Blade tip coating that can be rubbed off

US9260784B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9260784-B2
Application numberUS-201013384462-A
CountryUS
Kind codeB2
Filing dateJul 31, 2010
Priority dateAug 6, 2009
Publication dateFeb 16, 2016
Grant dateFeb 16, 2016

How to read this patent

A practical reading order for non-experts. Skip the full description unless you need deep technical detail.

  1. Title

    What the patent document calls the invention.

  2. Abstract

    A short plain-language summary of the technical disclosure.

  3. Assignees and inventors

    Who owns or filed the patent and who is credited as inventor.

  4. Key dates

    Filing, priority, publication, and grant dates set the timeline.

  5. First independent claim

    The legal scope of protection — read this for what is actually claimed.

  6. CPC / IPC classifications

    Technology tags used to group this patent with similar filings.

  7. Citations and related patents

    Prior art links and similar publications in this corpus.

Abstract

Official abstract text for this publication.

The present invention relates to a method for producing a component, in particular a blade for a gas turbine, wherein a main body ( 2 ) is provided, to which a running-in layer ( 6 ) is applied, which can be worn away at least partially during operation to form an accurately fitting surface ( 11 ), wherein the running-in layer is applied by kinetic cold-gas compacting, and a component, in particular a blade for a gas turbine, comprising a main body, to which a running-in layer is applied, which can be worn away at least partially during operation to form an accurately fitting surface, wherein the running-in layer is a porous layer made of a Ti alloy.

First claim

Opening claim text (preview).

The invention claimed is: 1. A method for producing a blade for a gas turbine, the method comprising the steps of: providing a main body ( 2 ) having a blade tip, applying onto the main body ( 2 ) a running-in layer ( 6 ), which can be rubbed away at least partially to form an accurately fitting surface ( 11 ) during operation, wherein the running-in layer is applied by kinetic cold-gas compacting; the running-in layer is introduced on the blade tip; and wherein the running…

Assignees

Inventors

Classifications

  • Mechanical Engineering · mapped topic

  • C23C24/04Primary

    Chemistry & Metallurgy · mapped topic

  • Mechanical Engineering · mapped topic

  • Cross-Sectional Technologies · mapped topic

  • Cross-Sectional Technologies · mapped topic

Patent family

Related publications grouped by family.

External sources

Next steps

Free tools are coming soon. Tell us what you want to track and we'll notify you.

Frequently asked questions

Answers are generated from the same data shown on this page.

What does patent US9260784B2 cover?
The present invention relates to a method for producing a component, in particular a blade for a gas turbine, wherein a main body ( 2 ) is provided, to which a running-in layer ( 6 ) is applied, which can be worn away at least partially during operation to form an accurately fitting surface ( 11 ), wherein the running-in layer is applied by kinetic cold-gas compacting, and a component, in parti…
Who is the assignee on this patent?
Jakimov Andreas, Schneiderbanger Stefan, Hertter Manuel, and 1 more
What technology area does this patent fall under?
Primary CPC classification C23C24/04. Mapped technology areas include Chemistry & Metallurgy.
When was this patent published?
Publication date Tue Feb 16 2016 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).