Patents by Inventor Didier Pasquiet
Didier Pasquiet has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).
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Patent number: 9546561Abstract: A labyrinth disk for a turbomachine is provided. The disk includes a hub, a web and a frustoconical peripheral portion, having on one face labyrinth seal teeth and on the other face radial ribs. The flanks of the ribs delimit, between one another, channels which open out at the periphery of the disk. The width of the channels decreases from the base of the frustoconical portion to the opening at the periphery. The ribs are split close to the periphery, and a recess is created between the two flanks of one and the same rib.Type: GrantFiled: July 17, 2013Date of Patent: January 17, 2017Assignee: SNECMAInventors: Emilie Pouzet, Didier Pasquiet, Frederic Lespinasse
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Patent number: 9494042Abstract: A sealing ring configured to be pressed against a rotor disc of a turbine stage for an aircraft turbomachine, the ring including a plurality of anti-rotation pegs which prevent it from rotating in relation to the rotor disc, each peg protruding axially from a ring body and including two opposite circumferential-end surfaces, respectively configured to be located facing two directly consecutive blades carried on the rotor disc. An axially opening slot passes radially through at least one of the anti-rotation pegs.Type: GrantFiled: March 29, 2012Date of Patent: November 15, 2016Assignee: SNECMAInventors: Emilie Pouzet, Pascal Casaliggi, Didier Pasquiet
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Patent number: 9114469Abstract: A wall in which there is formed at least one cooling channel, said wall being cooled by cool air flowing in the channel, the channel comprising a hole and a diffusion portion, the hole opening out at one end into the inside surface of the wall, and at its other end into the diffusion portion where it forms an orifice, the diffusion portion flaring around said orifice and opening out into the outside surface of the wall, the diffusion portion having a bottom whose front end is substantially plane, sloping, and extending in front of the orifice, and also having a margin extending behind, round the sides, and in front of the orifice, said margin joining the sides of the front end. A method and an electrode for making such a cooling channel. A turbomachine blade presenting such a wall.Type: GrantFiled: August 18, 2014Date of Patent: August 25, 2015Assignee: SNECMAInventors: Emmanuel Pierre Camhi, Laurent Crouilbois, Jean Pierre Mareix, Didier Pasquiet
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Publication number: 20150159496Abstract: A sealing ring configured to be pressed against a rotor disc of a turbine stage for an aircraft turbomachine, the ring including a plurality of anti-rotation pegs which prevent it from rotating in relation to the rotor disc, each peg protruding axially from a ring body and including two opposite circumferential-end surfaces, respectively configured to be located facing two directly consecutive blades carried on the rotor disc. An axially opening slot passes radially through at least one of the anti-rotation pegs.Type: ApplicationFiled: March 29, 2012Publication date: June 11, 2015Applicant: SNECMAInventors: Emilie Pouzet, Pascal Casaliggi, Didier Pasquiet
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Publication number: 20140353284Abstract: A wall in which there is formed at least one cooling channel, said wall being cooled by cool air flowing in the channel, the channel comprising a hole and a diffusion portion, the hole opening out at one end into the inside surface of the wall, and at its other end into the diffusion portion where it forms an orifice, the diffusion portion flaring around said orifice and opening out into the outside surface of the wall, the diffusion portion having a bottom whose front end is substantially plane, sloping, and extending in front of the orifice, and also having a margin extending behind, round the sides, and in front of the orifice, said margin joining the sides of the front end. A method and an electrode for making such a cooling channel. A turbomachine blade presenting such a wall.Type: ApplicationFiled: August 18, 2014Publication date: December 4, 2014Applicant: SNECMAInventors: Emmanuel Pierre CAMHI, Laurent Crouilbois, Jean Pierre Mareix, Didier Pasquiet
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Patent number: 8875393Abstract: A method for forming at least one cooling channel in a wall which is cooled by cool air flowing in the channel is provided. The channel includes a hole and a diffusion portion, the hole opening out at one end into the inside surface of the wall, and at its other end into the diffusion portion where it forms an orifice. The diffusion portion flares around the orifice and opens out into the outside surface of the wall. The diffusion portion has a bottom whose front end is substantially plane, sloping, and extending in front of the orifice, and also has a margin extending behind, round the sides, and in front of the orifice, the margin joining the sides of the front end.Type: GrantFiled: May 26, 2010Date of Patent: November 4, 2014Assignee: SNECMAInventors: Emmanuel Pierre Camhi, Laurent Crouilbois, Jean Pierre Mareix, Didier Pasquiet
