Patents by Inventor Pierre Caron
Pierre Caron 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: 11725261Abstract: The invention relates to a nickel-based superalloy comprising, in percentages by mass, 4.0 to 5.5% rhenium, 1.0 to 3.0 ruthenium, 2.0 to 14.0% cobalt, 0.3 to 1.0% molybdenum, 3.0 to 5.0% chromium, 2.5 to 4.0% tungsten, 4.5 to 6.5% aluminum, 0.50 to 1.50% titanium, 8.0 to 9.0% tantalum, 0.15 to 0.30% hafnium, 0.05 to 0.15% silicon, the balance being nickel and unavoidable impurities. The invention also relates to a single-crystal blade (20A, 20B) comprising such an alloy and a turbomachine (10) comprising such a blade (20A, 20B).Type: GrantFiled: April 6, 2022Date of Patent: August 15, 2023Assignees: SAFRAN, OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALESInventors: Jérémy Rame, Virginie Jaquet, Joël Delautre, Jean-Yves Guedou, Pierre Caron, Odile Lavigne, Didier Locq, Mikael Perrut
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Publication number: 20220364208Abstract: The invention relates to a nickel-based superalloy comprising, in percentages by mass, 4.0 to 5.5% rhenium, 1.0 to 3.0 ruthenium, 2.0 to 14.0% cobalt, 0.3 to 1.0% molybdenum, 3.0 to 5.0% chromium, 2.5 to 4.0% tungsten, 4.5 to 6.5% aluminum, 0.50 to 1.50% titanium, 8.0 to 9.0% tantalum, 0.15 to 0.30% hafnium, 0.05 to 0.15% silicon, the balance being nickel and unavoidable impurities. The invention also relates to a single-crystal blade (20A, 20B) comprising such an alloy and a turbomachine (10) comprising such a blade (20A, 20B).Type: ApplicationFiled: April 6, 2022Publication date: November 17, 2022Applicants: SAFRAN, OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALESInventors: Jérémy RAME, Virginie JAQUET, Joël DELAUTRE, Jean-Yves GUEDOU, Pierre CARON, Odile LAVIGNE, Didier LOCQ, Mikael PERRUT
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Patent number: 11396685Abstract: A nickel-based superalloy comprises, in percentages by mass, 4.0 to 5.5% rhenium, 1.0 to 3.0 ruthenium, 2.0 to 14.0% cobalt, 0.3 to 1.0% molybdenum, 3.0 to 5.0% chromium, 2.5 to 4.0% tungsten, 4.5 to 6.5% aluminum, 0.50 to 1.50% titanium, 8.0 to 9.0% tantalum, 0.15 to 0.30% hafnium, 0.05 to 0.15% silicon, the balance being nickel and unavoidable impurities. A single-crystal blade comprises such an alloy and a turbomachine comprising such a blade.Type: GrantFiled: November 14, 2018Date of Patent: July 26, 2022Assignees: SAFRAN, OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALESInventors: Jérémy Rame, Virginie Jaquet, Joël Delautre, Jean-Yves Guedou, Pierre Caron, Odile Lavigne, Didier Locq, Mikael Perrut
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Patent number: 11268170Abstract: A nickel-based superalloy comprises, in percentages by mass, 4.0 to 5.5% rhenium, 3.5 to 12.5% cobalt, 0.30 to 1.50% molybdenum, 3.5 to 5.5% chromium, 3.5 to 5.5% tungsten, 4.5 to 6.0% aluminum, 0.35 to 1.50% titanium, 8.0 to 10.5% tantalum, 0.15 to 0.30% hafnium, 0.05 to 0.15% silicon, the balance being nickel and unavoidable impurities. A single-crystal blade comprises such an alloy and a turbomachine comprising such a blade.Type: GrantFiled: November 14, 2018Date of Patent: March 8, 2022Assignees: SAFRAN, OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALESInventors: Jérémy Rame, Virginie Jaquet, Joël Delautre, Jean-Yves Guedou, Pierre Caron, Odile Lavigne, Didier Locq, Mikael Perrut
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Patent number: 11220727Abstract: A nickel-based superalloy comprises in mass percent: 4.0% to 6.0% chromium; 0.4% to 0.8% molybdenum; 2.5% to 3.5% rhenium; 6.2% to 6.6% tungsten; 5.2% to 5.7% aluminum; 0.0 to 1.6% titanium; 6.0% to 9.9% tantalum; 0.0 to 0.7% hafnium; and 0.0 to 0.3% silicon; the balance being constituted by nickel and any impurities. A monocrystalline blade comprises such an alloy and a turbomachine including such a blade.Type: GrantFiled: October 24, 2017Date of Patent: January 11, 2022Assignees: Safran, Safran Aircraft Engines, Office National D'Etudes et de Recherches Aerospatiales, Safran Helicopter EnginesInventors: Jérémy Rame, Philippe Belaygue, Pierre Caron, Joël Delautre, Virginie Jaquet, Odile Lavigne
