An emergency exit system.

Abstract

The invention relates to an emergency exit system that connects the transparent and the frame to the structural part using a flanged connection on the pipeline, providing emergency exit in case of emergency without relying on human force. Specifically, the invention relates to an emergency exit system from transparent panels with a spring-loaded fitting mechanism comprising a frame (outer and inner), a shaft with a housing, a spring-loaded claw, a shaft with a hole, and a handle.

Description

1 TARIFF AN EMERGENCY EXIT SYSTEM The technical field to which the invention relates: The invention involves structurally combining transparency and framing using flanged connections onto a pipeline. emergency exit 5, which connects to the part and does not rely on human power in case of emergency exit. It relates to an emergency exit system that provides access. The invention specifically refers to a frame consisting of an outer frame and an inner frame, a shaft containing a housing, a spring-loaded fitting mechanism consisting of a spring-loaded claw, a shaft with a hole, and a handle It is related to the emergency exit system via transparent panels. State of the art: 10 There are currently several different methods for transparent emergency exit systems. The best known of these is the transparent silicone-based gasket and compression fitting used in the vehicle structure. It is a design solution where the element is connected with a filler. The risk in this design solution is; For emergency exits, depending on the transparent material and the hardness value of the gasket used. The difference is that the force that needs to be applied varies. This amount of force can be 15 Time is the weakest human being in terms of strength, as defined by human factors standards. It reaches levels of force that its profile cannot apply. Another well-known and frequently used emergency exit method is the blasting system on transparent material. It is a design solution that includes integration. When this method is preferred, the system the cost increases significantly and human health is at risk due to the presence of explosives. It carries risks in this regard. Emergency exit windows breaking or opening without force during exit Strong seals are used to ensure this. These seals protect the glass from damage. by ensuring a tight fit to the body, providing leak-proof and pressure-resistant properties. This increases the risk of water, air, or polluted air entering the helicopter during flight. Entry is prevented. Strong seals ensure the structural integrity of the helicopter. It provides protection; exit windows are normally fitted very tightly, while an emergency 2 In this situation, these seals need to be able to come loose quickly. This feature is important for passengers. It enables them to get out safely in a short time. Various proposals and applications for emergency exits through transparencies in the current state of the art. Although improvements have been made, these improvements are insufficient. Developed for this purpose... Some applications for inventions are given below. 5 United States registration number “US20070079854A1” in the known state of the art. The patent application originating from the state describes a lock mounted on a large umbrella. Its mechanism consists of a sliding sleeve with an opening on the surface of the lower extension, in a stem. a telescopic handle that includes a fixed lower tube and a sliding upper tube It is mentioned that the umbrella opens and locks with a sliding sleeve and locking device. 10 The umbrella also features a spring-loaded extension element that allows it to stretch. The user uses the handle to open and close the umbrella. The handle consists of the lower tube, the upper tube, and... Parts like the locking device ensure the umbrella functions properly and safely. It is helpful. The patent application originating from the United States is for an umbrella. While focusing on the opening, closing, and adjustment functions, the 15 that are the subject of the current application The invention is designed as an emergency exit system and provides emergency exits in aircraft. It includes a mechanism aimed at this. A patent originating from the United States. The locking mechanism in the application controls the slippage of the extension and sleeve. It includes spring elements and locking devices. This affects the length adjustment of the handle. It has a telescopic structure and 20 extension elements and rib fixing mechanisms. When closing the umbrella, the ends of the ribs are secured in place. (Existing) The locking mechanism in the invention that is the subject of the application concerns the movement between the shaft and the spindle. It uses a spring-loaded claw mechanism that controls the rotation of the shaft. a system that, triggered by movement, enables the transparent part to open and close It operates. Furthermore, this mechanism allows the transparency to pass through the outer and inner frames at 25°. It allows for an emergency exit. This is a patent application originating from the United States. telescopic handle, sliding tubes, spring extensions, rib fixing device and extensions It includes a structure based on the interaction between expansion and elastic elements. Using the elements, the umbrella is locked in the closed position. (Regarding the current application) The invention in question includes a spring-loaded coupling mechanism, a shaft, spring-loaded claws, a hole, and a handle. 30 It has a structure consisting of housings and splines. In this structure, spring-loaded claws drive the shaft's movement. while guiding, the transparency opens through the slots on the shaft. 3 It triggers a patent application originating in the United States, related to umbrellas. among the elements are the connections between telescopic tubes and extensions. Various mechanical fasteners are used, taking into account the existing The emergency exit system mentioned in the invention that is the subject of the application is transparent with a frame. It includes a mechanism that provides the structural connection between them. Pipeline flanged 5 Using connections and sealing elements, between the transparent and the structural part. It ensures a secure installation. The utility vehicle of Chinese origin, numbered “CN201696419U”, is in the known state of the art. in the model application, the positioning pin belonging to aircraft assembly tool technology A one-way nut with a steel ball bearing is described. The positioning pin is a 10 steel ball, a limiting block, a release rod, a knurled nut, a spring, a pin It consists of a housing and a pressing lever. This mechanism uses a steel ball, spring, and nut. elements such as these coming together to form a one-way locking system It provides. The spring is used to lock the steel ball and nut and trigger. Its mechanism initiates movement by working with a ball and spring system. This structure, 15 It allows for quick one-way assembly of the nut. Made in China. utility model application, positioning stud, steel ball, constrained block, knockout It includes components such as a pin, knurled nut, spring, shaft, and pressing