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53 条记录 (耗时 0.022 秒)

    Mold Stack, a Molding System Incorporating Same and a Method of Aligning the Mold Stack
    22.
    发明申请
    Mold Stack, a Molding System Incorporating Same and a Method of Aligning the Mold Stack 失效
    模具堆叠，与其组合的成型系统和对准模具堆叠的方法

    公开(公告)号：US20090020915A1

    公开(公告)日：2009-01-22

    申请号：US11876139

    申请日：2007-10-22

    申请人： Arnold MAI ,  Friedhelm Schmitz ,  Sven Kmoch ,  Laurent Christel Sigler

    发明人： Arnold MAI ,  Friedhelm Schmitz ,  Sven Kmoch ,  Laurent Christel Sigler

    IPC分类号： B29C45/36

    CPC分类号： B29C45/36 ,  B29C33/76 ,  B29C45/2606 ,  B29K2067/00 ,  B29K2067/046 ,  B29K2105/253

    摘要： According to embodiments of the present invention, there are provided a mold stack, a molding system incorporating same and a method of aligning the mold stack. For example, a mold stack is provided. The mold stack comprises a first molding cavity defining component, a second molding cavity defining component and a third molding cavity defining component, with the second molding cavity defining component being located, in use, in-between the first molding cavity defining component and the third molding cavity defining component. At least one of the first molding cavity defining component and the third molding cavity defining component is associated with a respective compensator, the respective compensator configured to allow the at least one of the first molding cavity defining component and the third molding cavity defining component to align itself relative to the second molding cavity defining component.

    摘要翻译： 根据本发明的实施例，提供了一种模具叠层，其结合的模制系统以及对准模具叠层的方法。 例如，提供了模具堆叠。 模具堆叠包括第一模制腔限定部件，第二模腔定义部件和第三模腔定义部件，第二模腔定义部件在使用中位于第一模腔定义部件和第三模腔之间 模腔确定部件。 第一模制腔限定部件和第三模腔限定部件中的至少一个与相应的补偿器相关联，相应的补偿器被配置为允许第一模腔定义部件和第三模腔中的至少一个限定部件对准 本身相对于第二模腔限定部件。

    Metallic component of a gas turbine installation having protective coatings
    23.
    发明授权
    Metallic component of a gas turbine installation having protective coatings 失效
    具有保护涂层的燃气轮机装置的金属部件

    公开(公告)号：US5499905A

    公开(公告)日：1996-03-19

    申请号：US406662

    申请日：1995-03-20

    申请人： Friedhelm Schmitz ,  Norbert Czech ,  Bruno Deblon

    发明人： Friedhelm Schmitz ,  Norbert Czech ,  Bruno Deblon

    IPC分类号： C23C28/02 ,  F01D5/28

    CPC分类号： C23C28/321 ,  C23C28/34 ,  C23C28/3455 ,  Y10T428/12576 ,  Y10T428/1259 ,  Y10T428/12618 ,  Y10T428/12854 ,  Y10T428/12931 ,  Y10T428/12944

    摘要： A metallic component of a gas-turbine installation is formed of a nickel-based base material and at least two coating layers superimposed on the base material for improving corrosion-resistance thereof. The coating layers include a first layer having a composition and/or thickness for resisting corrosive attack of the nickel-based base material at temperatures of 600.degree. C. to 800.degree. C. (HTCII), and a second coating layer having a composition and/or thickness for resisting corrosive attack of the base material at temperatures of 800.degree. C. to 900.degree. C. (HTCI).

    摘要翻译： 燃气轮机装置的金属部件由镍基基材和叠层在基材上的至少两层涂层形成，以提高其耐腐蚀性。 涂层包括具有用于抵抗镍基基材在600℃至800℃（HTCII）的腐蚀攻击的组成和/或厚度的第一层，以及第二涂层，其具有组成和/ /或用于抵抗基材在800℃至900℃（HTCI）的温度下的腐蚀性侵蚀的厚度。

    Highly corrosion and/or oxidation-resistant protective coating containing rhenium applied to gas turbine component surface and method thereof
    24.
    发明授权
    Highly corrosion and/or oxidation-resistant protective coating containing rhenium applied to gas turbine component surface and method thereof 失效
    含有应用于燃气轮机部件表面的铼的高度腐蚀和/或抗氧化保护涂层及其方法

    公开(公告)号：US5268238A

    公开(公告)日：1993-12-07

    申请号：US984541

    申请日：1992-12-02

    申请人： Norbert Czech ,  Friedhelm Schmitz

    发明人： Norbert Czech ,  Friedhelm Schmitz

    IPC分类号： C22C19/00 ,  C23C30/00

    CPC分类号： C23C30/00 ,  C22C19/00 ,  Y10T428/12931 ,  Y10T428/12937

    摘要： A method of protecting and a protective coating for metal components formed of nickel or cobalt-based superalloys are disclosed. The protective coating essentially consists of the following constituents (in percent by weight):1 to 20% rhenium,15 to 50% chromium,0 to 15% aluminum, the share of chromium and aluminum taken together being at least 25% and at most 53%,0.3 to 2% in total of at least one reactive element from the group consisting of the rare earths, and0 to 3% silicon,impurities, as well as the following elective components:0 to 5% hafnium,0 to 12% tungsten,0 to 10% manganese,0 to 15% tantalum,0 to 5% titanium,0 to 4% niobium, and0 to 2% zirconium,the total share of the elective components being from 0 to a maximum of 15%, and a remainder primarily being at least one of the elements iron, nickel, and cobalt. The protective coating is primarily suited for use with metal components in gas turbines and aircraft engines.

