초록 ▼

The invention relates to a high-pressure compressor of a gas turbine having at least one blisk, specifically a disk with a plurality of blades that are disposed on the disk, wherein the blisk has at least one titanium material from the group that comprises Ti-6246 and Ti-6242, wherein the materials

The invention relates to a high-pressure compressor of a gas turbine having at least one blisk, specifically a disk with a plurality of blades that are disposed on the disk, wherein the blisk has at least one titanium material from the group that comprises Ti-6246 and Ti-6242, wherein the materials of the disk and the blades of the blisk differ in their chemical composition and/or their microstructure. The blades are welded to the disk, in particular, by means of a pressure welding method supported by high-frequency current, whereby the current is conducted through the joint surfaces and leads to local limited melting therein.

대표청구항 ▼

1. A method for the production of an integrally bladed rotor of a high-pressure compressor having a compression ratio of more than 30 to 1, the method comprising the steps of: providing a disk that is formed from Ti-6246 or lamellar Ti-6246;providing blades that are formed from Ti-6242 or bimodal Ti

1. A method for the production of an integrally bladed rotor of a high-pressure compressor having a compression ratio of more than 30 to 1, the method comprising the steps of: providing a disk that is formed from Ti-6246 or lamellar Ti-6246;providing blades that are formed from Ti-6242 or bimodal Ti-6246, the blades having joint surfaces that can each be secured to respective joint surfaces on the disk;heating and melting the joint surface on one of the blades and the respective joint surface on the disk by direct high frequency pressure welding, the step of heating and melting the joint surfaces further comprising the steps of: disposing one of the blades at a distance of 0.5 mm to 1 mm from the disk, at the same time electrically connecting the respective blade and the disk in series and conducting a high frequency current in the range of 0.75 MHz to 2.5 MHz in the respective blade and the disk, whereby a skin effect of the current and a proximity effect of the blade and the disk cause local melting in the region of the respective joint surfaces; andafter the step of heating and melting, pressing the joint surface of the respective blade in a linear path onto the respective joint surface on the disk, the linear path being perpendicular to the respective joint surface of the blade, and the linear path being perpendicular to the respective joint surface of the disk. 2. A method for the production of an integrally bladed rotor of a high-pressure compressor, the method comprising the steps of: providing a disk that is configured for use on a high-pressure compressor, the disk being formed from Ti-6246;providing a plurality of blades that are configured for use on a high-pressure compressor, the blades being formed from Ti-6242 or Ti-6246; andwelding each blade to the disk at joint surfaces by means of a conductive high-frequency pressure welding method supported by high-frequency current in the range of 0.75 MHz to 2.5 MHz;wherein the step of welding further comprises arranging electrodes on the disk and at least one of the blades, connecting the disk and the at least one of the blades in series in an electrical circuit, disposing the disk and the at least one of the blades between 0.5 mm to 1 mm apart so that a skin effect and a proximity effect of the high-frequency current leads to local heating and local melting of the joint surfaces;wherein the disk and the at least one of the blades are connected in series in an electrical circuit when they are disposed between 0.5 mm to 1 mm apart; andwherein the step of welding further comprises pressing the joint surface of the respective blade in a linear path onto the respective joint surface on the disk, the linear path being perpendicular to the respective joint surface of the blade, and the linear path being perpendicular to the respective joint surface of the disk. 3. The method of claim 2, wherein in the step of providing a disk, the disk has a lamellar structure. 4. The method of claim 2, wherein the step of providing a plurality of blades, the blades have a bimodal structure.