| 摘要 |
A mounting arrangement 30 for abradable liners used with respect to stator vanes with gas turbine engines. The arrangement 30 comprises a single strut 39 secured through a mounting end 34 to a mounting recess 33 of a vane platform 32. The strut 39 is part of a shroud ring 35 which incorporates a metal abradable liner 37 in order to create a seal between stages within the gas turbine engine. A mounting end 34 incorporates divergent limbs 40, 41 which act through their respective entrant axes X-X, Y-Y to facilitate axial and radial location of the single strut 39 and therefore the shroud ring 35 with liner 37. |
