发明名称 High-lift system for an aircraft
摘要 The system has transmission units for transmitting driving power of a drive unit to a load station. The transmission units are designed as transmission shafts (1), which consist of titanium-containing material. The transmission units consist of aluminum and vanadium, where aluminum is present in a larger mass fraction as vanadium. The transmission shafts are connected to connection elements (2, 3), where the system comprises tensile strength of preset value and/or elastic modulus within the range of 100 to 120 giga pascal (GPa) and/or shear modulus within the range of 39 GPa to 42 GPa. An independent claim is also included for a method for manufacturing a transmission shaft.
申请公布号 EP2436597(A2) 申请公布日期 2012.04.04
申请号 EP20110007892 申请日期 2011.09.28
申请人 LIEBHERR-AEROSPACE LINDENBERG GMBH 发明人 Kleinhans, Reinhold, Dipl.-Ing. (FH);Huth, Stefan, Dipl.-Ing. (FH);Weiss, Werner, Dipl.-Ing. (FH);Schievelbusch, Bernd
分类号 B64C13/28;B64C13/38 主分类号 B64C13/28
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