Resistance spot welding system and method
US-9844831-B2 · Dec 19, 2017 · US
US9114476B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9114476-B2 |
| Application number | US-201113185627-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jul 19, 2011 |
| Priority date | Jul 28, 2010 |
| Publication date | Aug 25, 2015 |
| Grant date | Aug 25, 2015 |
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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.
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What is claimed is: 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 b…
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
Operations & Transport · mapped topic
Mechanical Engineering · mapped topic
Operations & Transport · mapped topic
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