초록 ▼

A component of a turbine includes a vane, a carrier element and at least four interfaces between the vane and the carrier element. The at least four interfaces are sealed via leaf seals. A method for sealing against leakage between a vane and a carrier element of the above-mentioned turbine componen

A component of a turbine includes a vane, a carrier element and at least four interfaces between the vane and the carrier element. The at least four interfaces are sealed via leaf seals. A method for sealing against leakage between a vane and a carrier element of the above-mentioned turbine component includes sealing the at least four interfaces by way of leaf seals.

대표청구항 ▼

1. A component of a turbine comprising: a vane,a carrier element, andat least four interfaces between the vane and the carrier element, wherein the at least four interfaces are sealed via respective four leaf seals,wherein the leaf seals are connected to the vane and/or to the carrier element,wherei

1. A component of a turbine comprising: a vane,a carrier element, andat least four interfaces between the vane and the carrier element, wherein the at least four interfaces are sealed via respective four leaf seals,wherein the leaf seals are connected to the vane and/or to the carrier element,wherein at least one leaf seal is connected to the vane and/or to the carrier element such that a movement between the vane and the carrier element is possible,wherein the turbine comprises a rotation axis and at least one leaf seal is connected to the vane and/or to the carrier element such that a movement between the vane and the carrier element in axial and/or tangential and/or radial direction is possible,wherein the vane comprises a radially inner platform having an underside,wherein at least two of the interfaces are located at the radially inner platform,wherein an impingement plate is located at the underside of the radially inner platform,wherein the impingement plate includes a plurality of openings therethrough that facilitate cooling the underside of the radially inner platform,wherein at least one of the leaf seals that seals one of the at least two interfaces comprises at least one opening configured to supply a cooling medium to the underside of the radially inner platform,wherein the at least one opening in the at least one leaf seal is smaller than at least one of the openings through the impingement plate. 2. A method for sealing against leakage between a vane and a carrier element of a turbine component, wherein the turbine comprises a rotation axis,wherein the turbine component comprises at least four interfaces between the vane and the carrier element, the method comprising: sealing the at least four interfaces via respective four leaf seals, wherein the leaf seals are connected to the vane and/or to the carrier element,wherein at least one leaf seal is connected to the vane and/or to the carrier element such that a movement between the vane and the carrier element is possible,wherein the at least one leaf seal is connected to the vane and/or to the carrier element such that a movement between the vane and the carrier element in axial and/or tangential and/or radial direction is possible,wherein the vane comprises a radially inner platform having an underside,wherein at least two of the interfaces are located at the radially inner platform,wherein an impingement plate is located at the underside of the radially inner platform,wherein the impingement plate includes a plurality of openings therethrough that facilitate cooling the underside of the radially inner platform,wherein at least one of the leaf seals that seals one of the at least two interfaces comprises at least one opening,wherein the at least one opening in the at least one leaf seal is smaller than at least one of the openings through the impingement plate,supply a cooling medium through the at least one opening in the at least one of the leaf seals to the underside of the radially inner platform.