Lean premix burner of a gas-turbine engine provided with a flow-guiding element

US8943829B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-8943829-B2
Application numberUS-201113098621-A
CountryUS
Kind codeB2
Filing dateMay 2, 2011
Priority dateMay 7, 2010
Publication dateFeb 3, 2015
Grant dateFeb 3, 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.

This invention relates to a lean premix burner of a gas-turbine engine with an annular central body 2 , which, while being essentially concentric to a burner center axis 1 , is connected to a film applicator 3 , which conically widens at the fuel exit side, as well as to an outer ring 4 concentrically arranged to the burner center axis 1 and surrounding at least the film applicator 3 at a certain distance, characterized in that an annular flow-guiding element 6 is provided in an annular duct 5 formed between the outer ring 4 and the film applicator 3 which, in the axial direction of the annular duct 5 , is at least partly situated outside of the outer ring 4.

First claim

Opening claim text (preview).

What is claimed is: 1. A lean premix burner of a gas-turbine engine, comprising: an annular central body being essentially concentric to a burner center axis, a film applicator having a conical film application surface for supplying with fuel from a fuel exit opening, the film application surface having a fuel flow off edge at a downstream area; the film application surface conically widening between a conical surface upstream of the fuel exit opening and to the fuel flow off ed…

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 US8943829B2 cover?
This invention relates to a lean premix burner of a gas-turbine engine with an annular central body 2 , which, while being essentially concentric to a burner center axis 1 , is connected to a film applicator 3 , which conically widens at the fuel exit side, as well as to an outer ring 4 concentrically arranged to the burner center axis 1 and surrounding at least the film applicator 3 a…
Who is the assignee on this patent?
Bagchi Imon-Kalyan, Lazik Waldemar, Rolls Royce Deutschland
What technology area does this patent fall under?
Primary CPC classification F23R3/286. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Feb 03 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).