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Piece of metal matrix composite high rigidity and high stability in a longitudinal direction material.

机译:一种金属基复合材料,在纵向材料中具有高刚性和高稳定性。

摘要

An elongated piece, COMPOSITE WITH METAL MATRIX, respectively comprises between 35% and 45% by volume of alloy matrix with aluminum or magnesium, and between 65% and 55% fiber volume ONGOING CARBON PARALLEL TO layered length. At least about 90% of the carbon fibers are fibers with a module ULTRA HIGH. IN BETWEEN 25% AND 60% OF LAYERS, these fibers are oriented at 0 ° +/- 5 ° to the longitudinal direction of the piece when the matrix is ​​aluminum base. IN OTHER COATS, THEN ARE ORIENTED FIBERS BETWEEN +/- 20 ° to +/- 40 ° to this direction. WHEN THE WOMB IS BASED MAGNESIUM FIBER MODULE WITH ULTRA HIGH 0 ° are aimed at +/- 5 ° by at least 90% of the layers. This results in a high rigidity and high stability at the above address, favoring the applications in the space industry.
机译:细长的金属复合材料片,分别包含35%至45%体积的铝或镁合金基体,以及65%至55%的纤维体积的连续碳平行层长。至少约90%的碳纤维是具有超高模量的纤维。在基质为铝基的情况下,在25%和60%的层之间,这些纤维相对于片的纵向方向为0°+/- 5°。在其他涂层中,则将纤维定向在此方向的+/- 20°至+/- 40°之间。当基于胎面的超高镁纤维模块时,至少90%的层瞄准+/- 5°。这导致上述地址的高刚性和高稳定性,有利于航天工业中的应用。

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