公开(公告)号：US20150300293A1

公开(公告)日：2015-10-22

申请号：US14441633

申请日：2013-03-04

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Gabriel L. Suciu ,  Jesse Chandler

IPC: F02K1/64 ,  F02C3/04

CPC classification number: F02K1/64 ,  F02C3/04 ,  F02C3/045 ,  F02C6/00 ,  F02K3/06 ,  F05D2250/314

Abstract: A gas turbine engine has a fan inlet and a fan configured to deliver air to an exhaust nozzle. A core gas turbine engine. including in serial order extending further into the engine, a core turbine section, a combustor and a core compressor section. A core engine inlet duct is spaced from the fan inlet. A method is also described.

Abstract translation: 燃气涡轮发动机具有风扇入口和风扇，其构造成将空气输送到排气喷嘴。 核心燃气轮机。 包括进一步延伸到发动机中的串联顺序，核心涡轮部分，燃烧器和核心压缩机部分。 核心发动机入口管道与风扇入口间隔开。 还描述了一种方法。

公开(公告)号：US10202941B2

公开(公告)日：2019-02-12

申请号：US14441633

申请日：2013-03-04

Applicant: United Technologies Corporation

Inventor： Gabriel L. Suciu ,  Jesse Chandler

IPC: B64D27/00 ,  F02K1/64 ,  F02C3/045 ,  F02K3/06 ,  F02C6/00 ,  F02C3/04

Abstract: A gas turbine engine has a fan inlet and a fan configured to deliver air to an exhaust nozzle. A core gas turbine engine. including in serial order extending further into the engine, a core turbine section, a combustor and a core compressor section. A core engine inlet duct is spaced from the fan inlet. A method is also described.