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1. 发明授权

US09358645B2 Adaptive machining method for smelted blades 有权
标题翻译：冶炼刀片自适应加工方法
公开(公告)号：US09358645B2
公开(公告)日：2016-06-07
申请号：US14127063
申请日：2012-06-21
申请人： Yvon Marie-Joseph Louesdon , Joseph Tami-Lizuzu , Daniel Quach , Patrick Wehrer , Didier Legeai
发明人： Yvon Marie-Joseph Louesdon , Joseph Tami-Lizuzu , Daniel Quach , Patrick Wehrer , Didier Legeai
IPC分类号： B23P15/02 , G05B19/4097 , B23P15/00
CPC分类号： B23P15/02 , B23P15/006 , F05D2230/10 , G05B19/4097 , G05B2219/35117 , G05B2219/35128 , G05B2219/45147 , Y10T29/49336
摘要： A method for finishing a shape of a component by machining, in which one area is produced by smelting with a thickened portion forming a first surface with a surrounding profile and a theoretical profile defined by a second surface, the method including: defining, on the second surface, a grid forming nodes and squares; defining each point over which the machining tool is to pass according to weighting coefficients equal to weight to be given to the nodes of the square in which the tool is located, to be the barycenter of assigned nodes of the coefficients; measuring, for each node located outside an outer limit, the delta between the first surface at the node and the theoretical position of the node; calculating deltas for each node within the outer limit by interpolation from already known deltas; using the weighting coefficients, defining the delta to be applied at each point.
摘要翻译：一种用于通过机加工来完成部件形状的方法，其中通过用形成具有周边轮廓的第一表面的加厚部分和由第二表面限定的理论轮廓进行熔炼来生产一个区域，所述方法包括：第二面，网格形成节点和正方形; 根据加权系数来确定加工工具要通过的每个点，该加权系数等于要提供给工具所在的平方的节点的权重，作为系数的分配节点的重心; 测量位于外界外部的每个节点，节点处的第一表面与节点的理论位置之间的增量; 通过已知三角形的插值计算外限内每个节点的三角洲; 使用加权系数，定义要在每个点应用的增量。

2. 发明申请

US20140137409A1 ADAPTIVE MACHINING METHOD FOR SMELTED BLADES 有权
标题翻译：自适应加工方法
公开(公告)号：US20140137409A1
公开(公告)日：2014-05-22
申请号：US14127063
申请日：2012-06-21
申请人： Yvon Marie-Joseph Louesdon , Joseph Tami-Lizuzu , Daniel Quach , Patrick Wehrer , Didier Legeai
发明人： Yvon Marie-Joseph Louesdon , Joseph Tami-Lizuzu , Daniel Quach , Patrick Wehrer , Didier Legeai
IPC分类号： B23P15/02
CPC分类号： B23P15/02 , B23P15/006 , F05D2230/10 , G05B19/4097 , G05B2219/35117 , G05B2219/35128 , G05B2219/45147 , Y10T29/49336
摘要： A method for finishing a shape of a component by machining, in which one area is produced by smelting with a thickened portion forming a first surface with a surrounding profile and a theoretical profile defined by a second surface, the method including: defining, on the second surface, a grid forming nodes and squares; defining each point over which the machining tool is to pass according to weighting coefficients equal to weight to be given to the nodes of the square in which the tool is located, to be the barycenter of assigned nodes of the coefficients; measuring, for each node located outside an outer limit, the delta between the first surface at the node and the theoretical position of the node; calculating deltas for each node within the outer limit by interpolation from already known deltas; using the weighting coefficients, defining the delta to be applied at each point.
摘要翻译：一种用于通过机械加工来形成部件的形状的方法，其中通过用形成具有周边轮廓的第一表面的加厚部分和由第二表面限定的理论轮廓进行熔炼来生产一个区域，所述方法包括：第二面，网格形成节点和正方形; 根据加权系数来确定加工工具要通过的每个点，该加权系数等于要提供给工具所在的平方的节点的权重，作为系数的分配节点的重心; 测量位于外界外部的每个节点，节点处的第一表面与节点的理论位置之间的增量; 通过已知三角形的插值计算外限内每个节点的三角洲; 使用加权系数，定义要在每个点应用的增量。

