Patents by Inventor Laurent Ferrer

Laurent Ferrer 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).

  • Patent number: 11673186
    Abstract: The invention relates to a method for manufacturing a metal ingot by continuous casting, comprising the following steps: S1: melting the metal, S2: transferring the liquid metal (2) by pouring it into a crucible (12), S3: moving the base plate (14) of the crucible (12), S4: progressive solidification of the liquid metal (2) from the base plate (14) of the crucible (12), and S5: during the step S3 of moving the base plate (14), applying a compression force to the metal (3) which is present between the base plate (14) and the side wall (13), the compression force being applied along a second axis (X2) parallel to the first axis (X1) so as to deform the metal and to obtain an ingot (3) which has a smaller width (L2).
    Type: Grant
    Filed: December 13, 2019
    Date of Patent: June 13, 2023
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventor: Laurent Ferrer
  • Publication number: 20230083765
    Abstract: A device for cleaning a vent of a first forging die suitable for receiving, between the first die and a second die, a metal blank to be shaped in order to produce a metal part, the device for cleaning including a pump for injecting an aqueous solution, suitable for injecting the aqueous solution into the vent, an ultrasound generator, suitable for generating ultrasound waves within the vent, an air intake suitable for ensuring a venting of the vent, and a valve system for alternately controlling at least the injection of aqueous solution and ultrasound and the venting of the vent.
    Type: Application
    Filed: January 18, 2021
    Publication date: March 16, 2023
    Inventor: Laurent FERRER
  • Patent number: 11560612
    Abstract: A method of fabricating a low alloy steel ingot, the method including a) melting all or part of an electrode by a vacuum arc remelting method, the electrode, before melting, including iron and carbon, the melted portion of the electrode being collected in a crucible, thus forming a melt pool within the crucible; and b) solidifying the melt pool by heat exchange between the melt pool and a cooling fluid, the heat exchange applied serving to impose a mean solidification speed during step b) that is less than or equal to 45 ?m/s and to obtain an ingot of low alloy steel.
    Type: Grant
    Filed: June 24, 2019
    Date of Patent: January 24, 2023
    Assignees: SAFRAN AIRCRAFT ENGINES, SAFRAN LANDING SYSTEMS
    Inventors: Laurent Ferrer, Nicolas Binot
  • Patent number: 11512369
    Abstract: A method for manufacturing an ingot made of titanium-based metallic compound, includes providing raw material fragments; melting the raw material fragments into a liquid metal in at least one basin; keeping in the molten state the liquid metal in the at least one basin; pouring the liquid metal from the at least one basin into a crucible by overflow from the at least one basin into the crucible; forming an ingot by cooling of the liquid metal into the crucible; wherein the method further includes preheating the raw material fragments before the melting of the raw material fragments with a preheating temperature higher than or equal to 75% of the liquidus temperature of the raw material fragments, and lower less than the liquidus temperature of the raw material fragments.
    Type: Grant
    Filed: June 24, 2019
    Date of Patent: November 29, 2022
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Bruno Vitorino Lopes, Laurent Ferrer
  • Patent number: 11433453
    Abstract: A device (10) for manufacturing a metal alloy blank by centrifugal casting of a molten metal alloy, comprising a centrifugal casting wheel (20), the centrifugal casting wheel (20) being rotary about an axis of rotation (A) and comprising a mold (22) for receiving the molten metal alloy, the mold extending in a radial direction (R1) with respect to the axis of rotation (A). The device (10) comprises at least one magnet arranged in such a way as to induce an electric current in the mold (22) during the rotation of the centrifugal casting wheel (20) about the axis of rotation (A).
    Type: Grant
    Filed: November 6, 2018
    Date of Patent: September 6, 2022
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventor: Laurent Ferrer
  • Patent number: 11427897
    Abstract: A production method of a maraging steel includes: the step of producing, by vacuum melting, a remelt electrode which comprises from 0.2 to 3.0% by mass of Ti and from 0.0025 to 0.0050% by mass of N; and the step of remelting the remelt electrode to produce a steel ingot having an average diameter of 650 mm or more; wherein the resulting maraging steel includes from 0.2 to 3.0% by mass of Ti.
    Type: Grant
    Filed: June 10, 2014
    Date of Patent: August 30, 2022
    Assignees: HITACHI METALS, LTD., SAFRAN AIRCRAFT ENGINES
    Inventors: Takahiko Kamimura, Laurent Ferrer, Pascal Poulain
  • Publication number: 20220062975
    Abstract: The invention relates to a method for manufacturing a metal ingot by continuous casting, comprising the following steps: S1: melting the metal, S2: transferring the liquid metal (2) by pouring it into a crucible (12), S3: moving the base plate (14) of the crucible (12), S4: progressive solidification of the liquid metal (2) from the base plate (14) of the crucible (12), and S5: during the step S3 of moving the base plate (14), applying a compression force to the metal (3) which is present between the base plate (14) and the side wall (13), the compression force being applied along a second axis (X2) parallel to the first axis (X1) so as to deform the metal and to obtain an ingot (3) which has a smaller width (L2).
