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1. 发明授权

US07052782B2 High-temperature protection layer 有权
标题翻译：高温保护层
公开(公告)号：US07052782B2
公开(公告)日：2006-05-30
申请号：US10893326
申请日：2004-07-19
申请人： Hans-Peter Bossmann , Dietrich Eckardt , Klaus Erich Schneider , Christoph Toennes
发明人： Hans-Peter Bossmann , Dietrich Eckardt , Klaus Erich Schneider , Christoph Toennes
IPC分类号： B32B15/04 , C22C19/03
CPC分类号： C23C30/00 , C23C4/073 , Y10T428/12611 , Y10T428/12937 , Y10T428/12944 , Y10T428/26
摘要： A high-temperature protection layer contains (% by weight) 23 to 27% Cr, 4 to 7% Al, 0.1 to 3% Si, 0.1 to 3% Ta, 0.2 to 2% Y, 0.001 to 0.01% B, 0.001 to 0.01% Mg and 0.001 to 0.01% Ca, remainder Ni and inevitable impurities. Optionally, the Al content is in a range from over 5 up to 6% by weight.
摘要翻译：高温保护层含有23〜27％的Cr，4〜7％的Al，0.1〜3％的Si，0.1〜3％的Ta，0.2〜2％的Y，0.001〜0.01％的B，0.001〜 0.01％Mg和0.001〜0.01％Ca，余量为Ni和不可避免的杂质。任选地，Al含量在超过5至6重量％的范围内。

2. 发明申请

US20050042474A1 High-temperature protection layer 有权
标题翻译：高温保护层
公开(公告)号：US20050042474A1
公开(公告)日：2005-02-24
申请号：US10893326
申请日：2004-07-19
申请人： Hans-Peter Bossmann , Dietrich Eckardt , Klaus Schneider , Christoph Toennes
发明人： Hans-Peter Bossmann , Dietrich Eckardt , Klaus Schneider , Christoph Toennes
IPC分类号： F01D5/18 , C22C19/05 , C23C4/073 , C23C26/00 , C23C28/00 , C23C30/00 , F01D5/28 , F01D9/02 , F02C7/00 , F23R3/42 , B32B15/01
CPC分类号： C23C30/00 , C23C4/073 , Y10T428/12611 , Y10T428/12937 , Y10T428/12944 , Y10T428/26
摘要： A high-temperature protection layer contains (% by weight) 23 to 27% Cr, 4 to 7% Al, 0.1 to 3% Si, 0.1 to 3% Ta, 0.2 to 2% Y, 0.001 to 0.01% B, 0.001 to 0.01% Mg and 0.001 to 0.01% Ca, remainder Ni and inevitable impurities. Optionally, the Al content is in a range from over 5 up to 6% by weight.
摘要翻译：高温保护层含有23〜27％的Cr，4〜7％的Al，0.1〜3％的Si，0.1〜3％的Ta，0.2〜2％的Y，0.001〜0.01％的B，0.001〜 0.01％Mg和0.001〜0.01％Ca，余量为Ni和不可避免的杂质。任选地，Al含量在超过5至6重量％的范围内。

3. 发明授权

US08252601B2 Method for designating a component having a heat insulation layer and for determining its operating time 有权
标题翻译：用于指定具有绝热层并用于确定其工作时间的部件的方法
公开(公告)号：US08252601B2
公开(公告)日：2012-08-28
申请号：US12197742
申请日：2008-08-25
申请人： Hans-Peter Bossmann , Dietrich Eckardt
发明人： Hans-Peter Bossmann , Dietrich Eckardt
IPC分类号： G01N21/00
CPC分类号： G01K3/04 , G01K11/30
摘要： A method for designating a component, coated with a heat insulation layer including zirconium dioxide (ZrO2) stabilized with yttrium oxide (Y2O3) [YSZ], and for determining its operating time or operating temperature is provided. The method includes doping the heat insulation layer and marking the doped heat insulation layer, with at least one metal oxide in at least one surface region of the component. The metal oxide is selected such that the doped region of YSZ is visible or can be made optically visible in order to designate the component. The method also includes comparing a slower or faster change in lattice parameters of the doped YSZ region, as compared with undoped YSZ, and determining the operating time of the component under temperature by comparing the lattice parameters with a known calibrating characteristic curve.
摘要翻译：提供涂覆有包含用氧化钇（Y 2 O 3）[YSZ]稳定的二氧化锆（ZrO 2）和用于确定其操作时间或操作温度的绝热层的组分的方法。该方法包括掺杂绝热层并且在该组件的至少一个表面区域中用至少一种金属氧化物标记掺杂的隔热层。选择金属氧化物使得YSZ的掺杂区域是可见的或可以被制成光学可见的以便表示该组分。该方法还包括比较与未掺杂YSZ相比掺杂YSZ区域的晶格参数更慢或更快的变化，并且通过将晶格参数与已知校准特性曲线进行比较来确定组件在温度下的操作时间。

