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公开(公告)号:US20180030853A1
公开(公告)日:2018-02-01
申请号:US15222102
申请日:2016-07-28
Applicant: General Electric Company
Inventor: Laxmikant MERCHANT , Dinesh VENUGOPAL SETTY , Avishetti SRINIVAS , S.T. DEEPAK
CPC classification number: F01D25/14 , F01D15/10 , F01D25/04 , F05D2220/32 , F05D2220/76 , F05D2240/14 , F05D2260/96 , H02K7/003 , H02K7/1823 , H02K9/10 , Y10T464/10
Abstract: A gas turbine system includes a load coupling connecting a gas turbine to a generator. A load coupling guard surrounds the load coupling to define an enclosed spaced around the load coupling. The load coupling guard includes a porous sleeve such that hydrogen coolant leaked into the load coupling guard from the generator is vented to ambient air.
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公开(公告)号:US20170292456A1
公开(公告)日:2017-10-12
申请号:US15096922
申请日:2016-04-12
Applicant: General Electric Company
Inventor: Laxmikant MERCHANT , Hua ZHANG , Dinesh VENUGOPAL SETTY , Valery Ivanovich PONYAVIN , James den Outer
CPC classification number: F02C9/18 , F01D9/02 , F02C7/045 , F02C7/047 , F05D2220/32 , F05D2260/96 , F05D2270/101
Abstract: An inlet system for a gas turbine includes an integrated inlet bleed heat system, wherein the inlet bleed design is integrated in, e.g., a silencer or inlet.
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