-
1.发明授权Process for manufacturing a component with an insert made of a composite consisting of a metal matrix and ceramic fibers 有权用由金属基体和陶瓷纤维组成的复合体制成的嵌件的制造方法公开(公告)号：US07987574B2
公开(公告)日：2011-08-02
申请号：US11441156
申请日：2006-05-26
CPC分类号： C22C47/064 , B22F2998/00 , B23K11/0026 , B23K2101/34 , B23K2103/16 , C22C49/11 , Y10T29/49801 , Y10T29/49968 , B22F1/025
摘要： A process for manufacturing a component with an insert made of a composite is disclosed. The composite includes a metal matrix, within which ceramic fibers extend. The insert is made of a composite which is obtained from a plurality of coated filaments, each filament includes a ceramic fiber coated with a metal sheath. The process includes winding a bundle or bonded sheet of coated filaments around a body of revolution perpendicular to the axis of rotation of said body. The insert is then subjected to a hot isostatic pressing step in a container. The process is applied to the manufacture of aeronautical turbomachine components.
摘要翻译： 公开了一种制造具有由复合材料制成的插入件的部件的方法。 复合材料包括金属基体，陶瓷纤维在其中延伸。 该插入物由多个涂覆的长丝获得的复合材料制成，每个细丝包括涂有金属护套的陶瓷纤维。 该方法包括绕垂直于所述主体的旋转轴线的旋转体围绕卷绕或粘合的涂覆丝的片材。 然后将该插入物在容器中进行热等静压步骤。 该过程适用于航空涡轮机组件的制造。
-
2.发明申请CUTTING OF PREFORMS PRIOR TO RTM INJECTION BY MEANS OF A WATER JET AND CRYONICS 有权通过水喷射和CRYONICS切割RTM注射器前的切片公开(公告)号：US20120297943A1
公开(公告)日：2012-11-29
申请号：US13577289
申请日：2011-02-10
IPC分类号： B26D7/08
CPC分类号： B26D7/10 , B26F3/00 , B26F3/004 , B26F3/008 , B26F2003/006 , Y10T83/041 , Y10T83/283
摘要： A device for cutting a fibrous preform, for production of a part made of a composite material by injection of resin under vacuum. The device includes a die for receiving the preform, on which a template of outer edges of the part is referenced, a mechanism cutting outer edges of the preform according to the template, and a mechanism for cooling the preform that is suitable for solidifying a liquid forming a substrate for the preform.
摘要翻译： 一种用于切割纤维预型件的装置，用于通过在真空下注射树脂来生产由复合材料制成的零件。 该装置包括用于接收预成型件的模具，在该模具上以部件的外边缘的模板为参照，根据模板切割预成型件的外边缘的机构，以及用于冷却预成型件的机构，其适于固化液体 形成预成型件的基底。
-
3.发明授权Cutting of preforms prior to RTM injection by means of a water jet and cryonics 有权在通过水射流和冷冻法进行RTM注射前切割预成型件公开(公告)号：US09108331B2
公开(公告)日：2015-08-18
申请号：US13577289
申请日：2011-02-10
CPC分类号： B26D7/10 , B26F3/00 , B26F3/004 , B26F3/008 , B26F2003/006 , Y10T83/041 , Y10T83/283
摘要： A device for cutting a fibrous preform, for production of a part made of a composite material by injection of resin under vacuum. The device includes a die for receiving the preform, on which a template of outer edges of the part is referenced, a mechanism cutting outer edges of the preform according to the template, and a mechanism for cooling the preform that is suitable for solidifying a liquid forming a substrate for the preform.
摘要翻译： 一种用于切割纤维预型件的装置，用于通过在真空下注射树脂来生产由复合材料制成的零件。 该装置包括用于接收预成型件的模具，在该模具上以部件的外边缘的模板为参照，根据模板切割预成型件的外边缘的机构，以及用于冷却预成型件的机构，其适于固化液体 形成预成型件的基底。
-
4.发明申请Process for manufacturing a component with an insert made of a composite consisting of a metal matrix and ceramic fibers 有权用由金属基体和陶瓷纤维组成的复合体制成的嵌件的制造方法公开(公告)号：US20070051455A1
公开(公告)日：2007-03-08
申请号：US11441156
申请日：2006-05-26
IPC分类号： B65H81/00
CPC分类号： C22C47/064 , B22F2998/00 , B23K11/0026 , B23K2101/34 , B23K2103/16 , C22C49/11 , Y10T29/49801 , Y10T29/49968 , B22F1/025
摘要： Process for manufacturing a component with an insert made of a composite comprising a metal matrix, within which ceramic fibers extend, the insert made of a composite being obtained from a plurality of coated filaments, each comprising a ceramic fiber coated with a metal sheath, characterized in that it comprises the manufacture of an insert with a step of winding a bundle or bonded sheet of coated filaments around a body of revolution perpendicular to the axis of rotation of said body. The insert is then subjected to a hot isostatic pressing step in a container. The process is applied to the manufacture of aeronautical turbomachine components.
摘要翻译： 制造具有由包含金属基质（其中陶瓷纤维延伸的）的复合材料制成的嵌件的组件的方法，由复合材料制成的插入件由多个涂覆的长丝获得，每个包括涂覆有金属护套的陶瓷纤维，其特征在于 因为它包括制造插入件，该插入件具有绕垂直于所述主体的旋转轴线的旋转体周围卷绕包裹的纤维束或粘合片材的步骤。 然后将该插入物在容器中进行热等静压步骤。 该过程适用于航空涡轮机组件的制造。
-
-
-
搜索结果
4 条记录 (耗时 0.008 秒)
