发明名称 SUSPENSION OF A TUBULAR ELEMENT IN AN AIRCRAFT COMPARTMENT
摘要 The invention relates to an assembly including a structure (2) and a tubular element (6), isostatically mounted in the structure (2), said tubular element (6) comprising a first end (7) connected by at least four connecting rods (10a - 10b - 10c - 10d) to said structure, establishing four first degrees of freedom, and a second end (8) connected to said structure (2) by a linking means (20) establishing two second degrees of freedom, said connecting rods comprising a means for adjusting the length thereof. The invention relates, in particular, to an exhaust fitted to an auxiliary power unit in the compartment thereof and to the installation method for aligning same.
申请公布号 WO2015092207(A1) 申请公布日期 2015.06.25
申请号 WO2014FR53212 申请日期 2014.12.08
申请人 MICROTURBO 发明人 CAZENAVE, OLIVIER;BARNETO, XAVIER;LALANNE, CLÉMENT
分类号 B64D41/00 主分类号 B64D41/00
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