IP Library Granted Patent US 7,510,778
Granted Patent B2
US 7,510,778 · App. 11/279,675 · Granted Mar 31, 2009

Part for protecting the leading edge of a blade

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Quick Facts
Patent No.
US 7,510,778
App. No.
11/279,675
Granted
Mar 31, 2009
Kind
B2
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.

Claims (10)

1. 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.

2. An assembly according to claim 1 , wherein the content of SiC particles in said alloy lies in the range 15% to 30% by weight.

3. An assembly according to claim 1 , wherein the inner layer is reinforced with SiC particles.

4. An assembly according to claim 1 , wherein said at least two layers are assembled together by co-extrusion or by roll-bonding.

5. An assembly according to claim 1 , comprising a section that is substantially U-shaped.

6. An assembly according to claim 1 , wherein said protection part is bonded on the leading edge by an adhesive.

Assignments (2)
CORRECTIVE ASSIGNMENT TO CORRECT THE COVER SHEET TO REMOVE APPLICATION NOS. 10250419, 10786507, 10786409, 12416418, 12531115, 12996294, 12094637 12416422 PREVIOUSLY RECORDED ON REEL 046479 FRAME 0807. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF NAME. Recorded Aug 24, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046939/0336 →
CHANGE OF NAME Recorded May 23, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046479/0807 →