发明名称 SUSPENSION OF A TUBULAR ELEMENT IN AN AIRCRAFT COMPARTMENT
摘要 The invention relates to an assembly comprising a structure (2) and a tubular element (6), which is mounted isostatically in the structure (2), said tubular element (6) comprising a first end (7) connected to said structure by at least four connecting rods 10a-10b-10c-10d, thus setting four first degrees of freedom, and a second end (8) connected to said structure (2) by an attachment means (20) that sets two second degrees of freedom, said connecting rods comprising a means for adjusting the length thereof. In particular, it relates to an exhaust suitable for an auxiliary power unit in the compartment thereof and to the mounting method for aligning them.
申请公布号 EP3083404(A1) 申请公布日期 2016.10.26
申请号 EP20140821807 申请日期 2014.12.08
申请人 SAFRAN POWER UNITS 发明人 CAZENAVE, Olivier;BARNETO, Xavier;LALANNE, Clément
分类号 B64D41/00 主分类号 B64D41/00
代理机构 代理人
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