| 摘要 |
<p>The present invention relates to a laminated sheet (100) for a gas turbine component. The laminated sheet (100) comprises a first cover layer (110), a second cover layer (120) and a first intermediate layer (130), wherein the first cover layer (110), the second cover layer (120) and the first intermediate layer (130) are stacked together on top of each other. The first intermediate layer (130) is located between the first cover layer (110) and the second cover layer (120). The first intermediate layer (130) comprises at least one first elongated through hole (131), wherein a cooling fluid is flowable through the first elongated through hole (131).</p> |
