Patents by Inventor Simon Pierre

Simon Pierre 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: 10801369
    Abstract: An intermediate casing for a turbine engine, comprising at least one central hub and one shroud (12) which are positioned concentrically, and mutually mechanically connected by structural arms (11), with such casing comprising at least one sealing part (13) attached between the shroud (12) and a structural arm (11), with the sealing part (13) including at least one metal core and one seal.
    Type: Grant
    Filed: May 18, 2017
    Date of Patent: October 13, 2020
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Simon Pierre Claude Charbonnier, Patrick Jean-Louis Reghezza, Julien Roset, Yann Christophe Maurice Sarazin
  • Publication number: 20200174784
    Abstract: A data center may include a software defined infrastructure in a computing environment. The data center may also include a computer readable medium having instructions which when executed by a processor cause the processor to implement cognitive agents to perform adaptive deep reinforcement learning to reconfigure the software defined infrastructure based upon changes in the computing environment.
    Type: Application
    Filed: December 3, 2018
    Publication date: June 4, 2020
    Inventors: Luis A. BATHEN, Simon-Pierre GENOT, Mu QIAO, Ramani ROUTRAY
  • Publication number: 20200171727
    Abstract: A molded article suitable for subsequent blow-molding into a final-shaped container. The article includes a neck portion; a gate portion; and a body portion extending between the neck portion and the gate portion, at least a majority of the body portion having an overall shape which is symmetric about a body axis extending longitudinally through a center of the body portion. The body portion includes an inner exterior layer and an outer exterior layer of a first polymeric material; and a core layer of a second polymeric material disposed between the inner exterior layer and the outer exterior layer. A radial thickness or a material of the core layer is selectively varied to govern non-uniform blow molding of the molded article into the final-shaped container.
    Type: Application
    Filed: June 21, 2018
    Publication date: June 4, 2020
    Inventors: Jean-Christophe WITZ, Christophe Simon Pierre BECK, Joachims Johannes NIEWELS, Lee Richard RIDDLE
  • Publication number: 20200124084
    Abstract: A clevis, particularly for a turbomachine includes a body that is attachable to a casing and at least one aperture for fitting a hinge pin. The body is formed in one piece and includes, about the at least one aperture, a honeycomb-type annular portion. The annular portion acts as a vibration filter and has a compressive and/or flexural strain capacity greater than that of the rest of the body.
    Type: Application
    Filed: January 30, 2018
    Publication date: April 23, 2020
    Applicant: SAFRAN TRANSMISSION SYSTEMS
    Inventor: Simon Pierre Mathieu Mabire
  • Patent number: 10556374
    Abstract: Disclosed herein, amongst other things, is a method for converting a design of an original preform that is blow moldable to form a container into a converted preform having less molding material that is blow moldable to form the same container. The method includes retaining a neck finish and body of the original preform on the converted preform. The method further includes replacing the original base of the original preform with a converted base having an outer base surface that joins with an outer body surface of the body at an base split-line of the original base and that fits offset within an outer body surface of the original base, whereby the converted preform has a reduced total length, disregarding any gate vestige that may be formed thereon, relative to a total length of the original preform.
    Type: Grant
    Filed: November 4, 2015
    Date of Patent: February 11, 2020
    Assignee: Husky Injection Molding Systems Ltd.
    Inventor: Christophe Simon Pierre Beck
  • Publication number: 20200008511
    Abstract: A protective helmet including an outer shell, and a liner assembly received in the outer shell and connected to the outer shell, the liner assembly defining a front portion configured to overlay a front of a head of a wearer, a rear portion configured to overlay a rear of the head of the wearer, a top portion disposed above and out of contact with a top of the head of the wearer when the helmet is worn, and two opposed side portions each configured to overlay a respective side of the head of the wearer. Each of the front, rear, side and top portions includes at least one zone where the liner assembly includes a plurality of overlapping layers.
    Type: Application
    Filed: September 20, 2019
    Publication date: January 9, 2020
    Inventors: Nicole Jacqueline WIART, Daniel CHARTRAND, Maurice DYKMANS, Philippe MARTIN, Simon-Pierre GERMAIN, Brian William STEENBRINK, Pierre-Luc BEAUCHAMP, Simon LANGLOIS, Evangelos SPYROU
  • Publication number: 20190375015
    Abstract: A connecting rod, in particular for a turbine engine, includes an intermediate body with a general elongated shape. Connecting heads may be located at the longitudinal ends of the elongated shape, which may include holes having axes that are, for example, substantially parallel. The connecting rod is characterized in that the heads are assembled or formed as a single piece with at least one part of the body. At least one of the heads includes an alveolar annular part, about the axis of the hole, forming a vibrating filter and having a flexural and/or compressive deformation capacity greater than that of the rest of the connecting rod and, in particular, that of the body.
    Type: Application
    Filed: January 31, 2018
    Publication date: December 12, 2019
    Applicant: SAFRAN TRANSMISSION SYSTEMS
    Inventors: Simon Pierre Mathieu Mabire, Fanélie Violaine Drevon
  • Patent number: 10458247
    Abstract: A stator of an aircraft turbine engine, comprising an annular row of fixed vanes and an annular row of arms, wherein the trailing edges of the fixed vanes are positioned substantially in a first transverse plane that is positioned downstream of a second transverse plane that passes substantially through the leading edges of the arms.
