Inventor · disambiguated record
Francois Marie Paul Marlin
Also filed as: MARLIN FRANCOIS · MARLIN FRANCOIS MARIE PAUL · MARLIN FRANÇOIS · MARLIN FRANÇOIS MARIE PAUL
20 granted patents·304 citations·filing 2000–2021
94Inventor score
Files withSAFRAN AIRCRAFT ENGINES7MARLIN FRANCOIS MARIE PAUL3SNECMA3SNECMA MOTEURS3ALBERT BRICE BRUNO1
Top patents by PatentIndex Score
20 records- 0196US8322971B2Method of manufacturing a gas turbine casing out of composite material, and a casing as obtained therebyCOUPE DOMINIQUE·Filed 2008·Granted Dec 4, 2012·70 cites·12 claims
- 0295US6398483B1Protection device for protecting control mechanism of inlet guide-vanes of turbojet engineSNECMA MOTEURS·Filed 2000·Granted Jun 4, 2002·48 cites·14 claims
- 0391US10723476B2Ring of turbojet vanes including an acoustic treatment structureSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Jul 28, 2020·7 cites·15 claims
- 0491US6676373B2Assembly formed by at least one blade and a blade-fixing platform for a turbomachine, and a method of manufacturing itSNECMA MOTEURS·Filed 2001·Granted Jan 13, 2004·49 cites·35 claims
- 0588US8424921B2Composite coupling with a machining portionMARLIN FRANCOIS MARIE PAUL·Filed 2008·Granted Apr 23, 2013·11 cites·10 claims
- 0686US8544598B2Soundproofing panel for turbomachine and turbomachine comprising such a panelGAUDRY FLORIAN·Filed 2012·Granted Oct 1, 2013·19 cites·18 claims
- 0782US8061967B2Panel for supporting abradable material in a turbomachineMARLIN FRANCOIS MARIE PAUL·Filed 2008·Granted Nov 22, 2011·17 cites·15 claims
- 0882US7055304B2De-icing device for turbojet inlet guide wheel vane, vane provided with such a de-icing device, and aircraft engine equipped with such vanesSNECMA MOTEURS·Filed 2004·Granted Jun 6, 2006·55 cites·32 claims
- 0980US10494997B2Device for de-icing a splitter nose of an aviation turbine engineSAFRAN AIRCRAFT ENGINES·Filed 2017·Granted Dec 3, 2019·3 cites·10 claims
- 1080US9441494B2Turbomachine rotor with a means for axial retention of the bladesMARLIN FRANCOIS MARIE PAUL·Filed 2012·Granted Sep 13, 2016·7 cites·9 claims
- 1174US9545762B2Composite coupling with a machining portionSNECMA·Filed 2013·Granted Jan 17, 2017·3 cites·9 claims
- 1260US9528441B2Aircraft turbofan comprising an intermediate ring with simplified downstream supportSNECMA·Filed 2014·Granted Dec 27, 2016·2 cites·9 claims
- 1359US10100859B2Riveted assembly and associated production methodSAFRAN AIRCRAFT ENGINES·Filed 2015·Granted Oct 16, 2018·1 cites·12 claims
- 1459US9657644B2Method for mounting an acoustic panel in a housing of a turbomachine and turbomachine comprising an acoustic panelSNECMA·Filed 2013·Granted May 23, 2017·2 cites·9 claims
- 1558US8075246B2Relief device for a turbojet and a turbojet comprising sameALBERT BRICE BRUNO·Filed 2008·Granted Dec 13, 2011·7 cites·13 claims
- 1656US11591970B2Assembly for retaining a gear train in a turbomachineSAFRAN AIRCRAFT ENGINES·Filed 2019·Granted Feb 28, 2023·0 cites·20 claims
- 1756US8123465B2Mounting tubes for pressurizing an internal enclosure in a turbomachineLARGILLIER CHRISTIAN·Filed 2008·Granted Feb 28, 2012·3 cites·10 claims
- 1848US12110829B2Turbomachine fan assembly comprising a roller bearing and a double-row ball bearing with oblique contactSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Oct 8, 2024·0 cites·8 claims
- 1938US12168942B2Intermediate flow-straightening casing with monobloc structural armSAFRAN AIRCRAFT ENGINES·Filed 2021·Granted Dec 17, 2024·0 cites·16 claims
- 2030US10760501B2Arm for turbine-engine casing comprising a removable additional pieceSAFRAN AIRCRAFT ENGINES·Filed 2017·Granted Sep 1, 2020·0 cites·10 claims
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