发明名称 TURBOMACHINE FAN CASING ASSEMBLY
摘要 A turbomachine casing assembly including an inner casing element for arrangement radially outward of a turbomachine fan; an outer casing element for arrangement radially further outward of the turbomachine fan; a retaining lip arranged radially inward of a portion of the inner casing element; and a separator extending between the inner and outer casing elements and arranged to urge a portion of the inner casing element against the lip. The separator is arranged in compression between the inner and outer casing elements to urge the portion of the inner casing element against the lip. The separator is arranged to engage a frangible region of the inner casing element such that the frangible region is configured to break in response to an impact satisfying predetermined conditions, allowing the inner casing element to displace radially outwards exposing features to improve retention of a released fan blade.
申请公布号 US2015275695(A1) 申请公布日期 2015.10.01
申请号 US201514657601 申请日期 2015.03.13
申请人 ROLLS-ROYCE PLC 发明人 EVANS Dale Edward;CHRISTMAS David Laker
分类号 F01D25/26;F01D25/28;F01D25/24 主分类号 F01D25/26
代理机构 代理人
主权项 1. A turbomachine casing assembly comprising: an inner casing element for arrangement radially outward of a turbomachine fan; an outer casing element for arrangement radially further outward of the turbomachine fan; a retaining lip arranged radially inward of at least a region of the inner casing element; a separator extending between the inner and outer casing elements and arranged to urge a portion of the inner casing element against the lip; wherein the separator is arranged to engage a frangible region of the inner casing element such that the frangible region is configured to break in preference to the separator.
地址 London GB