Turbine overspeed protection
US-2024368999-A1 · Nov 7, 2024 · US
Turbomachine casing assembly
US8926263B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-8926263-B2 |
| Application number | US-201213358080-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jan 25, 2012 |
| Priority date | Mar 4, 2011 |
| Publication date | Jan 6, 2015 |
| Grant date | Jan 6, 2015 |
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- Title
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- Abstract
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Abstract
Official abstract text for this publication.
A turbomachine casing assembly including: a first casing element arrangeable adjacent to one or more rotating aerofoil structures of a turbomachine; a second casing element provided at a radially outer position with respect to the first casing element; and an infill member disposed between the first and second casing elements, wherein an end of the infill member is set back from an end of the first casing element such that a void is provided between the first and second casing elements.
First claim
Opening claim text (preview).
The invention claimed is: 1. A turbomachine casing assembly comprising: a first casing element arrangeable adjacent to one or more rotating aerofoil structures of a turbomachine; a second casing element provided at a radially outer position with respect to the first casing element; and a liner arranged between the first and second casing elements, wherein an infill member disposed between the first and second casing elements is arranged between the liner and the first casing…
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Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
Cross-Sectional Technologies · mapped topic
- F01D21/045Primary
Mechanical Engineering · mapped topic
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Frequently asked questions
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- What does patent US8926263B2 cover?
- A turbomachine casing assembly including: a first casing element arrangeable adjacent to one or more rotating aerofoil structures of a turbomachine; a second casing element provided at a radially outer position with respect to the first casing element; and an infill member disposed between the first and second casing elements, wherein an end of the infill member is set back from an end of the f…
- Who is the assignee on this patent?
- Reed Julian M, Harper Cedric B, Rolls Royce Plc
- What technology area does this patent fall under?
- Primary CPC classification F01D21/045. Mapped technology areas include Mechanical Engineering.
- When was this patent published?
- Publication date Tue Jan 06 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).