Active tip clearance control for shrouded gas turbine blades and related method

US8939715B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-8939715-B2
Application numberUS-72887010-A
CountryUS
Kind codeB2
Filing dateMar 22, 2010
Priority dateMar 22, 2010
Publication dateJan 27, 2015
Grant dateJan 27, 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 turbine bucket tip clearance control system includes a rotor assembly having a rotor supporting a plurality of axially spaced wheels, each wheel mounting an annular row of buckets, the annular row of buckets on at least one of the plurality of axially-spaced wheels having a radially outer tip shroud provided with at least one seal tooth. A stator assembly includes a radially inwardly facing, axially-stepped surface, formed with radially inner and outer seal surfaces connected by a shoulder. The stator assembly and rotor assembly are moveable axially relative to each other, enabling selective positioning of the at least one seal tooth radially opposite one of the radially inner and outer seal surfaces to thereby selectively alter a clearance gap between the at least one seal tooth and the radially inward facing axially-stepped surface.

First claim

Opening claim text (preview).

I claim: 1. A turbine bucket tip clearance control system comprising: a rotor assembly including a rotor having a plurality of axially spaced wheels, each of said axially-spaced wheels mounting an annular row of buckets, said annular row of buckets on at least one of said plurality of axially-spaced wheels having a radially outer tip shroud provided with at least one seal tooth; a stator assembly including a radially inwardly facing, axially-stepped surface arranged to be opposi…

Assignees

Inventors

Classifications

  • F01D11/22Primary

    Mechanical Engineering · mapped topic

  • Mechanical Engineering · 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 US8939715B2 cover?
A turbine bucket tip clearance control system includes a rotor assembly having a rotor supporting a plurality of axially spaced wheels, each wheel mounting an annular row of buckets, the annular row of buckets on at least one of the plurality of axially-spaced wheels having a radially outer tip shroud provided with at least one seal tooth. A stator assembly includes a radially inwardly facing, …
Who is the assignee on this patent?
Miller Harold Edward, Gen Electric
What technology area does this patent fall under?
Primary CPC classification F01D11/22. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Jan 27 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).