Tailorable design configuration topologies for aircraft engine mid-turbine frames
展开▼
机译:飞机发动机中涡轮机架的可定制设计配置拓扑
展开▼
页面导航
摘要
著录项
相似文献
摘要
An expandable mid-turbine frame assembly includes a first bearing cone, a second bearing cone and a mid-turbine frame. The mid-turbine frame assembly connects to a gas turbine engine casing and transfers a first load from a first bearing and a second load from a second bearing towards the engine casing. The first bearing cone transfers the first load from the first bearing. The second bearing cone transfers the second load from the second bearing. The mid-turbine frame is connected to the first and second bearing cones and includes segments. Each segment includes a pre-stressed support for equilibrating the first and second loads.
展开▼