发明名称 Fixed part for labyrinth seal device for open rotor turbomachine e.g. turbojet, has intermediate piece between support portion and wear part, where thermal expansion coefficient of intermediate piece is greater than that of support portion
摘要 <p>The fixed part (80) has a stationary part (70) including a support portion (61) mounted with a wear part (62) from an abradable material. An intermediate piece (63) is partially inserted between the support portion of the stationary part and the wear part, where the coefficient of thermal expansion of the intermediate piece is greater than that of the support portion, and the coefficient of thermal expansion of the wear part is greater than or equal to that of the intermediate piece. The intermediate piece is made of a material selected from titanium-aluminum alloys. Independent claims are also included for the following: (1) a labyrinth seal device (2) a turbomachine.</p>
申请公布号 FR2991404(A1) 申请公布日期 2013.12.06
申请号 FR20120055028 申请日期 2012.05.31
申请人 SNECMA 发明人 LEMATTRE BORIS;DUFFET JEAN-CHRISTOPHE;IGEL DOMINIK;PIERROT ARNAUD, JEAN-MARIE
分类号 F04D29/10 主分类号 F04D29/10
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