发明名称 CONE D'ENTREE D'UNE TURBOMACHINE
摘要 <p>The bullet (24) is mounted on a shaft (10) by controlled units including a hydraulic jack (42) that displaces the axial position of the bullet with respect to fan blades (18). The cylinder of the jack is fixed at the end of the shaft, and the piston stem (46) of the jack carries the bullet. The bullet is displaced axially between an advanced position (40) and a retreated position (38). An independent claim is also included for a turbo machine.</p>
申请公布号 FR2873751(B1) 申请公布日期 2006.09.29
申请号 FR20040008338 申请日期 2004.07.28
申请人 SNECMA MOTEURS SOCIETE ANONYME 发明人 LEBRET YANN;RAMSTEIN EDOUARD
分类号 F02C7/042;F02C7/05;F02C7/057;F02K3/06 主分类号 F02C7/042
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