| 摘要 |
<p><P>PROBLEM TO BE SOLVED: To provide a transition piece (230) used for a turbine engine (100). <P>SOLUTION: The transition piece includes a cooling sleeve (300) having the inner wall (240), the first end (233) and the opposite second end (235) of a combustor assembly (104). The cooling sleeve is coupled to the inner wall, such that an annular passage (238) is defined between the inner wall and the cooling sleeve. The first end defines an annular inlet (237) and second end defines an annular outlet (306). <P>COPYRIGHT: (C)2010,JPO&INPIT</p> |
