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公开(公告)号:EP3106620A1
公开(公告)日:2016-12-21
申请号:EP16171542.0
申请日:2016-05-26
申请人: Rolls-Royce Corporation , Rolls-Royce High Temperature Composites Inc , Rolls-Royce North American Technologies, Inc.
摘要: A cartridge for a ceramic matrix composite (CMC) seal segment of a segmented turbine shroud of a gas turbine engine is provided. The cartridge comprises a carrier segment and a CMC seal segment. A surface of the carrier segment and a surface of the CMC seal segment form a mating region proximate the entire perimeter of the CMC seal segment. The carrier segment surface may comprise a channel, and a compressible mating element may be disposed within the channel. Air may be supplied to a cavity, formed by the carrier and CMC seal segment, and the mating region.
摘要翻译: 提供了一种用于燃气涡轮发动机的分段涡轮机护罩的陶瓷基质复合材料(CMC)密封段的筒。 盒包括载体区段和CMC密封区段。 载体区段的表面和CMC密封区段的表面形成接近CMC密封区段的整个周边的配合区域。 载体段表面可以包括通道,并且可压缩配合元件可以设置在通道内。 可以将空气供应到由载体和CMC密封段形成的空腔以及配合区域。
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公开(公告)号:EP3106620B1
公开(公告)日:2019-10-30
申请号:EP16171542.0
申请日:2016-05-26
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