Workpiece with a recess which is closed from the exterior by means of a solder film and method for closing a recess by means of a solder film

Abstract

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.

Description

FIELD OF INVENTION

The present invention relates to a workpiece in accordance with the preamble of claim 1 and to a method for closing a recess.

BACKGROUND OF INVENTION

Soldering foils are used, for example, to cohesively join components, as is known from U.S. Pat. No. 5,557,837. In this case, the soldering foil, which consists of a soldering material whose melting point is significantly below the melting point of the components to be joined to one another, is melted and joins a non-melting insert part which is fitted into a recess in another component.

It is also known to fill cracks or openings with solder powder, with the solder powder being piled up above the crack or opening and being melted by the supply of heat so that it runs into the crack or opening, as is known, for example, from U.S. Pat. No. 4,098,450. In particular if large recesses are to be filled, the shrinkage involved in solidification often gives rise to cracks during cooling of the solder. The solder may undesirably penetrate into the interior of hollow bodies (e.g. a hollow turbine blade or vane) which are provided with a hole which is to be closed up.

It is also known to use soldering foils to coat materials, for example from U.S. Pat. No. 5,968,299.

In particular in the case of castings, such as for example turbine blades or vanes (cast, directionally solidified, single-crystalline), for manufacturing reasons there are in many cases blind bores or through-holes which need to be closed up since, for example, cooling air would otherwise escape in an undesired way from the interior of the turbine blade or vane through these holes, which reduces the efficiency of the turbine.

SUMMARY OF INVENTION

It is an object of the invention to develop a workpiece of the generic type in such a way that its recesses have crack-free closures, and to provide a method for closing up recesses in a workpiece which can be carried out in a simple way.

This object is achieved, with regard to the workpiece, by the characterizing features of patent claim 1. Advantageous refinements will emerge from the dependent claims. According to the invention, a method for closing off recesses has the features of patent claim 13 and can advantageously be developed further by the features of claim 14.

The invention provides for the workpiece to have a soldering foil which covers the respective opening of the recess and, at least in the edge region of the recess, is soldered to the base body at a surface of the workpiece. In this context, it is important that the soldering surface only partially comprises solder material in order to avoid cracks during the solidification which follows the soldering.

The recess may be a blind bore or a through-hole, so that various types of recesses are advantageously closed off by the soldering foil.

The workpiece may advantageously be a turbine blade or vane for use in the high-temperature region of a turbine or gas turbine in a cohesive and erosive environment.

The composition of the soldering foil comprising base material and solder is adapted to the workpiece and the operating conditions envisaged and/or the size of the recess, so that the recess also remains closed throughout the duration of use of the workpiece.

The soldering foil may advantageously be up to four millimeters thick, so that sufficient mechanical stability is ensured and even large holes are closed off in a sealed manner by the soldering foil.

If the supply of heat for closing off the recess, i.e. for melting the solder material, is provided during a heat treatment of the workpiece, in particular during a precipitation hardening or solution annealing of the workpiece, there is no need for a separate method step to join soldering foil and workpiece.

BRIEF DESCRIPTION OF THE DRAWINGS

A plurality of exemplary embodiments of the workpiece according to the invention and/or the method according to the invention are illustrated in the figures and are explained in more detail below together with further details of the invention.

In the drawing:

FIGS. 1 a, b, c show two exemplary embodiments of a workpiece according to the invention,

FIG. 2 shows a further exemplary embodiment of a workpiece according to the invention,

FIGS. 3 a to c show various method steps involved in closing off a recess in a workpiece using a soldering foil, and

FIGS. 4 a, b show complete filling of a recess.

DETAILED DESCRIPTION OF INVENTION

FIG. 1 a shows a workpiece 1 comprising a base body 2 which has at least one recess 4, for example a blind bore 5.

A soldering foil 7 is laid over this blind hole 5 on a surface 6 of the workpiece 1. The soldering foil 7 is soldered onto the surface 6 by a subsequent treatment at elevated temperatures, so that there is a cohesive closed join between soldering foil 7 and workpiece 1 or base body 2.

