Patents by Inventor Marc VIE
Marc VIE 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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Publication number: 20210354845Abstract: A human-machine interface system enables interactions between aeronautical applications and aircraft control and display instruments. The human-machine interface system comprises an interface server communicating, by virtue of a common core protocol, with the aeronautical applications and control and display managers performing an abstraction of control and display instruments. The human-machine interface comprises application extension libraries providing an implementation of the common core protocol dedicated to each aeronautical application, as well as a display window definition dedicated to each aeronautical application. The human-machine interface comprises at least one control and display utility extension library providing an implementation of the common core protocol dedicated to the control and display managers. Hence, a flexible, portable and reusable architecture with easy extension and scalability opportunities is provided.Type: ApplicationFiled: May 14, 2021Publication date: November 18, 2021Inventors: Neset SOZEN, Marc VIE
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Patent number: 10490090Abstract: A method and device for adjusting performance variables of an aircraft. The device which is intended for adjusting performance variables, the performance variables being generated by at least one performance module, includes an auxiliary data input unit for entering into a flight management system correction data intended to be used for adjusting at least one associated performance variable, and a correction unit for carrying out a correction, the correction including adjusting the associated performance variable on the basis of the input correction data.Type: GrantFiled: December 13, 2017Date of Patent: November 26, 2019Assignee: Airbus Operations (S.A.S.)Inventors: Esteban Quiroz-Hernandez, Christophe Bouchet, Jean-Pierre Demortier, Sylvain Raynaud, François Cusset, Marc Vie, Alexandre Grattard
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Patent number: 10216180Abstract: A flight management system architecture with separate core and supplementary modules. In the core module, generic functionalties relative to the flight management of the aircraft are implemented. In the supplementary module, supplementary functions are implemented. The supplementary functionalities include functionalties specific to an entity to which the aircraft belongs such as the specific aircraft model, a family of aircraft, a company, an alliance, and so on. The flight management system also includes a message exchange interface in which enables the core and supplementary modules to exchanges messages with each other. The core and supplementary modules includes corresponding core module and supplementary module interfacing functionaltities that respectively interface with generic and specific man-machine interfaces.Type: GrantFiled: February 1, 2017Date of Patent: February 26, 2019Assignee: Airbus Operations (S.A.S.)Inventors: Jean-Claude Mere, Pierre Neri, Julien Bernat, Marc Vie
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Publication number: 20180174473Abstract: A method and device for adjusting performance variables of an aircraft. The device which is intended for adjusting performance variables, the performance variables being generated by at least one performance module, includes an auxiliary data input unit for entering into a flight management system correction data intended to be used for adjusting at least one associated performance variable, and a correction unit for carrying out a correction, the correction including adjusting the associated performance variable on the basis of the input correction data.Type: ApplicationFiled: December 13, 2017Publication date: June 21, 2018Inventors: Esteban Quiroz-Hernandez, Christophe Bouchet, Jean-Pierre Demortier, Sylvain Raynaud, François Cusset, Marc Vie, Alexandre Grattard
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Patent number: 9709982Abstract: A flight management system with core and supplementary modules is proposed. The core module may include generic applications that implement generic functionalities related to a flight management of the aircraft. The supplementary module may include supplementary applications that implement supplementary functionalities specific to an entity to which the aircraft belongs. The supplementary module may be divided into principal and auxiliary partitions (or entities), and the supplementary applications, also referred to as principal applications, may be implemented in the principal partition. One or more auxiliary applications may be implemented in the auxiliary partition. Each auxiliary application may be associated with one or more principal applications such that the execution of the principal application requires the associated auxiliary application to be executed.Type: GrantFiled: November 25, 2014Date of Patent: July 18, 2017Assignee: Airbus Operations (SAS)Inventors: Jean-Claude Mere, Pierre Neri, Julien Bernat, Marc Vie
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Publication number: 20170147008Abstract: A flight management system architecture with separate core and supplementary modules. In the core module, generic functionalties relative to the flight management of the aircraft are implemented. In the supplementary module, supplementary functions are implemented. The supplementary functionalities include functionalties specific to an entity to which the aircraft belongs such as the specific aircraft model, a family of airdraft, a company, an alliance, and so on. The flight management system also includes a message exchange interface in which enables the core and supplementary modules to exchanges messages with each other. The core and supplementary modules includes corresponding core module and supplementary module interfacing functionaltities that respectively interface with generic ans specific man-machine interfaces.Type: ApplicationFiled: February 1, 2017Publication date: May 25, 2017Inventors: Jean-Claude MERE, Pierre NERI, Julien BERNAT, Marc VIE
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Patent number: 9606534Abstract: A flight management system architecture with two separate modules is proposed. In the core module, generic functionalities relative to the flight management of the aircraft are implemented. In the supplementary module, supplementary functions are implemented. The supplementary functionalities include functionalities specific to an entity to which the aircraft belongs such as the specific aircraft model, a family of airdraft, a company, an alliance, and so on. The flight management system also includes a message exchange interface in which enables the core and supplementary modules to exchanges messages with each other. The core and supplementary modules includes corresponding core module and supplementary module interfacing functionalities that respectively interface with generic and specific man-machine interfaces.Type: GrantFiled: November 25, 2014Date of Patent: March 28, 2017Assignee: Airbus Operations (SAS)Inventors: Jean-Claude Mere, Pierre Neri, Julien Bernat, Marc Vie
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Patent number: 9583008Abstract: A flight management system includes: an avionics core implementing generic aircraft management functionalities and providing services associated with the generic functionalities; at least one remote functionality in an open world part performing a function of interfacing between the avionics core and the open world applications run on the open world part which need to communicate with the avionics core, wherein the remote functionality ensures homogeneity and consistency of data exchanged and guaranteeing integrity and security of data exchanges, and an exchange interface of between the avionics core and the open world functionality supporting data exchanges.Type: GrantFiled: December 4, 2015Date of Patent: February 28, 2017Assignee: Airbus Operations (S.A.S.)Inventors: Gaetan Marion, Jean-Claude Mere, Pierre Neri, Julien Bernat, Marc Vie
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Patent number: 9529356Abstract: A system to manage transmissions of data between a flight management system (e.g., of an avionics type) of an aircraft and a portable electronic (e.g., of an open world type) is proposed. The data management system may be implemented in flight management system architecture with core and supplementary modules that are distinct from each other. The core module may implement a set of generic functionalities related to a flight management of the aircraft, and the supplementary module may implement supplementary functionalities specific to an entity to which the aircraft belongs. The data management system may comprise a data securing module that monitors data to be transmitted between the flight management system and the portable electronic device, and allows or prevents the data transmission based on the monitoring results.Type: GrantFiled: November 25, 2014Date of Patent: December 27, 2016Assignee: Airbus Operations (S.A.S.)Inventors: Jean-Claude Mere, Pierre Neri, Julien Bernat, Marc Vie
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Publication number: 20160163202Abstract: A flight management system includes: an avionics core implementing generic aircraft management functionalities and providing services associated with the generic functionalities; at least one remote functionality in an open world part performing a function of interfacing between the avionics core and the open world applications run on the open world part which need to communicate with the avionics core, wherein the remote functionality ensures homogeneity and consistency of data exchanged and guaranteeing integrity and security of data exchanges, and an exchange interface of between the avionics core and the open world functionality supporting data exchanges.Type: ApplicationFiled: December 4, 2015Publication date: June 9, 2016Inventors: Gaetan MARION, Jean-Claude MERE, Pierre NERI, Julien BERNAT, Marc VIE
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Patent number: 9323248Abstract: A mission management system to manage both ground and flight phases of a mission of an aircraft is proposed. The mission management system may be implemented in flight management system architecture with core and supplementary modules distinct from each other. The core module may implement a set of generic functionalities related to a flight management of the aircraft, and the supplementary module may implement supplementary functionalities specific to an entity to which the aircraft belongs. The mission management system may include a flight management unit to define and manage a flight plan and associated flight trajectory, an airport navigation unit to define and manage a ground plan and associated ground trajectory, and a mission management unit to manage a continuity between the ground and flight phases of the mission and prediction computations made by the flight management and the airport navigation units.Type: GrantFiled: November 25, 2014Date of Patent: April 26, 2016Assignee: Airbus Operations (S.A.S.)Inventors: Jean-Claude Mere, Pierre Neri, Julien Bernat, Marc Vie
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Publication number: 20150148998Abstract: A flight management system with core and supplementary modules is proposed. The core module may include generic applications that implement generic functionalities related to a flight management of the aircraft. The supplementary module may include supplementary applications that implement supplementary functionalities specific to an entity to which the aircraft belongs. The supplementary module may be divided into principal and auxiliary partitions (or entities), and the supplementary applications, also referred to as principal applications, may be implemented in the principal partition. One or more auxiliary applications may be implemented in the auxiliary partition. Each auxiliary application may be associated with one or more principal applications such that the execution of the principal application requires the associated auxiliary application to be executed.Type: ApplicationFiled: November 25, 2014Publication date: May 28, 2015Inventors: Jean-Claude MERE, Pierre NERI, Julien BERNAT, Marc VIE
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Publication number: 20150150095Abstract: A system to manage transmissions of data between a flight management system (e.g., of an avionics type) of an aircraft and a portable electronic (e.g., of an open world type) is proposed. The data management system may be implemented in flight management system architecture with core and supplementary modules that are distinct from each other. The core module may implement a set of generic functionalities related to a flight management of the aircraft, and the supplementary module may implement supplementary functionalities specific to an entity to which the aircraft belongs. The data management system may comprise a data securing module that monitors data to be transmitted between the flight management system and the portable electronic device, and allows or prevents the data transmission based on the monitoring results.Type: ApplicationFiled: November 25, 2014Publication date: May 28, 2015Inventors: Jean-Claude MERE, Pierre NERI, Julien BERNAT, Marc VIE
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Publication number: 20150148996Abstract: A flight management system architecture with two separate modules is proposed. In the core module, generic functionalties relative to the flight management of the aircraft are implemented. In the supplementary module, supplementary functions are implemented. The supplementary functionalities include functionalties specific to an entity to which the aircraft belongs such as the specific aircraft model, a family of airdraft, a company, an alliance, and so on. The flight management system also includes a message exchange interface in which enables the core and supplementary modules to exchanges messages with each other. The core and supplementary modules includes corresponding core module and supplementary module interfacing functionaltities that respectively interface with generic and specific man-machine interfaces.Type: ApplicationFiled: November 25, 2014Publication date: May 28, 2015Inventors: Jean-Claude MERE, Pierre NERI, Julien BERNAT, Marc VIE
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Publication number: 20150148999Abstract: A mission management system to manage both ground and flight phases of a mission of an aircraft is proposed. The mission management system may be implemented in flight management system architecture with core and supplementary modules distinct from each other. The core module may implement a set of generic functionalities related to a flight management of the aircraft, and the supplementary module may implement supplementary functionalities specific to an entity to which the aircraft belongs. The mission management system may include a flight management unit to define and manage a flight plan and associated flight trajectory, an airport navigation unit to define and manage a ground plan and associated ground trajectory, and a mission management unit to manage a continuity between the ground and flight phases of the mission and prediction computations made by the flight management and the airport navigation units.Type: ApplicationFiled: November 25, 2014Publication date: May 28, 2015Inventors: Jean-Claude MERE, Pierre NERI, Julien BERNAT, Marc VIE