发明名称 LINEAR SEAL OF AN INTER BLADE PLATFORM AND ASSOCIATED INTER BLADE PLATFORM ROTOR AND TURBOJET ENGINE
摘要 <p>A linear seal (10; 10 ) of an inter blade platform having a length comprising a linear base (12; 12 ) intended to be secured to the inter blade platform (40) and a linear lip (14; 14 ) extending from the linear base (12; 12 ) said linear lip (14; 14 ) having a linear distal end portion (14a) configured to come into contact with a wall on the lower surface side (52a) or a wall on the upper surface side (52d) of a blade (50) a linear groove (16; 16 ) being formed between the linear base (12; 12 ) and the linear lip (14; 14 ) along at least one portion of the length of said linear seal (10; 10 ). The linear distal end portion (14a; 14 a) has at least one linear slot (120; 120 ) extending along at least one portion of the length of said seal (10; 10 ).</p>
申请公布号 IN6758DEN2014(A) 申请公布日期 2015.05.22
申请号 IN2014DE06758 申请日期 2014.08.12
申请人 SNECMA 发明人 RAVIER ANNE LAURE
分类号 F01D11/00 主分类号 F01D11/00
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