A containment assembly is provided for an aircraft engine having a rotor with a set of blades. The containment assembly comprises a containment casing annularly surrounding the rotor radially outward of the set of blades. The containment casing is made of a material having a density less than that of steel. A layer of thermal insulation is disposed radially inward of the containment casing. The layer of thermal insulation is radially disposed between the containment casing and the set of blades.
CONTAINMENT ASSEMBLY FOR AN AIRCRAFT ENGINE
2023-12-14
Patent
Electronic Resource
English
REPORT ON AIRCRAFT ENGINE CONTAINMENT
SAE Technical Papers | 1977
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British Library Conference Proceedings | 1995
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