Patents by Inventor Jean Brousseau

Jean Brousseau 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: 11977570
    Abstract: Content of different formats may be sourced from various data sources such as content servers and ingested into a data integration server by an ingestion broker embodied on a non-transitory computer readable medium. The ingestion broker may normalize the content of different formats into a uniform representation that can be indexed and delivered across multiple digital channels for a variety of applications. The normalized content may be analyzed and semantic metadata may be determined from the normalized content. The normalized content can be semantically enriched by associating the semantic metadata and the like with the content. The semantic metadata can be stored in a semantic index that can be used for searching via the data integration server. During search, the semantic metadata can be instantiated as facets for user navigation and refinement of search criteria and additional semantic relationships can be assigned to the words in the normalized content.
    Type: Grant
    Filed: May 16, 2022
    Date of Patent: May 7, 2024
    Assignee: OPEN TEXT SA ULC
    Inventors: Pascal Dimassimo, Steve Pettigrew, Martin Brousseau, Charles-Olivier Simard, Eric Williams, Francis Lacroix, Alex Dowgailenko, Agostino Deligia, Jean-Michel Texier
  • Publication number: 20200130851
    Abstract: Systems and methods to facilitate a steep final approach phase of flight of an aircraft are disclosed. In one embodiment, a method for operating an aircraft during a steep approach phase of flight of the aircraft comprises operating an engine of the aircraft at an idle speed associated with the steep approach type that is lower than an idle speed associated with a non-steep approach type capable of being executed by the aircraft. The method also comprises operating an ice protection system of the aircraft during the steep approach phase of flight of the aircraft.
    Type: Application
    Filed: June 29, 2017
    Publication date: April 30, 2020
    Inventors: Remi HAMEL, Olivier LEBEGUE, Valerie DESILETS, Jean BROUSSEAU, Sigit AFRIANTO, Andrew J. BYRNE, Eric HODGE
  • Patent number: 10253691
    Abstract: A device for protecting aircraft equipment against contact by a foreign object including an interference arrangement disposed in an air inlet upstream from the aircraft equipment where the interference arrangement is configured to physically obstruct passage of the foreign object within the air inlet.
    Type: Grant
    Filed: February 25, 2014
    Date of Patent: April 9, 2019
    Assignee: C SERIES AIRCRAFT LIMITED PARTNERSHIP
    Inventors: Sigit Afrianto, Jean Brousseau
  • Publication number: 20170184030
    Abstract: A method for controlling a pressure control mechanism in a turbofan engine having a precooler permitting heat exchange between ambient air and bleed air includes detecting at least one of an engine failure or a bleed system failure, detecting at least one of an ice condition or an activation of an anti-ice system, and actuating the pressure control mechanism, thereby altering the heat exchange between the ambient air and the bleed air.
    Type: Application
    Filed: March 13, 2017
    Publication date: June 29, 2017
    Inventors: Jean BROUSSEAU, Sigit AFRIANTO, Remi HAMEL, Valerie DESILETS
  • Patent number: 9624831
    Abstract: An aircraft engine includes a precooler disposed within a nacelle. The precooler defines an ambient air passage and a bleed air passage. Air passes through the precooler from an ambient air inlet to an ambient air outlet. Bleed air passes through the precooler from a bleed air inlet to a bleed air outlet. Heat is transferred between the air and the bleed air via heat exchange within the precooler. At least one pressure relief door disposed proximate to the air outlet of the engine. A controller is operatively connected to the pressure relief door. The controller at least opens the pressure relief door based on a demand for increased flow of air through the ambient air passage.
    Type: Grant
    Filed: March 16, 2012
    Date of Patent: April 18, 2017
    Assignee: BOMBARDIER INC.
    Inventors: Jean Brousseau, Sigit Afrianto, Remi Hamel, Valerie Desilets
  • Publication number: 20160017804
    Abstract: A device for protecting aircraft equipment against contact by a foreign object including an interference arrangement disposed in an air inlet upstream from the aircraft equipment where the interference arrangement is configured to physically obstruct passage of the foreign object within the air inlet.
    Type: Application
    Filed: February 25, 2014
    Publication date: January 21, 2016
    Inventors: Sigit Afrianto, Jean Brousseau
  • Publication number: 20140000279
    Abstract: An aircraft engine includes a precooler disposed within a nacelle. The precooler defines an ambient air passage and a bleed air passage. Air passes through the precooler from an ambient air inlet to an ambient air outlet. Bleed air passes through the precooler from a bleed air inlet to a bleed air outlet. Heat is transferred between the air and the bleed air via heat exchange within the precooler. At least one pressure relief door disposed proximate to the air outlet of the engine. A controller is operatively connected to the pressure relief door. The controller at least opens the pressure relief door based on a demand for increased flow of air through the ambient air passage.
    Type: Application
    Filed: March 16, 2012
    Publication date: January 2, 2014
    Applicant: BOMBARDIER INC.
    Inventors: Jean Brousseau, Sigit Afrianto, Remi Hamel, Valerie Desilets
  • Publication number: 20080098291
    Abstract: The present invention is directed to systems and methods of creating and deploying electronic forms for collecting information from a user using a browser, where the browser may be one of a plurality of browser platforms. Characteristics of forms are entered by a human designer using a form designer by using drag-and-drop operations, and stored in XML template files. The form may be previewed by the designer. When a user on the Internet (or an intranet) requests a form by a browser, the characteristics of the browser are sensed and a form appropriate for the browser is deployed to the browser by a form server. Information is then captured from the user. The form may also be saved or printed.
    Type: Application
    Filed: October 8, 2007
    Publication date: April 24, 2008
    Applicant: Adobe Systems Incorporated
    Inventors: George Bradley, Jean Brousseau, Kevin Matassa, Ernest Foster, Andrew Neilson, Mark Leyden, Keith McLellan, Mark Brooks, Zbigniew Rachniowski, Anthony Rumsey, Nasif Dawd