Patents by Inventor Frederic Leclerc
Frederic Leclerc 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: 10673138Abstract: An electronic-scanning antenna composed of radiating elements each forming an active channel in which the signals arising from the channels are grouped together to form deviometry signals, each deviometry signal forming a deviometry channel, and are grouped together according to sectors to form a sector-based signal forming a sector channel, a computation-based beam being formed on the basis of the signals arising from each of the sectors, the method comprises the following steps: measuring the response to a calibration signal of each active channel at one and the same time on the sum deviometry channel and on the sector channel to which it belongs, the responses on the sum channel to obtain the calibration of the sum channel; computing, for each active channel, the disparity between the mean of the responses measured on the sum channel and the mean of the responses measured on the sector to which it belongs; in the operational phase, forming the beam by computation on the basis of the measurements of the sigType: GrantFiled: September 30, 2016Date of Patent: June 2, 2020Assignee: THALESInventors: Philippe Freyssinier, Frédéric LeClerc, Alain Adamjee, Christian Renard, Pierre Levy
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Publication number: 20180248262Abstract: An electronic-scanning antenna composed of radiating elements each forming an active channel in which the signals arising from the channels are grouped together to form deviometry signals, each deviometry signal forming a deviometry channel, and are grouped together according to sectors to form a sector-based signal forming a sector channel, a computation-based beam being formed on the basis of the signals arising from each of the sectors, the method comprises the following steps: measuring the response to a calibration signal of each active channel at one and the same time on the sum deviometry channel and on the sector channel to which it belongs, the responses on the sum channel to obtain the calibration of the sum channel; computing, for each active channel, the disparity between the mean of the responses measured on the sum channel and the mean of the responses measured on the sector to which it belongs; in the operational phase, forming the beam by computation on the basis of the measurements of the sigType: ApplicationFiled: September 30, 2016Publication date: August 30, 2018Inventors: Philippe FREYSSINIER, Frédéric LECLERC, Alain ADAMJEE, Christian RENARD, Pierre LEVY
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Patent number: 7723977Abstract: An optical sensor configuration contains an optical current sensor and/or an optical voltage sensor. The sensor configuration further contains a first and a second hollow member, preferably ring shaped profiles, which are together disposed to form a hollow section. The sensor configuration further includes an optical fiber of the current sensor disposed in an annular groove, the groove being disposed at the boundary surface between the first hollow member and the second hollow member, and/or an optical fiber of the voltage sensor is disposed in a recess of the second hollow member. The first hollow member has an annular recess into which the second hollow member is disposed whereas the first hollow member is an L-shaped or U-shaped ring with two legs and the recess is formed between the two legs.Type: GrantFiled: March 15, 2006Date of Patent: May 25, 2010Assignees: Siemens AG, NXTPhase T&D CorporationInventors: James Norman Blake, Yves Doin, Cataldo Diaferia, Andrzej Klimek, Frédéric Leclerc, Farnoosh Rahmatian
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Publication number: 20080303510Abstract: An optical sensor configuration contains an optical current sensor and/or an optical voltage sensor. The sensor configuration further contains a first and a second hollow member, preferably ring shaped profiles, which are together disposed to form a hollow section. The sensor configuration further includes an optical fiber of the current sensor disposed in an annular groove, the groove being disposed at the boundary surface between the first hollow member and the second hollow member, and/or an optical fiber of the voltage sensor is disposed in a recess of the second hollow member. The first hollow member has an annular recess into which the second hollow member is disposed whereas the first hollow member is an L-shaped or U-shaped ring with two legs and the recess is formed between the two legs.Type: ApplicationFiled: March 15, 2006Publication date: December 11, 2008Applicants: Siemens Transmission & Distrubtion, NxtPhase T&D CorporationInventors: James Norman Blake, Yves Doin, Cataldo Diaferia, Andrzej Klimek, Frederic Leclerc, Farnoosh Rahmatian