    摘要翻译： 公开了一种用于由镍或钴基超级合金形成的金属部件的保护和保护涂层的方法。 保护涂层基本上由以下成分组成（以重量百分比计）：1至20％的铼，15至50％的铬，0至15％的铝，所占的铬和铝的比例至少为25％ 53％，至少一种来自稀土元素的反应性元素和0-3％硅，杂质以及以下选择性成分的总和为0.3至2％：0至5％的铪，0至12 ％钨，0〜10％的锰，0〜15％的钽，0〜5％的钛，0〜4％的铌，0〜2％的锆，选择性成分的总量为0〜15％ ，其余主要是铁，镍和钴中的至少一种元素。 保护涂层主要适用于燃气轮机和飞机发动机中的金属部件。

    Highly corrosion and/or oxidation-resistant protective coating containing rhenium
    25.
    发明授权
    Highly corrosion and/or oxidation-resistant protective coating containing rhenium 失效
    含有RHENIUM的高抗腐蚀和/或耐氧化保护涂层

    公开(公告)号：US5154885A

    公开(公告)日：1992-10-13

    申请号：US566154

    申请日：1990-08-10

    申请人： Norbert Czech ,  Friedhelm Schmitz

    发明人： Norbert Czech ,  Friedhelm Schmitz

    IPC分类号： C22C19/00 ,  C22C38/00 ,  C22C38/58 ,  C23C30/00

    CPC分类号： C22C19/00 ,  C23C30/00 ,  Y02T50/67

    摘要： A protective coating for metal components formed of nickel or cobalt-based superalloys essentially consists of the following constituents (in percentages by weight):1 to 20% rhenium,22 to 50% chromium,0 to 15% aluminum, the share of chromium and aluminum taken together being at least 25% and at most 53%,0.3 to 2% in total of at least one reactive element from the group consisting of the rare earths, and0 to 3% silicon,impurities, as well as the following elective components:0 to 5% hafnium,0 to 12% tungsten,0 to 10% manganese,0 to 15% tantalum,0 to 5% titanium,0 to 4% niobium, and0 to 2% zirconium,the total share of the elective components being from 0 to a maximum of 15%, and a remainder primarily being at least one of the elements iron, nickel, and cobalt.

    摘要翻译： 由镍或钴基超级合金形成的金属部件的保护涂层基本上由以下组分（按重量百分比计）：1至20％铼，22至50％铬，0至15％的铝，铬的份额和 一起收集的铝至少含有25％，至多53％，0.3％至2％的至少一种来自稀土元素的反应性元素和0至3％的硅，杂质，以及以下选修 成分：0〜5％的铪，0〜12％的钨，0〜10％的锰，0〜15％的钽，0〜5％的钛，0〜4％的铌，0〜2％的锆， 选择性组分为0至最多15％，余量主要为铁，镍和钴中的至少一种元素。

    Split Mold Insert for a Molding System
    30.
    发明申请
    Split Mold Insert for a Molding System 失效
    分模模具用于成型系统

    公开(公告)号：US20080268086A1

    公开(公告)日：2008-10-30

    申请号：US11740564

    申请日：2007-04-26

    申请人： Sven Kmoch ,  Ralf Walter Fisch ,  Arnold Mai ,  Friedhelm Schmitz

    发明人： Sven Kmoch ,  Ralf Walter Fisch ,  Arnold Mai ,  Friedhelm Schmitz

    IPC分类号： B29C49/42

    CPC分类号： B29C45/332 ,  B29B2911/1402 ,  B29B2911/14026 ,  B29B2911/14033 ,  B29B2911/1404 ,  B29B2911/14106 ,  B29B2911/14133 ,  B29C45/2618 ,  B29C49/06 ,  B29K2105/253 ,  B29K2105/258 ,  Y10S425/005 ,  Y10S425/058

    摘要： According to embodiments of the present invention, there is provided a split mold insert for a molding system. A first split mold insert complementary to a second split mold insert, the first and second split mold inserts configured, in use, to form a neck region of a preform capable of being blow-molded. The first split mold insert comprises a top portion and a bottom portion; the top portion for abutting, in use, a cavity plate assembly and the bottom portion being at an opposite extreme relative to the top portion; a back portion and a face portion opposite each other, extending between the top and bottom portions, the face portion defining a molding surface defining portion for forming, in use, at least a portion of the neck region of the preform; the back portion comprising a connecting interface for connecting, in use, to a slide bar.

    摘要翻译： 根据本发明的实施例，提供了一种用于成型系统的分割模具插入件。 与第二分割模具插入件互补的第一分割模具插入件，所述第一和第二分割模具插入件在使用中构造成形成能够被吹塑的预成型件的颈部区域。 第一分割模具插入件包括顶部和底部; 用于在使用中抵靠空腔板组件并且底部相对于顶部处于相反极端的顶部; 在顶部和底部之间延伸的背部部分和面部部分，所述面部部分限定模制表面限定部分，用于在使用中形成预成型件的颈部区域的至少一部分; 后部包括用于在使用中将其连接到滑杆的连接界面。