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1. 发明申请

US20140144887A1 TOOLSET AND METHOD FOR PRODUCING A METAL LINER 有权
标题翻译：用于生产金属衬里的工具和方法
公开(公告)号：US20140144887A1
公开(公告)日：2014-05-29
申请号：US13882623
申请日：2011-11-21
申请人： Sylvain Claudel , Dominique Lacour
发明人： Sylvain Claudel , Dominique Lacour
IPC分类号： B23K9/00
CPC分类号： B23K9/0026 , F17C1/06 , F17C2201/0109 , F17C2201/054 , F17C2201/056 , F17C2203/0604 , F17C2203/0619 , F17C2203/0636 , F17C2203/0646 , F17C2203/0648 , F17C2203/066 , F17C2203/0663 , F17C2203/0673 , F17C2209/2163 , F17C2209/221 , F17C2209/224 , F17C2223/0161 , F17C2260/012 , F17C2270/0194 , Y10T29/53
摘要： A method and a toolset for manufacturing a metal liner for a composite vessel includes a mandrel configured in several mandrel elements forming support elements of primary parts constituting the metal liner.
摘要翻译：用于制造用于复合容器的金属衬套的方法和工具集包括：心轴，其构成为形成构成金属衬垫的主要部件的支撑元件的多个心轴元件。

2. 发明申请

US20090075091A1 RIGIDIFICATION OF STRUCTURES TO BE DEPLOYED BY INFLATING, PARTICULARLY FOR USE IN SPACE 有权
标题翻译：通过自由化，特别是在空间中使用的结构的消除
公开(公告)号：US20090075091A1
公开(公告)日：2009-03-19
申请号：US11577758
申请日：2005-10-20
申请人： Brigitte Defoort , Xavier Coqueret , Dominique Lacour
发明人： Brigitte Defoort , Xavier Coqueret , Dominique Lacour
IPC分类号： B32B17/10 , B32B27/36 , B29C71/02
CPC分类号： C08G59/68 , Y10T428/13 , Y10T428/1303 , Y10T428/1352 , Y10T428/1359 , Y10T428/139 , Y10T428/31721 , Y10T428/31786
摘要： The invention relates to the stiffening of inflatably deployable structures, in particular for space use.More specifically, the invention relates to a flexible membrane for inflatably deployable structures, that comprises one layer of a composite and at least one polymer film that is permeable to visible radiation covering one of the faces of this layer, said composite being formed from a fibrous material impregnated with a composition incorporating an epoxide or epoxy/acrylate resin and a photoinitiator, and which is characterized in that the photoinitiator is an iron-arene complex salt of general formula (I): where A is an arene group, while X is a non-nucleophilic anion.Applications; manufacture of devices of the following types: radars, solar panels, reflectors, solar shields, antennas, solar mirrors or sails, intended to equip orbital vehicles or vehicles for space or planetary exploration.
摘要翻译：本发明涉及可膨胀展开结构的加强，特别是用于空间使用。更具体地，本发明涉及一种用于可膨胀展开结构的柔性膜，其包括一层复合材料和至少一层聚合物膜，该聚合物膜可透过该层的一个表面的可见辐射，所述复合材料由纤维状浸渍有包含环氧化物或环氧/丙烯酸酯树脂和光引发剂的组合物的材料，其特征在于光引发剂是通式（I）的铁 - 芳烃络合盐：其中A是芳族基团，而X是非亲核阴离子。应用; 制造以下类型的设备：雷达，太阳能电池板，反射器，太阳能屏蔽，天线，太阳能反射镜或帆，旨在为轨道车辆或车辆进行空间或行星探测。

