SEAL ASSEMBLY FOR A GAS TURBINE ENGINE

An assembly (60) for a gas turbine engine (20) comprising a component (66) that has a first interface portion (74), and a support (68) that has a mounting portion (76) and a second interface portion (78), the mounting portion (76) attachable to an engine static structure (36), a first retention feat...

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Bibliographic Details
Main Authors LUTJEN, Paul M, THILL, Carson A. Roy
Format Patent
LanguageEnglish
French
German
Published 02.06.2021
Subjects
BLASTING
ENGINE PLANTS IN GENERAL
HEATING
LIGHTING
MACHINES OR ENGINES IN GENERAL
MECHANICAL ENGINEERING
NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES
STEAM ENGINES
WEAPONS
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Summary:An assembly (60) for a gas turbine engine (20) comprising a component (66) that has a first interface portion (74), and a support (68) that has a mounting portion (76) and a second interface portion (78), the mounting portion (76) attachable to an engine static structure (36), a first retention feature (80) that releasably secures the first interface portion (74) to the support (68) in a first installed position of the gas turbine engine component (66), and a second retention feature (82) dimensioned to secure the first interface portion (74) to the second interface portion (78) in a second installed position of the gas turbine engine component (66). The first installed position differs from the second installed position, and one of first and second retention features is dimensioned to carry the gas turbine engine component (66) in response to release of another one of the first and second retention features.
Bibliography:Application Number: EP20200208790