4. 发明申请

US20090061530A1 METHOD FOR DESIGNATING A COMPONENT HAVING A HEAT INSULATION LAYER AND FOR DETERMINING ITS OPERATING TIME 有权
标题翻译：用于指定具有热绝缘层的组件并用于确定其操作时间的方法
公开(公告)号：US20090061530A1
公开(公告)日：2009-03-05
申请号：US12197742
申请日：2008-08-25
申请人： Hans-Peter Bossmann , Dietrich Eckardt
发明人： Hans-Peter Bossmann , Dietrich Eckardt
IPC分类号： G01N21/00
CPC分类号： G01K3/04 , G01K11/30
摘要： A method for designating a component, coated with a heat insulation layer including zirconium dioxide (ZrO2) stabilized with yttrium oxide (Y2O3) [YSZ], and for determining its operating time or operating temperature is provided. The method includes doping the heat insulation layer and marking the doped heat insulation layer, with at least one metal oxide in at least one surface region of the component. The metal oxide is selected such that the doped region of YSZ is visible or can be made optically visible in order to designate the component. The method also includes comparing a slower or faster change in lattice parameters of the doped YSZ region, as compared with undoped YSZ, and determining the operating time of the component under temperature by comparing the lattice parameters with a known calibrating characteristic curve.
摘要翻译：提供涂覆有包含用氧化钇（Y 2 O 3）[YSZ]稳定的二氧化锆（ZrO 2）和用于确定其操作时间或操作温度的绝热层的组分的方法。该方法包括掺杂绝热层并且在该组件的至少一个表面区域中用至少一种金属氧化物标记掺杂的隔热层。选择金属氧化物使得YSZ的掺杂区域是可见的或可以被制成光学可见的以便表示该组分。该方法还包括比较与未掺杂YSZ相比掺杂YSZ区域的晶格参数更慢或更快的变化，并且通过将晶格参数与已知校准特性曲线进行比较来确定组件在温度下的操作时间。

5. 外观设计

USD611510S1 Turbo machine blade platform 有权
标题翻译：涡轮机刀片平台
公开(公告)号：USD611510S1
公开(公告)日：2010-03-09
申请号：US29283946
申请日：2007-08-28
申请人： Alexander Anatolievich Khanin , Maxim Konter , Dietrich Eckardt , Alexander Bone
设计人： Alexander Anatolievich Khanin , Maxim Konter , Dietrich Eckardt , Alexander Bone

6. 外观设计

USD586831S1 Turbo machine double blade and platform 有权
标题翻译：涡轮机双刀片和平台
公开(公告)号：USD586831S1
公开(公告)日：2009-02-17
申请号：US29283947
申请日：2007-08-28
申请人： Alexander Anatolievich Khanin , Maxim Konter , Dietrich Eckardt , Victor Vladimirovich Odinokov
设计人： Alexander Anatolievich Khanin , Maxim Konter , Dietrich Eckardt , Victor Vladimirovich Odinokov

7. 发明授权

US4822249A Axial flow blade wheel of a gas or steam driven turbine 失效
标题翻译：气体或蒸汽驱动涡轮机的轴流叶片轮
公开(公告)号：US4822249A
公开(公告)日：1989-04-18
申请号：US946449
申请日：1986-12-23
申请人： Dietrich Eckardt , Arthur Schaffler
发明人： Dietrich Eckardt , Arthur Schaffler
IPC分类号： F01D5/14 , F04D29/68
CPC分类号： F04D29/681 , F01D5/145 , F05D2250/183 , F05D2250/184 , Y02T50/673
摘要： An axial blade wheel of a gas or steam-driven turbine comprising blades having substantially laminar boundary layer flow up to a point of maximum velocity on the upper surface of the blade, the upper surface of the blade being provided in a region downstream of the point of maximum velocity where the fluid flow velocity decreases with a spoiler edge of saw tooth profile which extends substantially over the entire blade length.
摘要翻译：气体或蒸汽驱动涡轮机的轴向叶轮包括具有基本上层流边界层的叶片，其流动到叶片上表面上的最大速度点，叶片的上表面设置在该点下游的区域的最大速度，其中流体流速随着基本上在整个叶片长度上延伸的锯齿轮廓的扰流器边缘而减小。

