| 摘要 |
PURPOSE: A flame propagation pipe for a gas turbine is provided to correspond to distance error between combustion chambers adjacent to each other by the adjustment of a flame propagation pipe. CONSTITUTION: A flame propagation pipe for a gas turbine comprises a flexible interlock metal pipe(20), and a sleeve. Flanges, installed at both ends of the interlock tube, are attached to the sleeve. The flame propagation pipe connects two adjacent combustion chambers among multiple combustion chambers. One of a part of spiral members(21) is wound around the other spiral member, so the interlock tube is formed.
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