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Patent number: 7338013Abstract: This invention relates to a floor (4) for an aircraft, and preferably a cockpit floor, this floor comprising a plurality of spars (14) running along a longitudinal direction (X) of the aircraft and a plurality of cross-beams (16) assembled to the spars and running along a transverse direction (Y) of the aircraft, the floor also comprising attachment means (64) for assembly onto a sealed bottom (68) of the aircraft. According to the invention, the attachment means comprise a plurality of fasteners (66) each comprising at least one junction element with two opposite ends, each of the two opposite ends being articulated about an axis parallel to the (Y) direction.Type: GrantFiled: June 3, 2005Date of Patent: March 4, 2008Assignee: Airbus FranceInventors: Alban Vetillard, Emmanuel Parro, Frederic Leclerc
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Patent number: 7191982Abstract: The invention relates to an aircraft floor (4), preferably a cockpit floor, this floor comprising a plurality of spars (14) running along a longitudinal direction (X) of the aircraft and a plurality of cross-beams (16) assembled to the spars and running along a transverse direction (Y) of the aircraft, the floor also comprising attachment means (64) used to assemble it to fuselage frames. According to the invention, the attachment means comprise a plurality of articulations (66) each connected to one end of one of the cross-beams (16), and enabling rotation about the (X) direction.Type: GrantFiled: June 2, 2005Date of Patent: March 20, 2007Assignee: Airbus FranceInventors: Alban Vetillard, Emmanuel Parro, Frederic Leclerc
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Publication number: 20060226288Abstract: The invention relates to an aircraft floor (4), preferably a cockpit floor, this floor comprising a plurality of spars (14) running along a longitudinal direction (X) of the aircraft and a plurality of cross-beams (16) assembled to the spars and running along a transverse direction (Y) of the aircraft, the floor also comprising attachment means (64) used to assemble it to fuselage frames. According to the invention, the attachment means comprise a plurality of articulations (66) each connected to one end of one of the cross-beams (16), and enabling rotation about the (X) direction.Type: ApplicationFiled: June 2, 2005Publication date: October 12, 2006Applicant: Airbus FranceInventors: Alban Vetillard, Emmanuel Parro, Frederic Leclerc
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Publication number: 20060006284Abstract: This invention relates to a floor (4) for an aircraft, and preferably a cockpit floor, this floor comprising a plurality of spars (14) running along a longitudinal direction (X) of the aircraft and a plurality of cross-beams (16) assembled to the spars and running along a transverse direction (Y) of the aircraft, the floor also comprising attachment means (64) for assembly onto a sealed bottom (68) of the aircraft. According to the invention, the attachment means comprise a plurality of fasteners (66) each comprising at least one junction element with two opposite ends, each of the two opposite ends being articulated about an axis parallel to the (Y) direction.Type: ApplicationFiled: June 3, 2005Publication date: January 12, 2006Applicant: Airbus FranceInventors: Alban Vetillard, Emmanuel Parro, Frederic Leclerc
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Patent number: 6691953Abstract: A plug type door intended particularly for use on a military cargo type aircraft is designed to enable its ejection if necessary. To do this, an operating device such as a handle (28) simultaneously controls retraction of hinge pins (16c) from the hinges about which the panel (10) of the door is hinged to its frame (12) and retraction of the mechanical elements (21) against which the stops (19) fitted on the panel usually bear by gravity, when the door is closed. Furthermore, guide ramps connected to the frame (12) and in which the rollers supported by the panel (10) open downwards, to enable the panel (10) to drop by gravity when the handle (28) is pulled.Type: GrantFiled: January 30, 2003Date of Patent: February 17, 2004Assignee: Airbus FranceInventor: Frédéric Leclerc
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Publication number: 20030141415Abstract: A plug type door intended particularly for use on a military cargo type aircraft is designed to enable its ejection if necessary. To do this, an operating device such as a handle (28) simultaneously controls retraction of hinge pins (16c) from the hinges about which the panel (10) of the door is hinged to its frame (12) and retraction of the mechanical elements (21) against which the stops (19) fitted on the panel usually bear by gravity, when the door is closed. Furthermore, guide ramps connected to the frame (12) and in which the rollers supported by the panel (10) open downwards, to enable the panel (10) to drop by gravity when the handle (28) is pulled.Type: ApplicationFiled: January 30, 2003Publication date: July 31, 2003Inventor: Frederic Leclerc