| 摘要 |
A supporting structure for gas turbine combustion chamber heat-insulating tiles, includes: a first connection element and second connection element (5, 6) having respective first ends (5a, 6a), configured to fit onto sides of a heat-insulating tile (2) of a gas turbine combustion chamber (20), and respective second ends (5b, 6b); a clamping device (7); and a fixing device (8), provided with a threaded pin (15), extending from the clamping device (7) on the side opposite to the heat-insulating tile (2) in use, and with a nut (16). The connection elements (5, 6) clamped by the clamping device (7), and extend in opposite directions from the clamping device (7). The threaded pin (15) is rigidly connected to the clamping device (7), so as to prevent rotations of the threaded pin (15) with respect to the clamping device (7). |
