A functional carrier.

Abstract

This invention relates to a fuselage (2) which is an aircraft, at least one display (D) located on the fuselage (2) which performs functions predetermined by the user and enables the user to display data, at least one instrument panel (3) on which the display (D) is located, and at least one detachable stabilizer (4) located between the instrument panel (3) and the fuselage (2) which carries the instrument panel (3).

Description

5778 / TR 1 TARIFF A FUNCTIONAL CARRIER This invention enables instrument panels in aircraft to have the desired durability and It is related to a functional carrier that ensures it is kept in its damping capacity. 5 In aircraft such as helicopters, airplanes, and unmanned aerial vehicles, the cockpit contains the pilot's control of the flight. It includes indicators that enable monitoring of related parameters. These indicators... When instrument panels, which are part of the structure, are manufactured with ergonomics and pilot usability in mind within the cockpit. Care is taken to ensure suitability. The instrument panels carry a lot of equipment. 10 Situations such as the accumulation of weight at a particular point can occur. The pilot's view... The instrument is designed to be unobstructed and to avoid colliding with surrounding structures during movement. the panel must remain within a certain displacement value and be as rigid as possible This is necessary. Since instrument panel structures do not behave as a completely rigid piece, some The vibration dampers can be subjected to higher loads, and therefore the damping efficiency is 15. It is falling. Instrument panel structures are not manufactured in a modular way, therefore the problem is due to assembly. When a problem occurs, the parts need to be reproduced. United States number US2022017233, included in the known state of the art. The patent document describes a lightweight, robust, and easy-to-manufacture instrument panel, 20 a system that allows the integration of any type of display screen It is explained that in the system described in the invention, the number of connecting elements is kept limited, portability of navigation control and / or monitor equipment components It features a single-piece instrument panel structured to provide this functionality. United States number US8256830B2, which is included in the known state of the art. at least two axial profiles with different cross-sectional configurations as stated in the originating patent document. A cross-sectional element with a profile cross-section is described as a front panel support for a motor vehicle. Thanks to a functional carrier developed with this invention, the load carried on the instrument panels is reduced by 30%. This ensures that the resulting distortion of the center of gravity is minimized. Another purpose of the invention is to address problems that arise during the assembly of instrument panels. with the use of modular parts, without the need to reproduce the parts. The goal is to ensure ease of assembly. 35 5778 / TR 2 Another purpose of the invention is to create panels of different sizes and weights on the instrument panel. Once the equipment is installed, there is no need to repeat the design and production processes, The key is the use of modular structures that can be used in different locations. Another aim of the invention is to create a multi-part and modular design for vibration dampers. Thanks to its connectable panel structure, it ensures an even distribution of displacement values. to provide. Another purpose of the invention is to transfer the load on the instrument panel carrying the equipment to panel 10 By distributing the load evenly across carriers and dampers, the user benefits both statically and dynamically. The goal is to use structures with sufficient rigidity and damping capability to meet the requirements. The initial demands and the demands dependent on this demand, which are implemented to achieve the purpose of the invention. The defined functional carrier includes a fuselage that can be an aircraft. The fuselage has 15 The cockpit contains displays that allow the pilot to view flight-related data. The indicators are mounted on an instrument panel. The connection between the instrument panel and the body is... This is achieved thanks to a removable fastener. The invention is a functional carrier, a 20-inch indentation located on the fastener. It includes sockets. Two stabilizers, defined by the user, that remain opposite each other. The device is attached to the slots between them so that it extends laterally. The device is attached to the instrument panel. the weight resulting from the installation of the indicator is evenly distributed among the stabilizers. It enables the distribution of the device between the user-defined fasteners and By being inserted into user-defined slots, the center of gravity is 25° This allows for balancing. In one application of the invention, the functional carrier is mounted on the instrument panel of the indicator. Depending on its mounting location, it is mounted in a position that is mirror-symmetrical to the indicator, thus aligning the indicator with the display. By attaching it to the panel, it creates a change in the center of gravity, at least partially 30 It includes a device that reduces [the effect of the shockwave]. In one application of the invention, the functional carrier has one end attached to the body and the other end to the indicator. It includes a carrier that attaches to the panel. The carrier has panels arranged in a row on it. It contains sockets. The apparatus 35 fits into the sockets on the opposing carriers. It is attached. 5778 / TR 3 In one application of the invention, the functional carrier is located on the instrument panel and It includes a slot that allows it to be placed inside the carrier. In one application of the invention, the functional carrier has user-defined slots. The instrument panel displacement value, which is installed between them, is set by the user in advance to 5. It includes a device that allows it to be kept below the threshold value. Thanks to the device, the load is distributed almost equally between the carriers. is provided. In one application of the invention, the functional carrier is positioned between the fuselage and the carrier, during the fuselage's flight 10 This allows the force acting on the carrier, resulting from its movement, to be dampened. It contains a damper. In one application of the invention, the functional carrier is mounted on the panel, allowing the user to use the carrier. It includes a rail that allows the device to be moved to the position determined by sliding motion. 15 In one application of the invention, the functional carrier is mounted on a rail by the user. It includes a stopper that allows it to be held in a predetermined position. In one application of the invention, the functional carrier is connected to the body and the instrument panel or to the body and 20 It contains a connector that provides the carrier's linkage. In one application of the invention, the functional carrier is the altimeter used by the pilot inside the cockpit. It includes gauges that can be a speedometer, variometer, and similar devices. The functional carrier attachment forms were created to achieve the purpose of this invention. as shown, from these figures; Figure 1 – Perspective view of the functional carrier. Figure 2 – Rear view of the functional carrier. 