发明名称 CONJOINED REVERSE CORE FLOW ENGINE ARRANGEMENT
摘要 A system of conjoined gas turbine engines has a first engine with a first propulsor having a first axis and a first engine core having a second axis, and a second engine with a second propulsor having a third axis and a second engine core having a fourth axis. The first axis and third axis are parallel to one another; and the second axis and fourth axis are angled from one another.
申请公布号 US2015121838(A1) 申请公布日期 2015.05.07
申请号 US201414190175 申请日期 2014.02.26
申请人 United Technologies Corporation 发明人 Suciu Gabriel L.;Merry Brian D.
分类号 F02C6/02;B64D29/06;F02K1/54 主分类号 F02C6/02
代理机构 代理人
主权项 1. A system of conjoined gas turbine engines, the system comprising: a first engine with a first propulsor having a first axis and a first engine core having a second axis; a second engine with a second propulsor having a third axis and a second engine core having a fourth axis; wherein the first axis and third axis are parallel to one another; and wherein the second axis and fourth axis are angled from one another.
地址 Hartford CT US