发明名称 Blade ring segment for a fluid flow engine and method for producing the same
摘要 The segment (1) has lower- and upper shrouds (5, 6) extended along a circle segment and integrally connected three blades (2-4). Each blade radially extends from the shroud and formed in a hollow form with a channel, where the segment is integrally formed by casting and directional solidification. The shrouds surround outlet openings (14-17) of the channels of the blades, and comprise a set of reinforcing ribs (10, 11) provided between two axially extending reinforcing ribs (9, 12). Each shroud comprises a U-shaped cross-section in an axial direction. An independent claim is also included for a method for manufacturing a blade ring segment.
申请公布号 EP2615243(A1) 申请公布日期 2013.07.17
申请号 EP20120150838 申请日期 2012.01.11
申请人 MTU AERO ENGINES GMBH 发明人 SCHLEMMER, MARKUS;ROZAK, MARCIN;BUCK, ALEXANDER
分类号 F01D5/14;F01D5/18;F01D5/28;F01D9/04 主分类号 F01D5/14
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