公开(公告)号：US20130216767A1

公开(公告)日：2013-08-22

申请号：US13820757

申请日：2011-09-07

申请人： Jacques Cinquin

发明人： Jacques Cinquin

IPC分类号： B29C45/02 ,  B64D45/02 ,  B64G1/50 ,  B32B5/06

CPC分类号： B29C45/02 ,  B29C70/228 ,  B29C70/24 ,  B29C70/882 ,  B29K2707/04 ,  B29K2995/0005 ,  B29K2995/0013 ,  B32B5/06 ,  B64C1/12 ,  B64D45/02 ,  B64G1/50 ,  Y02T50/43 ,  Y10T428/24033

摘要： In order to produce a part (16) from a composite material, which is conductive at least on one of the surfaces thereof, the method consists of: the conductive overstitching (30) of a preform (20) of the part using electrically or thermally conductive threads (31, 32) with substantially parallel stitch lines (34) oriented in at least two intersecting directions. The parts obtained are adapted for the production of aircraft structures that may be subjected to lightning strikes and allow return currents from the electrical or electronic aircraft equipment and/or the discharge of heat by conduction.

摘要翻译： 为了从复合材料的至少一个表面上导电的复合材料产生部分（16），该方法包括：使用电或热的部件的预成型件（20）的导电覆盖（30） 具有以至少两个相交方向定向的基本上平行的针脚线（34）的导电线（31,32）。 获得的部件适于生产可能遭受雷击并允许来自电气或电子飞行器设备的返回电流和/或通过传导放出热量的飞机结构。

公开(公告)号：US09895833B2

公开(公告)日：2018-02-20

申请号：US13820757

申请日：2011-09-07

申请人： Jacques Cinquin

发明人： Jacques Cinquin

IPC分类号： B29C45/02 ,  B29C70/22 ,  B29C70/24 ,  B29C70/88 ,  B64C1/12 ,  B64D45/02 ,  B64G1/50 ,  B32B5/06 ,  B29K707/04

CPC分类号： B29C45/02 ,  B29C70/228 ,  B29C70/24 ,  B29C70/882 ,  B29K2707/04 ,  B29K2995/0005 ,  B29K2995/0013 ,  B32B5/06 ,  B64C1/12 ,  B64D45/02 ,  B64G1/50 ,  Y02T50/43 ,  Y10T428/24033

摘要： In order to produce a part (16) from a composite material, which is conductive at least on one of the surfaces thereof, the method consists of: the conductive overstitching (30) of a preform (20) of the part using electrically or thermally conductive threads (31, 32) with substantially parallel stitch lines (34) oriented in at least two intersecting directions. The parts obtained are adapted for the production of aircraft structures that may be subjected to lightning strikes and allow return currents from the electrical or electronic aircraft equipment and/or the discharge of heat by conduction.

公开(公告)号：US20110036495A1

公开(公告)日：2011-02-17

申请号：US12672563

申请日：2008-08-05

申请人： Jacques Cinquin

发明人： Jacques Cinquin

IPC分类号： B32B37/02

CPC分类号： B29C65/5085 ,  B29C35/0266 ,  B29C65/4835 ,  B29C65/5057 ,  B29C65/5071 ,  B29C66/1142 ,  B29C66/12441 ,  B29C66/43 ,  B29C66/43421 ,  B29C66/43441 ,  B29C66/43461 ,  B29C66/721 ,  B29C66/7212 ,  B29C66/72141 ,  B29C66/72143 ,  B29C66/73754 ,  B29C66/73941 ,  B29K2105/243 ,  B29L2031/3076 ,  B29K2307/04 ,  B29K2309/08 ,  B29K2277/10

摘要： To produce a complex structure made of a composite, with assembled individual parts, a method includes the steps of: producing individual parts; producing assembly components, to ensure structural bonds between the individual parts, from fibers impregnated with a resin capable of curing by polymerization, comprising fins attached to a core that determine grooves, in order to receive edges, of the individual parts, subjected to a partial thermal cure to partially polymerize the resin and give the components a dimensional stability and thermoplastic properties; positioning of the individual parts and assembly components; raising the temperature to a thermoplastic forming temperature and applying pressure P in order to apply the fins to faces of the individual parts; and carrying out a complete thermal cure for polymerization of the resin of the assembly components.

摘要翻译： 为了生产由复合材料制成的复合结构，具有组装的单个部件，一种方法包括以下步骤：制造单个零件; 制造组装部件，以确保单个部件之间的结构粘合，从浸渍有能够通过聚合固化的树脂的纤维，包括连接到确定凹槽的芯的翅片，以便接收各个部件的边缘，经受部分 热固化以部分聚合树脂并赋予组分尺寸稳定性和热塑性能; 各部件和组装部件的定位; 将温度升高到热塑性成形温度并施加压力P以便将翅片施加到各个部件的面部; 并进行完全的热固化以聚合组件的树脂。