Combustion device for a gas turbine configured to suppress thermo-acoustical pulsations

US8991185B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-8991185-B2
Application numberUS-201113097221-A
CountryUS
Kind codeB2
Filing dateApr 29, 2011
Priority dateMay 3, 2010
Publication dateMar 31, 2015
Grant dateMar 31, 2015

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.

A combustion device ( 1 ) for a gas turbine includes portions ( 12 ) having an inner and an outer wall ( 13, 14 ) with an interposed noise absorption plate ( 15 ) having a plurality of holes ( 16 ). The combustion device ( 1 ) further has first passages ( 17 ) connecting zones between the inner wall ( 13 ) and the plate ( 15 ) to the inside of the combustion device ( 1 ) and second passages ( 21 ) for cooling the inner wall ( 13 ). The portions ( 12 ) also have an inner layer ( 22 ) between the inner wall ( 13 ) and the plate ( 15 ) defining inner chambers ( 23 ), each connected to at least a first passage ( 17 ), and an outer layer ( 24 ) between the outer wall ( 14 ) and the plate ( 15 ) defining outer chambers ( 25 ) connected to the inner chambers ( 23 ) via the holes ( 16 ) of the plate ( 15 ).

First claim

Opening claim text (preview).

We claim: 1. A combustion device for a gas turbine comprising: a portion having an inner wall and an outer wall and an interposed noise absorption plate having a plurality of holes between the inner wall and the plate, a plurality of zones being between the inner wall and the plate, the inner wall delimiting an inside of the combustion device; first passages connecting the zones between the inner wall and the plate to the inside of the combustion device; an inner layer between…

Assignees

Inventors

Classifications

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 US8991185B2 cover?
A combustion device ( 1 ) for a gas turbine includes portions ( 12 ) having an inner and an outer wall ( 13, 14 ) with an interposed noise absorption plate ( 15 ) having a plurality of holes ( 16 ). The combustion device ( 1 ) further has first passages ( 17 ) connecting zones between the inner wall ( 13 ) and the plate ( 15 ) to the inside of the combustion device ( 1 ) and second passages ( 2…
Who is the assignee on this patent?
Huber Andreas, Noiray Nicolas, Schuermans Bruno, and 2 more
What technology area does this patent fall under?
Primary CPC classification F23R3/002. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Mar 31 2015 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).