| 摘要 |
<p>The present invention relates to a fixing apparatus for a gas turbine combustor. The fixing apparatus for a gas turbine combustor comprises a combustor equipped horizontally in a direction of the shaft of a gas turbine to burn a fuel to generate exhaust gas to rotate a rotating member; an external casing covering the combustor and equipped spaced from the combustor by a certain distance; and a movable link unit which directly fixes the combustor on the external casing by being equipped between the combustor and the external casing to gather the stress generated by the thermal expansion of the combustor. Accordingly, the damage to the combustor can be prevented by inducing the stress of the gas turbine combustor generated by the thermal expansion in a restricted direction.</p> |
