Inventor · disambiguated record
Frédéric Chelin
Also filed as: CHELIN FREDERIC · CHELIN FRÉDÉRIC
24 granted patents·6 pending applications·111 citations·filing 2007–2024
94Inventor score
Top patents by PatentIndex Score
30 records- 0191US9010084B2Aircraft nacelle including an optimised acoustic processing systemCHELIN FRÉDÉRIC·Filed 2010·Granted Apr 21, 2015·19 cites·20 claims
- 0286US9719422B2Process for the production of an acoustic treatment panel that integrates channels juxtaposed with an alveolar structurePORTE ALAIN·Filed 2012·Granted Aug 1, 2017·5 cites·11 claims
- 0385US8851416B2Aircraft nacelle including at least one radial partition between two conductsPORTE ALAIN·Filed 2011·Granted Oct 7, 2014·9 cites·20 claims
- 0483US8993090B2Part for and method of repairing a damaged structure, in particular an airframe skin, and a repair kit for implementing itBOULET NICOLAS·Filed 2012·Granted Mar 31, 2015·7 cites·8 claims
- 0581US8434724B2Air outlet system for aircraft leading edgeCHELIN FREDERIC·Filed 2008·Granted May 7, 2013·19 cites·20 claims
- 0680US8794572B2Air intake of an aircraft nacelle that incorporates a reinforced lip with a defrost system by joule-effectPORTE ALAIN·Filed 2012·Granted Aug 5, 2014·8 cites·18 claims
- 0775US8628635B2Method for making a network of drainage pipes and acoustic processing panel including such a network of drainage pipesCHELIN FREDERIC·Filed 2010·Granted Jan 14, 2014·5 cites·17 claims
- 0874US9003810B2Aircraft cover including means for limiting the scoop phenomena of pneumatic typePORTE ALAIN·Filed 2011·Granted Apr 14, 2015·6 cites·10 claims
- 0973US9353648B2Panel for the acoustic treatment comprising hot air ducts and at least one annular channelPORTE ALAIN·Filed 2012·Granted May 31, 2016·6 cites·12 claims
- 1072US9114884B2Aircraft nacelle comprising a reinforced outer wallCHELIN FRÉDÉRIC·Filed 2010·Granted Aug 25, 2015·4 cites·20 claims
- 1172US8991054B2Process for the production of a panel for the acoustic treatment incorporating the frost treatment function with hot airPORTE ALAIN·Filed 2012·Granted Mar 31, 2015·4 cites·20 claims
- 1271US10377503B2Engine assembly of an aircraft including a display unitAIRBUS OPERATIONS SAS·Filed 2016·Granted Aug 13, 2019·2 cites·11 claims
- 1371US9003760B2Acoustic processing panel, more particularly adapted for an air intake in an aircraft nacelleCHELIN FRÉDÉRIC·Filed 2010·Granted Apr 14, 2015·5 cites·12 claims
- 1469US8960589B2Panel for an air intake of an aircraft nacelle that ensures optimized acoustic treatment and frost treatmentPORTE ALAIN·Filed 2010·Granted Feb 24, 2015·4 cites·20 claims
- 1567US8142144B2Turbine engine for aircraftPORTE ALAIN·Filed 2007·Granted Mar 27, 2012·7 cites·15 claims
- 1658US12012911B2Deflector provided with faces with different curvatures for a thrust reverser of an aircraft engine nacelleAIRBUS OPERATIONS SAS·Filed 2023·Granted Jun 18, 2024·0 cites·15 claims
- 1754US12247528B2Deflector provided with a spoiler for a thrust reverser of an aircraft engine nacelleAIRBUS OPERATIONS SAS·Filed 2023·Granted Mar 11, 2025·0 cites·12 claims
- 1852US9284060B2Aircraft nacelle including a rear frame inclined to the rearPORTE ALAIN·Filed 2011·Granted Mar 15, 2016·1 cites·11 claims
- 1950US12492668B2Aircraft nacelle provided with at least one thrust reversal device comprising at least one longitudinal deflector, aircraft comprising at least one propulsion assembly composed of such a nacelleAIRBUS OPERATIONS SAS·Filed 2024·Granted Dec 9, 2025·0 cites·12 claims
- 2048US12404820B2Aircraft nacelle equipped with at least one thrust reversal device comprising at least one longitudinal deflector configured to house a longitudinal actuatorAIRBUS OPERATIONS SAS·Filed 2024·Granted Sep 2, 2025·0 cites·13 claims
- 2147US12292015B2Aircraft nacelle equipped with at least one thrust reversal device comprising a downstream deflector, aircraft comprising at least one propulsion unit having such a nacelleAIRBUS OPERATIONS SAS·Filed 2024·Granted May 6, 2025·0 cites·11 claims
- 2246US8918977B2Process for the destruction of a blind fastener and device for its implementationAIRBUS OPERATIONS SAS·Filed 2012·Granted Dec 30, 2014·0 cites·6 claims
- 2345US2024124148A1Aircraft engine nacelle provided with a thrust reverser having a mobile ejection structureAIRBUS OPERATIONS SAS·Filed 2023·Application pending·0 cites
- 2443US9261021B2Turbine engine for aircraftPORTE ALAIN·Filed 2007·Granted Feb 16, 2016·0 cites·3 claims
- 2540US2012091285A1Aircraft nacelle including a continue joint area between an outer wall and a front framePORTE ALAIN·Filed 2011·Application pending·0 cites
- 2634US8757541B2Measurement instrument support interposed between a drive unit and an air intake of an aircraft nacelleCHELIN FRÉDÉRIC·Filed 2009·Granted Jun 24, 2014·0 cites·5 claims
- 2734US2020340426A1Thrust reverser door equipped with a projecting seal and aircraft propulsion unit comprising said doorAIRBUS OPERATIONS SAS·Filed 2020·Application pending·0 cites
- 2834US2013098471A1Aircraft nacelle comprising a hot air supply device for a panel combining acoustic and frost treatmentsPORTE ALAIN·Filed 2012·Application pending·0 cites
- 2933US2012097260A1Aircraft cover including means for limiting the scoop phenomena of electromagnetic typePORTE ALAIN·Filed 2011·Application pending·0 cites
- 3033US2009277181A1Aircraft propulsion unit that comprises an exhaust pipe with a scalloped trailing edgeAIRBUS FRANCE SAS·Filed 2007·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →