Attack-side shield, turbomachine blade equipped with such a shield, and method for manufacturing such a shield

FR3163105A1Pending Publication Date: 2025-12-12SAFRAN AIRCRAFT ENGINES SAS
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Patent Information

Application Number
FR2024006203
Authority / Receiving Office
FR · FR
Patent Type
Applications
Current Assignee / Owner
Filing Date
2024-06-11
Publication Date
2025-12-12
Patent Text Reader

Abstract

The invention relates to a leading-edge shield (30, 30') for a turbomachine blade, particularly for aircraft, the leading-edge shield (30, 30') being elongated along an elongation direction (A) and comprising an intrados fin (33) and an extrados fin which are connected by a leading edge (35). According to the invention, the leading-edge shield (30, 30') is composed of several portions (30a, 30b) assembled along the elongation direction (A), and the portions (30a, 30b) are joined together by means of complementary connecting members (36). Figure for the abstract: Fig. 5
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Citation Information

Patent Citations

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