Turbomachine component with a parting joint, and a steam turbine comprising said turbomachine component
US-9995178-B2 · Jun 12, 2018 · US
Composite duct assembly
US8973263B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-8973263-B2 |
| Application number | US-201113094037-A |
| Country | US |
| Kind code | B2 |
| Filing date | Apr 26, 2011 |
| Priority date | Jun 12, 2007 |
| Publication date | Mar 10, 2015 |
| Grant date | Mar 10, 2015 |
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Abstract
Official abstract text for this publication.
A method of manufacturing a carbon composite duct assembly includes providing a first carbon composite fabric layer having a first section. The first section is formed into a first portion and a second portion. The first portion is separately moveable relative to the second portion. The first portion overlaps the second portion to define a first corner of the first carbon composite fabric layer. The first carbon composite fabric layer is formed into at least a portion of a duct extending along an axis.
First claim
Opening claim text (preview).
The invention claimed is: 1. A method of manufacturing a carbon composite turbine engine duct assembly, comprising: a) providing a first carbon composite fabric layer having a first section; b) forming the first section into a first portion and a second portion, the first portion separately movable relative to the second portion; c) overlapping the first portion onto the second portion to define a first corner of the first carbon composite fabric layer; d) forming the first…
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Mechanical Engineering · mapped topic
Operations & Transport · mapped topic
Mechanical Engineering · mapped topic
Operations & Transport · mapped topic
- F16L9/22Primary
Mechanical Engineering · mapped topic
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- What does patent US8973263B2 cover?
- A method of manufacturing a carbon composite duct assembly includes providing a first carbon composite fabric layer having a first section. The first section is formed into a first portion and a second portion. The first portion is separately moveable relative to the second portion. The first portion overlaps the second portion to define a first corner of the first carbon composite fabric layer…
- Who is the assignee on this patent?
- Rivera Anthony, United Technologies Corp
- What technology area does this patent fall under?
- Primary CPC classification F16L9/22. Mapped technology areas include Mechanical Engineering.
- When was this patent published?
- Publication date Tue Mar 10 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).