公开(公告)号：US20170259318A1

公开(公告)日：2017-09-14

申请号：US15454896

申请日：2017-03-09

Applicant: STELIA AEROSPACE

Inventor： Damien Sireude ,  Daniel Perherin

IPC: B21D7/16

Abstract: Machine for bending at least one longitudinal cylindrical pipe, the bending machine having at least one heating module configured so as to heat a longitudinal cylindrical pipe and at least one deformation module configured so as to deform a longitudinal portion of a longitudinal cylindrical pipe in order to bend it, said heating module having a plurality of heating units, each heating unit can include a peripheral heating body defining an internal opening adapted to allow the passage of a longitudinal portion of a longitudinal cylindrical pipe to be heated.

公开(公告)号：US10711934B2

公开(公告)日：2020-07-14

申请号：US15377739

申请日：2016-12-13

Applicant: Stelia Aerospace

Inventor： Damien Sireude

IPC: F16L37/098 ,  F16L37/14 ,  B21D9/00 ,  F16L37/00 ,  F16L41/02 ,  F16L47/02

Abstract: A method for manufacturing a pipe is described, wherein the method comprises a step of fastening a second mechanical quick connection member to a rectilinear hollow tubular body, a step of positioning the rectilinear hollow tubular body in a bending machine so that the angular coding mechanism of the second mechanical quick connection member is in a reference angular position with respect to said bending machine, and a step of bending the rectilinear hollow tubular body as a function of said angular reference position.

公开(公告)号：US10471490B2

公开(公告)日：2019-11-12

申请号：US15454896

申请日：2017-03-09

Applicant: STELIA AEROSPACE

Inventor： Damien Sireude ,  Daniel Perherin

IPC: B21D7/00 ,  B21D7/16

Abstract: Machine for bending at least one longitudinal cylindrical pipe, the bending machine having at least one heating module configured so as to heat a longitudinal cylindrical pipe and at least one deformation module configured so as to deform a longitudinal portion of a longitudinal cylindrical pipe in order to bend it, said heating module having a plurality of heating units, each heating unit can include a peripheral heating body defining an internal opening adapted to allow the passage of a longitudinal portion of a longitudinal cylindrical pipe to be heated.

公开(公告)号：US20190316717A1

公开(公告)日：2019-10-17

申请号：US16469884

申请日：2017-12-06

Applicant: Stelia Aerospace

Inventor： Damien Sireude ,  Daniel Perherin ,  Thierry Aletrut ,  Pascal Solana ,  Dimitri Rouyard

IPC: F16L37/138 ,  F16L25/12 ,  F16L37/12 ,  F16L17/02

Abstract: A fluid circuit, particularly for an aircraft, comprising a first pipe, a second pipe and a coupling comprising an outer sleeve which extends along an axis X and is mounted with the ability to slide along the axis X at a connection ends of the first pipe, a sealing member which extends along the axis X and is mounted with the ability to slide along the axis X in said outer sleeve, the sealing member being configured to sealingly connect the connection ends of the pipes, locking means configured to collaborate with a blocking member of the second pipe so as to block the translational movement of said outer sleeve towards the first pipe, the coupling being configured to move the sealing member between the two connection ends in order to provide sealing as the outer sleeve is moved as far as the blocking member of the second pipe.

公开(公告)号：US20170191594A1

公开(公告)日：2017-07-06

申请号：US15377739

申请日：2016-12-13

Applicant: Stelia Aerospace

Inventor： Damien Sireude

IPC: F16L37/098 ,  B21D9/00 ,  F16L37/00

Abstract: A method for manufacturing a pipe, the method comprising: a step of fastening a second mechanical quick connection member to a rectilinear hollow tubular body, a step of positioning the rectilinear hollow tubular body in a bending machine so that the angular coding mechanism of the second mechanical quick connection member is in a reference angular position with respect to said bending machine, and a step of bending the rectilinear hollow tubular body as a function of said angular reference position.