given in Figure 15 below. And thanks to the detailed explanation written with reference to these figures, it becomes clearer. This will be understood as such. Therefore, the evaluation should also include these forms and detailed explanations. This should be done taking that into consideration. Explanation of the figures: FIGURE -1; Fluid pipe, liquid reservoir and tank of the liquid filling apparatus subject to the invention 20 It is a drawing that depicts the relationship. FIGURE -2; The connection of the male flange and the tank flange of the liquid filling apparatus, which is the subject of the invention. It is a drawing that gives an isometric view. FIGURE -3; Isometric view of the cap of the liquid filling apparatus, which is the subject of the invention. It is a drawing that gives the image. 25 4 FIGURE -4; Isometric view of the reservoir opening on which the liquid filling apparatus subject to the invention is seated. It is a drawing that gives the image. Reference numbers: 1. Device cover 2. Body 5 3. Liquid reservoir 301. Warehouse opening 302. Female flange 303. Ear openings 4. Tank 10 5. Fluid pipe 6. Device cover 7. Male flange 701. Ear protrusion 8. First sealing element 15 9. Second sealing element D. Hole B. Connector P. Liquid reservoir 10th Segment 20 Description of the invention: The invention involves transferring a liquid from a tank to a liquid reservoir located on board an aircraft. Enables transfer by pressurized filling, perfectly compatible with the tank opening. a liquid filling that overlaps and has a leak-proof feature during filling It is related to the apparatus (1). 5 On the fuselage (2) of the aircraft, there is a liquid storage compartment. There is a liquid reservoir (3). Liquid from this reservoir (3) opens to the outside of the body (2). a tank opening (301) that allows liquid to be transferred from outside into the tank (3) It is located. Around the part where the tank opening (301) opens to the outside of the body (2) There is a female flange (302) that forms an indentation shape. The female flange has 10 (302) located outside the body (2) carrying liquid transferred to the liquid reservoir (3) inside There is a tank (4). The pump (P) pumps the liquid from the tank (4) to the liquid reservoir (3). It enables pressurized transfer. It comes out of the tank (4) and goes to the pump. (P) connected and reaching the tank opening (301) from the tank (4) to the liquid storage tank (3) The transfer takes place via a fluid pipe (5). 15 The apparatus cover (6) has a fluid pipe (5) passing through it, and the fluid pipe (5) has a reservoir. The part that acts as a guide on the mouth (301). The apparatus cover (6) guides the reservoir mouth. (301) almost closes. The first sealing element (8) of the connecting parts is the male flange (7) the fluid tube (5) that passes through it is on both the liquid filling apparatus (1) and 20 It ensures that the reservoir opening (301) remains securely in place. By tightening by fixing it, it prevents the pressurized liquid from leaking and the liquid filling apparatus (1) to provide a leak-proof feature and the apparatus cover (6) and fluid pipe (5) It ensures a watertight seal between them. The second sealing element (9) is a conical 25 between the fluid pipe (5) and the female flange (302). It sits on the surface and provides a leak-proof seal here. It is located on the tank opening (301). By placing it in the conical region between the female flange (302) and the leakage that occurs in this region To prevent. In the liquid filling apparatus (1), the ear opening (303) is located on the male flange (7). at least one ear projection (701) in a fully compatible form, male flange (7) female flange (302) 30 6 when placed on it, by the user around the center direction by turning it, the form fits into the ear openings (303) and the male flange (7) Liquid filling is ensured by fully inserting the female flange (301). After the fluid tube (5) passes through the apparatus cover (6), the retaining ring (10) The assembly is being carried out. The segment (10) differs from its common use in the invention. When all the bolts are removed, the fluid pipe (5), the fluid tank (3) It is used to prevent it from falling inside. There is a female flange (302) located on the tank of the UAV. Female flange (302) Liquid filling apparatus (1) passing through the female flange (302) by matching with the opening. There is a male flange (7) on it. Liquid filling apparatus (1), tank 10 Due to the narrowness of the filling area, the existing reservoir opening (301) is in the form of a male mold. It has been developed. The male flange (7) is installed on the tank after being rotated. It contains at least one binder (B) which ensures the stability of its position. At least two of them facing each other at the warehouse mouth (301) opening, ear at least two ear openings (303) forming an indentation in the form of a female flange (302) opening 15 By ensuring a one-to-one form fit, the female flange (302) is fitted into the ear openings (303) and then rotated around the center line at an angle of 90 degrees to the female flange (302) and a male flange (7) that fits perfectly into the ear openings (303). The fluid pipe (5) passed through the male flange (7) is both a liquid filling apparatus It is securely tightened, ensuring it stays firmly in place both on the surface and on the warehouse entrance. 20 Prevents leakage of pressurized fluid and provides a leak-proof seal to the fluid filling apparatus. There is a primary sealing element (8) that provides a first seal. The primary seal sealing between element (8), tank cap (6) and fluid pipe (5) The second sealing element (9) is provided by the female flange (302) with the fluid pipe (5). It sits on the conical surface between them, ensuring a watertight seal. 25 First sealing element (8) and second sealing element (9), liquid filling It is also used to act as a spring in the apparatus (1). Liquid filling During the mounting of the apparatus (1) into the liquid reservoir (3), the hole (D) of the connector (B) The device cover (6) and fluid can be squeezed inside by the user. The gap between the pipe (5) is the first 30 provided by their structural rigidity. There is a sealing element (8) and a second sealing element (9). 7 sealing element (8) and second sealing element (9), chemical resistance and EPDM (Ethylene Propylene Diene) provides spring force. Monomer) has been selected. User error with the use of the circlip (10) and interlocking parts, A simple, straightforward, and reliable (fool-proof) 5 that leaves no room for misuse. This provides an advantage. Thanks to this feature of the liquid filling apparatus, both the bolt This eliminates the need for tightening and also prevents operator error in one of the devices. This eliminates the possibility of the aircraft falling into the cargo hold. 15 25

