发明名称 METHOD AND APPARATUS FOR FABRICATING FAN ASSEMBLY FOR USE WITH TURBINE ENGINE
摘要 <p><P>PROBLEM TO BE SOLVED: To provide a method and an apparatus for fabricating a fan assembly 14 capable of reducing a load imposed on an engine mounting body by allowing sacrificial abrasion of a fan blade 28 made of a frangible material, and increasing a vibration range of a rotor 31, and of reducing possibility of further damage to a casing 32 by reducing the weight of the fan blade 28 and allowing reduction of unbalance. <P>SOLUTION: This fan assembly 14 includes: a rotor 31 including a plurality of rotor blades at least one of which is made of a frangible material; and the casing 32 extending in the circumferential direction around the rotor. The casing is arranged at a predetermined distance from the plurality of rotor blades. The distance allows an amount of initial contact resistance created between the casing and the plurality of rotor blades after a bladeout to be increased. Contact resistance of a filling material 150 allows abrasion of the fan blade 28. <P>COPYRIGHT: (C)2008,JPO&INPIT</p>
申请公布号 JP2008163946(A) 申请公布日期 2008.07.17
申请号 JP20070335460 申请日期 2007.12.27
申请人 GENERAL ELECTRIC CO <GE> 发明人 CRALL DAVID WILLIAM;WORTHOFF FRANK;MOLLMANN DANIEL EDWARD;KRAY NICHOLAS JOSEPH;FARSON MAX
分类号 F04D29/38;F02K3/06;F04D29/52 主分类号 F04D29/38
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