首页>
外国专利>
ROTOR STACK BUSHING WITH ADAPTIVE TEMPERATURE METERING FOR A GAS TURBINE ENGINE
ROTOR STACK BUSHING WITH ADAPTIVE TEMPERATURE METERING FOR A GAS TURBINE ENGINE
展开▼
机译：转子堆叠衬套，具有用于燃气轮机的自适应温度计量
展开▼
页面导航
摘要
著录项
相似文献
摘要
A rotor stack for a gas turbine engine includes a first rotor disk with a first rotor spacer arm, the first rotor spacer arm having a first flange with an outboard flange surface and an inboard flange surface, a first hole along an axis through the first flange, the first hole having a counterbore in the outboard flange surface; a second rotor disk with a web having a second hole along the axis; a third rotor disk with a third rotor spacer arm, the third rotor spacer arm having a third flange with an outboard flange surface and an inboard flange surface, a third hole along the axis through the third flange, the third hole having a counterbore in the inboard flange surface; and a bushing with a tubular body and a flange that extends therefrom, the tubular body comprising at least one axial groove along an outer diameter thereof, the bushing extends through the first hole, the second hole and partially into the counterbore in the inboard flange surface of the third hole.
展开▼