FIG. 1 b shows a plan view of the recess 4, 5 shown in FIG. 1a with the soldering foil 7 applied to it.

The opening cross section or an opening 3 in the blind bore 5 is indicated by dashed lines. The outer contour of the soldering foil 7 is matched to the opening cross section of the blind bore 4 and at least partially projects beyond the opening cross section of the blind bore 5, so that it at least partially rests on the surface 6 in a bearing region 8. In this bearing region 8, there is a good join between soldering foil 7 and workpiece 1 after a soldering operation.

FIG. 1 c, proceeding from FIG. 1a, shows a further exemplary embodiment, in which the blind bore 5 has, for example, a stepped cross-sectional widening 10, in the region close to the surface, introduced while the blind bore was being produced or subsequently. The soldering foil 7 is laid in a closely fitting manner into this cross-sectional widening 10, so that the soldering foil 7 at least partially rests on the base of the, for example, annularly encircling depression created in this way and consequently a smooth surface 6 is restored after the soldering operation. The soldering foil 7, which is of thin design and therefore includes much less material than a plug which fills the recess 4, 5, has little tendency to form cracks during cooling, i.e. during shrinkage.

FIG. 2 shows a further exemplary embodiment of a workpiece according to the invention. Unlike in FIG. 1a, the workpiece 1 does not include a blind bore, but rather has a through hole 13, the opening 3 of which is closed off by the soldering foil 7.

FIGS. 3 a to c illustrate method steps involved in the production of a workpiece 1 with a closed recess 4, 5, 13.

FIG. 3 a shows a workpiece 1 having, for example, a blind bore 5. A correspondingly stamped-out or cut-out soldering foil 7 is laid onto the blind bore 5 at room temperature RT, as illustrated in FIG. 3b. The workpiece 1 with the soldering foil 7 laid onto it, in order to subject the base material of the base body 2 or of the workpiece 1, to, for example, a precipitation hardening treatment, is exposed to a heat treatment at elevated temperatures (HT), in the course of which the soldering foil is joined to the workpiece 1 so that a cavity 16 which is closed off with respect to the outside is formed beneath the soldering foil 7.

It is not necessarily the case that the entire workpiece 1 with the soldering foil 7 has to be subjected to a heat treatment at elevated temperatures. By way of example, it is sufficient for the bearing region 8 of the soldering foils 7, which rests on the surface 6 (FIG. 1b), to be heated, for example by a laser treatment or other energy-introducing methods, in such a way that soldering takes place in this region between soldering foil 7 and surface 6.

The composition of the soldering foil 7 consists, for example, of the base material of the workpiece 1 and a solder material, which can be matched to the prevailing operating conditions, such as for example in the high-temperature range, corrosive and/or erosive environment, of the workpiece 1. The composition and dimensions of the soldering foil, which consists, for example, of pressed, fine-particle material, are selected in such a way that they are also able to withstand the mechanical loads which occur in use. The soldering foil contains a high proportion of the base material, which does not melt under the soldering conditions, or of another, correspondingly high-melting material, and a small proportion of melting solder material. The proportion by volume of the material which does not melt exceeds the proportion by volume of the melting soldering material and is expediently over 60%, and in particular is 70%. Greater proportions are also possible, for example 80% or 90%. This composition and the temperature (soldering temperature) at which soldering is carried out are selected in such a way that the solder just melts and ensures a good join between soldering foil 7 and workpiece 1. Melting of the solder material causes the individual grains of the pressed, non-melting powder of the soldering foil 7 to be joined together. On account of the added non-melting material, the soldering foil 7 is still so viscous at the soldering temperature, i.e. has such a high viscosity, that there is little if any sinking of this material into the recess 4, 5, 13. However, the soldering foil 7 does not necessarily have to contain a proportion of the base material of the workpiece 1. The high proportion of non-melting material, with the remainder melting solder, in the soldering foil 7 in particular prevents the formation of cracks.

