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1.发明申请COMPACTING AND INJECTION MOLD FOR A FIBER PREFORM FOR FABRICATING A TURBINE ENGINE GUIDE VANE MADE OF COMPOSITE MATERIAL 有权用于制造复合材料的涡轮发动机引导件的纤维预制件的压制和注射模具公开(公告)号：US20140197567A1
公开(公告)日：2014-07-17
申请号：US14115771
申请日：2012-05-03
IPC分类号： B29C45/00
CPC分类号： B29C45/0005 , B29C70/48 , B29D99/0025
摘要： A compacting and injection mold for a fiber preform is for use in fabricating a turbine engine guide vane out of composite material. The mold includes a shell forming a trough that is to receive the fiber preform and that is closed in leaktight manner by bottom and top covers, compacting blocks arranged inside the trough each having a surface pressing normally against a surface of the fiber preform that is to be compacted, and closure blocks arranged inside the trough. Each closure block has a surface pressing normally against a surface of a compacting block and does not have a surface in contact with the fiber preform.
摘要翻译： 用于纤维预制棒的压实和注射模具用于从复合材料制造涡轮发动机引导叶片。 模具包括形成槽的壳体，其接收纤维预制件并且通过底部和顶盖以密封的方式封闭，排列在槽内的压实块各自具有正常地压靠在纤维预制件的表面上的表面， 压实，封闭块布置在槽内。 每个封闭块具有通常抵靠压实块的表面的表面，并且不具有与纤维预制件接触的表面。
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2.发明申请DEVICE FOR MANUFACTURING A CASING MADE OF A COMPOSITE MATERIAL AND MANUFACTURING METHOD USING SUCH A DEVICE 有权用于制造复合材料的壳体的装置和使用这种装置的制造方法公开(公告)号：US20130087955A1
公开(公告)日：2013-04-11
申请号：US13641974
申请日：2011-04-20
IPC分类号： B29C45/00
CPC分类号： B29C45/0005 , B29C33/38 , B29C33/3828 , B29C70/462 , B29C70/48 , B29C70/54 , B29K2105/258 , B29L2023/00 , B29L2031/7504 , F01D21/045 , F02C7/04 , F05D2300/603 , Y02T50/672
摘要： A device for manufacturing a fan casing of a turbomachine made of composite material, in which a mold includes a cylindrical body of lengthways axis and side flanges, and in which a counter-mold includes a cylindrical body and side counter-flanges. The counter-flanges are configured to be attached securely to the flanges, the body of the mold and the body of the counter-mold are concentric, the preform is configured to be positioned between the body of the mold and the body of the counter-mold, and the material of the body of the mold has an appreciably higher expansion coefficient than that of the body of the counter-mold.
摘要翻译： 一种用于制造由复合材料制成的涡轮机的风扇壳体的装置，其中模具包括纵向轴线和侧凸缘的圆柱体，并且其中对模具包括圆柱体和侧对置凸缘。 相对凸缘构造成牢固地附接到凸缘，模具的主体和对模的主体是同心的，预成型件构造成定位在模具的主体和反向模具的主体之间， 模具，并且模具的主体的材料具有比反模具的主体的膨胀系数明显更高的膨胀系数。
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3.发明申请SOUNDPROOFING PANEL FOR TURBOMACHINE AND TURBOMACHINE COMPRISING SUCH A PANEL 有权用于包含这种面板的涡轮机和涡轮机的防振面板公开(公告)号：US20130048414A1
公开(公告)日：2013-02-28
申请号：US13588669
申请日：2012-08-17
申请人： Florian Gaudry , Romain Plante , Noël Robin , Georges Jean Xavier Riou , Jacky Novi Mardjono , François Marie Paul Marlin
发明人： Florian Gaudry , Romain Plante , Noël Robin , Georges Jean Xavier Riou , Jacky Novi Mardjono , François Marie Paul Marlin
CPC分类号： F02C7/045 , B64D33/02 , B64D2033/0206 , F01D25/243 , F05D2250/283 , F05D2260/30 , F05D2260/962 , Y02T50/672 , Y10T29/49236
摘要： One-piece soundproofing panel intended to be attached within an circumferential air blower casing of a turbomachine, comprising an axis, in which circulates an airflow from upstream to downstream, the panel including a circumferential rigid seat comprising a longitudinal cylindrical part, arranged to axially extend with respect to the axis A of the turbomachine, comprising an outside surface, intended to come to extend facing with an internal surface of the air blower casing, and an internal surface to which is applied a soundproofing coating and an annular fastening flange, formed at the upstream end of the longitudinal cylindrical part, radially outwardly extending, the fastening flange being arranged to cooperate with a fastening flange of the air blower casing.
摘要翻译： 一体式隔音面板旨在附接在涡轮机的周向鼓风机壳体内，包括轴线，其中使来自上游到下游的气流循环，该轴线包括包括纵向圆柱形部分的周向刚性座，该圆周刚性座设置成轴向延伸 相对于涡轮机的轴线A，包括外表面，其旨在面向鼓风机壳体的内表面延伸，并且内表面上施加有隔音涂层和环形紧固凸缘，所述外表面形成在 纵向圆柱形部分的上游端径向向外延伸，紧固凸缘被布置成与鼓风机壳体的紧固凸缘配合。
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4.发明申请LIQUID SUCTION DEVICE COMPRISING A TIP REDUCING THE FORMATION OF A SUCTION VORTEX 审中-公开液体吸收装置，包括减少形成吸收口味的提示公开(公告)号：US20140083548A1
公开(公告)日：2014-03-27
申请号：US14118074
申请日：2012-05-25
申请人： Romain Plante , Louis Bettega , Frank Louis
发明人： Romain Plante , Louis Bettega , Frank Louis
IPC分类号： F16L35/00
CPC分类号： F16L35/005 , F04D29/708
摘要： A device for suctioning a liquid contained in a vessel, that includes a take-up tube that is received in the vessel such that a bottom end of the section is submerged in the liquid. The bottom end of the take-up tube is extended downward by a rotationally symmetrical tip which has a main substantially vertical axis open downward and which includes an outer radial collar.
