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公开(公告)号：US20130121368A1
公开(公告)日：2013-05-16
申请号：US13642022
申请日：2011-04-20
申请人： Alban Du Tertre , Alain Pyre , Didier Guichard , Daniel Cornu , Christophe Verdy , Christian Coddet
发明人： Alban Du Tertre , Alain Pyre , Didier Guichard , Daniel Cornu , Christophe Verdy , Christian Coddet
IPC分类号： G01N25/72
CPC分类号： G01N25/72 , F02K9/96 , G01N3/60 , G01N2203/0222 , G01N2203/0226 , G01N2203/0242
摘要： A system for cooling and holding a testpiece in an effective manner while the testpiece is subjected locally to high heat flux. The testpiece includes an inside face extended by parallel strips that leave between them channels for passing a cooling fluid, and parallel fins of an intermediate part are inserted between the strips.
摘要翻译： 一种用于在试件局部受到高热通量的情况下有效地冷却和保持试样的系统。 试件包括由平行的条带延伸的内表面，在其间留有用于通过冷却流体的通道，并且中间部分的平行翅片插入在条带之间。
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公开(公告)号：US08979360B2
公开(公告)日：2015-03-17
申请号：US13642022
申请日：2011-04-20
申请人： Alban Du Tertre , Alain Pyre , Didier Guichard , Daniel Cornu , Christophe Verdy , Christian Coddet
发明人： Alban Du Tertre , Alain Pyre , Didier Guichard , Daniel Cornu , Christophe Verdy , Christian Coddet
CPC分类号： G01N25/72 , F02K9/96 , G01N3/60 , G01N2203/0222 , G01N2203/0226 , G01N2203/0242
摘要： A system for cooling and holding a testpiece in an effective manner while the testpiece is subjected locally to high heat flux. The testpiece includes an inside face extended by parallel strips that leave between them channels for passing a cooling fluid, and parallel fins of an intermediate part are inserted between the strips.
摘要翻译： 一种用于在试件局部受到高热通量的情况下有效地冷却和保持试样的系统。 试件包括由平行的条带延伸的内表面，在其间留有用于通过冷却流体的通道，并且中间部分的平行翅片插入在条带之间。
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3.发明授权High heat flux regenerative circuit, in particular for the combustion chamber of a rocket engine 有权高热通量再生电路，特别是用于火箭发动机的燃烧室公开(公告)号：US06516872B1
公开(公告)日：2003-02-11
申请号：US09711186
申请日：2000-11-09
IPC分类号： F28F1318
CPC分类号： B23P15/008 , B23P15/26 , C23C4/137 , F02K9/64 , Y10T29/49336 , Y10T29/49346
摘要： A regenerative circuit structure is built up by implementing the following steps in particular: an intermediate layer is made on a support core representing the inner profile of the structure; a series of channels regularly distributed around the core is made with the channels opening to face the intermediate layer, each of the channels being provided with a soluble insert; the support core is preheated and the body of the structure is made by thermal spraying under a vacuum; channels are machined in the body from the outside, and said channels are filled by means of soluble inserts; a closure layer is formed to close the channels in the body, and an outer envelope is formed by thermal spraying under a vacuum, after preheating; and all of the soluble inserts and the intermediate layer are eliminated.
摘要翻译： 通过实施以下步骤来构建再生电路结构：在表示该结构的内部轮廓的支撑芯上形成中间层;围绕芯部规则分布的一系列通道被制成，通道开口面对 中间层，每个通道设置有可溶性插入物;支撑芯被预热，并且结构的主体通过真空下的热喷涂制成;通道从外部在主体中加工，并且所述通道由 手段的可溶性插入物;形成闭合层以封闭体内的通道，并且在预热之后通过真空热喷涂形成外壳; 并且所有可溶性插入物和中间层都被去除。
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4.发明授权Method of manufacturing a high heat flux regenerative circuit, in particular for the combustion chamber of a rocket engine 有权制造高热量再生回路的方法，特别是用于火箭发动机的燃烧室公开(公告)号：US06209199B1
公开(公告)日：2001-04-03
申请号：US09271394
申请日：1999-03-17
IPC分类号： B23P1500
CPC分类号： B23P15/008 , B23P15/26 , C23C4/137 , F02K9/64 , Y10T29/49336 , Y10T29/49346
摘要： A regenerative circuit structure is built up by implementing the following steps in particular: an intermediate layer is made on a support core representing the inner profile of the structure; a series of channels regularly distributed around the core is made with the channels opening to face the intermediate layer, each of the channels being provided with a soluble insert; the support core is preheated and the body of the structure is made by thermal spraying under a vacuum; channels are machined in the body from the outside, and said channels are filled by means of soluble inserts; a closure layer is formed to close the channels in the body, and an outer envelope is formed by thermal spraying under a vacuum, after preheating; and all of the soluble inserts and the intermediate layer are eliminated.
摘要翻译： 通过实施以下步骤来构建再生电路结构：在表示该结构的内部轮廓的支撑芯上形成中间层;围绕芯部规则分布的一系列通道被制成，通道开口面对 中间层，每个通道设置有可溶性插入物;支撑芯被预热，并且结构的主体通过真空下的热喷涂制成;通道从外部在主体中加工，并且所述通道由 手段的可溶性插入物;形成闭合层以封闭体内的通道，并且在预热之后通过真空热喷涂形成外壳; 并且所有可溶性插入物和中间层都被去除。
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