30 Figure 3 – Perspective view of the functional carrier with the indicator attached. Figure 4 – Perspective view of the functional carrier. Figure 5 – Perspective view of the functional carrier. Figure 6 – Perspective view of the functional carrier. Figure 7 – Perspective view of the functional carrier. 35 5778 / TR 4 The parts in the figures are individually numbered, and their corresponding numbers are shown below. It has been given. 1. Cutting mechanism 2. Body 3. Instrument panel 5 4. Stabilizer 5. Nest 6. Apparatus 7. Damper 8. Ray 10 9. Stopper 10. Connector (D) Indicator The functional carrier (1) is a fuselage (2) which is an aircraft, located on the fuselage (2) and performs functions predefined by the user and uses the user's data. at least one indicator (D) that enables its display, at least one on which the indicator (D) is located a dashboard (3) that can be removed and installed between the dashboard (3) and the body (2) It includes at least one stabilizer (4) which is located and supports the instrument panel (3). 20 The subject of the invention is a functional carrier (1) which is located on the stabilizer (4) and has an indentation form. multiple slots (5) located opposite each other, pre-selected by the user removable along the length of the slots (5) between the specified fasteners (4). installed and thus the weight created by the indicators (D) on the instrument panel (3) is 25 distributed almost evenly on the stabilizers (4) and the instrument panel (3) Allows the center of gravity to be maintained within a user-defined range. It includes at least one apparatus (6) that provides. The fuselage (2) located on the aircraft, the fuselage (2) located on the pilot, 30 performing predefined functions and allowing the pilot to view the data. There is at least one indicator (D). At least one instrument panel (3) carrying the indicator (D) It is located between the instrument panel (3) and the body (2). A removable and attachable stabilizer (4) is located between the instrument panel (3) and the body (2). It holds. The stabilizer (4) carries the instrument panel (3). 35 5778 / TR The stabilizer (4) has several slots (5) which have an indentation form. Two user-defined objects positioned opposite each other. between the (4) of the stabilizer, along the length of the two slots (5) determined by the user. There are removable mounting brackets (6). Thanks to bracket (6) the instrument panel (3) The weight resulting from the indicator (G) mounted on it is equal between the stabilizers (4) 5 It is possible to distribute the weight of the instrument panel (3) in this way. Thanks to the device, the weight of the instrument panel (3) The central location can be kept within the range defined by the user. This allows... Installed diagonally or mirror-symmetrically depending on where the indicator (D) is installed Weight balance is ensured. In one application of the invention, the functional carrier (1) is the indicator panel (3) of the indicator (D) positioned almost mirror-symmetrically to the location on which it is placed. the change that the indicator (D) causes in the center of gravity of the instrument panel (3) apparatus that balances the center of gravity by allowing at least a partial reduction (6) It includes. The position where the apparatus (6) is mounted on the instrument panel (3) is approximately 15 By attaching it to a mirror-symmetrical surface, the center of gravity is balanced. In one application of the invention, the functional carrier (1) is connected from one end to the body (2) to another. The carrier (4) attached to the instrument panel (3) from its end, is placed sequentially on the carrier (4). at least two 20s located opposite each other at at least two ends of the area and apparatus (6). It has an indentation form that allows it to be placed lengthwise between the carriers (4). It contains the housing (5). At least two of the apparatus (6) are placed consecutively on the carrier (4). between at least two carriers (4) that are positioned opposite each other at the end. There are recessed slots (5) that help in placing it along the way. (5) allows the user to attach the device (6) to the desired position and increase the rigidity of the instrument panel (3) by 25 It is ensured that it is increased. In one application of the invention, the functional carrier (1) is located on the instrument panel (3), The housing (5) into which the carrier (4) is inserted at least at one end is located. Indicator Thanks to the slot (5) on the panel (3), the carrier (4) can be moved to the user-determined position 30 It is ensured that it is installed. In one application of the invention, the functional carrier (1) has two slots determined by the user. (5) is installed between the (3) displacement value of the instrument panel by the user. enabling the load to be kept below a specified threshold value and the carriers (4) 35 the apparatus (6) that allows the distribution of the facilities almost equally among them 5778 / TR 6 It includes. The displacement value is below a certain threshold value thanks to the apparatus (6). Thanks to its holding, unwanted movement of the instrument panel (3) is reduced. In one application of the invention, the functional carrier (1) is located between the body (2) and the carrier (4). The force acting on the carrier (4) resulting from the movement of the area and the body (2) is at least 5 It contains at least one damper (7) that dampens at least partially. Damper (7) resulting from the movement of the fuselage (2) during flight which can be an aircraft thanks to the load directly affects the instrument panel (3) and thus the indicators (D) vibrate Exposure to its movement is reduced. In one application of the invention, the functional carrier (1) is located on the instrument panel (3) and The carrier (4) can be brought to the position determined by the user by sliding it. It includes at least one rail (8) that provides access. Thanks to the rail (8), the carrier (4) can be used by the user. It can be positioned precisely on the instrument panel (3) by sliding it. In one application of the invention, the functional carrier (1) is located on the rail (8) and the carrier (4) at least the minimum that allows it to be fixed in the position determined by the user. It includes a stopper (9). Thanks to the stopper (9), the carrier (4) can pass over the rail (8). Its exit is prevented. In one application of the invention, the functional carrier (1), the body (2) and the instrument panel (3) and / or It contains at least one connector (10) that provides the link between the carrier (4). Connector (10) The structures are fixed to each other. In one application of the invention, the functional carrier (1) can be used to mount an altimeter, speedometer, variometer, etc. 25 It includes indicator (D) that can be used to monitor flight data. It can display it.