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Publication number: 20210246533Abstract: A nickel-based superalloy comprises, in percentages by mass, 4.0 to 5.5% rhenium, 1.0 to 3.0 ruthenium, 2.0 to 14.0% cobalt, 0.3 to 1.0% molybdenum, 3.0 to 5.0% chromium, 2.5 to 4.0% tungsten, 4.5 to 6.5% aluminum, 0.50 to 1.50% titanium, 8.0 to 9.0% tantalum, 0.15 to 0.30% hafnium, 0.05 to 0.15% silicon, the balance being nickel and unavoidable impurities. A single-crystal blade comprises such an alloy and a turbomachine comprising such a blade.Type: ApplicationFiled: November 14, 2018Publication date: August 12, 2021Applicants: SAFRAN, OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALESInventors: Jérémy RAME, Virginie JAQUET, Joël DELAUTRE, Jean-Yves GUEDOU, Pierre CARON, Odile LAVIGNE, Didier LOCQ, Mikael PERRUT
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Publication number: 20200299808Abstract: A nickel-based superalloy comprises, in percentages by mass, 4.0 to 5.5% rhenium, 3.5 to 12.5% cobalt, 0.30 to 1.50% molybdenum, 3.5 to 5.5% chromium, 3.5 to 5.5% tungsten, 4.5 to 6.0% aluminum, 0.35 to 1.50% titanium, 8.0 to 10.5% tantalum, 0.15 to 0.30% hafnium, 0.05 to 0.15% silicon, the balance being nickel and unavoidable impurities. A single-crystal blade comprises such an alloy and a turbomachine comprising such a blade.Type: ApplicationFiled: November 14, 2018Publication date: September 24, 2020Applicants: SAFRAN, OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALESInventors: Jérémy RAME, Virginie JAQUET, Joël DELAUTRE, Jean-Yves GUEDOU, Pierre CARON, Odile LAVIGNE, Didier LOCQ, Mikael PERRUT
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Publication number: 20190330714Abstract: A nickel-based superalloy comprises in mass percent: 4.0% to 6.0% chromium; 0.4% to 0.8% molybdenum; 2.5% to 3.5% rhenium; 6.2% to 6.6% tungsten; 5.2% to 5.7% aluminum; 0.0 to 1.6% titanium; 6.0% to 9.9% tantalum; 0.0 to 0.7% hafnium; and 0.0 to 0.3% silicon; the balance being constituted by nickel and any impurities. A monocrystalline blade comprises such an alloy and a turbomachine including such a blade.Type: ApplicationFiled: October 24, 2017Publication date: October 31, 2019Applicants: Safran, Safran Aircraft Engines, Office National D'Etudes et de Recherches Aerospatiales, Safran Helicopter EnginesInventors: Jérémy RAME, Philippe BELAYGUE, Pierre CARON, Joël DELAUTRE, Virginie JAQUET, Odile LAVIGNE
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Patent number: 9259697Abstract: The invention relates to a manufacturing process of stirred or drinking fermented milk or fresh cheese comprising a smoothing step after fermentation wherein said smoothing step is performed by a ring-shaped rotor-stator mixer, each ring of the rotor and the stator being provided with radial slots having a given width, and adjusting the rotational speed to adjust the peripheral velocity.Type: GrantFiled: February 22, 2006Date of Patent: February 16, 2016Assignee: Compagnie Gervais DanoneInventors: Ana Ospina Martinez, Jean-Pierre Caron, Thierry Di Tecco, Noémie Genovesi, Sébastien Biloe
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Patent number: 9114419Abstract: Method for dip treatment of an optical element, wherein the optical element is held, while it is being dipped, by a holding ring, the ring including a hoop for draining and encircling a peripheral edge of the optical element, thereby exerting continuous linear contact with the peripheral edge, the hoop forming an arc over more than 180° and being provided at each of its two ends with an outwardly-directed drip tab pointing away from the optical element.Type: GrantFiled: November 30, 2010Date of Patent: August 25, 2015Assignee: ESSILOR INTERNATIONAL (COMPAGNIE GENERALE D'OPTIQUE)Inventors: Pierre Caron, Annette Cretier, Annick Gascons