3. 发明授权

US08763678B2 Mold for producing parts by wax injection 有权
标题翻译：通过注蜡生产零件的模具
公开(公告)号：US08763678B2
公开(公告)日：2014-07-01
申请号：US13823829
申请日：2011-10-05
申请人： Daniel Quach , Yvon Marie-Joseph Louesdon , Patrick Pourfilet , Jean-Louis Martial Verger , Patrick Wehrer
发明人： Daniel Quach , Yvon Marie-Joseph Louesdon , Patrick Pourfilet , Jean-Louis Martial Verger , Patrick Wehrer
IPC分类号： B22C9/06 , B22C7/02 , B22D17/22 , B22D17/26
CPC分类号： B22C7/02 , B22C9/062 , B29C33/26 , B29C45/33 , B29C45/332 , B29C45/4005 , B29K2091/00
摘要： A mold for producing a part, such as a turbomachine blade model, by injecting wax into a cavity, the cavity including at least two cavity elements, each of which is supported in a cavity block. The two cavity blocks are mobile relative to one another between a closed position for injecting the wax and an open position for removing the part following the injection of the wax. The two cavity blocks are mobile in a horizontal plane.
摘要翻译：一种用于通过将蜡注入空腔中来制造诸如涡轮机刀片模型的部件的模具，所述模腔包括至少两个腔体元件，每个腔体元件被支撑在空腔模块中。在注入蜡的关闭位置和在注入蜡之后去除部件的打开位置之间，两个空腔块相对于彼此是可移动的。两个空腔块在水平面移动。

4. 发明申请

US20130174997A1 MOULD FOR PRODUCING PARTS BY WAX INJECTION 有权
标题翻译：通过WAX注射生产零件的模具
公开(公告)号：US20130174997A1
公开(公告)日：2013-07-11
申请号：US13823829
申请日：2011-10-05
申请人： Daniel Quach , Yvon Marie-Joseph Louesdon , Patrick Pourfilet , Jean-Louis Martial Verger , Patrick Wehrer
发明人： Daniel Quach , Yvon Marie-Joseph Louesdon , Patrick Pourfilet , Jean-Louis Martial Verger , Patrick Wehrer
IPC分类号： B22C7/02
CPC分类号： B22C7/02 , B22C9/062 , B29C33/26 , B29C45/33 , B29C45/332 , B29C45/4005 , B29K2091/00
摘要： A mold for producing a part, such as a turbomachine blade model, by injecting wax into a cavity, the cavity including at least two cavity elements, each of which is supported in a cavity block. The two cavity blocks are mobile relative to one another between a closed position for injecting the wax and an open position for removing the part following the injection of the wax. The two cavity blocks are mobile in a horizontal plane.
摘要翻译：一种用于通过将蜡注入空腔中来制造诸如涡轮机刀片模型的部件的模具，所述模腔包括至少两个腔体元件，每个腔体元件被支撑在空腔模块中。在注入蜡的关闭位置和在注入蜡之后去除部件的打开位置之间，两个空腔块相对于彼此是可移动的。两个空腔块在水平面移动。

5. 发明授权

US08490673B2 Method for deburring a ceramic foundry core 有权
标题翻译：陶瓷铸造核心去毛刺的方法
公开(公告)号：US08490673B2
公开(公告)日：2013-07-23
申请号：US12988447
申请日：2009-04-17
申请人： Christian Defrocourt , Serge Prigent , Daniel Quach , Patrick Wehrer
发明人： Christian Defrocourt , Serge Prigent , Daniel Quach , Patrick Wehrer
IPC分类号： B22C9/10 , B22C9/12
CPC分类号： B28B11/18 , B24B9/06 , B24B19/14
摘要： A method for deburring a ceramic foundry core obtained by injecting a ceramic paste, the paste including a binder having a predetermined glass transition temperature, into a mold and having at least one surface portion with a surplus of material forming a burr to be eliminated. The method includes the following stages: a) disposing and attaching the molded, unfired foundry core onto a mounting; b) placing a milling tool, having an elongated shape with a helically cut edge, onto a tool holder; c) causing the tool to rotate around its axis and touching the milling tool to the surface portion to be deburred; and d) freezing the surface portion to be deburred such that the foundry core is maintained at a temperature lower than a glass transition temperature during the deburring operation.
摘要翻译：一种通过将具有预定玻璃化转变温度的粘合剂的陶瓷糊剂注入到模具中并且具有至少一个表面部分而形成毛刺以除去的至少一个表面部分而将陶瓷铸造芯去毛刺的方法。该方法包括以下步骤：a）将模制的未烧结的铸造芯体放置并附接到安装件上; b）将具有螺旋切割边缘的细长形状的铣削工具放置在工具架上; c）使工具围绕其轴线旋转并且将铣削工具接触到待去毛刺的表面部分; 以及d）冷冻待去毛刺的表面部分，使得在去毛刺操作期间，铸造芯保持在低于玻璃化转变温度的温度。

