发明名称 Turbomachine vane damper
摘要 <p>The damper (10) has a base plate (13) supported on a disk rim of a rotor of a turbomachine e.g. high pressure gas turbine engine axial compressor, and a spring plate (12). The plate (12) connects an elongated conterweight (11) with the plate (13), where the counterweight is made of composite material i.e. impregnated fabric. The counterweight has contact surface portions that are contacted with platforms of vanes. The portions form an angle that is lower than 90 degree, with the plate (13), when the plate (12) is at rest.</p>
申请公布号 EP1985810(A1) 申请公布日期 2008.10.29
申请号 EP20080155206 申请日期 2008.04.25
申请人 SNECMA 发明人 LEFEBVRE, ERIC;CAUCHETEUX, MATHIEU;DURDEVIC, GORAN
分类号 F01D25/06;F01D5/26 主分类号 F01D25/06
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