PILOT HELMET VISOR OPENING AND CLOSING SYSTEM
The guide rail assembly with slots and holding device addresses issues of uncontrolled visor movement and mechanical wear by securing the visor at specific angles, ensuring stable and ergonomic operation.
Patent Information
- Application Number
- TR202512622
- Authority / Receiving Office
- TR · TR
- Patent Type
- Applications
- Current Assignee / Owner
- Filing Date
- 2025-09-03
- Publication Date
- 2026-10-21
AI Technical Summary
Current pilot helmet visor systems suffer from uncontrolled position changes due to vibrations, inability to fix the visor at desired angles, risk of involuntary movement during one-handed use, and mechanical wear leading to security risks.
A guide rail assembly with slots and a holding device that secures the visor at specific angles, allowing gradual, user-controlled movement and dual-hand operation, ensuring stability and durability.
The system provides controlled and secure visor operation, preventing involuntary movements and mechanical loosening, enhancing flight safety and ergonomics.
Smart Images

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Abstract
Description
1 TARIFF PILOT HELMET VISOR OPENING AND CLOSING SYSTEM Technical Area 5 The invention is a visor integrated into pilot helmets, primarily for military and civil aviation. It relates to an on / off system for these systems. The invention is particularly useful for protecting pilots' eyes from sunlight, wind, and foreign objects during flight. or visors that protect against sudden weather changes, in a controlled and safe manner It relates to an on / off system that allows it to be opened and closed. State of the Art The current technology is developed for opening and closing pilot helmet visors. These mechanisms generally consist of hinged, spring-loaded, or sliding structures. Most mechanisms involve manually moving the visor up or down. Although it provides this, it does not offer a stepped positioning feature or provides this feature insufficiently. It cannot provide security and stability. 20 Common technical problems encountered in systems used in current technology. These are: • Uncontrolled changes in visor position: Vibrations that occur during flight, Due to sudden maneuvers or mechanical loosening, the visor may malfunction. 25 It can be opened or closed. • Inability to fix the visor at the desired angle: In most current systems, the visor... It is not possible to fix it at different angles. This affects the pilot's vision requirements. It does not provide sufficient flexibility. • Risk of involuntary movement due to one-handed use: Some visor systems have a single 30 It is designed to be operated manually. This is especially true in shaky environments. It can cause involuntary movements and negatively affect flight safety. It can have an impact. • Problems with parts that wear out or loosen over time: Spring and hinge parts. Mechanical wear due to prolonged use in systems, position 35 There may be a decrease in sensitivity and a security risk may arise. 2 In the literature review, an example of the current state of the technique is given. Document number US20100132085 can be shown. This document mentions a protective measure. A multi-position adjustable viewfinder system is defined for the headsets. However, The system uses a friction-based position fixing logic instead of a claw-like structure. It has and there is no mention of a rail system. 5 Another example of the prior art is document number EP0651952. This can be demonstrated. The document in question describes rotating the viewfinder around an axis. A system with a hinge mechanism that provides two-hand control has been described. This design incorporates a stepped movement or locking claw system on the rail. It does not receive. Another example of the prior art is document number US12064001. This can be shown. In the document in question, a multi-part structure is integrated into a heading. The viewfinder system has been explained. However, details of the mechanism for securing the viewfinder are not provided in section 15. It is limited and does not include a user-controlled incremental pause feature. Another example of the prior art is document number US20120272484. This can be shown. The document in question describes sliding controls for positioning the viewfinders. The mechanism has been defined. This structure resembles a rail system, but with clawed 20 No locking or stepped control features have been included. Another example of the prior art is document number US11583026. This can be shown. In the document mentioned, the hinge is used when changing the position of the viewfinder. A spring support system integrated into its structure is described. However, the system has 25 The safety mechanism and two-handed control approach are not included. In conclusion, the existence of the above problems and the inadequacy of the current solutions, This has made it necessary to make improvements in the technical field. Purpose of the Invention The present invention eliminates the aforementioned disadvantages and contributes to the relevant technical field. This relates to the pilot helmet visor opening and closing system, which brings new advantages. 