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公开(公告)号:US09625151B2
公开(公告)日:2017-04-18
申请号:US13626285
申请日:2012-09-25
Applicant: United Technologies Corporation
Inventor: Jonathan M. Jause , Dennis John Duhamel , James B. Hoke , John S. Tu
CPC classification number: F23R3/002 , F23R3/06 , F23R2900/00005 , F23R2900/00012 , F23R2900/03042 , Y02T50/675 , Y10T16/05
Abstract: A combustor liner grommet is disclosed. The grommet may include a peripheral wall defining a hole in a combustor liner and further including at least one cooling air flow channel. The cooling air flow channel in the grommet wall may be a slot or a hole. The channel may increase cooling flow to the grommet and the combustor liner around the grommet to prevent cracking from heat stress.
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公开(公告)号:US20150241067A1
公开(公告)日:2015-08-27
申请号:US14429087
申请日:2013-03-15
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: Jonathan M. Jause , Kevin Joseph Low , Dennis John Duhamel
CPC classification number: F23R3/60 , F01D5/082 , F01D25/243 , F02C3/04 , F02C7/12 , F02C7/20 , F05D2220/32 , F05D2230/60 , F05D2240/55 , F05D2260/30 , F05D2260/31 , F23R3/50 , F23R2900/00017 , Y02T50/676 , Y10T29/49346
Abstract: A combustor assembly for a gas turbine engine includes a combustor shell, a TOBI, a case, and a joint for securing the combustor shell, TOBI and case together. The joint has a combustor flange integral to the combustor shell. A TOBI flange is integral to the TOBI and a case flange is integral to the case. The combustor flange, the TOBI flange and the case flange are secured together.
Abstract translation: 用于燃气涡轮发动机的燃烧器组件包括燃烧器壳体,TOBI,壳体和用于将燃烧器壳体,TOBI和壳体固定在一起的接头。 接头具有与燃烧器壳体成一体的燃烧器凸缘。 TOBI法兰与TOBI是一体的,外壳法兰与箱体是一体的。 燃烧器法兰,TOBI法兰和外壳法兰固定在一起。
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