    Type: Application
    Filed: December 13, 2019
    Publication date: March 3, 2022
    Applicant: SAFRAN AIRCRAFT ENGINES
    Inventor: Laurent FERRER
  • Publication number: 20210262061
    Abstract: A method for manufacturing an ingot made of titanium-based metallic compound, includes providing raw material fragments; melting the raw material fragments into a liquid metal in at least one basin; keeping in the molten state the liquid metal in the at least one basin; pouring the liquid metal from the at least one basin into a crucible by overflow from the at least one basin into the crucible; forming an ingot by cooling of the liquid metal into the crucible; wherein the method further includes preheating the raw material fragments before the melting of the raw material fragments with a preheating temperature higher than or equal to 75% of the liquidus temperature of the raw material fragments, and lower less than the liquidus temperature of the raw material fragments.
    Type: Application
    Filed: June 24, 2019
    Publication date: August 26, 2021
    Inventors: Bruno Vitorino LOPES, Laurent FERRER
  • Publication number: 20200316682
    Abstract: A device (10) for manufacturing a metal alloy blank by centrifugal casting of a molten metal alloy, comprising a centrifugal casting wheel (20), the centrifugal casting wheel (20) being rotary about an axis of rotation (A) and comprising a mold (22) for receiving the molten metal alloy, the mold extending in a radial direction (R1) with respect to the axis of rotation (A). The device (10) comprises at least one magnet arranged in such a way as to induce an electric current in the mold (22) during the rotation of the centrifugal casting wheel (20) about the axis of rotation (A).
    Type: Application
    Filed: November 6, 2018
    Publication date: October 8, 2020
    Applicant: SAFRAN AIRCRAFT ENGINES
    Inventor: Laurent FERRER
  • Publication number: 20190309390
    Abstract: A method of fabricating a low alloy steel ingot, the method including a) melting all or part of an electrode by a vacuum arc remelting method, the electrode, before melting, including iron and carbon, the melted portion of the electrode being collected in a crucible, thus forming a melt pool within the crucible; and b) solidifying the melt pool by heat exchange between the melt pool and a cooling fluid, the heat exchange applied serving to impose a mean solidification speed during step b) that is less than or equal to 45 ?m/s and to obtain an ingot of low alloy steel.
    Type: Application
    Filed: June 24, 2019
    Publication date: October 10, 2019
    Inventors: Laurent FERRER, Nicolas BINOT
  • Patent number: 10364479
    Abstract: A method of fabricating a low alloy steel ingot, the method including a) melting all or part of an electrode by a vacuum arc remelting method, the electrode, before melting, including iron and carbon, the melted portion of the electrode being collected in a crucible, thus forming a melt pool within the crucible; and b) solidifying the melt pool by heat exchange between the melt pool and a cooling fluid, the heat exchange applied serving to impose a mean solidification speed during step b) that is less than or equal to 45 ?m/s and to obtain an ingot of low alloy steel.
    Type: Grant
    Filed: June 3, 2015
    Date of Patent: July 30, 2019
    Assignees: SAFRAN AIRCRAFT ENGINES, SAFRAN LANDING SYSTEMS
    Inventors: Laurent Ferrer, Nicolas Binot
  • Patent number: 10174391
    Abstract: The invention relates to a method for producing martensitic steel that comprises a content of other metals such that the steel can be hardened by an intermetallic compound and carbide precipitation, with an Al content of between 0.4% and 3%, comprising the following steps: (a) heating the entirety of the steel above its austenizing temperature, (b) cooling said steel approximately to ambient temperature, (c) placing said steel in a cryogenic medium. The temperature T1 is substantially lower than the martensitic transformation temperature Mf, and the time t during which said steel is kept in said cryogenic medium at a temperature T1 from the moment when the hottest part of the steel reaches a temperature lower than the martensitic transformation temperature Mf is at least equal to a non-zero time t1, the temperature T1 (in ° C.
    Type: Grant
    Filed: July 2, 2010
    Date of Patent: January 8, 2019
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventor: Laurent Ferrer
  • Patent number: 9943908
    Abstract: A method of fabricating a part (10) having a housing (20) that includes an opening (25) opening out in a free surface (15) of the part (10). The method comprises the following steps: (a) closing the opening (25) with a sheath (30), the sheath having a vacuum orifice (31) and a filling orifice (32); (b) filling the housing (20) with an abradable material (50) constituted by particles by using the filling orifice (32), and evacuating the housing (20) using the vacuum orifice (31); (c) closing the orifices (31, 32) in leaktight manner; (d) deforming the sheath (30) so as to compress the abradable material (50) in the housing (20) and heating the abradable material (50) to a temperature higher than 150° C. so that the abradable material (50) becomes sintered; and (e) subsequently lowering the temperature and the pressure.