lever. This structure, Steel balls and springs trigger the movement, ensuring the nut is tightened. The invention that is the subject of the present application concerns the use of helicopter windows or similar structural elements. It is an emergency exit mechanism used in the parts. It consists of an outer frame and an inner frame. A structure includes elements such as a spring-loaded claw, shaft, housing, and hole. The spring-loaded claw, It protrudes from the hole on the shaft, triggering the spring-loaded claw and providing movement for emergency exit. is doing. In the known state of the art, only pipeline flanges 25 are used when strong seals are employed. By using a connection, it is lighter and can be used in emergency exit situations without relying on human power. An emergency exit system is needed. In conclusion, due to the negative aspects described above and the current solutions, the subject matter... Due to its shortcomings, an improvement is needed in the relevant technical field. It has been made. 30 4 The purpose of the invention: The main purpose of the invention is to create pipeline flanged connections and sealing elements using transparent and framed to connect the structural part and provide human support in case of emergency exit. The aim is to provide an exit without needing to use a spring. To this end, the invention incorporates a spring mechanism. The connecting mechanism consists of a shaft, spindle, spring-loaded lugs, hole, handle, and sockets. It has a structure. In this structure, which has a spring connection mechanism, spring claws, While guiding the movement of the shaft, the slots on the shaft open the transparent opening. It triggers. Another purpose of the invention is to dislodge the claw from its socket by the movement of the shaft while the shaft is held stationary. Except for the possibility of the nail coming out of its socket by holding the shaft stationary and moving the shaft, 10 The goal is to develop a mechanism that provides this, both from the internal and external perspectives. It provides an emergency exit from the frame. Another purpose of the invention is to utilize emergency exit systems located in helicopter transparencies. an emergency exit that does not rely on human power thanks to an emergency release mechanism to provide. 15 Explanation of the figures: FIGURE-1; This is a drawing showing the emergency exit system that is the subject of the invention. FIGURE-2; Spring connection mechanism of the emergency exit system, which is the subject of the invention, to the structure. It is a drawing that provides an isometric view of the connection. FIGURE-3; Spring connection mechanism of the emergency exit system, which is the subject of the invention. It is a drawing that gives the image. Reference numbers: 1: Emergency exit system 2: Frame 3: Mile 25 4: Hole 5: Spring-loaded nails 6: Shaft 7: Nest 8: Handle 9: Spring coupling mechanism 5 Description of the invention: The invention is an emergency exit system (1) used in helicopter transparencies. It provides emergency exit without relying on human effort, thanks to its exit mechanism. The invention provides an emergency exit from transparencies, with 10 openings in the outer and inner frames. the frame (2) formed, shaft (6) containing housing (7), spring claw (5) and hole (4) containing spindle (3) and It includes at least one spring-loaded connection mechanism (9) which includes a handle (8). The invention relates to pipeline flanged connections and seals that provide leak-proof sealing. By using the gasket, which is the element, both the transparency and the frame (2) are connected to the structural part. It connects and also provides emergency exit without relying on human power in case of emergency. 15 It provides. The spring coupling mechanism (9) of the invention is in which the shaft (3) is held while the shaft (6) is fixed. Its movement causes the spring-loaded claw (5) to come out of the socket (7). Also, the spring-loaded The connecting mechanism (9) is activated by holding the shaft (3) fixed and moving the shaft (6) and the spring-loaded claw (5) This allows it to come out of the nest (7). Thus, it can come out of both the inner frame and the outer frame. Emergency exit is possible from the frame (2). Frame (2) consists of an outer frame and an inner frame and is located on an aircraft a transparent (glass) that is mounted on a structural part, holding the structural part in place. It is a structure. The spring coupling mechanism (9) consists of a shaft (3) and a spindle (6), shaft (3) The spring-loaded claw (5) which will act as a claw connection, is located inside the shaft (3) 25 (5) a hole (4) into which the spring is placed, connected to the shaft (3) inside the hole (4). and there is a slot (7) on the shaft (6) into which the spring-loaded claw (5) fits in a form-fitting manner. The spring-loaded claw (5) is triggered by hitting the wall of the socket (7) and enters the socket (7) or 6 It comes out. The spring claw (5) is two opposite each other on the shaft (3) and the shaft (3) When triggered to move, another trigger from the slot (7) on the shaft (6) It can be removed without needing a mechanism. The spring-loaded claw (5) moves the shaft (3). When triggered to activate, it goes from the socket (6) on the shaft to another trigger mechanism (7). It can exit without needing to. Here, the trigger is in the direction in which the shaft (6) extends. This is achieved by the rotational movement of the shaft (3) around it. The handle (8) is on the shaft (6) and The shaft (6) is triggered by holding the shaft (3) by the user. It is a structure. When mounting the transparent and frames (2) to the structural part, the frame (2) structural The frame (2) and structural part 10 are connected by passing the shaft (6) through the hole to which they are attached. It is connected. Then the shaft (3) is slid through the shaft (6) channel, and the shaft (3) is connected to the shaft. (6) until it is brought to the position where it will sit in the slots (7) on the shaft (6) when rotated. It is pushed. The shaft (3) is rotated at an angle determined by the user, i.e. the shaft (6) is placed in the socket (7) on which the spring tabs (5) fit directly. and thus the spring connection mechanism (9) 15 mounted on glass and frames The movement is locked. While the shaft (6) is brought to the locking position, the handle (8) The tip of the spring-loaded claw (5) is turned in the direction of the shaft (6) through which the shaft is turned into the wall of the socket (7). It moves by striking the shaft (3) into the hole (4) inside, which triggers the spring. and compresses. After this compression, the spring claw (5) contacts the wall of the socket (7). as it is being cut, the spring claw (5) releases the spring as it enters the housing (7) and the spring 20 It releases the energy it has stored. With this released energy, the spring pulls the spring claw (5) It pushes into the housing (7). The spring-loaded claw (5) moves in one direction only when the shaft (6) rotates. By making the movement, the shaft (3) enters and exits the housing (7) and is locked in the same direction. By turning it, the spring claw (5) comes out of the housing (7).

