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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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