35 3 The main purpose of the invention is to protect pilots' eyes from sunlight, wind, and foreign objects during flight. Visors that protect against objects or sudden weather changes, ensuring controlled and safe operation. The goal is to create an on / off system that allows it to be opened and closed in this way. The purpose of the invention is to allow the pilot to open and close the visor according to their needs. while recognizing, it prevents the position from being disrupted by sudden movements or jolts, and the visor... a system that allows for gradual, user-controlled and safe movement The goal is to create an on / off system. Another purpose of the invention is for the visor to move along the guide rail, and the guide rail 10 The visor is secured in place by a clip-on structure at specific locations. opening and closing gradually in a smooth and controlled manner, and the visor's specific By ensuring that it is securely fixed at various angles, it protects both flight safety and the user. The goal is to create an opening and closing system that improves ergonomics. Another aim of the invention is to prevent involuntary movements that require the use of both hands. by passing through and guaranteeing the conscious operation of the system, and being durable, long-lasting and The goal is to create an opening and closing system that offers a mechanically stable structure. Another aim of the invention is the design of materials and structures with high mechanical strength, 20 a switching system is developed that ensures the system operates safely for a long time. to place. Another aim of the invention is to overcome the sudden loosening encountered in existing visor mechanisms, It offers solutions to problems such as loss of position or difficulty in control, and the viewfinder can be positioned at the desired 25°. stepped stop structures that allow it to be fixed at the angle, simultaneous dual hand control. and with its mechanical design that provides locking security even in vibrating environments to enable pilots to have a more stable and safer field of vision during flight The goal is to create an on / off system. Another aim of the invention is to provide an original contribution to the state of the art and to pilot making helmet visor systems safer, more ergonomic and user-friendly The goal is to create an on / off system that allows for this. To fulfill all the objectives stated above and those that can be derived from the detailed explanation. 35 The invention, in particular, is integrated into pilot helmets for military and civil aviation applications. 4 The opening and closing system used in visors that allows the visor to be opened and closed. being, - a guide rail that attaches to both sides of the helmet and has slots inside including guide rail assembly, - Intermediate connecting element, which is attached to the visor and placed on the guide rail assembly, 5 - moves on the guide rail assembly by connecting to the intermediate connecting element. front cover, positioned on the connecting element, front cover a guide rail located inside the back cover that is closed The viewfinder position can be adjusted by gradually sliding it into the slots on it. This is related to the fact that it includes a holding device that allows it to be secured. 10 The structural and characteristic features and all the advantages of the invention are given in the figures below. And thanks to the detailed explanation written with references 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 this into consideration. 15 Figures that will help understand the invention. Figure 1: On / off system of the invention mounted on the helmet. It is the appearance. 20 Figure 2: Guide rail assembly of the opening and closing system subject to the invention. It is the appearance. Figure 3: View of the guide rail of the opening and closing system that is the subject of the invention. Figure 4: Helmet fastening element of the on / off system, which is the subject of the invention. It is the appearance. 25 Figure 5: Intermediate connection element of the opening and closing system that is the subject of the invention. It is the appearance. Figure 6: Intermediate connection element of the opening and closing system subject to the invention, visor and This is a view of the vehicle assembled with the mounting bracket. Figure 7: General description of the holding device of the opening and closing system subject to the invention. It is the appearance. Figure 8: Front cover of the holding device of the opening and closing system subject to the invention, open. It is the appearance of its state. Figure 9: View of the latch of the opening and closing system that is the subject of the invention. 