INTEGRATING AN EXTINGUISHER INTO A "FIRE" ZONE OF A TURBOMACHINE
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United States of America
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Issued Date -
Feb 13, 2025
app pub date -
Dec 21, 2022
filing date -
Dec 21, 2022
priority date (Note) -
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status (Latency Note)
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Abstract
An assembly for an aircraft gas turbine engine includes a nacelle extending substantially around a longitudinal axis and including a fixed structure disposed around the aircraft gas turbine engine, the fixed structure including an internal surface suitable for delimiting with an external surface of the gas turbine engine a fire zone of the nacelle, a thermal protection covering the internal surface of the fixed structure of the nacelle at the level of the fire zone of the nacelle, and an extinguisher designed to extinguish a fire in the fire zone of the nacelle, the extinguisher including a tank suitable for containing an extinguishing agent. The tank is located between the thermal protection and the internal surface of the fixed structure of the nacelle.
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