Part for protecting the leading edge of a blade
AssigneeSnecma
InventorsJacques Bernard, Claude Marcel Mons, Isabelle Peslerbe, Thierry Thomas
Life of this patent
Estimating the term…
Abstract
A protection part comprising at least two layers including an outer layer and an inner layer has its outer layer made of an aluminum alloy that is reinforced with particles of SiC, the SiC particle content in said alloy lying in the range 15% to 40% by weight, while the inner layer is made of an aluminum alloy that is optionally reinforced with SiC particles, the SiC particle content within the layers increasing from the inner layer towards the outer layer. The part is for use in protecting the leading edge of a blade, in particular a blade or vane in a turbomachine, a helicopter blade, or a propeller blade.
Claims6
An assembly comprising:
- a blade of a turbomachine, a helicopter, or a propeller, said blade having a leading edge, and
- a protection part for protecting a leading edge of a blade, said protection part being configured to fit onto the leading edge of said blade, said protection part comprising an outer protection face made of an aluminum alloy reinforced by particles of SiC, an SiC particle content in said aluminum alloy lying in a range 15% to 40% by weight, said protection part comprising at least two layers, including an outer layer and an inner layer, the outer layer being made of said reinforced aluminum alloy and the inner layer being made of an aluminum alloy, a content of SiC particles in the outer and inner layers increasing from the inner layer to the outer layer,
- wherein said protection part is fitted onto the leading edge in order to protect said leading edge,
- wherein the blade is made of an organic-matrix composite material.
Dependencies are inferred from the claim text.