Exhaust gas temperature indicator for a gas turbine engine
AssigneeB&D Instruments and Avionics, Inc.
InventorsSaied Barakchi, Jerry C. Black, II
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AssigneeB&D Instruments and Avionics, Inc.
InventorsSaied Barakchi, Jerry C. Black, II
Estimating the term…
An exhaust gas temperature indicator for a gas turbine engine is disclosed in which data representing discrete overtemperature events occurring at different times is stored in a nonvolatile memory for later retrieval and display on an event-by-event basis. A character display is used to provide detailed digital, alphanumeric or other character information relating to each overtemperature event, such as the number, temperature zone, peak temperature and duration of the event. An indicator is provided for indicating the presence of unacknowledged temperature data in the memory device, and a maximum exhaust gas temperature value for an aircraft flight is stored. An analog display for continuously displaying current exhaust gas temperature values is provided in conjunction with a character display for displaying either current or stored values. Separate caution and warning indicators are utilized for alerting the flight crew to developing overtemperature conditions without the need to rely solely on an analog or digital display.
An exhaust gas temperature indicator for detecting, storing and displaying overtemperature events occurring during operation of a gas turbine engine, comprising:
An exhaust gas temperature indicator for detecting, storing and displaying an overtemperature event occurring during operation of a gas turbine engine, comprising:
An exhaust gas temperature indicator for monitoring the peak temperature value occurring during operation of a gas turbine engine, comprising:
An exhaust gas temperature indicator for displaying exhaust gas temperatures occurring during operation of a gas turbine engine, comprising:
An exhaust gas temperature indicator for providing indications of overtemperature conditions occurring during operation of a gas turbine engine, comprising:
A method for detecting, storing and displaying exhaust gas overtemperature events occurring during operation of a gas turbine engine, comprising the steps of:
A method for detecting, storing and displaying exhaust gas overtemperature events occurring during operation of a gas turbine engine, comprising the steps of:
A method for detecting, storing and displaying exhaust gas overtemperature events occurring during the operation of a gas turbine engine, comprising the steps of:
A method for detecting, storing and displaying exhaust gas overtemperature events occurring during operation of a gas turbine engine, comprising the steps of:
A method for detecting, storing and displaying exhaust gas overtemperature events occurring during operation of a gas turbine engine, comprising the steps of:
A method for generating, storing and displaying exhaust gas temperature data during operation of a gas turbine engine, comprising the steps of:
A method for monitoring the peak exhaust gas temperature value occurring during operation of a gas turbine engine, comprising the steps of:
A method for generating, storing and displaying exhaust gas temperature data during operation of a gas turbine engine, comprising the steps of:
A method for providing indications of exhaust gas overtemperature conditions occurring during operation of a gas turbine engine, comprising the steps of:
Dependencies are inferred from the claim text.