公开(公告)号：US11852024B2

公开(公告)日：2023-12-26

申请号：US17540779

申请日：2021-12-02

申请人： GE Aviation Systems LLC

发明人： Pawel Piotr Hanczewski ,  Mohamed Osama ,  Pawel Pawlowski

IPC分类号： F01D25/12 ,  F01D9/02 ,  F01D5/18 ,  F01D15/10 ,  F01D25/16 ,  F01D25/30 ,  F01D9/06 ,  F01D9/04 ,  F01D25/00 ,  H02G5/10 ,  H05K9/00

CPC分类号： F01D25/12 ,  F01D9/02 ,  H02G5/10 ,  F05D2220/323 ,  F05D2240/12 ,  F05D2260/20 ,  H05K9/0081

摘要： A turbine engine that includes an engine core, a core casing surrounding the engine core, at least one cowl surrounding the core casing, a power converter located between the at least one cowl and the core casing, an electrical generator disposed within the engine core, at least one electrical strut having an outer wall defining an interior and extending radially between the engine core and the core casing; and at least one electrical conduit located within the interior and electrically coupling the generator to the power converter.

公开(公告)号：US20220195887A1

公开(公告)日：2022-06-23

申请号：US17540779

申请日：2021-12-02

申请人： GE Aviation Systems LLC

发明人： Pawel Piotr Hanczewski ,  Mohamed Osama ,  Pawel Pawlowski

IPC分类号： F01D25/12 ,  F01D9/02 ,  H02G5/10

摘要： A turbine engine that includes an engine core, a core casing surrounding the engine core, at least one cowl surrounding the core casing, a power converter located between the at least one cowl and the core casing, an electrical generator disposed within the engine core, at least one electrical strut having an outer wall defining an interior and extending radially between the engine core and the core casing; and at least one electrical conduit located within the interior and electrically coupling the generator to the power converter.