公开(公告)号：US20250115040A1

公开(公告)日：2025-04-10

申请号：US18903734

申请日：2024-10-01

Applicant: SAFRAN AIRCRAFT ENGINES

Inventor： Pierre Antoine BOSSAN ,  Sophie ESSAYAN ,  Allison GLUGLA ,  Jordan KUSCH ,  Benjamin SAMSON

IPC: B32B37/12 ,  B29C65/00 ,  B29C65/48 ,  B29C65/50 ,  B29C65/52 ,  B29L31/08 ,  B32B7/06 ,  B32B7/12 ,  B32B15/08 ,  B32B27/20

Abstract: An adhesively bonded assembly of a first substrate on a second substrate by means of an adhesive joint integrating a support mesh, wherein the support mesh is present after curing over the entire adhesively bonded zone between the first and second substrates.

公开(公告)号：US20230182411A1

公开(公告)日：2023-06-15

申请号：US17980931

申请日：2022-11-04

Applicant: SAFRAN AIRCRAFT ENGINES

Inventor： Maxime Marie Désiré BLAISE ,  Allison GLUGLA ,  Lauren CHIN ,  Cali LAPENTA

IPC: B29C70/44

CPC classification number: B29C70/44 ,  B64C21/10

Abstract: A method for producing an aerodynamic element for an aircraft, including a wall which is covered, at least partially, by a printed film including a plurality of ribs and/or grooves, the method including: providing a raw film made of a deformable material which is devoid of grooves and ribs; providing a pressure plate which includes a face provided with ribs and/or grooves complementary to the ribs and/or grooves of the printed film; placing said raw film on the wall of the element; positioning the pressure plate on the raw film, the printed side of the pressure plate facing the raw film; and a forming step during which the raw film is bonded with the wall of the component and during which the raw film is shaped by cooperation with the pressure plate to obtain the printed film including the ribs and/or the grooves.

公开(公告)号：US20220266584A1

公开(公告)日：2022-08-25

申请号：US17618182

申请日：2020-06-18

Applicant: SAFRAN AIRCRAFT ENGINES

Inventor： Pierre Antoine BOSSAN ,  Sophie ESSAYAN ,  Allison GLUGLA ,  Jordan KUSCH ,  Benjamin SAMSON

IPC: B32B37/12 ,  B32B7/12 ,  B32B7/06 ,  B32B15/08 ,  B32B27/20 ,  B29C65/48 ,  B29C65/50 ,  B29C65/52 ,  B29C65/00

Abstract: A method of adhesively bonding a first substrate on a second substrate in an adhesive bonding zone by an adhesive joint integrating a support mesh, wherein surplus adhesive joint is folded over onto one or the other of the first or second substrates so that the support mesh is present over the entire adhesively bonded zone after curing.