公开(公告)号：EP3044437A4

公开(公告)日：2016-09-28

申请号：EP14863476

申请日：2014-09-08

申请人： UNITED TECHNOLOGIES CORP

发明人： LAPIERRE TODD M ,  YUEN YUK-KWAN BRIAN

IPC分类号： F02C7/06 ,  F01D25/16 ,  F01D25/20 ,  F16L5/00 ,  F16L21/02 ,  F16L21/08 ,  F16N21/00

CPC分类号： F04D29/063 ,  F01D25/162 ,  F01D25/20 ,  F02C7/06 ,  F04D29/053 ,  F04D29/056 ,  F04D29/102 ,  F04D29/321 ,  F04D29/582 ,  F16L5/025 ,  F16L5/12 ,  F16L21/002 ,  F16N21/00

摘要： A gas turbine engine includes a bearing support positioned fore of a compressor section along a primary flowpath. The bearing support internally includes a fluid reservoir with a reservoir tube, a fluid pump with a fluid pump tube, and a fluid coupler coupling the reservoir tube to the fluid pump tube.