发明名称 Abradable layer for gas turbine shrouds
摘要 The abradable coating (24), designed to ensure the necessary clearance from blade tips and made from a material able to withstand high temperatures, such as a super-alloy or ceramic, has cavities that are open on the surface of the coating and extend for part of its depth. The cavities, or rectangular or polygonal section, are separated by partitions (27) set at an angle to the radial plane and forming a series of continuous trajectories between axial end faces. The depth of the cavities is between 0.3 and 1 mm, and at least a proportion part of the walls lies at an angle of 0 - 20 degrees to the radial plane.
申请公布号 EP1312761(A1) 申请公布日期 2003.05.21
申请号 EP20020292792 申请日期 2002.11.08
申请人 SNECMA MOTEURS 发明人 LE BIEZ, PHILIPPE;VIGNEAU, JOEL
分类号 F01D5/20;F01D11/12;(IPC1-7):F01D11/12 主分类号 F01D5/20
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