35 Explanation of Part References 10. Guide rail assembly 11. Guide rail Nest 111, 5 12. Helmet fastener 20. Intermediate connector 30. Holding device 31. Front cover 32. Back cover 10 33. Elastic part 34. Nail S. On / Off system K. Helmet 15 V. Viewfinder Detailed Description of the Invention In this detailed description, the preferred 20 of the on / off system (S) that is the subject of the invention alternatives, solely for the purpose of better understanding the subject and without any limitations It is explained in a way that will not create an impact. Figure 1 shows the appearance of the on / off system (S), which is the subject of the invention, on the helmet (K). It is given. Accordingly, the opening and closing system (S) in its most basic form; both 25 of the helmet (K). The guide rail assembly (10) connected to the side is connected to the visor (V) and the guide rail intermediate connecting element placed inside (12) helmet connecting element (10) in the assembly (20) is connected to the intermediate connecting element (20) on the guide rail assembly (10). the guide rail assembly (10) of the moving and contained claw (34) The visor (V) 30 fits into the slots (111) on the rail (11) in a stepwise manner. It includes a holding device (30) that ensures its position is fixed. The invention concerns an on / off system (S) that protects pilots' eyes from sunlight during flight. The visor (V) of the helmet protects against wind, foreign objects or sudden weather changes. (K) enables it to be opened and closed and fixed at specific angles. 35 6 The guide rail assembly (10) shown in Figure 2 is a guide rail with slots (111) inside. Helmet mount that is connected to the helmet (K) by being fixed to the rail (11) and guide rail (11). It consists of elements (12). The guide rail (11) enables the movement of the visor (V). It is a structure. The helmet mounting element (12), which is combined with the guide rail (11), guide rail The guide rail assembly (10) ensures that the (10) is fixed to the helmet (K). 5 It is attached to both sides of the helmet (K). The intermediate connector (20) shown in Figure 5 is connected to the visor (V) as shown in Figure 6. It is connected and placed in the helmet connector (12). The said intermediate fastening element (20), through the guide rail assembly (10) of the visor (V) to the helmet (K) 10 It allows the device to be fixed in place while remaining mobile. A holding device (30) is attached to the connecting element (20) as shown in figure 6. It is connected. The holding device (30) shown in Figure 7 is connected to the guide rail assembly (10) in the guide rail assembly. It moves on the rail (11). The said holding device (30) moves every 15 of the helmet (K). Adjusting the position of the viewfinder (V) by holding it manually on both sides by the user It provides. The holding device (30) is basically a connecting element (20) that is positioned on the connecting element (20). front cover (31), rear cover (32) which is closed on the front cover (31), intermediate connecting element 20 (20) and positioned between the front cover (31) and the front cover (31) and Elastic part that enables the holding device (30) to move on the guide rail (11). (33) is positioned on the intermediate connecting element (20) and the front cover (31) and front cover (31) and the claw that fits into the slots (11) in the guide rail (111) (34) includes. 25 In the opening and closing system (S) which is the subject of the invention, on both sides of the helmet (K), the holding device (30) by pulling the visor (V) backward on the guide rail (11) The movement is enabled. When the visor (V) is brought to the desired position, the holding device (30) is left and the claw (34) is made to enter the socket (111) visor (V) 30 It is being fixed.
Claims
7 REQUESTS 1. Integrated into pilot helmets (K), especially in military and civil aviation. The opening mechanism used in the visors (V) that enables the visor (V) to be opened and closed. Closing system (S), its feature is; 5 - connected to both sides of the helmet (K) and containing sockets (111) guide rail assembly (10) containing a guide rail (11), - The intermediate part is placed on the guide rail assembly (10) by connecting to the visor (V). fastener (20), - Guide rail assembly (10) connected to the intermediate connecting element (20) 10 moving on and on the connecting element (20) positioned front cover (31), rear cover closed on front cover (31) a guide rail (11) of a tab (34) located inside the cover (32) by means of gradually entering the slots (111) on the visor (V) It includes a holding device (30) that ensures its position is fixed. 15 2. A shut-off system (S) that conforms to Claim 1, and its feature is; as stated in the guide. The guide rail assembly (10) is fixed to the raya (11) and connected to the helmet (K). It includes a helmet fastening element (12) which enables it to be fixed to the helmet (K).
3. A switching system (S) that conforms to Claim 1, and its feature is; the aforementioned intermediate positioned on the connecting element (20) front cover (31) and front cover (31) placed between and the holding device (30) on the guide rail (11) It contains an elastic part (33) that enables it to move.
