Patent EP0282386A1 successfully refreshed from Google Patents.
EP0282386A1
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EP
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Composite material with matrix and reinforcement fibres of carbon, and method of making the same
Assignee: Airbus Group SAS
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Filing: 1988-02-22
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Granted: —
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Expires: 2008-02-22
Abstract
Abstract Composite material with matrix and reinforcing fibres of carbon and its production process. The composite material according to the invention comprises a substrate (2) of carbon fibres covered with a fine silicon carbide coating (6) and embedded in a carbon matrix (4) containing 2 to 10% by weight silicon carbide, an outer silicon carbide covering (10), followed by a first filling of the cracks with silica (14) and a second filling with borosilicate glass (16) (SiO2-B2O3). This unoxidizable material can in particular be used as a heat shield for a spacecraft.
Inventors
- 👤 Gérard Rousseau
- 👤 Nicole Pastureau
Bibliographic Details
Application Number
—
Jurisdiction
EP
Data Source
google_patents
Last Synchronized
2026-10-23 13:45
CPC Classifications
C; C04; C04B; C04B41/00; C04B41/009; C04B35/00; C04B35/515; C04B35/52; C04B35/524; C04B35/622; C04B35/626; C04B35/628; C04B35/62844; C04B35/62857; C04B35/6286; C04B35/62863; C04B35/62884; C04B35/62894; C04B35/62897; C04B35/71; C04B35/78; C04B35/80; C04B35/83; C04B41/45; C04B41/52; C04B41/80; C04B41/81; C04B41/89; C04B2235/00; C04B2235/02; C04B2235/30; C04B2235/38; C04B2235/3817; C04B2235/3826; C04B2235/48; C04B2235/483; C04B2235/50; C04B2235/52; C04B2235/5208; C04B2235/5216; C04B2235/524; C04B2235/5248; C04B2235/5252; C04B2235/70; C04B2235/74; C04B2235/77; Y; Y10; Y10T; Y10T428/00; Y10T428/23; Y10T428/29; Y10T428/2913; Y10T428/2915; Y10T428/2918; Y10T428/292; Y10T428/2933; Y10T428/2938; Y10T428/30
Claims Analysis
Total Claims: 0
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References Cited (Backward Citations)
FR1594182A
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FR2104563A5
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US4425407A
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