Claims

7 REQUESTS 1. Emergency exit system (1) is a structural system located on an aircraft. a transparent part mounted on the component holds the structural part and the outer frame and a frame consisting of an inner frame (2); shaft (3) and shaft (6) outwards 5 that extends straight and is triggered by hitting the wall of the nest (7) and enters and exits the nest (7). spring claw (5), a hole (4) on which the spring claw (5) is placed and this hole (4) shaft containing a spring (3) and spring-loaded claw (5) form-fitting at least one spring coupling containing the shaft (6) which has the socket (7) into which it enters its mechanism is (9).

2. Emergency exit system (1) in accordance with claim 1, its feature is that it extends 10 due to its form. when triggered to move the shaft (3) by rotation around the direction without needing another trigger mechanism from the slot (7) in the shaft (6) It contains removable spring-loaded claws (5).

3. Emergency exit system (1) in accordance with claim 1, and its feature is that it is activated by the user. The moving glass and frames (2) are connected to the structural part through the hole 15 passing through the shaft (6), and sliding the shaft (3) through the shaft (6) channel, the shaft (3) shaft (6) until it is brought to the position where it will sit in the slots (7) on the shaft (6) when rotated Pushed in until the spring claws (5) fit directly into the slot (7) on the shaft (6) and a spring-loaded linkage mechanism that is brought in and mounted in such a way that its movement is locked. (9) includes. 20 4. Emergency exit system (1) in accordance with claim 1, the feature of which is; user locking When bringing it to position, the spring-loaded tab (5) is turned in the direction indicated by the handle (8). the end part hitting the wall of the housing (7) and being positioned inside the shaft (3) By entering the shaft (3) into the hole (4), it triggers the spring and compresses the spring claw. When the contact between (5) and the wall of the socket (7) is broken and the spring claw (5) enters the socket (7), the spring 25 The spring releases its stored energy by ceasing compression, thus becoming a spring-loaded spring. push the claw (5) into the socket (7) and the spring claw (5) in one direction into the socket (7) It contains a shaft (6) that enables it to go in and out by rotating.

5. Emergency exit system (1) in accordance with Claim 1 or Claim 2, the feature of which is that when locked The shaft (3) coming out of the slots (7) on the shaft (6) by rotating it in the direction 30 It contains a spring-loaded tab (5) on it. 8 6. Emergency exit system (1) in accordance with claim 1, and its feature is; located in the shaft (6) and the shaft (3). The area is in a form that can be held by the user, holding the shaft (6) It contains a handle (8) that triggers it.

7. Emergency exit system (1) in accordance with claim 1, its feature is; fixing of the shaft (3) and With the shaft (6) being moved by the user, both from the inner frame and 5 a spring-loaded coupling that allows for emergency exit from the outer frame its mechanism is (9).

8. Claim 1' is a suitable emergency exit system (1), the feature of which is; on the shaft (3) opposite. It contains two spring-loaded claws (5) which remain in place.

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