Fiber-based ablative and high temperature pre-preg material
Number of patents in Portfolio can not be more than 2000
United States of America Patent
Stats
-
Jun 2, 2015
Grant Date -
Dec 9, 2010
app pub date -
Jan 28, 2009
filing date -
Jan 28, 2008
priority date (Note) -
In Force
status (Latency Note)
Importance
Abstract
A fabric-matrix composite structure [10] for making parts [13] suitable for use in hostile, high-temperature environments, such as rocket exhaust nozzles. The structure [10] includes a fabric [11] formed of polyacrylonitrile fiber, especially a polyacrylonitrile fiber that has been oxidized, and especially a combination of polyacrylonitrile fibers that have been oxidized to different degrees. The structure [10] also includes a binder [12] that impregnates the fabric [11]. The binder [12] might be a phenolic resin. The structure is formed [30], partially cured [40], formed into a product [50], and finish cured [60].
First Claim
Family
International Classification(s)
- [Classification Symbol]
- [Patents Count]
Cited Art Landscape
Patent Citation Ranking
Recipient Email Address
Recipient Email Address
Comment
Recipient Email Address
Add to Portfolio(s)
To add this patent to one, or more, of your portfolios, simply click the add button.
This Patent is in these Portfolios:
Add to additional portfolios:
Last Refreshed On:
Changes done successfully