发明名称 HEAT EXCHANGE MODULE FOR A TURBINE ENGINE
摘要 A heat exchange module is provided for a turbine engine. The heat exchange module includes a duct and a plurality of heat exchangers. The duct includes a flowpath defined radially between a plurality of concentric duct walls. The flowpath extends along an axial centerline through the duct between a first duct end and a second duct end. The heat exchangers are located within the flowpath, and arranged circumferentially around the centerline.
申请公布号 US2017122210(A1) 申请公布日期 2017.05.04
申请号 US201715412729 申请日期 2017.01.23
申请人 United Technologies Corporation 发明人 Schwarz Frederick M.;Schmitz John T.
分类号 F02C7/18 主分类号 F02C7/18
代理机构 代理人
主权项 1. A turbine engine with an axial centerline, comprising: a heat exchange module that includes: a duct including a duct flowpath defined radially between a plurality of concentric duct walls, the duct flowpath extending along an axial centerline through the duct between a first duct end and a second duct end; anda plurality of heat exchangers arranged circumferentially around the centerline; the turbine engine includes a first case, a second case, and a third case, wherein a central core flowpath is defined by the first case; wherein a primary bypass flowpath is defined radially between the first case and the second case; wherein a secondary bypass flowpath is defined radially between the second case and the third case; and wherein the duct flowpath is fluidly coupled inline with the secondary bypass flowpath, and the pluarality of heat exchangers is arranged to pivotally translate within the secondary bypass flowpath between a deployed position and a stowed position.
地址 Farmington CT US