3. 发明申请

US20090200427A1 CONTROL DEVICE FOR DEPLOYMENT OF INFLATABLE STRUCTURES 有权
标题翻译：用于配置可充气结构的控制装置
公开(公告)号：US20090200427A1
公开(公告)日：2009-08-13
申请号：US11718109
申请日：2005-10-14
申请人： Dominique Lacour , Brigitte Defoort , Vincent Peypoudat , Cyril Gautrias
发明人： Dominique Lacour , Brigitte Defoort , Vincent Peypoudat , Cyril Gautrias
IPC分类号： B64G1/22
CPC分类号： B64G1/222
摘要： The invention relates to a device for controlling the deployment of an inflatable structure including, in the non-deployed state, a flexible tube (12) which is folded in zigzags and fixed to one end of a plug (13) provided with a buoyant gas admission (15), the other end of the tube being closed; means (25 to 29) for controlling the change of state of the tube from the folded state (12a) to the deployed state (30), the means being arranged inside the tube (12) and consisting of a set of interconnected flexible blades (25) which are radially arranged around the strut (16) in the form of petals, in such a way that the set can be displayed along the strut; and means (28, 29) for bringing the set of petals (25) towards the plug (13) in such a way as to press the folded part (12a) of the tube, each petal (25) being applied to a series of superimposed folds (21 to 24) of the folded part of the tube.
摘要翻译：本发明涉及一种用于控制可膨胀结构的展开的装置，包括在非展开状态下的柔性管（12），其以锯齿形折叠并固定到设置有浮力气体的塞子（13）的一端入院（15），管的另一端关闭; 用于控制管从折叠状态（12a）到展开状态（30）的状态变化的装置（25至29），所述装置布置在管（12）的内部，并且由一组互连的柔性叶片 25），其以花瓣的形式径向布置在支柱（16）周围，使得该组可沿支柱显示; 以及用于将所述一组花瓣（25）朝向所述插头（13）以使所述管的折叠部分（12a）按压的方式（28,29），每个花瓣（25）被施加到一系列管的折叠部分的叠合折叠（21至24）。

4. 发明授权

US5951808A Method for producing high dimensional precision composite elements using ionization polymerization and elements produced by said method 失效
标题翻译：使用电离聚合制造高维度精密复合元件的方法和由所述方法制造的元件
公开(公告)号：US5951808A
公开(公告)日：1999-09-14
申请号：US790896
申请日：1997-01-29
申请人： Dominique Lacour , Sylvie His , Fran.cedilla.ois Raut , Christian Desagulier , Nathalie Chieusse
发明人： Dominique Lacour , Sylvie His , Fran.cedilla.ois Raut , Christian Desagulier , Nathalie Chieusse
IPC分类号： B32B7/12 , B29C35/08 , B29C70/34 , B32B19/06 , C08F2/54 , C09J133/04 , C09J183/04 , B32B31/28
CPC分类号： B29C70/342 , B29C2035/0844 , B29C2035/0877 , B29L2007/002 , B29L2009/00 , Y10T156/1028
摘要： A method for producing a high dimensional precision composite element using ionization polymerization and an element made by such method. The element includes a support panel flanked on at least one side with a skin fixed by an adhesive resin and including at least one lap of organic or mineral fibers and an organic linking matrix. The method includes placing at least one lap of fibers preimpregnated with an ionization polymerizable resin on a mold to form the skin, the mold having a predetermined shape and dimensions for the element to be produced; placing a film of an ionization polymerizable adhesive resin on the skin; placing the support panel on the film to form a skin/film/panel unit, the support panel having a predetermined thickness; compacting the skin/film/panel unit; and polymerizing the polymerizable resins during the compacting by subjecting the skin/film/panel unit to ionization.
摘要翻译：使用电离聚合制造高维度精密复合元件的方法和通过这种方法制成的元件。该元件包括在至少一侧的侧面的支撑面板，其中皮肤由粘合剂树脂固定，并且包括至少一圈的有机或矿物纤维和有机连接基质。该方法包括将预先浸有电离可聚合树脂的纤维的至少一圈放置在模具上以形成皮肤，所述模具具有用于待生产的元件的预定形状和尺寸; 将电离可聚合粘合剂树脂的膜放置在皮肤上; 将所述支撑面板放置在所述薄膜上以形成皮肤/薄膜/面板单元，所述支撑面板具有预定厚度; 压实皮肤/胶片/面板单元; 并且通过使皮肤/薄膜/面板单元进行离子化，在压实过程中聚合可聚合树脂。

