Turbine aft frame link assembly for turbofan engine

In one aspect, the disclosure relates to a turbine aft frame linkage assembly for a turbofan engine. A turbofan engine includes an outer bypass duct and a gas turbine engine having a housing. The gas turbine engine is disposed in the outer bypass conduit such that a bypass airflow passage is formed between the outer casing of the gas turbine engine and the outer bypass conduit. The turbine aft frame link assembly includes a set of links coupled between the outer bypass duct and the housing to support the gas turbine engine relative to the outer bypass duct. The connecting rod is arranged around the gas turbine engine on a plane perpendicular to a centerline axis of the turbofan engine. None of the links extends through the bypass airflow passage at a location intersecting a radius extending in a vertically downward direction from the centerline axis. 一方面，本公开涉及一种用于涡轮风扇发动机的涡轮后框架连杆组件。涡轮风扇发动机包括外旁通管道和具有外壳的燃气涡轮发动机。燃气涡轮发动机设置在外旁通管道中，使得在燃气涡轮发动机的外壳和外旁通管道之间形成旁通气流通道。涡轮后框架连杆组件包括联接在外旁通管道和外壳之间一组连杆，以相对于外旁通管道支撑燃气涡轮发动机。连杆在垂直于涡