8. 发明授权

US07017646B2 Method for casting a directionally solidified article 有权
标题翻译：铸造定向凝固制品的方法
公开(公告)号：US07017646B2
公开(公告)日：2006-03-28
申请号：US10982957
申请日：2004-11-08
申请人： Martin Balliel , Dietrich Eckardt , Maxim Konter , Andreas Weiland
发明人： Martin Balliel , Dietrich Eckardt , Maxim Konter , Andreas Weiland
IPC分类号： B22D27/04
CPC分类号： B22D27/045
摘要： A method of casting a directionally solidified (DS) or single crystal (SX) article with a casting furnace having a heating chamber (4), a cooling chamber (5), a separating baffle (3) between the both chambers includes a first step in which the shell mould (12) is filled with liquid metal (15), and the liquid metal (15) is directionally solidified by withdrawing the shell mould (12) from the heating to the cooling chamber (4, 5). An inert gas impinges from nozzles (8) arranged below the baffle (3) on the shell mould (12) and in steep transitions in outer surface area of the shell mould (12) the flow of the inert gas (9) is reduced or even stopped and when a protruding geometrical feature has passed the impingement area of the gas jets, the gas flow (9) is restored to a value adjusted to the geometry of the cast part presently passing the impingement area.
摘要翻译：一种用具有加热室（4），冷却室（5），两个室之间的分离挡板（3）的铸造炉铸造定向凝固（DS）或单晶（SX）制品的方法包括：第一步骤其中壳体模具12充满液态金属15，并且液态金属15通过将壳模12从加热引导到冷却室4,5而定向凝固。惰性气体从设置在外壳模具（12）上的挡板（3）下方的喷嘴（8）和壳模（12）的外表面区域的陡峭过渡部分入射，惰性气体（9）的流动减少或甚至停止，并且当突出的几何特征已经通过气体射流的冲击区域时，气流（9）恢复到调整到目前通过冲击区域的铸造件的几何形状的值。

9. 发明申请

US20050103462A1 Method for casting a directionally solidified article 有权
标题翻译：铸造定向凝固制品的方法
公开(公告)号：US20050103462A1
公开(公告)日：2005-05-19
申请号：US10982957
申请日：2004-11-08
申请人： Martin Balliel , Dietrich Eckardt , Maxim Konter , Andreas Weiland
发明人： Martin Balliel , Dietrich Eckardt , Maxim Konter , Andreas Weiland
IPC分类号： B22D27/04 , B22C9/04
CPC分类号： B22D27/045
摘要： A method of casting a directionally solidified (DS) or single crystal (SX) article with a casting furnace having a heating chamber (4), a cooling chamber (5), a separating baffle (3) between the both chambers includes a first step in which the shell mould (12) is filled with liquid metal (15), and the liquid metal (15) is directionally solidified by withdrawing the shell mould (12) from the heating to the cooling chamber (4, 5). An inert gas impinges from nozzles (8) arranged below the baffle (3) on the shell mould (12) and in steep transitions in outer surface area of the shell mould (12) the flow of the inert gas (9) is reduced or even stopped and when a protruding geometrical feature has passed the impingement area of the gas jets, the gas flow (9) is restored to a value adjusted to the geometry of the cast part presently passing the impingement area.
摘要翻译：一种用具有加热室（4），冷却室（5），两个室之间的分离挡板（3）的铸造炉铸造定向凝固（DS）或单晶（SX）制品的方法包括：第一步骤其中壳体模具12充满液态金属15，并且液态金属15通过将壳模12从加热引导到冷却室4,5而定向凝固。惰性气体从设置在外壳模具（12）上的挡板（3）下方的喷嘴（8）和壳模（12）的外表面区域的陡峭过渡部分入射，惰性气体（9）的流动减少或甚至停止，并且当突出的几何特征已经通过气体射流的冲击区域时，气流（9）恢复到调整到目前通过冲击区域的铸造件的几何形状的值。

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