Abstract: A sealing system is described for effecting a seal of a gap (G1; G2) in a turbomachine (1) between a first structural member (21; 23) and a second structural member (31). The sealing system includes a sealing apparatus comprising a sealing member (47; 77) comprising a first edge portion (49; 79) and a second edge portion (51; 81). The two edge portions are parallel to one another and the first edge portion (49; 79) forms a pivoting connection to the first structural member (21; 23). The first structural member (21; 23) further comprises a seat (55; 85) rotatably housing the first edge portion (49; 79) of the sealing member (47; 77). The second edge portion (51; 81) comprises a curved contact surface (51.1; 81.1), in sealing contact with a contact surface (67; 97) of the second structural member (31).

Abstract: A gas turbine combustor is disclosed, comprising: a combustor liner; a combustor casing, at least partly housing the combustor liner, and a liner support arrangement. The liner support arrangement comprises individual support elements located between the combustor liner and the combustor casing. Each support element comprises a liner support member fixed to the combustor liner and a casing support member fastened to the combustor casing. Each casing support member comprises a casing stop seat fixed on the combustor casing and a replaceable casing stop, detachably coupled to the casing stop seat.

Abstract: A gas turbine combustor is disclosed, comprising: a combustor liner; a combustor casing, at least partly housing the combustor liner, and a liner support arrangement. The liner support arrangement comprises individual support elements located between the combustor liner and the combustor casing. Each support element comprises a liner support member fixed to the combustor liner and a casing support member fastened to the combustor casing. Each casing support member comprises a casing stop seat fixed on the combustor casing and a replaceable casing stop, detachably coupled to the casing stop seat.