FIGS. 4 a, b show a workpiece 1 in which a blind bore 5 is completely filled by a soldering foil 7.

In this case, a soldering foil 7 is, for example, placed in an approximately tight-fitting manner into the blind bore 5, i.e. its dimensions in cross section correspond to the blind bore 5. The height of the soldering foil 7 is such that, after at least partial melting in the edge region of the soldering foil 7, there is as far as possible no material projecting at the surface 6 (FIG. 4b).

However, the soldering foil 7 does not necessarily have to be placed into the recess 4, 5. It is merely necessary for the mass of soldering foil 7 to be such that the melted soldering foil 7 penetrates into and fills the recess 4, 5. In this case, the composition of the soldering foil 7 comprising base material and solder material, and its resultant viscosity at the soldering temperature, are selected in such a way that the solder material and the base material can penetrate into the recess 4 and completely fill it.

The advantage of the soldering foil 7 is that the soldering foil 7 has a very high density compared to a paste or a bed of powder and the mass introduced can be measured very accurately by selection of the size of the soldering foil 7, and consequently the shrinkage is minimal and the formation of cracks is reproducibly prevented or at least reduced.

The workpiece 1 is, for example, a turbine blade or vane, consisting, for example, of a nickel-base superalloy.

By way of example after its production or during refurbishment (restoration of a used workpiece), the workpiece 1 has to be subjected to particular heat treatments in order to attain certain materials properties.

If the entire workpiece 1 is heated together with the soldering foil 7 during a heat treatment of this type, in order to externally close off the recess 4 or to completely fill it with a solder material, the composition of the soldering foil 7 can be selected in such a way that during this heat treatment, which is intended, for example, to effect solution annealing or precipitation hardening of the workpiece 1, the solder material is also melted, and consequently there is no need for a separate thermal method step for soldering purposes during production of the workpiece 1.

Claims

1-14. (canceled)

15. A turbine component, comprising: a base body having an exterior surface; 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.

16. The turbine component as claimed in claim 15, wherein the cover of the blind hole or through hole completely covers the blind hole or through hole.

17. The turbine component as claimed in claim 15, wherein the turbine component is a turbine blade or vane.

18. The turbine component as claimed in claim 15, wherein the turbine component is used in high-temperature applications.

19. The turbine component as claimed in claim 15, wherein the turbine component is used in corrosive and/or erosive environments.

20. The turbine component as claimed in claim 15, wherein the soldering foil is a mixture of a material that does not melt at the soldering temperature and a solder material which does melt at the soldering temperature.

21. The turbine component as claimed in claim 15, wherein the material in the mixture that does not melt at the soldering temperature is the base material of the turbine component.

22. The turbine component as claimed in claim 15, wherein the proportion by volume of the non-melting material exceeds the proportion by volume of the solder material.

23. The turbine component as claimed in claim 15, wherein the proportion by volume of the non-melting material is about 70% of the total volume of the soldering foil mixture.

24. The turbine component as claimed in claim 15, wherein the soldering foil has a thickness up to four millimeters.

25. The turbine component as claimed in claim 15, wherein the base material of the base body is a nickel-base superalloy.

26. The turbine component as claimed in claim 15, wherein the soldering foil completely fills the blind hole or through hole.

27. The turbine component as claimed in claim 15, 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.

28. A method for closing a blind hole or through hole opening on a surface of a turbine component, comprising: covering the blind hole or through hole, or at least partially filling the blind hole or through hole with a soldering foil; and soldering the soldering foil to the turbine component with the soldering foil.

29. The method as claimed in claim 28, wherein the soldering heat is applied by a heat treatment of the turbine component.

30. The method as claimed in claim 28, wherein the soldering foil includes a soldering material.

31. The method as claimed in claim 28, wherein the soldering heat is applied by precipitation hardening or solution annealing of the turbine component.