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    • 3. 发明授权
    • Methods for fabricating a wafer structure having a strained silicon utility layer
    • 用于制造具有应变硅实用层的晶片结构的方法
    • US07465646B2
    • 2008-12-16
    • US11080936
    • 2005-03-14
    • Yves-Matthieu Le Vaillant
    • Yves-Matthieu Le Vaillant
    • H01L21/30
    • H01L21/02032H01L21/02381H01L21/0245H01L21/02502H01L21/02532H01L21/02658H01L21/02664
    • Methods for fabricating a wafer structure having a strained silicon utility layer are described. In an embodiment, the method includes providing a prototype wafer having at least a support substrate and a strained silicon model layer upon the support substrate, and then providing a relaxed silicon-germanium layer on the strained silicon model layer. Next, a strained silicon utility layer is provided on the relaxed silicon-germanium layer to form an intermediate structure. The strained silicon utility layer has substantially the same characteristics as the strained silicon model layer. The method also includes detaching the strained silicon utility layer from the intermediate structure at a predetermined zone of weakness in the relaxed silicon-germanium layer to form a wafer structure having a strained silicon utility layer.
    • 描述了制造具有应变硅实用层的晶片结构的方法。 在一个实施例中,该方法包括提供在支撑衬底上具有至少支撑衬底和应变硅模型层的原型晶片,然后在应变硅模型层上提供松弛的硅 - 锗层。 接下来,在松散的硅 - 锗层上提供应变硅实用层以形成中间结构。 应变硅实用层具有与应变硅模型层基本相同的特性。 该方法还包括在松弛的硅 - 锗层中的预定弱化区域将应变硅应用层从中间结构分离,以形成具有应变硅实用层的晶片结构。
    • 8. 发明申请
    • SUBSTRATE WITH DETERMINATE THERMAL EXPANSION COEFFICIENT
    • 具有确定热膨胀系数的基板
    • US20110094668A1
    • 2011-04-28
    • US12983543
    • 2011-01-03
    • Yves-Matthieu Le Vaillant
    • Yves-Matthieu Le Vaillant
    • B32B38/10C30B25/02C30B23/02
    • H01L21/76254C30B25/18
    • A process for reducing defects during formation of a transfer layer on a composite support having a central layer with a first thermal expansion coefficient. The method includes providing the composite support with at least one pair of lateral layers about the central layer, with the layers of each pair having second thermal expansion coefficients and thicknesses that are substantially identical to one another to thus provide the composite support with an overall thermal expansion coefficient that is sufficiently close to that of the transfer layer; conducting crystalline growth of the transfer layer on a growth substrate; bonding the transfer layer to the composite support; and removing the growth substrate to provide the transfer layer on the composite support without generating an excessive number of defects in the transfer layer due to the matching of the overall thermal expansion coefficients of the composite substrate and transfer layer.
    • 一种在具有第一热膨胀系数的中心层的复合载体上形成转移层期间减少缺陷的方法。 该方法包括为复合载体提供围绕中心层的至少一对横向层,每对层具有彼此基本相同的第二热膨胀系数和厚度,从而为复合载体提供整体热 膨胀系数足够接近转印层的膨胀系数; 在生长衬底上进行转移层的结晶生长; 将转移层粘合到复合载体上; 并且除去生长衬底以在复合衬底上提供转印层,而不会由于复合衬底和转印层的总热膨胀系数的匹配而在转印层中产生过多的缺陷。
    • 10. 发明授权
    • Substrate with determinate thermal expansion coefficient
    • 具有确定的热膨胀系数的基体
    • US07887936B2
    • 2011-02-15
    • US11472663
    • 2006-06-21
    • Yves-Matthieu Le Vaillant
    • Yves-Matthieu Le Vaillant
    • B32B9/04B32B13/04B32B9/00B32B19/00
    • H01L21/76254C30B25/18
    • A composite support designed to successfully receive a transfer layer made of a crystalline material so that the assembly forms an epitaxy substrate, with the support having a longitudinal plane of symmetry parallel to its principal surfaces and a plurality of layers. The support includes a central first layer having a first thermal expansion coefficient at a specified temperature T and extending transversely on either side of the plane of symmetry and at least one pair of lateral layers. The layers of each pair, one with respect to the other, have arrangements in the composite support that are substantially symmetrical with respect to the plane of symmetry; second thermal expansion coefficients at the temperature T that are substantially identical to one another; and thicknesses that are substantially identical to one another. The layers of the support are made of materials that are chosen in such a way that the composite support has an overall thermal expansion coefficient at the temperature T that is sufficiently close to the thermal expansion coefficient of the material of the transferred layer at the temperature T to avoid generating an excessive number of defects in the transfer layer.
    • 一种复合支撑件,其被设计成成功地接收由结晶材料制成的转移层,使得所述组件形成外延衬底,所述支撑体具有平行于其主表面的纵向对称平面和多个层。 支撑体包括具有在特定温度T下的第一热膨胀系数并在对称平面的任一侧上横向延伸的中心第一层和至少一对横向层。 每对的层,一个相对于另一个,在复合载体中具有相对于对称平面基本对称的布置; 在温度T下彼此基本相同的第二热膨胀系数; 和彼此基本相同的厚度。 载体层由以下方式选择的材料制成:复合载体在温度T处具有足够接近转移层材料的热膨胀系数的总体热膨胀系数,温度T 以避免在转移层中产生过多的缺陷。