5. 发明授权

US09492878B2 Toolset and method for producing a metal liner 有权
标题翻译：用于生产金属衬里的工具和方法
公开(公告)号：US09492878B2
公开(公告)日：2016-11-15
申请号：US13882623
申请日：2011-11-21
申请人： Sylvain Claudel , Dominique Lacour
发明人： Sylvain Claudel , Dominique Lacour
IPC分类号： B23K9/16 , B23K9/00 , F17C1/06
CPC分类号： B23K9/0026 , F17C1/06 , F17C2201/0109 , F17C2201/054 , F17C2201/056 , F17C2203/0604 , F17C2203/0619 , F17C2203/0636 , F17C2203/0646 , F17C2203/0648 , F17C2203/066 , F17C2203/0663 , F17C2203/0673 , F17C2209/2163 , F17C2209/221 , F17C2209/224 , F17C2223/0161 , F17C2260/012 , F17C2270/0194 , Y10T29/53
摘要： A method and a toolset for manufacturing a metal liner for a composite vessel includes a mandrel configured in several mandrel elements forming support elements of primary parts constituting the metal liner.
摘要翻译：用于制造用于复合容器的金属衬套的方法和工具集包括：心轴，其构成为形成构成金属衬垫的主要部件的支撑元件的多个心轴元件。

6. 发明授权

US08025942B2 Rigidification of structures to be deployed by inflating, particularly for use in space 有权
标题翻译：通过膨胀，特别是用于空间来部署的结构的刚性
公开(公告)号：US08025942B2
公开(公告)日：2011-09-27
申请号：US11577758
申请日：2005-10-20
申请人： Brigitte Defoort , Xavier Coqueret , Dominique Lacour
发明人： Brigitte Defoort , Xavier Coqueret , Dominique Lacour
IPC分类号： B32B27/12 , B32B27/14
CPC分类号： C08G59/68 , Y10T428/13 , Y10T428/1303 , Y10T428/1352 , Y10T428/1359 , Y10T428/139 , Y10T428/31721 , Y10T428/31786
摘要： The invention relates to the stiffening of inflatably deployable structures, in particular for space use.More specifically, the invention relates to a flexible membrane for inflatably deployable structures, that comprises one layer of a composite and at least one polymer film that is permeable to visible radiation covering one of the faces of this layer, said composite being formed from a fibrous material impregnated with a composition incorporating an epoxide or epoxy/acrylate resin and a photoinitiator, and which is characterized in that the photoinitiator is an iron-arene complex salt of general formula (I): where A is an arene group, while X is a non-nucleophilic anion. Applications: manufacture of devices of the following types: radars, solar panels, reflectors, solar shields, antennas, solar mirrors or sails, intended to equip orbital vehicles or vehicles for space or planetary exploration.
摘要翻译：本发明涉及可膨胀展开结构的加强，特别是用于空间使用。更具体地，本发明涉及一种用于可膨胀展开结构的柔性膜，其包括一层复合材料和至少一层聚合物膜，该聚合物膜可透过该层的一个表面的可见辐射，所述复合材料由纤维状浸渍有包含环氧化物或环氧/丙烯酸酯树脂和光引发剂的组合物的材料，其特征在于光引发剂是通式（I）的铁 - 芳烃络合盐：其中A是芳族基团，而X是非亲核阴离子。应用：制造以下类型的设备：雷达，太阳能电池板，反射器，太阳能屏蔽，天线，太阳能反射镜或帆，旨在配备轨道车辆或车辆进行太空或行星探测。

