Flow body for a gas turbine, gas turbine, method for manufacturing a flow body for a gas turbine, and method for repairing a flow body of a gas turbine
US-2024376825-A1 · Nov 14, 2024 · US
Turbine and method for separating particulates from a fluid
US8961111B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-8961111-B2 |
| Application number | US-201213342556-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jan 3, 2012 |
| Priority date | Jan 3, 2012 |
| Publication date | Feb 24, 2015 |
| Grant date | Feb 24, 2015 |
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- Title
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Abstract
Official abstract text for this publication.
According to one aspect of the invention, a turbine airfoil includes a first cavity inside the turbine airfoil configured to receive a fluid and a second cavity inside the turbine airfoil. The turbine airfoil also includes a passage inside the turbine airfoil that provides fluid communication between the first and second cavities, wherein the passage includes a curved portion configured to separate particulates from the fluid as the fluid flows through the passage.
First claim
Opening claim text (preview).
The invention claimed is: 1. A turbine airfoil comprising: a first cavity inside the turbine airfoil configured to receive a fluid; a second cavity inside the turbine airfoil; and a passage extending through the turbine airfoil from a pressure side surface to a suction side surface, the passage providing fluid communication between the first and second cavities, wherein the passage includes a straight portion, a curved portion, and a hairpin portion arranged between the straig…
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Classifications
Mechanical Engineering · mapped topic
- F01D5/187Primary
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
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Frequently asked questions
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- What does patent US8961111B2 cover?
- According to one aspect of the invention, a turbine airfoil includes a first cavity inside the turbine airfoil configured to receive a fluid and a second cavity inside the turbine airfoil. The turbine airfoil also includes a passage inside the turbine airfoil that provides fluid communication between the first and second cavities, wherein the passage includes a curved portion configured to sepa…
- Who is the assignee on this patent?
- Benson Adebukola Oluwaseun, Itzel Gary Michael, Kirtley Kevin Richard, and 1 more
- What technology area does this patent fall under?
- Primary CPC classification F01D5/187. Mapped technology areas include Mechanical Engineering.
- When was this patent published?
- Publication date Tue Feb 24 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).