公开(公告)号：WO2014123626A3

公开(公告)日：2014-11-20

申请号：PCT/US2013075623

申请日：2013-12-17

Applicant: UNITED TECHNOLOGIES CORP

Inventor： JONES ANTHONY C ,  TRAVELBEE CHARLES BRIAN ,  LYDON PATRICK M ,  ALEXANDER ERIC J ,  THAYALAKHANDAN NAGAMANY

IPC: F02C7/12 ,  F01D25/12 ,  F02C7/04 ,  F02C7/18

CPC classification number: F02K3/02 ,  B64C39/02 ,  B64C2201/048 ,  B64D27/20 ,  B64D33/02 ,  B64D33/08 ,  B64D2033/0273 ,  F02C7/18 ,  F02C9/18 ,  F02K1/822 ,  F42B15/10 ,  Y02T50/675

Abstract: A gas turbine engine has an inlet duct, which is configured to communicate with an inlet to a compressor. The inlet duct is further configured to communicate air outwardly of an outer casing of the gas turbine engine, and to pass the air along an axial length of the gas turbine engine to cool a component associated with the gas turbine engine.

Abstract translation: 燃气涡轮发动机具有入口管道，该入口管道被构造成与压缩机的入口连通。 进气管进一步构造成使空气与燃气涡轮发动机的外壳向外连通，并沿着燃气涡轮发动机的轴向长度传递空气以冷却与燃气涡轮发动机相关联的部件。

公开(公告)号：EP2935835A4

公开(公告)日：2015-12-23

申请号：EP13874584

申请日：2013-12-17

Applicant: UNITED TECHNOLOGIES CORP

Inventor： JONES ANTHONY C ,  TRAVELBEE CHARLES BRIAN ,  LYDON PATRICK M ,  ALEXANDER ERIC J ,  THAYALAKHANDAN NAGAMANY

IPC: F02C7/12 ,  B64D33/02 ,  B64D33/08 ,  F01D25/12 ,  F02C7/04 ,  F02C7/18

CPC classification number: F02K3/02 ,  B64C39/02 ,  B64C2201/048 ,  B64D27/20 ,  B64D33/02 ,  B64D33/08 ,  B64D2033/0273 ,  F02C7/18 ,  F02C9/18 ,  F02K1/822 ,  F42B15/10 ,  Y02T50/675

Abstract: A gas turbine engine has an inlet duct, which is configured to communicate with an inlet to a compressor. The inlet duct is further configured to communicate air outwardly of an outer casing of the gas turbine engine, and to pass the air along an axial length of the gas turbine engine to cool a component associated with the gas turbine engine.