A WARNING PANEL

Abstract

A warning panel (1) is characterized by a fuselage containing an FPGA block (21) located inside the fuselage, a system control block (2) containing a screen (22) connected to the FPGA block (21), a data interface block (3) providing data input and output to the FPGA block, a bezel block (4) with buttons connected to the FPGA block (21) providing the power needed by the system control block (2), and a fan (6) providing cooling for the system control block (2), data interface block (3) and power block (4), enabling the display of multiple warnings for aircraft.

Description

1 TARIFF A WARNING PANEL Technical Area This invention transmits warning signals on avionics platforms via an interface. providing information and warnings in a way that the user can understand. It relates to a warning panel that provides information. Previous Technique Screen-based warning panels provide important information to pilots and crew on aircraft. These are electronic devices that visually convey information and warnings. These panels are used during flights. This is critically important in terms of safety and operational efficiency. Generally It is manufactured using LCD, LED, or OLED technologies and is used inside the aircraft. It works integrated with various systems. The first electronic warning in the known state of the art. The panels consist of simple lamps and mechanical indicators. The 15 in question... Screen systems provided limited information and were generally controlled manually. This was the case. With the advancement of technology, more complex and digital screens emerged. The emergence of high-resolution and multi-processor displays in modern aircraft. to be used, pilots should not be given more information and operations should be made more efficient It ensures that it is made safe. 20 Warning panels inside aircraft in the known state of the art, It performs various critical functions, e.g., speed, altitude, direction, and other flight parameters. Flight instruments that display parameters such as engine status and fuel level. System status information screens providing information; in case of emergencies or 25 Warning and alarm screens are included to alert pilots to abnormal conditions. Air Warnings on the vehicles are given to the panel as separate inputs for the equipment. This can be demonstrated. Redundancy in warning panels used on aircraft. The situation is not currently the same. There is no fault with any of the LEDs on the panel. Otherwise, the warnings cannot be displayed. Additionally, the warning panel includes LEDs. 30 The number of warnings that can be displayed is limited. 2 Brief Description of the Invention The aim of this invention is to display multiple warnings for aircraft and The goal is to create an alert panel that provides backup in case of failure. The first step taken to achieve the purpose of this invention, and the steps associated with that step... displaying multiple warnings for aircraft defined in the requests a warning panel that provides access; a body and a device located inside the body. A system control block containing an FPGA block and a display connected to the FPGA block, A data interface block (3) that provides data input and data output to the FPGA block, FPGA 10 a bezel block with keys attached to the block, system control block a power block that provides the necessary power, system control block, data interface It includes a fan that provides cooling for the block and power block, and a warning. The panel's structure allows multiple warnings to be displayed. is provided. 15 Detailed Description of the Invention This invention includes a warning panel, which was created to achieve its purpose. as shown, in this form; Figure 1 - Schematic top view of the warning panel that is the subject of the invention. The parts in the figures are individually numbered, and each number corresponds to the following: It is given below. 1. Warning panel 25 2. System control block Block 21 FPGA Screen 22 3. Data interface block 4. Bezel block 30 5. Power block 3 6. Fan A system that allows the display of multiple warnings for aircraft. warning panel (1); a housing and an FPGA block located inside the housing (21) and a system control block containing a display (22) connected to the FPGA block (21). (2), 5 on the body that provides data input and data output to the FPGA block. a positioned data interface block (3) is connected to the FPGA block (21) a bezel block (4) located on the body with buttons, system control a block (2) that provides the power needed by the fuse, positioned on the fuselage power block (5), located on the housing and system control block (2), data A fan (6) that provides cooling for the interface block (3) and the power block (5) 10 It includes. The warning panel (1) includes a housing, preferably with a square structure, and At least one opening has been made on one surface of the body. The screen (22) is inserted into the opening. It is located. Thanks to the screen (22), users can access the data interface block (3) 15 It can see the warnings transmitted to the FPGA block (21) via the square structure. a bezel block (4) is positioned. The bezel is positioned on the body. The data displayed on the screen (22) with block (4) is controlled by the user. It has been adapted for implementation. Data interface block (3) on the fuselage. It is located on the data interface block (3), preferably RS-422. 20 In a preferred application of the invention, multiple openings on the body It has been opened, and the data interface block containing the connection interfaces to these openings. (3), bezel block (4) is positioned. The said opening on the fuselage The screen (22), interface data block (3) and 25 are positioned to close the openings. bezel block (4), contact surfaces to prevent liquid from entering the body. A leak-proof gasket is positioned between them. In one application of the invention, the display is (22) Active Matrix Liquid Crystal (AMLCD). It was manufactured using. In one of its preferred applications, the screen (22) is 5” x 5” 30 It has an active display area and is capable of displaying 588 alerts. 4 It has an image resolution of x 600. In a preferred application of the invention, Warning panel (1); key press information and detailed maintenance on the bezel block (4) It provides its information via the data interface block (3) which includes RS-422. RS-422 data interface block (3) containing the flexible communication interface of the warning panel (1) It creates. The warning panel (1) provides access to extended test and maintenance interfaces and the user 5 It may include different configurations to support specific configurations. The subject of the invention is the warning panel (1) from the RS422 systems on the avionics platform. interpreting the warning information received through the interface and displaying its own image Task computer 10 with rendering capability and discrete input / output processing capabilities This enables its use in applications.

Claims

REQUESTS 1. Allows the display of multiple warnings for aircraft. providing; - containing a body, - an FPGA block located inside the housing (21), 5 FPGA blocks (21) a system control block (22) which includes a connected screen, - The connector on the housing provides data input and output to the FPGA block. a positioned data interface block (3), - A switchboard with buttons on it, connected to the FPGA block (21), mounted on the body. a positioned bezel block (4), 10 - housing which provides the power required by the system control block (2) a power block positioned on it (5), - system control block (2), data interface block (3) and power block (5) with a fan (6) located inside the body which provides cooling a warning panel characterized by (1). 15 2. Characterized by at least one opening on one surface of the fuselage. A warning panel like the one in request 1 (1).

3. Characterized by a screen (22) positioned in the aforementioned opening. A warning panel like the one in request 2 (1).

4. A data interface block containing openly positioned connection interfaces (3) and a warning panel as in claim 2 characterized by a bezel block (4). (1). 25 5. To close the aforementioned openings on the fuselage positioned screen (22), interface data block (3) and bezel block (4), body between the contact surfaces to prevent liquid from entering The above 30 are characterized by a positioned leak-proof seal. a warning panel (1) like any of the requests. 6 6. Request 1, characterized by a data interface block (3) containing RS-422 such a warning panel (1).

7. Characterized by a data interface block (3) containing RS-422 and RS-232 5 A warning panel like the one in request 1 (1). It has an 8.5” x 5” active display area, the ability to display 588 alerts, and a 600 x The request is characterized by a screen with a resolution of 600 (22). A warning panel like the one in 1 (1). 10

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