发明名称 INTEGRATED OUTER FLOWPATH DUCTING AND FRONT FRAME SYSTEM FOR USE IN A TURBOFAN ENGINE AND METHOD FOR MAKING SAME
摘要 A system and method is provided for an integrated aircraft turbofan engine outer flowpath ducting and front frame that minimizes assembly interfaces and reduces overall aircraft engine weight. The system and method provide an integrated turbofan engine outer flowpath ducting and front frame system that decouples the fairing/aerodynamic duties from the struts/weight bearing duties thereby enabling efficient distribution of mechanical load.
申请公布号 US2016108757(A1) 申请公布日期 2016.04.21
申请号 US201414516270 申请日期 2014.10.16
申请人 HONEYWELL INTERNATIONAL INC. 发明人 Mickelsen Justin C.;Liston Laurence David Noble;Knowles Mark;Alstad Shawn
分类号 F01D25/24;F01D25/28;F01D25/00 主分类号 F01D25/24
代理机构 代理人
主权项 1. An outer flowpath ducting and front frame system in a turbofan engine, the engine outer flowpath ducting and front frame system comprising: a load housing comprising a primary composite load path circumferentially surrounding an engine centerline and defining the outer flowpath; and a front frame assembly centered within the load housing and configured to i) direct air through the outer flowpath, and ii) bear weight, the front frame assembly detachably coupled to the load housing.
地址 Morristown NJ US