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Publication number: 20110070364Abstract: Method for dip treatment of an optical element, wherein the optical element is held, while it is being dipped, by a holding ring, the ring including a hoop for draining and encircling a peripheral edge of the optical element, thereby exerting continuous linear contact with the peripheral edge, the hoop forming an arc over more than 180° and being provided at each of its two ends with an outwardly-directed drip tab pointing away from the optical element.Type: ApplicationFiled: November 30, 2010Publication date: March 24, 2011Applicant: ESSILOR INTERNATIONAL (COMPAGNIE GENERALE D'OPTIQUE)Inventors: Pierre CARON, Annette Cretier, Annick Gascons
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Publication number: 20100044372Abstract: A portable and collapsible isolator is taught for containing radioactive, chemical or biological agents. The isolator is comprised of a collapsible frame, movable between a collapsed transport position and an open operational position, and a flexible and collapsible envelope in the form of an airtight bag attached to the frame to define a cavity. The envelope remains airtight in both the collapsed and open positions. One or more sealable openings are formed in the envelope for insertion and removal of the radioactive, chemical and biological agents into and out of the cavity. The isolator may optionally include at least one glove extending from one or more of said sealable openings into the cavity, for handling said radioactive, chemical and biological agents inside the cavity.Type: ApplicationFiled: October 27, 2008Publication date: February 25, 2010Applicant: Her Majesty The Queen in Right of Canada as Represented by the Minister of Public SafetyInventors: Bill Kournikakis, Tim Patraboy, Daniel Perreault, James Peeke, Carl McDiarmid, Ian Summerell, Andrew Burczyk, Marianne Heisz, Pierre Caron, Sylvain Poirier
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Publication number: 20090252831Abstract: The invention relates to a manufacturing process of stirred or drinking fermented milk or fresh cheese comprising a smoothing step after fermentation wherein said smoothing step is performed by a ring-shaped rotor-stator mixer, each ring of the rotor and the stator being provided with radial slots having a given width, and adjusting the rotational speed to adjust the peripheral velocity.Type: ApplicationFiled: February 22, 2006Publication date: October 8, 2009Inventors: Ana Ospina Martinez, Jean-Pierre Caron, Thierry Di Tecco, Noemie Genovesi, Sebastien Biloe
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Publication number: 20090188429Abstract: The ring comprises a hoop (1, 20) for draining and encircling the edge of the optical element, forming an arc over more than 180° and provided at each of its two ends with an outwardly-directed drip tab (10, 30).Type: ApplicationFiled: November 22, 2004Publication date: July 30, 2009Inventors: Pierre Caron, Annette Cretier, Annick Gascons
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Publication number: 20070227630Abstract: The invention provides alloys or superalloys based on nickel essentially comprising the following elements in the amounts indicated as percentages by weight: Cr: 11.5% to 13.5%; Co: 11.5% to 16.0%; Mo: 3.4% to 5.0%; W: 3.0% to 5.0%; Al: 2.2% to 3.2%; Ti: 3.5% to 5.0%; Nb: 0.5% to 2.0%; Hf: 0.25% to 0.35%; Zr: 0 to 0.07%; C: 0.015% to 0.030%; B: 0.01% to 0.02%; and Ni: complement to 100%. The alloy is for use in the production of turbine or compressor disks for turbo-machines, using powder metallurgy techniques.Type: ApplicationFiled: March 30, 2007Publication date: October 4, 2007Applicants: SNECMA, ARMINES, ONERA(OFF NAT D'ETUDES ET DE RECHERCHES AEROS)Inventors: Isabelle Augustins Lecallier, Pierre Caron, Jean-yves Guedou, Didier Locq, Loeiz Naze
