发明名称 REINFORCEMENT MATERIAL OF LOW PRESSURE COMPRESSOR FOR AIRCRAFT ENGINE
摘要 PROBLEM TO BE SOLVED: To solve a problem with an unbalanced mass which may occur in a low pressure compressor without correcting an existing engine. SOLUTION: An unbalanced mass effect may occur in the low pressure compressor 5 of the aircraft engine. To increase the rigidity of an assembly and reduce cracking which may occur by an accidental unbalanced mass, a reinforcement material 20 is proposed. One end 22 of the reinforcement material may be fixed to an engine casing 7 through a structural arm 10, and the other 32 may be fixed to the compressor 5 desirably on the upstream side of a third guide vane RD3. The reinforcement material 20 is advantageously formed of two portions fixed to each other, and its manufacture is optimized so as to suppress the addition of a weight required for the presence thereof. COPYRIGHT: (C)2006,JPO&NCIPI
申请公布号 JP2006022812(A) 申请公布日期 2006.01.26
申请号 JP20050196064 申请日期 2005.07.05
申请人 SNECMA MOTEURS 发明人 MACE JEROME;LEJARS CLAUDE;MAILLARD PIERRE-YVES;BUFFENOIR FRANCOIS;NICLOT THIERRY
分类号 F04D29/64;F01D21/04;F01D25/24;F02C7/00;F02C7/04 主分类号 F04D29/64
代理机构 代理人
主权项
地址