7. 发明申请

US20100166988A1 ASSEMBLY OF PREPREGS FOR PRODUCING STRUCTURES, FOR EXAMPLE ONES WHICH DEPLOY THROUGH INFLATION 有权
标题翻译：组建生产结构的准备工作，例如通过通货膨胀的实例
公开(公告)号：US20100166988A1
公开(公告)日：2010-07-01
申请号：US12305656
申请日：2007-07-10
申请人： Brigitte Defoort , Dominique Lacour , Olivier Le-Couls
发明人： Brigitte Defoort , Dominique Lacour , Olivier Le-Couls
IPC分类号： B32B1/00 , B32B37/00 , B32B38/00 , B32B1/08 , B32B3/30 , B32B3/02 , B32B3/28 , B32B3/10
CPC分类号： B32B7/045 , B29C35/0894 , B29C53/30 , B29C65/14 , B29C65/1403 , B29C65/1406 , B29C65/1409 , B29C65/1435 , B29C65/1496 , B29C65/48 , B29C65/4815 , B29C65/4845 , B29C66/1122 , B29C66/21 , B29C66/52241 , B29C66/63 , B29C66/71 , B29C66/721 , B29C66/7212 , B29C66/72141 , B29C66/73754 , B29C66/7394 , B29C66/73941 , B29C70/305 , B29C70/54 , B29C70/86 , B29C2035/0827 , B29K2063/00 , B29K2105/243 , B29K2105/258 , B29L2022/02 , B29L2031/3097 , B29L2031/605 , B29L2031/703 , B64G2001/224 , C08G59/68 , Y10T156/1049 , Y10T156/1051 , Y10T428/13 , Y10T428/1362 , Y10T428/24479 , Y10T428/24488 , Y10T428/2457 , Y10T428/24802 , Y10T428/24826 , B29K2309/08 , B29C65/00
摘要： The invention relates to a method of assembling pre-impregnated plies by local isolated polymerization of the assembly region (30) under the action of a radiation to which the resin of the prepreg is sensitive.The assembly method makes it possible in particular to produce very large sized gossamer structures (7) in the form of a concertina-folded tube which is deployed by injecting pressurized gas once in space then stiffened by polymerization under the effect of the same radiation. The pylon concerned (7) thus comprises two structural elements (10, 20) secured end to end while at the same time maintaining its flexibility and firmness qualities.
摘要翻译：本发明涉及一种通过在预浸料树脂对其敏感的辐射作用下组装区域（30）的局部分离聚合来组装预浸层的方法。组装方法使得可以特别地生产以三角折叠管形式的非常大尺寸的游丝结构（7），其通过在空间中注入加压气体而展开，然后在相同辐射的作用下通过聚合加强。因此，所涉及的挂架（7）包括两个结构元件（10,20），同时保持其柔性和坚固性质。

8. 发明授权

US07740203B2 Control device for deployment of inflatable structures 有权
标题翻译：用于部署充气结构的控制装置
公开(公告)号：US07740203B2
公开(公告)日：2010-06-22
申请号：US11718109
申请日：2005-10-14
申请人： Dominique Lacour , Brigitte Defoort , Vincent Peypoudat , Cyril Gautrias
发明人： Dominique Lacour , Brigitte Defoort , Vincent Peypoudat , Cyril Gautrias
IPC分类号： B64G1/00
CPC分类号： B64G1/222
摘要： The invention relates to a device for controlling the deployment of an inflatable structure including, in the non-deployed state, a flexible tube (12) which is folded in zigzags and fixed to one end of a plug (13) provided with a buoyant gas admission (15), the other end of the tube being closed; means (25 to 29) for controlling the change of state of the tube from the folded state (12a) to the deployed state (30), the means being arranged inside the tube (12) and consisting of a set of interconnected flexible blades (25) which are radially arranged around the strut (16) in the form of petals, in such a way that the set can be displayed along the strut; and means (28, 29) for bringing the set of petals (25) towards the plug (13) in such a way as to press the folded part (12a) of the tube, each petal (25) being applied to a series of superimposed folds (21 to 24) of the folded part of the tube.
摘要翻译：本发明涉及一种用于控制可膨胀结构的展开的装置，包括在非展开状态下的柔性管（12），其以锯齿形折叠并固定到设置有浮力气体的塞子（13）的一端入院（15），管的另一端关闭; 用于控制管从折叠状态（12a）到展开状态（30）的状态变化的装置（25至29），所述装置布置在管（12）的内部，并且由一组互连的柔性叶片 25），其以花瓣的形式径向布置在支柱（16）周围，使得该组可沿支柱显示; 以及用于将所述一组花瓣（25）朝向所述插头（13）以使所述管的折叠部分（12a）按压的方式（28,29），每个花瓣（25）被施加到一系列管的折叠部分的叠合折叠（21至24）。

