Process for manufacturing a part of a metal matrix composite...

B - Operations – Transporting – 21 – D

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B21D 22/02 (2006.01) B22D 19/00 (2006.01) B32B 15/20 (2006.01) C22C 47/08 (2006.01)

Patent

CA 2583701

A part is manufactured from a composite material containing an aluminum alloy as a metal matrix. Blanks are prepared from a billet of the composite material, and worked on in a press, while they are held at a temperature ranging from the solidus temperature, Ta, of the aluminum alloy minus 50 (Ta - 50) deg. C to Ta deg. C. At a temperature below (Ta - 50), the blanks have too high a resistance to plastic deformation to be easily worked on. At a temperature over Ta, a liquid phase is produced and makes the blanks likely to crack easily during plastic deformation. At the specified temperature range of Ta-50 deg. C these problems are avoided and improvements in manufacture are realized.

Une pièce est fabriquée à partir d'un matériau composite contenant un alliage d'aluminium comme matrice métallique. Des flans sont préparés à partir d'une billette du matériau composite et travaillés dans une presse, tandis qu'ils sont gardés à une température allant de la température dite « solidus », Ta, de l'alliage d'aluminium moins 50 (Ta - 50) degrés Celsius à Ta degré Celsius. € une température inférieure (Ta - 50), les flancs ont une résistance trop élevée à la déformation plastique pour être facilement travaillés. € une température plus élevée que la Ta, une phase liquide est produite et rend les flancs susceptibles de se craquer facilement pendant la déformation plastique. € la plage de température précisée de Ta-50 degrés Celsius, on évite ces problèmes et on réalise des améliorations à la fabrication.

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