| 摘要 |
<P>PROBLEM TO BE SOLVED: To provide a seal member for a hot gas path component in a gas turbine system. <P>SOLUTION: The seal member 100 includes a first seal pin 112, a second seal pin 114 spaced from the first seal pin 112, and at least one cross member 120. The at least one cross member 120 has a first end 122 and a second end 124, and may be joined at the first end 122 to the first seal pin 112 and at the second end 124 to the second seal pin 114. The at least one cross member 120 forces the first and second seal pins 112, 114 apart from each other when the seal member 100 is subjected to a centrifugal force. <P>COPYRIGHT: (C)2012,JPO&INPIT |
