发明名称 Contoured abradable shroud structure
摘要 <p>An abradable fan containment structure within a fan section of a turbofan engine is provided. The fan section of the turbofan engine has fan blades and an abradable fan shroud (44). The abradable fan shroud includes an inner fan casing circumscribing the fan blades such that the inner annular surface (48) of the fan shroud is disposed adjacent the blade tips of the fan blades within the fan section. The inner annular surface is formed from an abradable material (46). The abradable material contour is substantially triangular along the axial length from a forward edge (50) to an aft edge (52). The abradable material has a contoured surface characterized by a trapezoidal shape after being worn when rubbed by the tips of the fan blades during operation of the engine. &lt;IMAGE&gt;</p>
申请公布号 EP1004750(A2) 申请公布日期 2000.05.31
申请号 EP19990309315 申请日期 1999.11.23
申请人 GENERAL ELECTRIC COMPANY 发明人 ALLEN, JEFFREY SCOTT;BREEZE-STRINGFELLOW, ANDREW;MANHARTH, GARY BRENT
分类号 F01D11/12;(IPC1-7):F01D11/12 主分类号 F01D11/12
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