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Publication number: 20140271150Abstract: The present invention relates to a labyrinth disk for a turbomachine comprising a hub, a web and a frustoconical peripheral portion, having on one face labyrinth seal teeth and on the other face radial ribs (78?) the flanks (78?f) of which delimit, between one another, channels (80) which open out at the periphery of the disk, the width of said channels decreasing from the base of the frustoconical portion to the opening at the periphery, wherein the ribs are split close to the periphery, a recess (79?) being created between the two flanks (78?f) of one and the same rib.Type: ApplicationFiled: July 17, 2013Publication date: September 18, 2014Inventors: Emilie POUZET, Didier Pasquiet, Frederic Lespinasse
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Patent number: 7950902Abstract: A wall in which there is formed at least one cooling channel, said wall being cooled by cool air flowing in the channel, the channel comprising a hole and a diffusion portion, the hole opening out at one end into the inside surface of the wall, and at its other end into the diffusion portion where it forms an orifice, the diffusion portion flaring around said orifice and opening out into the outside surface of the wall, the diffusion portion having a bottom whose front end is substantially plane, sloping, and extending in front of the orifice, and also having a margin extending behind, round the sides, and in front of the orifice, said margin joining the sides of the front end. A method and an electrode for making such a cooling channel. A turbomachine blade presenting such a wall.Type: GrantFiled: July 25, 2006Date of Patent: May 31, 2011Assignee: SNECMAInventors: Emmanuel Pierre Camhi, Laurent Crouilbois, Jean Pierre Mareix, Didier Pasquiet
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Publication number: 20100229388Abstract: A wall in which there is formed at least one cooling channel, said wall being cooled by cool air flowing in the channel, the channel comprising a hole and a diffusion portion, the hole opening out at one end into the inside surface of the wall, and at its other end into the diffusion portion where it forms an orifice, the diffusion portion flaring around said orifice and opening out into the outside surface of the wall, the diffusion portion having a bottom whose front end is substantially plane, sloping, and extending in front of the orifice, and also having a margin extending behind, round the sides, and in front of the orifice, said margin joining the sides of the front end. A method and an electrode for making such a cooling channel. A turbomachine blade presenting such a wall.Type: ApplicationFiled: May 26, 2010Publication date: September 16, 2010Applicant: SNECMAInventors: Emmanuel Pierre CAMHI, Laurent CROUILBOIS, Mareix Jean Pierre, Didier PASQUIET
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Patent number: 7371050Abstract: A device for axially retaining blades on a rotor disk of a turbomachine, includes an annulus which is mounted via a radially inner edge in an annular groove of the disk and which presses against the roots of the blades mounted in grooves in the periphery of the disk, and an annular lock received in the annular groove of the disk to prevent the annulus from turning, the annular lock being turnable in the annular groove between an annulus-locking position and a position for mounting and dismounting in the annular groove.Type: GrantFiled: March 22, 2005Date of Patent: May 13, 2008Assignee: SnecmaInventor: Didier Pasquiet
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Publication number: 20070025852Abstract: A wall in which there is formed at least one cooling channel, said wall being cooled by cool air flowing in the channel, the channel comprising a hole and a diffusion portion, the hole opening out at one end into the inside surface of the wall, and at its other end into the diffusion portion where it forms an orifice, the diffusion portion flaring around said orifice and opening out into the outside surface of the wall, the diffusion portion having a bottom whose front end is substantially plane, sloping, and extending in front of the orifice, and also having a margin extending behind, round the sides, and in front of the orifice, said margin joining the sides of the front end. A method and an electrode for making such a cooling channel. A turbomachine blade presenting such a wall.Type: ApplicationFiled: July 25, 2006Publication date: February 1, 2007Applicant: SNECMAInventors: Emmanuel Camhi, Laurent Crouilbois, Jean Mareix, Didier Pasquiet
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Publication number: 20050271511Abstract: A device for axially retaining blades on a rotor disk of a turbomachine, the device comprising an annulus which is mounted via a radially inner edge in an annular groove of the disk and which presses against the roots of the blades mounted in grooves in the periphery of the disk, and an annular lock received in the annular groove of the disk to prevent the annulus from turning, said lock being turnable in the annular groove between an annulus-locking position and a position for mounting and dismounting in the annular groove.Type: ApplicationFiled: March 22, 2005Publication date: December 8, 2005Applicant: SNECMA MOTEURSInventor: Didier Pasquiet