公开(公告)号：US20150274912A1

公开(公告)日：2015-10-01

申请号：US14432751

申请日：2013-10-08

Applicant: AIRBUS GROUP SAS

Inventor： Frédérick Cavaliere ,  Alain Renoncourt ,  Patrice Lefebure

IPC: C08J5/24 ,  B32B5/02 ,  B29C43/30

CPC classification number: C08J5/24 ,  B29B15/10 ,  B29C43/305 ,  B29C70/386 ,  B29K2101/10 ,  B29K2105/0872 ,  B29L2009/00 ,  B32B5/02 ,  B32B2260/02 ,  B32B2260/046 ,  B32B2262/106 ,  B32B2305/076 ,  C08J2363/00 ,  Y10T428/31511

Abstract: A process for fabricating a partially polymerized prepreg material. Fibers are impregnated with thermosetting resin. The resin is partially polymerized to a degree of polymerization between 10% and 60%. The thermosetting composite parts are produced by placement of fibers of the prepreg material. The material is laid-up in the form of rovings and heated at a temperature above the glass transition temperature of the prepreg state. The laid-up material is pressed and cooled to return to a temperature below the glass transition temperature of the prepreg state. The temperatures and the pressure are determined so that the part obtained has a void content of less than 4% by volume.

Abstract translation: 一种制备部分聚合的预浸料坯材料的方法。 纤维用热固性树脂浸渍。 树脂部分聚合至10％至60％之间的聚合度。 通过放置预浸料坯料的纤维来制造热固性复合部件。 将材料以粗纱的形式放置并在高于预浸料状态的玻璃化转变温度的温度下加热。 将被压材料压制并冷却以回到低于预浸料状态的玻璃化转变温度的温度。 确定温度和压力使得所获得的部分的空隙含量小于4体积％。

公开(公告)号：US10576692B2

公开(公告)日：2020-03-03

申请号：US15508446

申请日：2015-09-01

Applicant: AIRBUS GROUP SAS

Inventor： Frédérick Cavaliere ,  Christophe Paris ,  Daniel Aliaga

IPC: B29C65/00 ,  B29C65/50 ,  B29C70/44 ,  B29C35/02 ,  B29C70/54 ,  B29C65/48 ,  C08J5/24 ,  B29K101/10 ,  B29K105/08

Abstract: A part made of a fiber-reinforced composite material includes a structure made from a set of fibers supported in a thermosetting resin and a peel ply across all or part of the outer surface of the structure. The part has a gradient of polymerization at the interface between the structure and the peel ply. Also, methods for making such a part and methods for bonding such parts.