公开(公告)号：US20230373134A1

公开(公告)日：2023-11-23

申请号：US18309374

申请日：2023-04-28

Applicant: Airbus Operations (S.A.S.)

Inventor： Gérard Millet ,  Vincent Delpy ,  Simon Foucart-Gaudy

IPC: B29C39/10 ,  B64D37/04

CPC classification number: B29C39/10 ,  B64D37/04 ,  B29L2031/3076

Abstract: A tool for laying a sealing strip around a protruding part of a connecting element protruding from a bearing surface, the laying tool including an annular duct having an outer surface configured to delimit, with the bearing surface and the protruding part, a cavity when the annular duct is positioned around the protruding part and in contact with the bearing surface, the annular duct including at least one orifice for supplying pasty composition and outlet orifices for injecting the pasty composition into the cavity to form the sealing strip. A method for laying a sealing strip using the tool is disclosed and an aircraft with at least one sealing strip obtained using the method.

公开(公告)号：US12038036B2

公开(公告)日：2024-07-16

申请号：US17477981

申请日：2021-09-17

Applicant: Airbus Operations S.A.S.

Inventor： Simon Foucart-Gaudy ,  Vincent Delpy ,  Gerard Millet

IPC: F16B43/02 ,  F16B43/00 ,  F16J15/02 ,  F16B5/02

CPC classification number: F16B43/001 ,  F16J15/022 ,  F16B5/02

Abstract: A seal includes a barrel extending between a base and a top, in which the barrel has a cylindrical cavity passing through it between its base and its top, and a skirt indissociable from the barrel and extending around said barrel, in which the skirt adopts the shape of a dome of which the exterior edges extend out beyond the base starting from the top. The seal is able to divert the fluid and keep the space under the skirt fluid tight.

公开(公告)号：US20240200707A1

公开(公告)日：2024-06-20

申请号：US18538069

申请日：2023-12-13

Applicant: Airbus Operations (S.A.S.)

Inventor： Gérard Millet ,  Vincent Delpy ,  Simon Foucart-Gaudy ,  Marc-Antoine Brocard

IPC: F16L41/08

CPC classification number: F16L41/08

Abstract: A sleeve fastening system fastened to a joist pierced with a hole and receiving two pipes and including a cylinder fitted into the hole of which each end receives a pipe, wherein the wall of the cylinder has cut into it at least one tunnel, a flange, each tunnel having openings that emerge on either side of the flange that has a bearing face bearing against the joist and a free face, and for each tunnel, a holding system having a link, a shoe and a locking system, the link being housed in the tunnel with the shoe blocked in a first opening on the side of the free face and wherein the link exits via a second opening on the side of the bearing face and wherein the locking system attaches.

公开(公告)号：US20220106978A1

公开(公告)日：2022-04-07

申请号：US17477981

申请日：2021-09-17

Applicant: Airbus Operations S.A.S.

Inventor： Simon Foucart-Gaudy ,  Vincent Delpy ,  Gerard Millet

IPC: F16B43/00 ,  F16J15/02

Abstract: A seal includes a barrel extending between a base and a top, in which the barrel has a cylindrical cavity passing through it between its base and its top, and a skirt indissociable from the barrel and extending around said barrel, in which the skirt adopts the shape of a dome of which the exterior edges extend out beyond the base starting from the top. The seal is able to divert the fluid and keep the space under the skirt fluid tight.