公开(公告)号：US11572151B2

公开(公告)日：2023-02-07

申请号：US16706933

申请日：2019-12-09

Applicant: Airbus Operations SAS

Inventor： Gerard Millet ,  Bruno Alquier

IPC: B64C1/14 ,  F16L11/12 ,  F16L41/00 ,  F16L57/02

Abstract: A drain configured to evacuate leaks of fluid, such as fuel, from a leak collecting system of an aircraft, the drain comprising a rigid tube secured to a plate, the plate being configured to be attached to an external wall of the aircraft, a flexible pipe configured to join the collecting system to the rigid tube, one end of the flexible pipe being received within the rigid tube. The rigid tube comprises a channel, the channel being configured to allow separation of the rigid tube from the plate at the location of the channel.

公开(公告)号：US20180087707A1

公开(公告)日：2018-03-29

申请号：US15716064

申请日：2017-09-26

Applicant: Airbus Operations SAS

Inventor： Bruno Alquier ,  Gerard Millet ,  Thomas Menage

IPC: F16L55/168 ,  F16K27/12

CPC classification number: F16L55/168 ,  F16K27/12 ,  F16L55/07 ,  F16L57/00 ,  F16L2201/30 ,  G01M3/2861

Abstract: A connection comprising a first duct, a second duct, a flexible tube which comprises a first end configured to cover part of the first duct, and a second end configured to cover part of the second duct, a first clamping system configured to clamp the first end of the flexible tube around the first duct, and a second clamping system configured to clamp the second end of the flexible tube around the second duct.

公开(公告)号：US10415737B2

公开(公告)日：2019-09-17

申请号：US15716064

申请日：2017-09-26

Applicant: Airbus Operations SAS

Inventor： Bruno Alquier ,  Gerard Millet ,  Thomas Menage

IPC: F16L55/168 ,  F16K27/12 ,  F16L57/00 ,  F16L55/07 ,  G01M3/28

Abstract: A connection comprising a first duct, a second duct, a flexible tube which comprises a first end configured to cover part of the first duct, and a second end configured to cover part of the second duct, a first clamping system configured to clamp the first end of the flexible tube around the first duct, and a second clamping system configured to clamp the second end of the flexible tube around the second duct.

公开(公告)号：US10190703B2

公开(公告)日：2019-01-29

申请号：US15294353

申请日：2016-10-14

Applicant: Airbus Operations SAS

Inventor： Bruno Alquier ,  Clément Rivera ,  Gérard Millet

IPC: F16L3/10 ,  F16L3/12 ,  F16L3/16

Abstract: A support for a pipe which comprises a body which comprises a through-orifice for the pipe. The through-orifice has a diameter which is greater than an external diameter of the pipe. At least one base of the support is configured so as to be in contact with and connected to a fixing surface. A first ring and a second ring each have an eccentric orifice and are configured so as to be fitted one into the other in the orifice of the body about the pipe when the support is put in position. By rotating at least one of the first and second rings, the position of the axis of the pipe may be adjusted radially relative to the support.

公开(公告)号：US20170108145A1

公开(公告)日：2017-04-20

申请号：US15294353

申请日：2016-10-14

Applicant: Airbus Operations SAS

Inventor： Bruno Alquier ,  Clément Rivera ,  Gérard Millet

IPC: F16L3/12 ,  F16L3/10

CPC classification number: F16L3/1207 ,  F16L3/10 ,  F16L3/1091 ,  F16L3/16

Abstract: A support for a pipe which comprises a body which comprises a through-orifice for the pipe. The through-orifice has a diameter which is greater than an external diameter of the pipe. At least one base of the support is configured so as to be in contact with and connected to a fixing surface. A first ring and a second ring each have an eccentric orifice and are configured so as to be fitted one into the other in the orifice of the body about the pipe when the support is put in position. By rotating at least one of the first and second rings, the position of the axis of the pipe may be adjusted radially relative to the support.