发明名称 VIRTUAL MULTI-STREAM GAS TURBINE ENGINE
摘要 A gas turbine engine is provided that includes a core flow path to direct a core stream flow. A common flow path is outboard of the core flow path, where the common flow path directs both a second stream flow and a third stream flow. Another gas turbine engine is provided that includes an outer case structure around a central longitudinal engine axis. An intermediate case structure is inboard of the outer case structure, where the intermediate case structure and the outer case structure direct both a third stream flow and a second stream flow. An inner case structure is inboard of the intermediate case structure, where the inner case structure and the intermediate case structure direct a core stream flow.
申请公布号 US2015361819(A1) 申请公布日期 2015.12.17
申请号 US201514604228 申请日期 2015.01.23
申请人 United Technologies Corporation 发明人 Epstein Alan H.
分类号 F01D17/12;F01D9/04;F01D25/24;F01D5/02 主分类号 F01D17/12
代理机构 代理人
主权项 1. A gas turbine engine, comprising: a core flow path to direct a core stream flow; and a common flow path outboard of the core flow path, the common flow path to direct both a second stream flow and a third stream flow.
地址 Hartford CT US