Protection element for a compressor drum and method for repairing a compressor drum
AssigneeSafran Aircraft Engines
InventorsJean-Hilaire Lexilus, Thomas Jean Georges Seguin, Davy Clerc
Life of this patent
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AssigneeSafran Aircraft Engines
InventorsJean-Hilaire Lexilus, Thomas Jean Georges Seguin, Davy Clerc
Estimating the term…
A protection element (45.1, 45.2) for a compressor drum (20) can be arranged at least in part between a blade root (25) and the compressor drum (20). The protection element can include: a first lateral wall (51.1, 51.2) including an inner portion (54.1, 54.2) intended to cover an inner rounded portion of a pocket (24), a bearing surface portion (55.1, 55.2) intended to cover a blade root bearing surface of the pocket (24), and an outer portion (56.1, 56.2) intended to cover an outer rounded portion of the compressor drum (20), a connecting wall (53.1, 53.2) intended to cover an outer face of the compressor drum (20), and a second lateral wall (52.1, 52.2) including a projecting portion (57.1, 57.2) intended to engage with a mounting groove (46.1, 46.2) formed in a vertical face of the compressor drum (20).
An assembly comprising:
A protection element for a compressor drum to be arranged at least partly between a blade root and the compressor drum, the protection element comprising:
A protection element for a compressor drum to be arranged at least partly between a blade root and the compressor drum, the protection element comprising:
Dependencies are inferred from the claim text.