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Patent number: 7077922Abstract: A method for forming odd-shaped mufflers is achieved by first introducing an unfilled muffler insert having a desired number of pipes and partitions within a two-piece shaped tool. Fibrous material is introduced within desired compartments formed between the shaped tool and unfilled insert to form a filled insert. The shaped tool and filled insert are then placed on a winding device. A yarn thread is then wound and secured around the fibrous material within a gap created between the two pieces of the shaped tool. The winding device and shaped tool are then removed from the filled and wound muffler insert. The wound and filled muffler insert may then either be pressed into a previously formed muffler shell, or alternatively, the muffler shell may be formed around the wound and filled muffler insert to form the muffler.Type: GrantFiled: July 2, 2003Date of Patent: July 18, 2006Assignee: Owens Corning Composites S.P.R.L.Inventors: Luc Brandt, Jean-Pierre Caron
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Patent number: 7008690Abstract: An optical item comprising an organic or mineral glass substrate (1) and a transparent polymeric material layer (3), characterized in that it comprises at least one intermediate layer (2) in direct contact with one main side of the substrate and the polymeric material layer, the intermediate layer(s) being made of particles of at least one colloidal mineral oxide and optionally of a binder, such (an) intermediate layer(s) having an initial porosity, and the initial porosity of the intermediate layer(s) being filled either by material from the polymeric material layer or by the substrate material if the latter is made in an organic glass and, optionally partly by the binder when present, so that the intermediate layer(s), after initial porosity filling, each represent a quarter waveplate with a wavelength in the range from 400 to 700 nm, preferably from 450 to 650 nm.Type: GrantFiled: December 26, 2002Date of Patent: March 7, 2006Assignee: Essilor International Compagnie Generale d'OptiqueInventors: Pierre Caron, Jean-Paul Cano, Annette Cretier
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Publication number: 20050194068Abstract: Nickel-based superalloy, suitable for monocrystalline solidification, having the following composition by weight: Co: ?4.75 to 5.25% Cr: ?15.5 to 16.5% Mo: ?0.8 to 1.2% W: ?3.75 to 4.25% Al: ?3.75 to 4.25% Ti: ?1.75 to 2.25% Ta: ?4.75 to 5.25% C: 0.006 to 0.04% B: ?0.01% Zr: ?0.01% Hf: ???1% Nb: ???1% Ni and any impurities: complement to 100%.Type: ApplicationFiled: February 28, 2005Publication date: September 8, 2005Inventors: Pierre Caron, Michael Blackler, Gordon McColvin, Rajeshwar Wahi, Andre Escale, Laurent Lelait
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Publication number: 20050001012Abstract: A method for forming odd-shaped mufflers is achieved by first introducing an unfilled muffler insert having a desired number of pipes and partitions within a two-piece shaped tool. Fibrous material is introduced within desired compartments formed between the shaped tool and unfilled insert to form a filled insert. The shaped tool and filled insert are then placed on a winding device. A yarn thread is then wound and secured around the fibrous material within a gap created between the two pieces of the shaped tool. The winding device and shaped tool are then removed from the filled and wound muffler insert. The wound and filled muffler insert may then either be pressed into a previously formed muffler shell, or alternatively, the muffler shell may be formed around the wound and filled muffler insert to form the muffler.Type: ApplicationFiled: July 2, 2003Publication date: January 6, 2005Inventors: Luc Brandt, Jean-Pierre Caron
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Patent number: 6821543Abstract: The invention concerns fermented dairy products whereof the Dornic acidity ranges from 20 to 80° D, the pH from 4.5 to 5.5, flavored with a warm flavour such as chocolate, caramel, vanilla, coffee, burnt almond, nougat, walnut, hazelnut, almond, peanut, cashew nut. The dairy raw material is treated in order to reduce its mineral salts and/or its protein contents, then subjected to fermentation by a lactic ferment.Type: GrantFiled: September 7, 2001Date of Patent: November 23, 2004Assignee: Compagnie Gervais DanoneInventors: Denis Paquet, Jean-Pierre Caron, Jacques De Villeroche, David Lam, Paul Skrochowski, Stéphane Doat, Nathalie Trial, Blas Tarodo De La Fuente, Jean-Louis Cuq