Claims

8 REQUESTS 1. A fuselage (2) located on the aircraft, located on the fuselage (2), inside a liquid storage tank (3), liquid storage tank (3) out of the body (2) an opening that allows liquid to be transferred from the outside into the liquid reservoir (3) tank opening (301), where the tank opening (301) opens to the outside of the body (2) 5 a female flange (302) that forms an indentation around the circumference, outside the body (2) carrying liquid transferred to the liquid reservoir (3) a tank (4) pumps the liquid from tank (4) into the liquid reservoir (3) under pressure a pump (P) that enables the transfer, comes out of the tank (4) and to the pump (P) connected, eventually reaching the tank opening (301) and from the tank (4) to the liquid reservoir 10 (3) a fluid pipe that provides fluid transfer (5), through which the fluid pipe (5) acts as a guide on the reservoir opening (301) of the fluid pipe (5). seeing, a device cover (6) that closes the tank opening (301), pump from the tank (3) (P) enables the filling of liquid into the liquid reservoir (2) by the pressure it provides. Liquid filling apparatus (1), its feature is; 15 - at least 2 of them will face each other at the tank opening (301) at least two ear openings that form an ear-shaped indentation (303) provides a perfect form match with the female flange (302) opening. flange (302) is fitted into the ear openings (303) and then centered rotated at an angle of 90 degrees around its direction to the female flange (302) and 20 At least one male flange (7) that fits perfectly into the ear openings (303),  The fluid pipe (5) passed through the male flange (7) is both liquid secure on the filling apparatus (1) and on the tank opening (301) secured by tightening, preventing pressurized fluid from leaking. 25 sealing between apparatus cover (6) and fluid pipe (5) a first sealing element (8), - by sitting on the conical surface between the fluid pipe (5) and the female flange (302) a second sealing element that provides the seal here (9) It includes. 30 2. Liquid filling apparatus (1) conforming to claim 1, its features are; fluid tube (5), apparatus by passing through the cover (6) it remains fixed on the tank opening (301) 9 enabling the fluid pipe during disassembly of the apparatus cover (6). (5), fluid in such a way as to prevent it from falling into the liquid tank (301) until the pipe (5) and the apparatus cover (6) are completely removed from the body (2) It must contain at least one retaining ring (10) that holds it in place.

3. Liquid filling apparatus (1) conforming to claim 1, its feature is; 5 on male flange (7). At least one hole (D) located in the hole (D) passes through the apparatus cover (6) male At least one connector (B) connecting to the flange (7), assembly of the liquid filling apparatus (1) and It includes a hole (D) and a connector (B) through which disassembly is enabled.

4. Liquid filling apparatus (1) conforming to claim 1, its feature is; on the male flange (7) at least one ear located in a form that is perfectly in line with the ear opening (303) 10 When the projection (701) is fitted onto the male flange (7) and the female flange (302), the center rotated by the user around its direction to fit into the ear openings. (303) fitting in form compatible and male flange (7) to female flange (301) Liquid filling apparatus (1) that enables liquid filling by fully entering. It includes. 15 5. Liquid filling apparatus (1) conforming to claim 1, and its feature is that the liquid filling apparatus has a first sealing element (8) and second sealing element which act as a spring (9) is included.

6. Liquid filling apparatus (1) conforming to Claim 1, and its feature is; liquid filling apparatus (1), During the assembly of the liquid reservoir (3), the connector (B) should be inserted into the hole (D) 20 The device cover (6) and fluid tube (5) can be tightened by the user. the gap between them is the primary seal provided by their structural rigidity. It includes element (8) and second sealing element (9).

7. Liquid filling apparatus (1) conforming to Claim 1, its characteristic is; chemical resistance and The first seal, which has an EPDM structure providing the spring force, is 25. It includes element (8) and second sealing element (9).

8. Liquid filling apparatus (1) conforming to claim 1, its features are; fluid pipe (5), tank all bolts that are assembled after passing through the cover (6) When removed, the fluid pipe (5) prevents it from falling into the tank. It contains at least one segment (10). 30