发明名称 AIRCRAFT JET ENGINE
摘要 In various embodiments, a jet engine, as described herein, may include a fan case, a fan cowl, and an air inlet. Further, in various embodiments, at least one of the fan case and the fan cowl may be directly coupled to the air inlet. In addition, in various embodiments, the fan case, the fan cowl, and the air inlet may be manufactured as a single, unitary, engine part.
申请公布号 US2014352797(A1) 申请公布日期 2014.12.04
申请号 US201313909772 申请日期 2013.06.04
申请人 Rohr, Inc. 发明人 Aten Michael;Ratajac Aleksandar
分类号 F02C7/04;B23P15/00 主分类号 F02C7/04
代理机构 代理人
主权项 1. A turbofan engine comprising: a fan case; a fan cowl coupled to the fan case; and an air inlet coupled directly to at least one of the fan case and the fan cowl.
地址 Chula Vista CA US