摘要翻译： 一种用于抽吸容纳在容器中的液体的装置，其包括容纳在容器中的卷取管，使得该部分的底端浸没在液体中。 卷取管的底端向下延伸一个旋转对称的顶端，该顶端具有向下敞开的主要基本上垂直的轴线，并且包括一个外径向套环。
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公开(公告)号：US09868235B2
公开(公告)日：2018-01-16
申请号：US14115771
申请日：2012-05-03
CPC分类号： B29C45/0005 , B29C70/48 , B29D99/0025
摘要： A compacting and injection mold for a fiber preform is for use in fabricating a turbine engine guide vane out of composite material. The mold includes a shell forming a trough that is to receive the fiber preform and that is closed in leaktight manner by bottom and top covers, compacting blocks arranged inside the trough each having a surface pressing normally against a surface of the fiber preform that is to be compacted, and closure blocks arranged inside the trough. Each closure block has a surface pressing normally against a surface of a compacting block and does not have a surface in contact with the fiber preform.
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6.发明授权Device for manufacturing a casing made of a composite material and manufacturing method using such a device 有权用于制造由复合材料制成的壳体的装置和使用这种装置的制造方法公开(公告)号：US09399315B2
公开(公告)日：2016-07-26
申请号：US13641974
申请日：2011-04-20
IPC分类号： B29C70/48 , B29C45/00 , B29C33/38 , B29C70/46 , B29C70/54 , F01D21/04 , F02C7/04 , B29K105/00 , B29L23/00 , B29L31/00
CPC分类号： B29C45/0005 , B29C33/38 , B29C33/3828 , B29C70/462 , B29C70/48 , B29C70/54 , B29K2105/258 , B29L2023/00 , B29L2031/7504 , F01D21/045 , F02C7/04 , F05D2300/603 , Y02T50/672
摘要： A device for manufacturing a fan casing of a turbomachine made of composite material, in which a mold includes a cylindrical body of lengthways axis and side flanges, and in which a counter-mold includes a cylindrical body and side counter-flanges. The counter-flanges are configured to be attached securely to the flanges, the body of the mold and the body of the counter-mold are concentric, the preform is configured to be positioned between the body of the mold and the body of the counter-mold, and the material of the body of the mold has an appreciably higher expansion coefficient than that of the body of the counter-mold.
摘要翻译： 一种用于制造由复合材料制成的涡轮机的风扇壳体的装置，其中模具包括纵向轴线和侧凸缘的圆柱体，并且其中对模具包括圆柱体和侧对置凸缘。 相对凸缘构造成牢固地附接到凸缘，模具的主体和对模的主体是同心的，预成型件构造成定位在模具的主体和反向模具的主体之间， 模具，并且模具的主体的材料具有比反模具的主体的膨胀系数明显更高的膨胀系数。
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7.发明授权Soundproofing panel for turbomachine and turbomachine comprising such a panel 有权包括这种面板的涡轮机和涡轮机的隔音面板公开(公告)号：US08544598B2
公开(公告)日：2013-10-01
申请号：US13588669
申请日：2012-08-17
申请人： Florian Gaudry , Romain Plante , Noel Robin , Georges Jean Xavier Riou , Jacky Novi Mardjono , Francois Marie Paul Marlin
发明人： Florian Gaudry , Romain Plante , Noel Robin , Georges Jean Xavier Riou , Jacky Novi Mardjono , Francois Marie Paul Marlin
IPC分类号： B64D33/02
CPC分类号： F02C7/045 , B64D33/02 , B64D2033/0206 , F01D25/243 , F05D2250/283 , F05D2260/30 , F05D2260/962 , Y02T50/672 , Y10T29/49236
摘要： A one-piece soundproofing panel which is attached within an circumferential air blower casing of a turbomachine, with an axis, in which circulates an airflow from upstream to downstream, is disclosed. The panel includes a circumferential rigid seat with a longitudinal cylindrical part, arranged to axially extend with respect to the axis A of the turbomachine, having an outside surface, intended to come to extend facing with an internal surface of the air blower casing, and an internal surface to which is applied a soundproofing coating; and an annular fastening flange, formed at the upstream end of the longitudinal cylindrical part, radially outwardly extending, the fastening flange being arranged to cooperate with a fastening flange of the air blower casing.
摘要翻译： 公开了一种连接在涡轮机的周向鼓风机壳体内的一体式隔音板，其具有从上游到下游循环气流的轴线。 面板包括具有纵向圆柱形部分的圆周刚性座，该圆周刚性座被布置为相对于涡轮机的轴线A轴向延伸，具有外表面，旨在面向鼓风机壳体的内表面延伸，并且 内表面应用隔音涂层; 以及形成在所述纵向圆柱形部分的上游端处的径向向外延伸的环形紧固凸缘，所述紧固凸缘被布置成与所述鼓风机壳体的紧固凸缘配合。
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