Damien Cellier

Person

Paris, FR

People

Patents Grantslast 30 patents

Information Patent Grant
Dimensioning of the skeleton angle of the trailing edge of the arms...
- Patent number 11,221,020
- Issue date Jan 11, 2022
- SAFRAN AIRCRAFT ENGINES
- Ghislain Maxime Romuald Madiot
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Grant
Stage of variable-pitch blades for a turbine engine, turbine engine...
- Patent number 10,753,371
- Issue date Aug 25, 2020
- SAFRAN AIRCRAFT ENGINES
- Pierre-Alain Francis Claude Sebrecht
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Turbomachine part with a non-axisymmetric surface
- Patent number 10,352,330
- Issue date Jul 16, 2019
- SAFRAN AIRCRAFT ENGINES
- Damien Joseph Cellier
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Grant
Angular stator sector for a turbomachine compressor comprising a br...
- Patent number 10,330,117
- Issue date Jun 25, 2019
- SAFRAN AIRCRAFT ENGINES
- Damien Joseph Cellier
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Grant
Turbomachine centre blade comprising a curved portion
- Patent number 10,309,419
- Issue date Jun 4, 2019
- SAFRAN AIRCARFT ENGINES
- Damien Cellier
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Turbine engine rotor blade
- Patent number 10,301,941
- Issue date May 28, 2019
- SAFRAN AIRCARFT ENGINES
- Damien Joseph Cellier
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Method for modeling a non-axisymmetric surface
- Patent number 10,216,867
- Issue date Feb 26, 2019
- SAFRAN AIRCRAFT ENGINES
- Damien Joseph Cellier
- G06 - COMPUTING CALCULATING COUNTING
Information Patent Grant
Blade and blade dihedral angle
- Patent number 10,138,897
- Issue date Nov 27, 2018
- SAFRAN AIRCRAFT ENGINES
- Damien Cellier
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Method for modelling a part, in particular a blading
- Patent number 10,002,209
- Issue date Jun 19, 2018
- SNECMA
- Damien Joseph Cellier
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Turbine engine blade, in particular for a one-piece bladed disk
- Patent number 9,556,740
- Issue date Jan 31, 2017
- SNECMA
- Vincent Paul Gabriel Perrot
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Airfoil and platform assembly for subsonic flow
- Patent number 9,464,526
- Issue date Oct 11, 2016
- SNECMA
- Damien Cellier
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Airfoil and platform assembly for supersonic flow
- Patent number 9,458,720
- Issue date Oct 4, 2016
- SNECMA
- Damien Cellier
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...

Patents Applicationslast 30 patents

Information Patent Application
DIMENSIONING OF THE SKELETON ANGLE OF THE TRAILING EDGE OF THE ARMS...
- Publication number 20180252230
- Publication date Sep 6, 2018
- SAFRAN AIRCRAFT ENGINES
- Ghislain Maxime Romuald MADIOT
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
TURBOMACHINE PART WITH A NON-AXISYMMETRIC SURFACE
- Publication number 20160245299
- Publication date Aug 25, 2016
- SNECMA
- Damien Joseph CELLIER
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Application
TURBINE ENGINE ROTOR BLADE
- Publication number 20160195104
- Publication date Jul 7, 2016
- SNECMA
- Damien Joseph CELLIER
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Application
Method for modeling a non-axisymmetric surface
- Publication number 20160154901
- Publication date Jun 2, 2016
- SNECMA
- Damien Joseph Cellier
- G06 - COMPUTING CALCULATING COUNTING
Information Patent Application
METHOD FOR MODELLING A PART, IN PARTICULAR A BLADING
- Publication number 20160063139
- Publication date Mar 3, 2016
- SNECMA
- Damien Joseph Cellier
- G06 - COMPUTING CALCULATING COUNTING
Information Patent Application
BLADE AND BLADE DIHEDRAL ANGLE
- Publication number 20160061218
- Publication date Mar 3, 2016
- SNECMA
- Damien Cellier
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Application
ANGULAR STATOR SECTOR FOR A TURBOMACHINE COMPRESSOR COMPRISING A BR...
- Publication number 20150071770
- Publication date Mar 12, 2015
- SNECMA
- Damien Joseph CELLIER
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Application
TURBINE ENGINE BLADE, IN PARTICULAR FOR A ONE-PIECE BLADED DISK
- Publication number 20140341749
- Publication date Nov 20, 2014
- SNECMA
- Vincent Paul Gabriel Perrot
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Application
TURBOMACHINE CENTRE BLADE COMPRISING A CURVED PORTION
- Publication number 20140248144
- Publication date Sep 4, 2014
- SNECMA
- Damien Cellier
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Application
AIRFOIL AND PLATFORM ASSEMBLY FOR SUPERSONIC FLOW
- Publication number 20130315738
- Publication date Nov 28, 2013
- SNECMA
- Damien Cellier
- G06 - COMPUTING CALCULATING COUNTING
Information Patent Application
AIRFOIL AND PLATFORM ASSEMBLY FOR SUBSONIC FLOW
- Publication number 20130315739
- Publication date Nov 28, 2013
- SNECMA
- Damien Cellier
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...

Damien Cellier

Person

Patents Grantslast 30 patents

Dimensioning of the skeleton angle of the trailing edge of the arms...

Stage of variable-pitch blades for a turbine engine, turbine engine...

Turbomachine part with a non-axisymmetric surface

Angular stator sector for a turbomachine compressor comprising a br...

Turbomachine centre blade comprising a curved portion

Turbine engine rotor blade

Method for modeling a non-axisymmetric surface

Blade and blade dihedral angle

Method for modelling a part, in particular a blading

Turbine engine blade, in particular for a one-piece bladed disk

Airfoil and platform assembly for subsonic flow

Airfoil and platform assembly for supersonic flow

Patents Applicationslast 30 patents

DIMENSIONING OF THE SKELETON ANGLE OF THE TRAILING EDGE OF THE ARMS...

TURBOMACHINE PART WITH A NON-AXISYMMETRIC SURFACE

TURBINE ENGINE ROTOR BLADE

Method for modeling a non-axisymmetric surface

METHOD FOR MODELLING A PART, IN PARTICULAR A BLADING

BLADE AND BLADE DIHEDRAL ANGLE

ANGULAR STATOR SECTOR FOR A TURBOMACHINE COMPRESSOR COMPRISING A BR...

TURBINE ENGINE BLADE, IN PARTICULAR FOR A ONE-PIECE BLADED DISK

TURBOMACHINE CENTRE BLADE COMPRISING A CURVED PORTION

AIRFOIL AND PLATFORM ASSEMBLY FOR SUPERSONIC FLOW

AIRFOIL AND PLATFORM ASSEMBLY FOR SUBSONIC FLOW