发明名称 HIGH TEMPERATURE SEAL
摘要 A seal (1) comprises a first component (7) and second component (9), the first component comprising a first material having a high thermal and oxidation and wear resistance, and the second component (9) comprising a second material that is different from the first material and has a high spring load maintenance. The seal (1) is suitably applied to a combustion chamber for a gas turbine, where the first component (7) extends between the casing wall of the combustion chamber and adjacent liner segments (4). The spring load of the second component (9) provides a seal also in the case of vibrations in a combustion chamber. The lifetime of the seal (1) is increased due to the individual materials, which are optimally chosen for the functions of high thermal and wear resistance and spring load maintenance respectively. No wear resistant coating is necessary on the first component (7). <IMAGE>
申请公布号 KR101247068(B1) 申请公布日期 2013.03.25
申请号 KR20067006427 申请日期 2004.09.22
申请人 发明人
分类号 F16J15/02;F16J15/08;F23R3/00 主分类号 F16J15/02
代理机构 代理人
主权项
地址
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