Damien Merlot

Person

Moissy Cramayel, FR

People

Patents Grantslast 30 patents

Information Patent Grant
Airplane turbojet fan blade of cambered profile in its root sections
- Patent number 11,333,164
- Issue date May 17, 2022
- SAFRAN AIRCRAFT ENGINES
- Hanna Reiss
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Fan for a turbomachine
- Patent number 11,209,012
- Issue date Dec 28, 2021
- SAFRAN AIRCRAFT ENGINES
- Laurent Jablonski
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Blade with a platform and a hollow bumper
- Patent number 10,634,158
- Issue date Apr 28, 2020
- SAFRAN AIRCRAFT ENGINES
- Philippe Gérard Edmond Joly
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Grant
Blisk comprising a hub having a recessed face on which a filling me...
- Patent number 10,619,495
- Issue date Apr 14, 2020
- SAFRAN AIRCRAFT ENGINES
- Philippe Gérard Edmond Joly
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Fan for a turbomachine
- Patent number 10,502,227
- Issue date Dec 10, 2019
- SAFRAN AIRCRAFT ENGINES
- Laurent Jablonski
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Blade comprising a shank, provided with a depressed portion
- Patent number 10,458,257
- Issue date Oct 29, 2019
- SAFRAN AIRCRAFT ENGINES
- Marco Nucci
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Single-piece blisk for turbomachine fan comprising an upstream and/...
- Patent number 9,863,252
- Issue date Jan 9, 2018
- SNECMA
- Damien Merlot
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Blisk with low stresses at blade root, preferably for an aircraft t...
- Patent number 9,765,637
- Issue date Sep 19, 2017
- SNECMA
- Damien Merlot
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Turbine engine cowl capable of covering a fan cone
- Patent number 9,541,002
- Issue date Jan 10, 2017
- SNECMA
- Damien Merlot
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...

Patents Applicationslast 30 patents

Information Patent Application
FAN FOR A TURBOMACHINE
- Publication number 20190249683
- Publication date Aug 15, 2019
- SAFRAN AIRCRAFT ENGINES
- Laurent Jablonski
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
BLADE COMPRISING A SHANK, PROVIDED WITH A DEPRESSED PORTION
- Publication number 20180156047
- Publication date Jun 7, 2018
- SNECMA
- Marco NUCCI
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
BLISK COMPRISING A HUB HAVING A RECESSED FACE ON WHICH A FILLING ME...
- Publication number 20180087389
- Publication date Mar 29, 2018
- SAFRAN AIRCRAFT ENGINES
- Philippe Gérard Edmond Joly
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
BLADE WITH A PLATFORM AND A HOLLOW BUMPER
- Publication number 20170276145
- Publication date Sep 28, 2017
- SAFRAN AIRCRAFT ENGINES
- Philippe Gérard Edmond Joly
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Application
FAN FOR A TURBOMACHINE
- Publication number 20170167504
- Publication date Jun 15, 2017
- SNECMA
- Laurent Jablonski
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Application
SINGLE-PIECE BLISK FOR TURBOMACHINE FAN COMPRISING AN UPSTREAM AND/...
- Publication number 20160138403
- Publication date May 19, 2016
- SNECMA
- Damien Merlot
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
TURBINE ENGINE COWL CAPABLE OF COVERING A FAN CONE
- Publication number 20150267614
- Publication date Sep 24, 2015
- SNECMA
- Damien Merlot
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
BLISK WITH LOW STRESSES AT BLADE ROOT, PREFERABLY FOR AN AIRCRAFT T...
- Publication number 20150267545
- Publication date Sep 24, 2015
- SNECMA
- Damien MERLOT
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
BLADE COMPRISING A SUPPORT, PROVIDED WITH A PORTION WITH A DEPRESSION
- Publication number 20150176415
- Publication date Jun 25, 2015
- SNECMA
- Marco NUCCI
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
AIRPLANE TURBOJET FAN BLADE OF CAMBERED PROFILE IN ITS ROOT SECTIONS
- Publication number 20150152880
- Publication date Jun 4, 2015
- SNECMA
- Hanna Reiss
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...

Damien Merlot

Person

Patents Grantslast 30 patents

Airplane turbojet fan blade of cambered profile in its root sections

Fan for a turbomachine

Blade with a platform and a hollow bumper

Blisk comprising a hub having a recessed face on which a filling me...

Fan for a turbomachine

Blade comprising a shank, provided with a depressed portion

Single-piece blisk for turbomachine fan comprising an upstream and/...

Blisk with low stresses at blade root, preferably for an aircraft t...

Turbine engine cowl capable of covering a fan cone

Patents Applicationslast 30 patents

FAN FOR A TURBOMACHINE

BLADE COMPRISING A SHANK, PROVIDED WITH A DEPRESSED PORTION

BLISK COMPRISING A HUB HAVING A RECESSED FACE ON WHICH A FILLING ME...

BLADE WITH A PLATFORM AND A HOLLOW BUMPER

FAN FOR A TURBOMACHINE

SINGLE-PIECE BLISK FOR TURBOMACHINE FAN COMPRISING AN UPSTREAM AND/...

TURBINE ENGINE COWL CAPABLE OF COVERING A FAN CONE

BLISK WITH LOW STRESSES AT BLADE ROOT, PREFERABLY FOR AN AIRCRAFT T...

BLADE COMPRISING A SUPPORT, PROVIDED WITH A PORTION WITH A DEPRESSION

AIRPLANE TURBOJET FAN BLADE OF CAMBERED PROFILE IN ITS ROOT SECTIONS