公开(公告)号：US09447982B2

公开(公告)日：2016-09-20

申请号：US14735963

申请日：2015-06-10

Applicant: General Electric Company

Inventor： Robert Allen Baten ,  David Joseph Drobniak ,  Harley Matthew Ross

IPC: F24F7/06 ,  F24F7/007 ,  F24F7/08 ,  F02C3/32 ,  F02C7/12

CPC classification number: F24F7/08 ,  F01D25/12 ,  F02C3/32 ,  F02C7/12 ,  F05D2260/601 ,  Y02E20/16

Abstract: A turbine ventilation system includes at least one fan configured to provide a first air flow into a gas turbine enclosure, a fan bypass configured to circumvent the at least one fan to provide a second air flow into the gas turbine enclosure, and an eductor configured to draw the first or second air flows through and out of the gas turbine enclosure.

公开(公告)号：US20150276247A1

公开(公告)日：2015-10-01

申请号：US14735963

申请日：2015-06-10

Applicant: General Electric Company

Inventor： Robert Allen Baten ,  David Joseph Drobniak ,  Harley Matthew Ross

IPC: F24F7/08

CPC classification number: F24F7/08 ,  F01D25/12 ,  F02C3/32 ,  F02C7/12 ,  F05D2260/601 ,  Y02E20/16

Abstract: A turbine ventilation system includes at least one fan configured to provide a first air flow into a gas turbine enclosure, a fan bypass configured to circumvent the at least one fan to provide a second air flow into the gas turbine enclosure, and an eductor configured to draw the first or second air flows through and out of the gas turbine enclosure.

Abstract translation: 涡轮机通风系统包括至少一个风扇，其被配置为将第一空气流提供到燃气涡轮机外壳中，风扇旁路，其构造成绕过所述至少一个风扇以提供第二空气流进入所述燃气涡轮机壳体;以及喷射器， 将第一或第二空气流过和流出燃气轮机外壳。