Cooling structure for recovery-type air-cooled gas turbine combustor

US9512781B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9512781-B2
Application numberUS-201113806523-A
CountryUS
Kind codeB2
Filing dateAug 10, 2011
Priority dateSep 30, 2010
Publication dateDec 6, 2016
Grant dateDec 6, 2016

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  2. Abstract

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Abstract

Official abstract text for this publication.

In a cooling structure for a recovery-type air-cooled gas turbine combustor having a recovery-type air-cooling structure that bleeds, upstream of the combustor, and pressurizes compressed air supplied from a compressor, that uses the bled and pressurized air to cool a wall, and that recovers and reuses the bled and pressurized air as combustion air for burning fuel in the combustor together with a main flow of the compressed air, wall cooling in which cooling air is supplied to cooling air passages formed in the wall of the combustor to perform cooling involves a downstream wall region, closer to a turbine, that is cooled using the bled and pressurized air as the cooling air and an upstream wall region, closer to a burner, that is cooled using, as the cooling air, bled compressed air bled from a main flow of the compressed air through a housing inner space.

First claim

Opening claim text (preview).

The invention claimed is: 1. A cooling structure for a recovery-type air-cooled gas turbine combustor comprising: first cooling passages formed in a downstream wall region of a wall of the gas turbine combustor, the first cooling passages being configured to cool the downstream wall region of the gas turbine combustor by receiving first cooling air bled from a compressed air supply passage and pressurized; and second cooling passages formed in an upstream wall region of the wall…

Assignees

Inventors

Classifications

  • F02C7/18Primary

    Mechanical Engineering · mapped topic

  • Mechanical Engineering · mapped topic

  • Mechanical Engineering · mapped topic

  • Mechanical Engineering · mapped topic

  • Mechanical Engineering · mapped topic

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What does patent US9512781B2 cover?
In a cooling structure for a recovery-type air-cooled gas turbine combustor having a recovery-type air-cooling structure that bleeds, upstream of the combustor, and pressurizes compressed air supplied from a compressor, that uses the bled and pressurized air to cool a wall, and that recovers and reuses the bled and pressurized air as combustion air for burning fuel in the combustor together wit…
Who is the assignee on this patent?
Mizukami Satoshi, Ishiguro Tatsuo, Masada Junichiro, and 9 more
What technology area does this patent fall under?
Primary CPC classification F02C7/18. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Dec 06 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).