Masking arrangement for a gas turbine engine
AssigneeVolvo Aero Corporation
InventorsLinda Ström, Hans Martensson, Jonas Larsson, Lena Andersson
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Abstract
A masking arrangement for a gas turbine engine includes a plurality of annular elements arranged overlapping one another when these are viewed in an axial direction so as to mask at least a substantial portion of any interior hot and rotating gas turbine engine part at an aft end of the gas turbine engine from rear view when the masking arrangement is applied downstream the interior part in the gas turbine engine.
Claims19
A masking arrangement for a gas turbine engine, wherein the masking arrangement is configured to be attached between an outer wall and an inner wall defining an exhaust gas flow in the gas turbine engine, and the masking arrangement comprises at least one annular element, which is adapted to mask at least a substantial portion of an interior gas turbine engine part at an aft end of the gas turbine engine from rear view when the masking arrangement is applied downstream the interior part in the gas turbine engine.
Dependencies are inferred from the claim text.