-
公开(公告)号：EP2935835B1
公开(公告)日：2019-10-09
申请号：EP13874584.9
申请日：2013-12-17
-
公开(公告)号：EP2935835A2
公开(公告)日：2015-10-28
申请号：EP13874584.9
申请日：2013-12-17
发明人： JONES, Anthony C. , TRAVELBEE, Charles Brian , LYDON, Patrick M. , ALEXANDER, Eric J. , THAYALAKHANDAN, Nagamany
CPC分类号： F02K3/02 , B64C39/02 , B64C2201/048 , B64D27/20 , B64D33/02 , B64D33/08 , B64D2033/0273 , F02C7/18 , F02C9/18 , F02K1/822 , F42B15/10 , Y02T50/675
摘要： 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.
摘要翻译： 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：EP2981696B1
公开(公告)日：2019-08-28
申请号：EP14778145.4
申请日：2014-03-26
-
公开(公告)号：EP2981696A1
公开(公告)日：2016-02-10
申请号：EP14778145.4
申请日：2014-03-26
CPC分类号： F02C7/04 , B64D33/02 , B64D2033/0273 , F02C3/04 , F02C7/06 , F05D2220/323 , F05D2250/51 , F05D2250/80 , F05D2250/82
摘要： A gas turbine engine has a nose cone with a nose cone upstream end and an inlet housing including a plurality of separate flow paths at a housing upstream end which is downstream of the nose cone upstream end. The inlet housing includes a mixing portion downstream of the housing upstream end which mixes airflow from the separate flow paths, such that the airflow is generally around 360 degrees of a rotational axis of the gas turbine engine. A rotor and a turbine drive a shaft to drive the rotor with the shaft including a bearing mounted at a location downstream of the nose cone upstream end.
-
-
-
搜索结果
4 条记录 (耗时 0.009 秒)
