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name:-0.0070340633392334
name:-0.0077681541442871
name:-0.00038695335388184
Fremont; Elric Georges Andre Patent Filings

Fremont; Elric Georges Andre

Patent Applications and Registrations

Patent applications and USPTO patent grants for Fremont; Elric Georges Andre.The latest application filed is for "method of fabricating a composite material casing for a gas turbine engine, and a casing obtained thereby".

Company Profile
0.11.11
  • Fremont; Elric Georges Andre - Merignac N/A FR
*profile and listings may contain filings by different individuals or companies with the same name. Review application materials to confirm ownership/assignment.
Patent Activity
PatentDate
Assembly formed by a turbine nozzle or a compressor diffuser made of CMC for a turbine engine and by an abradable material support ring, and a turbine or a compressor incorporating such an assembly
Grant 9,822,655 - Beaujard , et al. November 21, 2
2017-11-21
Method of fabricating a composite material casing for a gas turbine engine, and a casing obtained thereby
Grant 9,784,122 - Beaujard , et al. October 10, 2
2017-10-10
Turbine engine blade or vane made of composite material, turbine nozzle or compressor stator incorporating such vanes and method of fabricating same
Grant 9,506,355 - Nunez , et al. November 29, 2
2016-11-29
Method Of Fabricating A Composite Material Casing For A Gas Turbine Engine, And A Casing Obtained Thereby
App 20150226084 - Beaujard; Antoine Jean-Philippe ;   et al.
2015-08-13
Composite material turbomachine engine blade or vane, compressor stator segment or turbine nozzle segment incorporating such vanes and method for manufacturing same
Grant 9,062,562 - Coupe , et al. June 23, 2
2015-06-23
Turbomachine blades or vanes having complementary even/odd geometry
Grant 9,045,992 - Roussille , et al. June 2, 2
2015-06-02
Turbomachine blade or vane having complementary asymmetrical geometry
Grant 9,033,673 - Roussille , et al. May 19, 2
2015-05-19
Assembly Formed By A Turbine Nozzle Or A Compressor Diffuser Made Of Cmc For A Turbine Engine And By An Abradable Material Support Ring, And A Turbine Or A Compressor Incorporating Such An Assembly
App 20140227088 - Beaujard; Antoine Jean-Philippe ;   et al.
2014-08-14
Turbine Engine Blade Or Vane Made Of Composite Material, Turbine Nozzle Or Compressor Stator Incorporating Such Vanes And Method Of Fabricating Same
App 20140030076 - NUNEZ; ROMAIN ;   et al.
2014-01-30
Turbomachine Blades Or Vanes Having Complementary Even/odd Geometry
App 20130243604 - Roussille; Clement ;   et al.
2013-09-19
Composite Material Turbomachine Engine Blade Or Vane, Compressor Stator Segment Or Turbine Nozzle Segment Incorporating Such Vanes And Method For Manufacturing Same
App 20130108422 - COUPE; DOMINIQUE ;   et al.
2013-05-02
Turbomachine Blade Or Vane Having Complementary Asymmetrical Geometry
App 20130101429 - Roussille; Clement ;   et al.
2013-04-25

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