Growing community of inventors

Moissy-Cramayel, France

Anthony Texier

Average Co-Inventor Count = 5.90

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 = 0

Anthony TexierSerge Alain Fargeas (3 patents)Anthony TexierPatrick Emilien Paul Emile Huchin (3 patents)Anthony TexierSébastien Digard Brou De Cuissart (3 patents)Anthony TexierMarc Soisson (3 patents)Anthony TexierValéry Piaton (3 patents)Anthony TexierKarine Deschandol (3 patents)Anthony TexierSebastien Digard Brou De Cuissart (1 patent)Anthony TexierMarie Mineur-Panigeon (1 patent)Anthony TexierCéline Jeanne Marcillaud (2 patents)Anthony TexierDamien Hebuterne (1 patent)Anthony TexierCeline Jeanne Marcillaud (1 patent)Anthony TexierNicolas Batista (1 patent)Anthony TexierAnthony Texier (4 patents)Serge Alain FargeasSerge Alain Fargeas (16 patents)Patrick Emilien Paul Emile HuchinPatrick Emilien Paul Emile Huchin (12 patents)Sébastien Digard Brou De CuissartSébastien Digard Brou De Cuissart (8 patents)Marc SoissonMarc Soisson (7 patents)Valéry PiatonValéry Piaton (5 patents)Karine DeschandolKarine Deschandol (3 patents)Sebastien Digard Brou De CuissartSebastien Digard Brou De Cuissart (10 patents)Marie Mineur-PanigeonMarie Mineur-Panigeon (3 patents)Céline Jeanne MarcillaudCéline Jeanne Marcillaud (2 patents)Damien HebuterneDamien Hebuterne (1 patent)Celine Jeanne MarcillaudCeline Jeanne Marcillaud (1 patent)Nicolas BatistaNicolas Batista (1 patent)
..
Inventor’s number of patents
..
Strength of working relationships

Company Filing History:

1. Snecma (3 from 1,659 patents)

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


4 patents:

1. 10363633 - Method for manufacturing at least one metal turbine engine part

2. 9969035 - Method for producing a turbine engine part, and resulting mould and intermediate blank

3. 9844843 - Method for producing turbine engine parts, and resulting blank and mould

4. 9796058 - Method for producing turbine engine parts, and resulting mould and blank compromising stacked parts

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as of
12/17/2025
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