초록 ▼

It is known from the prior art that holes in a workpiece are filled completely with a solder powder, which leads especially in the case of large holes to the formation of cracks within the solder due to the large volume filled in once the solder cools off after soldering. The invention provides a me

It is known from the prior art that holes in a workpiece are filled completely with a solder powder, which leads especially in the case of large holes to the formation of cracks within the solder due to the large volume filled in once the solder cools off after soldering. The invention provides a method for closing a recess of a workpiece, which allows closing an opening of a recess without the risk of crack formation, by using only a solder film for closing the recess. The solder film has a content of non-melting material and therefore is substantially less prone to form cracks.

대표청구항 ▼

The invention claimed is: 1. A turbine component, comprising: a base body comprising a nickel base super alloy base material; a blind hole or through hole in the base body; and a soldering foil including a solder material that covers the blind hole or through hole and is soldered to the base body;

The invention claimed is: 1. A turbine component, comprising: a base body comprising a nickel base super alloy base material; a blind hole or through hole in the base body; and a soldering foil including a solder material that covers the blind hole or through hole and is soldered to the base body; wherein the soldering foil comprises a pressed powder mixture of two different powders, where the first powder comprises the nickel base super alloy base material that does not melt at a soldering temperature and the second powder comprises the solder material which does melt at the soldering temperature. 2. The turbine component as claimed in claim 1, wherein the cover of the blind hole or through hole completely covers the blind hole or through hole. 3. The turbine component as claimed in claim 1, wherein the turbine component is a turbine blade or vane. 4. The turbine component as claimed in claim 1, wherein the turbine component is used in high-temperature applications. 5. The turbine component as claimed in claim 1, wherein the turbine component is used in corrosive and/or erosive environments. 6. The turbine component as claimed in claim 1, wherein the proportion by volume of the non-melting material exceeds the proportion by volume of the solder material. 7. The turbine component as claimed in claim 1, wherein the proportion by volume of the non-melting material is about 70% of the total volume of the soldering foil mixture. 8. The turbine component as claimed in claim 1, wherein the soldering foil has a thickness up to four millimeters. 9. The turbine component as claimed in claim 1, wherein the soldering foil completely fills the blind hole or through hole. 10. The turbine component as claimed in claim 1, wherein the blind hole or through hole in the region close to the surface has an encircling shoulder-like cross-sectional depression, and the soldering foil at least partially rests on a base of the cross-sectional depression. 11. A turbine component comprising: a super alloy material base body comprising at least one hole, the super alloy material processed at a heat treatment temperature; and a pressed powder soldering foil arranged over the at least one hole and soldered to the base body such that the hole is effectively sealed-off by the foil, wherein the soldering foil comprises a pressed powder mixture of the superalloy material and a solder material powder, the solder material powder exhibiting a melting temperature below the heat treatment temperature, such that the foil is soldered to the base body during heat treatment of the base body without a separate soldering step.