    Type: Grant
    Filed: September 30, 2013
    Date of Patent: April 17, 2018
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventor: Laurent Ferrer
  • Patent number: 9737932
    Abstract: A method of fabricating a part covered in an abradable coating (55), the method comprising the following steps: a blank (10) for the part, the blank having a housing (20) opening out into the surface (15) of the blank (10); filling the housing (20) with an abradable material in powder form; and hot rolling the blank (10) and the abradable material together so as to sinter the abradable material and cause it to adhere to the blank, in order to obtain an abradable coating (55).
    Type: Grant
    Filed: October 1, 2013
    Date of Patent: August 22, 2017
    Assignee: SNECMA
    Inventor: Laurent Ferrer
  • Publication number: 20170130297
    Abstract: A method of fabricating a low alloy steel ingot, the method including a) melting all or part of an electrode by a vacuum arc remelting method, the electrode, before melting, including iron and carbon, the melted portion of the electrode being collected in a crucible, thus forming a melt pool within the crucible; and b) solidifying the melt pool by heat exchange between the melt pool and a cooling fluid, the heat exchange applied serving to impose a mean solidification speed during step b) that is less than or equal to 45 ?m/s and to obtain an ingot of low alloy steel.
    Type: Application
    Filed: June 3, 2015
    Publication date: May 11, 2017
    Inventors: Laurent FERRER, Nicolas BINOT
  • Publication number: 20170096728
    Abstract: A production method of a maraging steel includes: the step of producing, by vacuum melting, a remelt electrode which comprises from 0.2 to 3.0% by mass of Ti and from 0.0025 to 0.0050% by mass of N; and the step of remelting the remelt electrode to produce a steel ingot having an average diameter of 650 mm or more; wherein the resulting maraging steel includes from 0.2 to 3.0% by mass of Ti.
    Type: Application
    Filed: June 10, 2014
    Publication date: April 6, 2017
    Applicants: HITACHI METALS, LTD., SAFRAN AIRCRAFT ENGINES
    Inventors: Takahiko KAMIMURA, Laurent FERRER, Pascal POULAIN
  • Patent number: 9464336
    Abstract: A method of fabricating a martensitic stainless steel including: 1) heating steel to a temperature higher than austenizing temperature of the steel, then quenching the steel until a hottest portion of the steel is at a temperature less than or equal to a maximum temperature, and greater than or equal to a minimum temperature, a cooling rate being sufficiently fast for austenite not to transform into a ferrito-perlitic structure; 2) performing a first anneal followed by cooling until the hottest portion of the steel is at a temperature less than or equal to the maximum temperature and greater than or equal to the minimum temperature; 3) performing a second anneal followed by cooling to ambient temperature; and at the end of each of 1) and 2), performing: ?) as soon as temperature of the hottest portion of the steel reaches the maximum temperature, immediately heating the steel once more.
    Type: Grant
    Filed: September 8, 2011
    Date of Patent: October 11, 2016
    Assignee: SNECMA
    Inventors: Jean-François Laurent Chabot, Laurent Ferrer, Pascal Charles Emile Thoison
  • Patent number: 9429183
    Abstract: The invention relates to a method of producing a martensitic steel comprising a content of other metals such that it can be hardened by intermetallic compound and carbide precipitation, with an Al content of between 0.4% and 3%. The heat shaping temperature of the last heat shaping pass of said steel is lower than the solubility temperature of the aluminum nitrides in the steel, and the treatment temperature for each potential heat treatment after said last heat shaping pass is lower than the solid-state solubility temperature of the aluminum nitrides in said steel.
    Type: Grant
    Filed: July 16, 2013
    Date of Patent: August 30, 2016
    Assignees: SNECMA, AUBERT & DUVAL
    Inventors: Laurent Ferrer, Philippe Heritier
  • Publication number: 20150266093
    Abstract: A method of fabricating a part (10) having a housing (20) that includes an opening (25) opening out in a free surface (15) of the part (10). The method comprises the following steps: (a) closing the opening (25) with a sheath (30), the sheath having a vacuum orifice (31) and a filling orifice (32); (b) filling the housing (20) with an abradable material (50) constituted by particles by using the filling orifice (32), and evacuating the housing (20) using the vacuum orifice (31); (c) closing the orifices (31, 32) in leaktight manner; (d) deforming the sheath (30) so as to compress the abradable material (50) in the housing (20) and heating the abradable material (50) to a temperature higher than 150° C. so that the abradable material (50) becomes sintered; and (e) subsequently lowering the temperature and the pressure.
    Type: Application
    Filed: September 30, 2013
    Publication date: September 24, 2015
    Applicant: SNECMA
    Inventor: Laurent Ferrer
  • Publication number: 20150231699
    Abstract: A method of fabricating a part covered in an abradable coating (55), the method comprising the following steps: a blank (10) for the part, the blank having a housing (20) opening out into the surface (15) of the blank (10); filling the housing (20) with an abradable material in powder form; and hot rolling the blank (10) and the abradable material together so as to sinter the abradable material and cause it to adhere to the blank, in order to obtain an abradable coating (55).
    Type: Application
    Filed: October 1, 2013
    Publication date: August 20, 2015
    Applicant: SNECMA
    Inventor: Laurent Ferrer