公开(公告)号：US10161311B2

公开(公告)日：2018-12-25

申请号：US15104479

申请日：2013-12-23

Applicant: General Electric Company

Inventor： Qiang Pang ,  Guohua Zhong ,  Yao Li

IPC: F02C7/18 ,  F02K1/70 ,  F02K1/72 ,  F02K1/76 ,  F02C6/08 ,  B64D27/16 ,  B64D29/00 ,  F02K3/06

Abstract: An aircraft with aturbofan engine assembly having at least one compressor, a nacelle surrounding the turbine engine and defimng an annular bypass duct between the nacelle and the turbine engine, a thrust reverser having at least one moveable control surface, a thrust reverser locking system configured to selectively lock the thrust reverserand an injection cooling system.