Patents by Inventor Jeremy Giordan
Jeremy Giordan 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: 10907507Abstract: A measuring device for measuring at least one parameter of an aerodynamic flow of a turbine engine. The device operates to collect parameters of the flow. A body extends along a radial axis (L). A connecting part is fastened to a first end of the body and designed to secure the measuring device to a radially outer wall of the turbine engine. A stud is inserted and mounted on a second end of the body radially opposite the first end. The stud includes at least a portion of a rubberlike material designed to come into contract with a radially inner wall of the turbine engine.Type: GrantFiled: October 8, 2018Date of Patent: February 2, 2021Assignee: SAFRAN AIRCRAFT ENGINESInventors: Jeremy Giordan, Thibault Xavier Alexis Berranger, Guillaume Jose Rodrigues, Stephane Rousselin, Mathieu Raymond Paul Sezeur
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Patent number: 10871402Abstract: A device for measuring the characteristics of an air flow intended to be mounted in an annular duct having a longitudinal axis in a turbine engine, comprising supporting means which support means for measuring the characteristics of an air flow. According to the invention, the supporting means comprise at least one first support including a main branch supporting first measuring means and a second support, structurally independent of the first support and including a main branch supporting second measuring means, with the first support and the second support being so formed that the main branch of the first support extends over a distance greater than the main branch of the second support in a common direction of extension of the branches.Type: GrantFiled: March 29, 2018Date of Patent: December 22, 2020Assignee: Safran Aircraft EnginesInventors: Jérémy Giordan, Florian Joseph Bernard Kockenpo, Thibault Xavier Alexis Berranger, Pascal Léon Georges Beilvert
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Patent number: 10519801Abstract: An annular air flow passage, particularly for a turbine engine, comprising two radially internal and external annular walls. A measuring element is elongated in a direction between the internal and external annular walls, and a first of the internal or external ends of the element is fixed rigidly to a first of the internal or external walls. The element includes at least one tubular cavity extending along the element and supplied with pressurized fluid.Type: GrantFiled: November 29, 2016Date of Patent: December 31, 2019Assignee: SAFRAN AIRCRAFT ENGINESInventors: Jérémy Giordan, Valentine Lucette Bader, André Pierre Jean Xavier Leroux, Stéphane Rousselin
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Patent number: 10513945Abstract: An annular air flow passage includes two radially internal and external annular walls. An element is elongated in a direction between the internal and external annular walls and a first of the internal or external ends of the element is fixed rigidly to a first of the internal or external walls. The center of gravity position of the element is variable.Type: GrantFiled: August 15, 2016Date of Patent: December 24, 2019Assignee: Safran Aircraft EnginesInventors: Jeremy Giordan, Florian Joseph Bernard Kockenpo, Stephane Rousselin
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Publication number: 20190107008Abstract: A measuring device for measuring at least one parameter of an aerodynamic flow of a turbine engine. The device operates to collect parameters of the flow. A body extends along a radial axis (L). A connecting part is fastened to a first end of the body and designed to secure the measuring device to a radially outer wall of the turbine engine. A stud is inserted and mounted on a second end of the body radially opposite the first end. The stud includes at least a portion of a rubberlike material designed to come into contract with a radially inner wall of the turbine engine.Type: ApplicationFiled: October 8, 2018Publication date: April 11, 2019Inventors: Jeremy GIORDAN, Thibault Xavier Alexis BERRANGER, Guillaume Jose RODRIGUES, Stephane ROUSSELIN, Mathieu Raymond Paul SEZEUR
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Patent number: 10190946Abstract: A measuring comb for temperature and/or pressure and/or chemical composition of the gases flowing at the outlet of a turbine engine flow path, in which the flow path extends around an axis of revolution of the flow path, is provided. The measuring comb includes: a comb body with an elongated shape, intended to face the outlet of the flow path, the comb body including at least one measuring opening arranged along an axis, the measuring opening being configured to tap gases flowing at the outlet of the flow path; and an adjusting system configured to adjust an angle between the axis of the at least one measuring opening and the axis of revolution, so as to allow orientation of the at least one measuring opening in the flow direction of the gases at the outlet of the flow path.Type: GrantFiled: May 27, 2015Date of Patent: January 29, 2019Assignee: SAFRAN AIRCRAFTS ENGINESInventors: Romain Nicolas Lunel, Laurent Bernard Cameriano, Jeremy Giordan, Denis Jean Maurice Sandelis, Aurelien Lionel Tedesco
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Patent number: 10138754Abstract: The present invention relates to a device for measuring aerodynamic magnitudes (1) intended to be placed transversally in a flow passage (12, 13) of a turbine engine comprising: an upstream body (2) having a profile of general cylindrical shape defining a leading edge (5) a plurality of sensors (4), the instrumentation lines (45) of the sensors being placed in the body (2), the sensitive elements (41) of the sensors extending at the leading edge (5); a downstream fairing (3) mounted on the upstream body (2) and defining a trailing edge (6); the downstream fairing (3) comprising, in the longitudinal direction of the upstream body (2), several sections (35) fixed independently of each other to the body (2), two successive sections (35) being connected by a flexible junction (37).Type: GrantFiled: November 10, 2016Date of Patent: November 27, 2018Assignee: SAFRAN AIRCRAFT ENGINESInventors: Jeremy Giordan, Bernard Joseph Florian Kockenpo
