Patents by Inventor Bruno Foucher

Bruno Foucher 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: 9418039
    Abstract: The invention relates to a device for monitoring the integrity and soundness of a mechanical structure, such as an aircraft. The device comprises a control unit, a radio frequency transmission means, and an electric battery. The control unit recovers data from a set of digital and/or analog sensors. The radio frequency transmission means enables the control unit to transmit the data received from the sensors to a man/machine interface. The electric battery powers the device and is rechargeable. The device further comprises a module for recovering electromagnetic energy capable of converting the recovered electromagnetic energy into electric power so as to recharge the battery and/or directly power the device.
    Type: Grant
    Filed: January 31, 2012
    Date of Patent: August 16, 2016
    Assignees: AIRBUS GROUP SAS, EUROCOPTER
    Inventors: Bruno Foucher, Vincent Rouet, Remy Reynet
  • Patent number: 9058574
    Abstract: A method for estimating the lifetime of a deep-submicron-generation integrated electronic component, linked to a wear mechanism occurring in previously defined special conditions of use, said component being of a deep submicron type, with very large-scale integration, commercially available off the shelf, wherein one assumes that the same sample population always experiences a failure due to: the most predominant failure mechanism, during the period of useful life, described by an exponential law, and the most critical wear mechanism, represented by a Weibull distribution at the end of the previous period.
    Type: Grant
    Filed: June 30, 2010
    Date of Patent: June 16, 2015
    Assignee: EUROPEAN AERONAUTIC DEFENCE AND SPACE COMPANY EADS FRANCE
    Inventors: Florian Moliere, Bruno Foucher
  • Publication number: 20130307703
    Abstract: The invention relates to a device for monitoring the integrity and soundness of a mechanical structure, such as an aircraft. The device comprises a control unit, a radio frequency transmission means, and an electric battery. The control unit recovers data from a set of digital and/or analog sensors. The radio frequency transmission means enables the control unit to transmit the data received from the sensors to a man/machine interface. The electric battery powers the device and is rechargeable. The device further comprises a module for recovering electromagnetic energy capable of converting the recovered electromagnetic energy into electric power so as to recharge the battery and/or directly power the device.
    Type: Application
    Filed: January 31, 2012
    Publication date: November 21, 2013
    Applicant: EUROPEAN AERNAUTIC DEFENCE AND SPACE COMPANY EADS FRANCE
    Inventors: Bruno Foucher, Vincent Rouet, Remy Reynet
  • Patent number: 8306785
    Abstract: To solve a leakage problem in a box, it is proposed to provide the box with an electronic circuit for measurement of its specific humidity. It is shown that by comparing this current specific humidity to an initial specific humidity and by evaluating the difference found in relation thereto, one has a reliable tool for measuring the permanence of tightness.
    Type: Grant
    Filed: March 5, 2008
    Date of Patent: November 6, 2012
    Assignee: European Aeronautic Defence and Space Company EADS France
    Inventors: Bruno Foucher, Vincent Rouet
  • Publication number: 20120143557
    Abstract: A large range of commercial VLSI Deep Submicron circuits are used in aeronautics for designs of electronic cards. Due to miniaturization, a continually increasing level of integration and the use of new materials in the foundries, the main failure mechanisms change whilst other ones appear. The lifetimes linked to these failure mechanisms are suspected of being shorter and shorter, so that predicting the lifetime becomes a significant challenge for the reliability of Deep Submicron (DSM) semiconductors. A new approach is proposed here, based on analyzing the technology so as to determine the potential risks to reliability with respect to the specific use of DSM components for avionics applications.
    Type: Application
    Filed: June 30, 2010
    Publication date: June 7, 2012
    Inventors: Florian Moliere, Bruno Foucher
  • Patent number: 8175818
    Abstract: A monitoring device of environmental parameter values of an environment surrounding a system. The device includes a sensor to these parameters, and includes a capability to transmit, in real time, each measurement to a processing unit. The processing unit is installed in the system and includes a capability to filter the transmitted measurements. This processing unit comprises a capability to determine cycles from the measurements thus simplified as well as a capability to calculate, in real time, of a percentage of length of consumed life of the system, from the thus determined cycles.
    Type: Grant
    Filed: January 23, 2007
    Date of Patent: May 8, 2012
    Assignee: European Aeronautic Defence and Space Company EADS France et EADS CCR
    Inventors: Bruno Foucher, Vincent Rouet
  • Publication number: 20110060547
    Abstract: To solve a leakage problem in a box, it is proposed to provide the box with an electronic circuit for measurement of its specific humidity. It is shown that by comparing this current specific humidity to an initial specific humidity and by evaluating the difference found in relation thereto, one has a reliable tool for measuring the permanence of tightness.
    Type: Application
    Filed: March 5, 2008
    Publication date: March 10, 2011
    Applicant: European Aeronautic Defence And Space Company Eads France
    Inventors: Bruno Foucher, Vincent Rouet
  • Publication number: 20110046996
    Abstract: According to the invention, to determine an operating forecast for a system, measurements are taken of an environmental value in an environment surrounding the system. Then these measurements are processed in a processing unit in order to determine how much of the system's lifetime has been consumed. The consumed lifetime is based on a history of the system in the environment. This is used to calculate a forecast of a good operating lifetime. According to the invention, this forecast determination is made by adaptive linear regression. Thus, all forecast calculations are simplified and can be performed by the system itself and in real-time.
    Type: Application
    Filed: April 1, 2009
    Publication date: February 24, 2011
    Applicant: European Aeronautic Defence and Space Company EADS France
    Inventors: Bruno Foucher, Katell Moreau, Vincent Rouet
  • Publication number: 20090306908
    Abstract: A monitoring device of environmental parameter values of an environment surrounding a system. The device includes a sensor to these parameters, and includes a means of transmission, in real time, of each measurement to a processing unit. The processing unit is installed in the system and includes the means of filtering the transmitted measurements. This processing unit comprises the means for determining cycles from the measurements thus simplified as well as the means for calculation, in real time, of a length of consumed life of the system, from the thus determined cycles.
    Type: Application
    Filed: January 23, 2007
    Publication date: December 10, 2009
    Applicants: EUROPEAN AERONAUTIC DEFENCE AND SPACE COMPANY EADS FRANCE, EADS CCR GROUPEMENT D'INTERET ECONOMIQUE
    Inventors: Bruno Foucher, Vincent Rouet