Claims

5778 / TR 7 REQUESTS 1. A fuselage (2) which is an aircraft, located on the fuselage (2) and by the user It performs predefined functions and allows the user to view data. 5 at least one indicator (D) that provides, at least one on which indicator (D) is located The instrument panel (3) can be removed and installed between the instrument panel (3) and the body (2). including at least one stabilizer (4) which is shown in the figure and supports the instrument panel (3). Multiple slots (5) located on the stabilizer (4) and having an indentation form, 10 user-defined groups positioned opposite each other removable and fitted along the length of the slots (5) between the (4) stabilizers and thus the weight that the indicators (D) create on the instrument panel (3), distributed almost evenly on the stabilizers (4) and the indicator the center of gravity of the panel (3) within a user-defined range of position a 15 characterized by having at least one apparatus (6) that allows it to be held functional carrier (1).

2. The position where the indicator (D) is placed on the instrument panel (3) is approximately positioned mirror-symmetrically and the weight of the indicator (D) instrument panel (3) This allows for at least partial reduction of the change it has caused in the center. The system is characterized by the apparatus (6) that balances the center of gravity by providing A functional carrier like in 1 (1).

3. The carrier (4) is attached to the body (2) at one end and to the instrument panel (3) at the other end, The carrier (4) is placed consecutively on the apparatus (6) and at least two ends of the apparatus (6) are connected to each other by 25 between at least two carriers (4) that are positioned opposite each other, lengthwise. characterized by a socket (5) which has an indentation form that allows it to be placed. a functional carrier (1) such as in request 1 or request 2.

4. Located on the instrument panel (3), 30 into at least one end of the carrier (4). any of the above claims characterized by the socket (5) in which it is placed such a functional carrier (1).

5. The instrument panel (3) is positioned by being installed between two slots (5) determined by the user. change the value below a user-defined threshold of 35 which allows the load to be held and almost equally distributed among the carriers (4) 5778 / TR 8 characterized by the apparatus (6) which enables its distribution in this way a functional carrier (1) like any of the above requests.

6. Located between the fuselage (2) and the carrier (4) and the movement of the fuselage (2) 5 which dampens at least partially the force acting on the carrier (4) by originating from it. any of the above requirements characterized by at least one damper (7) a functional carrier like one (1).

7. The instrument panel (3) located on the carrier (4) and determined by the user. 10 characterized by at least one rail (8) that allows it to be brought to position by sliding. a functional carrier (1) like any of the above requests.

8. Located on the rail (8) and the carrier (4) predetermined by the user characterized by having at least one stopper (9) that allows it to be held in a fixed position. The requested function is a functional carrier (1) as in 7. 15 9. Providing the connection between the body (2) and the instrument panel (3) and / or carrier (4). Any of the above claims characterized by at least one binding (10) a functional carrier like one (1).

10. Characterized by an indicator (D) which can be an altimeter, speedometer, variometer, etc. a functional carrier (1) like any of the above requests.

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