Interactive diagnostic display system and method for an aircraft
First Claim
1. A diagnostic display system for diagnosing avionics components of an aircraft using an interactive display accessible to a user in real time, the system comprising:
- a central diagnostic module configured for receiving at least one signal from a plurality of sensors for the aircraft, and at least one parameter from a related avionics system associated with the aircraft; and
a component information module configured for providing operational status information about at least one of the avionics components of the aircraft, and providing a detailed operational status configuration of each avionics component using a plurality of status messages stored in a database via a network;
wherein the central diagnostic module assesses a current operational status of the aircraft by evaluating the operational status configuration illustrated in the display for establishing a visual link between the plurality of status messages associated with the avionics components of the aircraft.
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Abstract
A diagnostic display system is provided for diagnosing avionics components of an aircraft using an interactive display accessible to a user in real time. A central diagnostic module receives at least one signal from a plurality of sensors for the aircraft, and at least one parameter from a related avionics system associated with the aircraft. A component information module provides operational status information about at least one of the avionics components of the aircraft, and provides a detailed operational status configuration of each avionics component using a plurality of status messages stored in a database via a network. The central diagnostic module assesses a current operational status of the aircraft by evaluating the operational status configuration illustrated in the display for establishing a visual link between the status messages associated with the avionics components of the aircraft.
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Citations
20 Claims
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1. A diagnostic display system for diagnosing avionics components of an aircraft using an interactive display accessible to a user in real time, the system comprising:
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a central diagnostic module configured for receiving at least one signal from a plurality of sensors for the aircraft, and at least one parameter from a related avionics system associated with the aircraft; and a component information module configured for providing operational status information about at least one of the avionics components of the aircraft, and providing a detailed operational status configuration of each avionics component using a plurality of status messages stored in a database via a network; wherein the central diagnostic module assesses a current operational status of the aircraft by evaluating the operational status configuration illustrated in the display for establishing a visual link between the plurality of status messages associated with the avionics components of the aircraft. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15)
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16. A computer-implemented method for diagnosing avionics components of an aircraft using an interactive display accessible to a user in real time, the method comprising:
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receiving at least one signal from a plurality of sensors for the aircraft, and at least one parameter from a related avionics system associated with the aircraft; providing operational status information about at least one of the avionics components of the aircraft; providing a detailed operational status configuration of each avionics component using a plurality of status messages stored in a database via a network; assessing a current operational status of the aircraft by evaluating the operational status configuration illustrated in the display; and establishing a visual link between the plurality of status messages associated with the avionics components of the aircraft. - View Dependent Claims (17, 18, 19, 20)
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Specification