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METHOD OF INCREASING FATIGUE LIMIT AND TENACITY OF HIGH STRENGTH ALUMINUM ALLOY

机译:提高高强度铝合金疲劳极限和强度的方法

摘要

The invention relates to a method for the object of the characteristics of fatigue and tenacity alloys of al wrought to the processes using a treatment thermomechanical practice on the product cast and optionally homogenized. / p & & p & it comprises the following steps: / p & & p & a.coulee of an initial product according to an axis xx by a method known; / p & & p & b.homogeneisation any; / p & & p & c.refoulement is hot, then to the press, along the axis xx, with a rate of delivery (final initialelongueur length along the axis xx) 1,4; / p & & p & d.etirage when hot in the direction of the axis xx, with a deformation ratio (initialesection final counted transverse cross section perpendicular to axis xx) 1,5; / p & & p & e.compression hot along an axis perpendicular to the axis xx, with a degree of reduction (cross section of the initial - finalesection initial transverse cross section) 15; / p & & p & f.laminage, extrusion or forging in the usual conditions, as well as the operations usual quenching and tempering with relaxation any of the stresses of deformation (state t6, t651 or t652 for example). / p & & p & for mechanical equivalent characteristics, it makes it possible to increase up to 50 about the characteristics of fatigue or tenacity for the treatment.
机译:本发明涉及一种方法,该方法的目的是通过对铸件进行产品热处理并任选地均质化的方法来加工的疲劳和韧性合金的特性。 & &它包括以下步骤: & & a。通过已知方法根据轴xx提取初始产品; & & b。均质化; & & c。驱回很热,然后沿xx轴压向压机,输送速度为(沿xx轴的最终初始伸长长度)1,4; & & d。沿xx轴方向变热时的堆积,变形比(初始横截面的最终计数垂直于xx轴的横截面)为1.5; & & e。沿垂直于轴线xx的轴线压缩,压缩程度减小(初始横截面-最终横截面初始横截面)15; & & f。在常规条件下进行分层,挤压或锻造,以及在松弛下进行任何常规的淬火和回火操作(例如,状态t6,t651或t652)。 & &对于机械等效特性,可使疲劳或韧性特性增加至多50。

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