    Type: Grant
    Filed: September 29, 2015
    Date of Patent: October 29, 2019
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Simon Pierre Claude Charbonnier, Matthieu Yoann Perrier
  • Patent number: 10455884
    Abstract: A protective helmet having a liner assembly received in an outer shell and connected to the outer shell, with front, rear, side and top portions each including at least one zone where the liner assembly includes a plurality of overlapping layers, each of the layers being made from one of first, second, third and fourth materials, where the first material has a greater density and/or hardness than that of the second, third and fourth materials, the second material has a greater density and/or hardness than that of the third and fourth materials, and the third material has a greater density and/or hardness than that of the fourth material, and wherein the liner assembly includes one or more particular zones set forth in Table 3 or 4.
    Type: Grant
    Filed: March 21, 2017
    Date of Patent: October 29, 2019
    Assignee: SPORT MASKA INC.
    Inventors: Nicole Jacqueline Wiart, Daniel Chartrand, Maurice Dykmans, Philippe Martin, Simon-Pierre Germain, Brian William Steenbrink, Pierre-Luc Beauchamp, Simon Langlois, Evangelos Spyrou
  • Patent number: 10426215
    Abstract: A protective helmet including a helmet body, a facemask extending from the front portion to cover at least a portion of a face of a wearer, and one or more adjustment mechanisms securing the facemask to the helmet body. The adjustment mechanism(s) is/are connected to the helmet, include(s) an engagement member engaged with the facemask, is/are selectively engageable with the facemask in at least two vertically spaced apart positions of the facemask relative to the helmet body, and allow(s) toolless adjustment between the vertically spaced apart positions. Adjustment mechanisms and methods of positioning a facemask are also discussed.
    Type: Grant
    Filed: December 16, 2016
    Date of Patent: October 1, 2019
    Assignee: SPORT MASKA INC.
    Inventors: Sebastien Morin, Pierre-Luc Beauchamp, Simon Langlois, Brian William Steenbrink, Nicole Jacqueline Wiart, Simon-Pierre Germain
  • Publication number: 20190211711
    Abstract: An intermediate casing for a turbine engine, comprising at least one central hub and one shroud (12) which are positioned concentrically, and mutually mechanically connected by structural arms (11), with such casing comprising at least one sealing part (13) attached between the shroud (12) and a structural arm (11), with the sealing part (13) including at least one metal core and one seal.
    Type: Application
    Filed: May 18, 2017
    Publication date: July 11, 2019
    Inventors: Simon Pierre Claude CHARBONNIER, Patrick Jean-Louis REGHEZZA, Julien ROSET, Yann Christophe Maurice SARAZIN
  • Publication number: 20190147300
    Abstract: A method, computer system, and computer program product to detect anomalies in a multivariate or multidimensional time series data set. The time series data set is retrieved from a monitored device. A pair of neural networks are trained simultaneously using the retrieved time series data set by implementing an adversarial training process, to generate a generative neural network and a discriminative neural network. The anomalies in the time series data set of the monitored device are detected by implementing one or both of the generative neural network and the discriminative neural network to monitor the time series data set.
    Type: Application
    Filed: November 16, 2017
    Publication date: May 16, 2019
    Inventors: Luis Angel D. Bathen, Simon-Pierre Genot, Mu Qiao, Ramani R. Routray
  • Publication number: 20190145283
    Abstract: An extraction device of a platform for holding a blade fitted with an upstream flange, out of a turbomachine rotor disc which includes a handle fitted with a radial annular shoulder extended by a threaded pin, a proximal ring and a distal ring which include a tube extended by a radial collar, and a sleeve, the proximal ring being arranged around the pin, the tapped distal ring being screwed onto the other end of the pin and the sleeve being arranged around the two rings between their respective collars, such that screwing of the handle results in moving the distal ring towards the proximal ring, radial deformation of the distal part of the sleeve against the flared part of the cylindrical orifice of the flange and its being joined to the latter, and that it is possible to conjointly extract said platform and the device from the disc.
    Type: Application
    Filed: November 14, 2018
    Publication date: May 16, 2019
    Inventors: Patrick Jean-Louis REGHEZZA, Pierrick Charles CHEVALLIER, Simon Pierre Claude CHARBONNIER
  • Patent number: 10253800
    Abstract: An attachment system intended to equip a wall, the system including a nut intended to receive a screw of which the orientation is normal to the wall, the screw passing through an element such as an outer panel in order to attach the element to the wall. The attachment system comprises a socket having a threaded cylindrical outer face intended to be screwed into a hole passing through the wall and having dimensions greater than the dimensions of the fastener that the repair socket replaces, the socket carrying, in the central region of same, a nut receiving the screw.
