发明名称 AIRCRAFT TURBO MACHINE ASSEMBLY AND AIRCRAFT TURBO MACHINE
摘要 FIELD: transport.SUBSTANCE: claimed assembly comprises metal connection structure between two parts and first circular part made of composite. Said metal connection structure includes, in any half of turbo machine lengthwise cross-section, two primary branches, the base, two secondary branches and two tertiary branches. Two primary branches and said base make the first U-like element extending radially from circular structure lengthwise axis. Two secondary branches make the second U-like element with one of primary branches extending in lengthwise direction. Circular edge of the first circular part is arranged in said second U-like element. Two tertiary branches are combined with the other of two primary branches to make the third U-like element extending in lengthwise direction opposite that of the second U-like element. Primary, secondary and tertiary branches and the base of the first U-like element are a single part. Another invention of proposed set covers aircraft turbo machine with above described assembly.EFFECT: decreased weight of connection structure.5 cl, 4 dwg
申请公布号 RU2566617(C2) 申请公布日期 2015.10.27
申请号 RU20120124073 申请日期 2010.11.10
申请人 SNEKMA 发明人 SEHZ GILEM;VENSAN TOMA ALEN KRISTIAN
分类号 F01D25/24;F01D25/28 主分类号 F01D25/24
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