GAS TURBINE ENGINE COMPRISING AN ANNULAR RETENTION STRAP AND CORRESPONDING METHOD OF ASSEMBLING
A gas turbine engine (20) includes an annular structure (210) disposed around an engine central longitudinal axis (A-A') of the gas turbine engine (20). The annular structure (210) defines an annular channel (212) and comprises a first density. The gas turbine engine (20) further includes a wei...
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Main Authors | , |
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Format | Patent |
Language | English French German |
Published |
07.04.2021
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Subjects | |
Online Access | Get full text |
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Summary: | A gas turbine engine (20) includes an annular structure (210) disposed around an engine central longitudinal axis (A-A') of the gas turbine engine (20). The annular structure (210) defines an annular channel (212) and comprises a first density. The gas turbine engine (20) further includes a weight-saving filler (220) disposed within the annular channel (212). The weight-saving filler (220) has a second density that is less than the first density. The gas turbine engine (20) further includes an annular retention strap (230) disposed around the engine central longitudinal axis (A-A') of the gas turbine engine (20). The annular retention strap (230) is at least partially embedded in the weight-saving filler (220). |
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Bibliography: | Application Number: EP20180206118 |