| 摘要 |
A guide vane assembly (26) for a turbomachine, comprising a guide vane (28) and a liner (34): the guide vane (28) comprising an aerofoil portion (30) having a radially outer platform (32), wherein one of the outer platform (32) and the liner (34) has a hook element (52), the hook element (52) comprising an opening (54) and a circumferentially extending channel (56); and the other one of the outer platform (32) and the liner (34) comprises a retaining element (64) having a head portion (68), wherein in an operational orientation the head portion (68) located within the channel (56) and is too wide to be withdrawn through the opening (54) of the hook element (52). |
