Growing community of inventors

Moissy-Cramayel, France

Samuel Laurent Noël Mathieu Juge

Average Co-Inventor Count = 7.87

ph-index = 1

The patent ph-index is calculated by counting the number of publications for which an author has been cited by other authors at least that same number of times.

Forward Citations = 1

Samuel Laurent Noël Mathieu JugeEdouard Emmanuel Garreau (2 patents)Samuel Laurent Noël Mathieu JugeThomas Tsassis (2 patents)Samuel Laurent Noël Mathieu JugeLucas Geoffrey Desbois (2 patents)Samuel Laurent Noël Mathieu JugeBa-Phuc Tang (1 patent)Samuel Laurent Noël Mathieu JugeEtienne Leon Francois (1 patent)Samuel Laurent Noël Mathieu JugeJosserand Jacques Andre Bassery (1 patent)Samuel Laurent Noël Mathieu JugeJosserand Jacques André Bassery (2 patents)Samuel Laurent Noël Mathieu JugeEric Jacques Delcoigne (1 patent)Samuel Laurent Noël Mathieu JugeJean-Philippe Mallat-Desmortiers (1 patent)Samuel Laurent Noël Mathieu JugeDenis Gabriel Trahot (1 patent)Samuel Laurent Noël Mathieu JugeElsa Maxime (1 patent)Samuel Laurent Noël Mathieu JugePeter Shamma Jeanty (1 patent)Samuel Laurent Noël Mathieu JugeSamuel Laurent Noël Mathieu Juge (2 patents)Edouard Emmanuel GarreauEdouard Emmanuel Garreau (2 patents)Thomas TsassisThomas Tsassis (2 patents)Lucas Geoffrey DesboisLucas Geoffrey Desbois (2 patents)Ba-Phuc TangBa-Phuc Tang (14 patents)Etienne Leon FrancoisEtienne Leon Francois (5 patents)Josserand Jacques Andre BasseryJosserand Jacques Andre Bassery (4 patents)Josserand Jacques André BasseryJosserand Jacques André Bassery (2 patents)Eric Jacques DelcoigneEric Jacques Delcoigne (2 patents)Jean-Philippe Mallat-DesmortiersJean-Philippe Mallat-Desmortiers (2 patents)Denis Gabriel TrahotDenis Gabriel Trahot (2 patents)Elsa MaximeElsa Maxime (2 patents)Peter Shamma JeantyPeter Shamma Jeanty (1 patent)
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Inventor’s number of patents
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Strength of working relationships

Company Filing History:

1. Safran Aircraft Engines (2 from 1,845 patents)


2 patents:

1. 11867065 - Blade for a rotating bladed disk for an aircraft turbine engine comprising a sealing lip having an optimized non-constant cross section

2. 11814982 - Vane for an aircraft turbine engine

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