ACTUATION APPARATUS FOR AN AIR MODULATING SYSTEM OF A GAS TURBINE
摘要
An air modulating system (70) for a gas turbine engine (20) includes a fixed plate (72) with a fluid passage inlet (74), a floating plate (76) with a first side (92) adjacent to the fluid passage inlet (74), an actuated mount (78) configured to move the floating plate (76) relative to the fixed plate (72), and a linkage element (80) for connecting the floating plate (76) to the actuated mount (78). The linkage element (80) includes a mounting flange (88) configured to slidably engage the floating plate (76).
申请公布号
EP3002418(A1)
申请公布日期
2016.04.06
申请号
EP20150179139
申请日期
2015.07.30
申请人
UNITED TECHNOLOGIES CORPORATION
发明人
KANTANY, NICHOLAS W.;BOUCHER, EDWARD;CARNAVOS, KRISTINE MARIE;COVINO, ADAM;HO, MELANIE;FARAH, JORGE I.;PETERS, DONALD W.