发明名称 Rotor wheel for a jet engine, and jet engine comprising same
摘要 <p>The impeller has an axisymmetric blade support (22) for supporting a set of blades. An intermediate part e.g. disk collar, extends in an axial direction from the support. A damping unit is placed on a face of the intermediate part. The damping unit has a layer made of viscoelastic material and a counterlayer made of rigid material. The damping unit is segmented in an axial and/or circumferential direction into two elementary damping units (301, 302). The layer and the counterlayer are attached to one another using an adhesive.</p>
申请公布号 EP2009238(A1) 申请公布日期 2008.12.31
申请号 EP20080159044 申请日期 2008.06.25
申请人 SNECMA 发明人 BAUMHAUER, STEPHANE, JEAN, JOSEPH;DUPEUX, JEROME, ALAIN;GARCIN, FRANCOIS, MAURICE;LOMBARD, JEAN-PIERRE, FRANCOIS;SEINTURIER, ERIC;BALMES, ETIENNE
分类号 F01D5/10;F01D5/26;F01D25/06;F16F15/12 主分类号 F01D5/10
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