6. 发明申请

US20110049748A1 METHOD FOR DEBURRING A CERAMIC FOUNDRY CORE 有权
标题翻译：淘汰陶瓷基岩芯的方法
公开(公告)号：US20110049748A1
公开(公告)日：2011-03-03
申请号：US12988447
申请日：2009-04-17
申请人： Christian Defrocourt , Serge Prigent , Daniel Quach , Patrick Wehrer
发明人： Christian Defrocourt , Serge Prigent , Daniel Quach , Patrick Wehrer
IPC分类号： B29C37/00
CPC分类号： B28B11/18 , B24B9/06 , B24B19/14
摘要： The present invention relates to a method for deburring a ceramic foundry core (10) obtained by injecting a ceramic paste, said paste including a binder having a predetermined glass transition temperature, into a mold and having at least one surface portion with a surplus of material forming a burr (B) to be eliminated. The method is characterized in that it includes the following stages: a) disposing and attaching the molded, unfired foundry core (10) onto a mounting (300); b) placing a milling tool (100), having an elongated shape with a helically cut edge, onto a tool holder; c) causing the tool to rotate around its axis and touching the milling tool to said surface portion to be deburred; and d) freezing (400) the surface portion to be deburred such that the foundry core is maintained at a temperature lower than said glass transition temperature during the deburring operation.
摘要翻译：本发明涉及一种通过将陶瓷膏（包括具有预定玻璃化转变温度的粘结剂）的糊料注入模具而得到的陶瓷铸造铁心（10）的去毛刺方法，并具有至少一个具有多余材料的表面部分形成要消除的毛刺（B）。该方法的特征在于它包括以下阶段：a）将模制的未烧结的铸造铁芯（10）设置并附接到安装件（300）上; b）将具有螺旋形切割边缘的细长形状的铣刀（100）放置在刀架上; c）使所述工具围绕其轴线旋转并且接触所述铣削工具以使所述表面部分被去毛刺; 以及d）冷冻（400）待去毛刺的表面部分，使得在去毛刺操作期间，铸造芯保持在低于所述玻璃化转变温度的温度。

7. 发明授权

US07533714B2 Process for manufacturing ceramic cores for turbomachine blades 有权
标题翻译：用于制造涡轮机叶片的陶瓷芯的方法
公开(公告)号：US07533714B2
公开(公告)日：2009-05-19
申请号：US11742850
申请日：2007-05-01
申请人： Didier Guerche , Serge Prigent , Patrick Wehrer
发明人： Didier Guerche , Serge Prigent , Patrick Wehrer
IPC分类号： B22C9/10 , B22C9/12
CPC分类号： B22C9/103
摘要： A process for manufacturing a ceramic foundry core having at least one thin region with a thickness “e”, in particular in of a turbomachine blade trailing edge, including the forming in a mold of a mixture including a ceramic particle filler and an organic binder, the extraction of the core from the mold, the binder removal and consolidation heat treatment of the core. The process is one in which a core is formed in the mold, the region of this core being thickened relative to the thickness “e” by an overthickness E and in which the overthickness is machined after the core has been extracted from the mold and before or after the heat treatment operation. In particular, the machining is carried out mechanically by milling, either with removal of chips on the cores before firing, or by abrasion on the fired cores.
摘要翻译：一种用于制造具有至少一个厚度为“e”的薄区域的陶瓷铸造铁芯的方法，特别是在涡轮机叶片后缘中，包括在模具中形成包括陶瓷颗粒填料和有机粘合剂的混合物，从模具中提取芯材，去除粘合剂并固化热处理芯。该方法是在模具中形成芯体，该芯部的区域通过厚度E相对于厚度“e”而变厚，并且在芯从模具中提取之后并且之前加工过厚度或在热处理操作之后。特别地，通过铣削机械地进行加工，或者在烧制之前去除芯上的切屑，或者通过在烧制的芯上的磨损来进行加工。

8. 发明申请

US20070261811A1 PROCESS FOR MANUFACTURING CERAMIC CORES FOR TURBOMACHINE BLADES 有权
标题翻译：用于制造涡轮叶片的陶瓷刀的方法
公开(公告)号：US20070261811A1
公开(公告)日：2007-11-15
申请号：US11742850
申请日：2007-05-01
申请人： Didier Guerche , Serge Prigent , Patrick Wehrer
发明人： Didier Guerche , Serge Prigent , Patrick Wehrer
IPC分类号： B22C9/10 , B22C9/04
CPC分类号： B22C9/103
摘要： The invention relates a process for manufacturing a ceramic foundry core having at least one thin region with a thickness “e”, in particular in of a turbomachine blade trailing edge, comprising the forming in a mold of a mixture comprising a ceramic particle filler and an organic binder, the extraction of the core from the mold, the binder removal and consolidation heat treatment of the core. The process is one in which a core is formed in said mold, said region of this core being thickened relative to the thickness “e” by an overthickness E and in which said overthickness is machined after the core has been extracted from the mold and before or after the heat treatment operation. In particular, the machining is carried out mechanically by milling, either with removal of chips on the cores before firing, or by abrasion on the fired cores.
摘要翻译：本发明涉及一种用于制造具有至少一个厚度为“e”的薄区域的陶瓷铸造芯的方法，特别是在涡轮机叶片后缘中，包括在模具中形成包含陶瓷颗粒填料和有机粘合剂，从模具中提取芯，去除粘合剂并固化热处理芯。该过程是在所述模具中形成芯部，该芯部的区域通过厚度E相对于厚度“e”而变厚，并且在从模具中取出芯部之后加工所述厚度或在热处理操作之后。特别地，通过铣削机械地进行加工，或者在烧制之前去除芯上的切屑，或者通过在烧制的芯上的磨损来进行加工。

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