    Type: Grant
    Filed: December 14, 2015
    Date of Patent: April 9, 2019
    Assignee: SAFRAN AIRCRAFT ENGINES
    Inventors: Yann Christophe Maurice Sarazin, Simon Pierre Claude Charbonnier, Patrick Jean-Louis Reghezza, Julien Roset
  • Publication number: 20190057181
    Abstract: Performing design optimization using an augmented reality system. Baseline data comprising baseline sensor data and baseline user input data is received by a computer system. An interactive baseline design optimization problem based on the baseline data is generated by the computer system. The baseline interactive optimization problem is transmitted by the computer system to the augmented reality system. Refined data comprising refined sensor data and refined user input data is received by the computer system. An interactive refined optimization problem based on the refined data and the baseline data is generated by the computer system. The interactive refined optimization problem is transmitted by the computer system to the augmented reality system.
    Type: Application
    Filed: December 21, 2017
    Publication date: February 21, 2019
    Inventors: Luis Angel D. Bathen, Simon-Pierre M. C. Genot, Rakesh Jain, Sunhwan Lee, Mu Qiao, Ramani R. Routray
  • Publication number: 20190057180
    Abstract: Performing design optimization using an augmented reality system. Baseline data comprising baseline sensor data and baseline user input data is received by a computer system. An interactive baseline design optimization problem based on the baseline data is generated by the computer system. The baseline interactive optimization problem is transmitted by the computer system to the augmented reality system. Refined data comprising refined sensor data and refined user input data is received by the computer system. An interactive refined optimization problem based on the refined data and the baseline data is generated by the computer system. The interactive refined optimization problem is transmitted by the computer system to the augmented reality system.
    Type: Application
    Filed: August 18, 2017
    Publication date: February 21, 2019
    Inventors: Luis Angel D. Bathen, Simon-Pierre M. C. Genot, Rakesh Jain, Sunhwan Lee, Mu Qiao, Ramani R. Routray
  • Publication number: 20180271202
    Abstract: A protective helmet having a liner assembly received in an outer shell and connected to the outer shell, with front, rear, side and top portions each including at least one zone where the liner assembly includes a plurality of overlapping layers, each of the layers being made from one of first, second, third and fourth materials, where the first material has a greater density and/or hardness than that of the second, third and fourth materials, the second material has a greater density and/or hardness than that of the third and fourth materials, and the third material has a greater density and/or hardness than that of the fourth material, and wherein the liner assembly includes one or more particular zones set forth in Table 3 or 4.
    Type: Application
    Filed: March 21, 2017
    Publication date: September 27, 2018
    Inventors: Nicole Jacqueline WIART, Daniel CHARTRAND, Maurice DYKMANS, Philippe MARTIN, Simon-Pierre GERMAIN, Brian William STEENBRINK, Pierre-Luc BEAUCHAMP, Simon LANGLOIS, Evangelos SPYROU
  • Patent number: 9849620
    Abstract: Described herein, amongst other things, is a container preform that is blow moldable into a container. The container preform includes a tubular body having a neck finish and a base at an open end and a closed end thereof respectively. The base is defined between inside and outside curved surfaces at least one of which is composed of multiple tangential curves, wherein an elongate portion is defined between adjacent inside and outside concentric curves that define a thinnest bottom wall thickness of the base having a constant minimum thickness that is smaller than or equal to a wall thickness of the body.
    Type: Grant
    Filed: November 21, 2014
    Date of Patent: December 26, 2017
    Assignee: HUSKY INJECTION MOLDING SYSTEMS LTD.
    Inventors: Marco Duarte, Alaeddin Khalighi, Marc Kleifges, Thomas Zeiler, Peter Gratz, Christophe Simon Pierre Beck
  • Publication number: 20170343033
    Abstract: An attachment system intended to equip a wall (17), the system including a nut intended to receive a screw (31) of which the orientation is normal to the wall (17), the screw (31) passing through an element such as an outer panel (32) in order to attach the element to the wall (17). The attachment system comprises a socket (26) having a threaded cylindrical outer face (34) intended to be screwed into a hole (29) passing through the wall (17) and having dimensions greater than the dimensions of the fastener that the repair socket (26) replaces, the socket (26) carrying, in the central region of same, a nut (28) receiving the attachment screw (32).
    Type: Application
    Filed: December 14, 2015
    Publication date: November 30, 2017
    Applicant: Safran Aircraft Engines
    Inventors: Yann Christophe, Maurice Sarazin, Simon Pierre, Claude Charbonnier, Patrick Jean-Louis Reghezza, Julien Roset
  • Publication number: 20170334125
    Abstract: Disclosed herein, amongst other things, is a method for converting a design of an original preform that is blow moldable to form a container into a converted preform having less molding material that is blow moldable to form the same container. The method includes retaining a neck finish and body of the original preform on the converted preform. The method further includes replacing the original base of the original preform with a converted base having an outer base surface that joins with an outer body surface of the body at an base split-line of the original base and that fits offset within an outer body surface of the original base, whereby the converted preform has a reduced total length, disregarding any gate vestige that may be formed thereon, relative to a total length of the original preform.
    Type: Application
    Filed: November 4, 2015
    Publication date: November 23, 2017
    Applicant: Husky Injection Molding Systems Ltd.
    Inventor: Christophe Simon Pierre BECK