Sealing arrangement and gas turbine with such sealing arrangement

A sealing arrangement at the interface between a combustor and a turbine of a gas turbine is disclosed. The turbine comprises deflecting vanes (2) at its inlet, which deflecting vanes (2) are each mounted within said turbine so as to define an inner or outer diameter platform (9) and are in sealing engagement by means of an inner or outer diameter vane tooth (9a) with a seal (10) arranged at the corresponding inner or outer diameter part of the outlet of said combustor, wherein the seal (10) is movable and is pressed on said inner or outer diameter vane tooth (9a) by a differential pressure such that the pressure of the mainstream hot gas flow is a lower pressure (P2). 种在燃气涡轮机的燃烧器和涡轮机之间的接口处的密封组件，所述涡轮机包括在其入口处的偏转导叶(2)，偏转导叶(2)各安装在所述涡轮机内以便限定内径或外径平台(9)并借助于内径或外径导叶齿(9a)与布置在所述燃烧器的出口的对应的内径或外径部分处的密封件(10)密封接合，其中，所述密封件(10)可移动，并且通过压差压在所述内径或外径导叶齿(9a)上，使得主流热气体流的压力为较低的压力(P2)。