Containment system for a gas turbine engine

Aeronautics and astronautics – Aircraft power plants – Mounting

Reexamination Certificate

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Details

C415S009000, C415S213100, C060S039091, C060S226100

Reexamination Certificate

active

07806364

ABSTRACT:
A containment system for a gas turbine engine comprises a force absorbing arrangement for absorbing the force exerted thereon by an ejected portion of a failed component of the engine. The force absorbing arrangement circumferentially surrounds a major proportion of the axial length of the engine.

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patent: 2 365 925 (2002-02-01), None

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