9. 发明授权

US09381719B2 Assembly of prepregs for producing structures, for example ones which deploy through inflation 有权
标题翻译：装配用于生产结构的预浸料，例如通过通货膨胀部署的预浸料
公开(公告)号：US09381719B2
公开(公告)日：2016-07-05
申请号：US12305656
申请日：2007-07-10
申请人： Brigitte Defoort , Dominique Lacour , Olivier Le-Couls
发明人： Brigitte Defoort , Dominique Lacour , Olivier Le-Couls
IPC分类号： B32B7/04 , B29C65/14 , B29C65/48 , B29C65/00 , B29C70/30 , B29C70/54 , B29C70/86 , C08G59/68 , B29C35/08 , B29C53/30 , B29K63/00 , B29K105/24 , B29K105/00 , B29L22/02 , B29L31/30 , B29L31/60 , B29L31/00 , B64G1/22
CPC分类号： B32B7/045 , B29C35/0894 , B29C53/30 , B29C65/14 , B29C65/1403 , B29C65/1406 , B29C65/1409 , B29C65/1435 , B29C65/1496 , B29C65/48 , B29C65/4815 , B29C65/4845 , B29C66/1122 , B29C66/21 , B29C66/52241 , B29C66/63 , B29C66/71 , B29C66/721 , B29C66/7212 , B29C66/72141 , B29C66/73754 , B29C66/7394 , B29C66/73941 , B29C70/305 , B29C70/54 , B29C70/86 , B29C2035/0827 , B29K2063/00 , B29K2105/243 , B29K2105/258 , B29L2022/02 , B29L2031/3097 , B29L2031/605 , B29L2031/703 , B64G2001/224 , C08G59/68 , Y10T156/1049 , Y10T156/1051 , Y10T428/13 , Y10T428/1362 , Y10T428/24479 , Y10T428/24488 , Y10T428/2457 , Y10T428/24802 , Y10T428/24826 , B29K2309/08 , B29C65/00
摘要： The invention relates to a method of assembling pre-impregnated plies by local isolated polymerization of the assembly region (30) under the action of a radiation to which the resin of the prepreg is sensitive.The assembly method makes it possible in particular to produce very large sized gossamer structures (7) in the form of a concertina-folded tube which is deployed by injecting pressurized gas once in space then stiffened by polymerization under the effect of the same radiation. The pylon concerned (7) thus comprises two structural elements (10, 20) secured end to end while at the same time maintaining its flexibility and firmness qualities.
摘要翻译：本发明涉及一种通过在预浸料树脂对其敏感的辐射作用下组装区域（30）的局部分离聚合来组装预浸层的方法。组装方法使得可以特别地生产以三角折叠管形式的非常大尺寸的游丝结构（7），其通过在空间中注入加压气体而展开，然后在相同辐射的作用下通过聚合加强。因此，所涉及的挂架（7）包括两个结构元件（10,20），同时保持其柔性和坚固性质。

10. 发明申请

US20090211188A1 MULTILAYERED WALL ESPECIALLY CONSISTING OF GOSSAMER-TYPE INFLATABLE STRUCTURES 审中-公开
标题翻译：多层墙壁特别包含GOSSAMER型可充气结构
公开(公告)号：US20090211188A1
公开(公告)日：2009-08-27
申请号：US11574030
申请日：2005-08-10
申请人： Brigitte Defoort , Dominique Lacour
发明人： Brigitte Defoort , Dominique Lacour
IPC分类号： E04C2/20
CPC分类号： B32B27/065 , B32B5/18 , B32B7/12 , B32B27/08 , B32B27/12 , B32B27/281 , B32B2260/021 , B32B2260/046 , B32B2266/025 , H01Q1/081
摘要： A multilayer wall includes Gossamer-type rigidifiable and inflatable structures, the wall including a layer of a composite material that can be rigidified by polymerisation, and is flanked, on the inside, by a gas-impermeable layer, and, on the outside, by at least one anti-adhesion and protection layer. The multilayer wall is characterised in that the external layer is partially permeable to gas and impermeable to liquid or viscous phases of the matrix of the composite material.
摘要翻译：多层壁包括Gossamer型可刚性和可膨胀的结构，该壁包括复合材料层，该复合材料层可通过聚合而被硬化，并且在内侧由不透气层侧面，并且在外侧由至少一个防粘附和保护层。多层壁的特征在于，外层对于气体是部分透气的，并且对于复合材料的基质的液体或粘性相是不可渗透的。

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