发明名称 VARIABLE VANE FOR GAS TURBINE ENGINE
摘要 A turbomachine includes a variably positioned vane, an outer spindle integral with a vane outer button, where the vane is coupled to the vane outer button, an annular sleeve defining the spindle, where the annular sleeve contacts the vane outer button at a radially inward extent and contacts a turbine casing at a radially outward extent. The annular sleeve includes a wall portion having an aperture and the spindle extends through the aperture. A nut engages spindle threads, where the nut applies force to the wall portion toward the radially inward extent. An end of the spindle extends through the turbine casing, and a cantilever rotation actuator is coupled to the end of the spindle. A first bearing and second bearing engage the annular sleeve. A vane inner button is coupled to the vane, and a third bearing engages the vane inner button.
申请公布号 US2012263571(A1) 申请公布日期 2012.10.18
申请号 US201113340983 申请日期 2011.12.30
申请人 RESS, JR. ROBERT A. 发明人 RESS, JR. ROBERT A.
分类号 F04D29/56 主分类号 F04D29/56
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