| 摘要 |
<p>A gas turbine 1 includes a combustor 39, a combustor casing 31 formed in a cylindrical shape to house the combustor 39 therein, and a combustor insertion hole 31a, which is a hole formed on a side periphery of the combustor casing 31, where a size thereof in a direction orthogonal to a circumferential direction of the combustor casing 31 is formed larger than that in the circumferential direction of the combustor casing 31, and when the combustor 39 inserted into the hole, a member moved together with the combustor 39, and the hole are viewed from a moving direction of the combustor 39, the hole includes an entire external form of the combustor 39 and the member moved together with the combustor 39.</p> |