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Publication number: 20180283960Abstract: A device for measuring the characteristics of an air flow intended to be mounted in an annular duct having a longitudinal axis in a turbine engine, comprising supporting means which support means for measuring the characteristics of an air flow. According to the invention, the supporting means comprise at least one first support including a main branch supporting first measuring means and a second support, structurally independent of the first support and including a main branch supporting second measuring means, with the first support and the second support being so formed that the main branch of the first support extends over a distance greater than the main branch of the second support in a common direction of extension of the branches.Type: ApplicationFiled: March 29, 2018Publication date: October 4, 2018Applicant: Safran Aircraft EnginesInventors: Jérémy Giordan, Florian Joseph Bernard Kockenpo, Thibault Xavier Alexis Berranger, Pascal Léon Georges Beilvert
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Patent number: 9856743Abstract: An annular air flow passage for a turbine engine such as a turbojet or a turboprop, crossed by an instrumented rod that includes mechanism(s) for measuring characteristics of a flow potentially traveling along the passage, the rod extending between an outer annular wall and an inner annular wall of the passage. Outer connection(s) fasten(s) an outer end of the instrumented rod to the outer wall in a manner that is rigid in all directions, and inner connection(s) fasten(s) an inner end of the instrumented rod to the inner wall, in a manner that is rigid in the circumferential direction and that has at least one degree of freedom to move in a first direction extending between the inner and outer walls of the passage and having at least a radial component.Type: GrantFiled: May 27, 2015Date of Patent: January 2, 2018Assignee: Safran Aircraft EnginesInventors: Florian Kockenpo, Jermone Acquaviva, Claude Gaston Corbin, Jeremy Giordan, Nicolas Seigneuret, Nicolas Lamarche
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Publication number: 20170159484Abstract: An annular air flow passage, particularly for a turbine engine, comprising two radially internal and external annular walls, wherein an element is elongated in a direction between the internal and external annular walls and a first of the internal or external ends of the element is fixed rigidly to a first of the internal or external walls. According to the invention, the annular flow passage comprises means of variation, along said direction, of the center of gravity position of the element.Type: ApplicationFiled: August 15, 2016Publication date: June 8, 2017Applicant: Safran Aircraft Engines PI (AJI)Inventors: Jeremy Giordan, Florian Joseph Bernard Kockenpo, Stephane Rousselin
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Publication number: 20170152757Abstract: An annular air flow passage, particularly for a turbine engine, comprising two radially internal and external annular walls. A measuring element is elongated in a direction between the internal and external annular walls, and a first of the internal or external ends of the element is fixed rigidly to a first of the internal or external walls. The element includes at least one tubular cavity extending along the element and supplied with pressurized fluid.Type: ApplicationFiled: November 29, 2016Publication date: June 1, 2017Applicant: Safran Aircraft EnginesInventors: Jérémy Giordan, Valentine Lucette Bader, André Pierre Jean Xavier Leroux, Stéphane Rousselin
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Publication number: 20170138216Abstract: The present invention relates to a device for measuring aerodynamic magnitudes (1) intended to be placed transversally in a flow passage (12, 13) of a turbine engine comprising: an upstream body (2) having a profile of general cylindrical shape defining a leading edge (5) a plurality of sensors (4), the instrumentation lines (45) of the sensors being placed in the body (2), the sensitive elements (41) of the sensors extending at the leading edge (5); a downstream fairing (3) mounted on the upstream body (2) and defining a trailing edge (6); the downstream fairing (3) comprising, in the longitudinal direction of the upstream body (2), several sections (35) fixed independently of each other to the body (2), two successive sections (35) being connected by a flexible junction (37).Type: ApplicationFiled: November 10, 2016Publication date: May 18, 2017Inventors: Jeremy GIORDAN, Bernard Joseph Florian KOCKENPO
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Patent number: 9400232Abstract: A measuring rod capable of receiving a plurality of instrumentation cables transmitting data to a data processing device, includes a section of epicycloidal shape.Type: GrantFiled: September 11, 2013Date of Patent: July 26, 2016Assignee: SNECMAInventor: Jeremy Giordan
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Publication number: 20150345335Abstract: The invention relates to an annular air flow passage (33) for a turbine engine such as a turbojet or a turboprop, crossed by an instrumented rod (50) that includes means for measuring characteristics of a flow potentially traveling along the passage, said rod extending between an outer annular wall (48) and an inner annular wall (42) of the passage. According to the invention, outer connection means (60, 86) fasten an outer end (58) of the instrumented rod to the outer wall in a manner that is rigid in all directions, and inner connection means (62) fasten an inner end (56) of the instrumented rod to the inner wall, in a manner that is rigid in the circumferential direction and that has at least one degree of freedom to move in a first direction (51) extending between the inner and outer walls (42, 48) of the passage and having at least a radial component.Type: ApplicationFiled: May 27, 2015Publication date: December 3, 2015Inventors: Florian Kockenpo, Jermone Acquaviva, Claude Gaston Corbin, Jeremy Giordan, Nicolas Seigneuret, Nicolas Lamarche
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Publication number: 20140069177Abstract: A measuring rod capable of receiving a plurality of instrumentation cables transmitting data to a data processing device, includes a section of epicycloidal shape.Type: ApplicationFiled: September 11, 2013Publication date: March 13, 2014Applicant: SNECMAInventor: Jeremy Giordan