| 摘要 |
<p><P>PROBLEM TO BE SOLVED: To provide a nozzle assembly in which gas turbine efficiency can be increased. <P>SOLUTION: In exemplary embodiments, a nozzle can include a first flow wall (220), a second flow wall (225) and a vane (205) disposed between the first and second flow walls (220, 225), wherein the vane (205) is mechanically coupled to the first flow wall (220) and in contact with the second flow wall (225). <P>COPYRIGHT: (C)2011,JPO&INPIT</p> |
