Inventor · disambiguated record
Gilles Pierre-Marie Notarianni
Also filed as: NOTARIANNI GILLES PIERRE-MARIE
12 granted patents·1 pending application·34 citations·filing 2016–2021
85Inventor score
Top patents by PatentIndex Score
13 records- 0195US10844725B2Leading edge shieldSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Nov 24, 2020·22 cites·8 claims
- 0285US11040465B2Preform and one-piece vane for turbomachineSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Jun 22, 2021·3 cites·13 claims
- 0383US11371357B2Fabric comprising aramid fibres for protecting a blade against impactsSAFRAN AIRCRAFT ENGINES·Filed 2019·Granted Jun 28, 2022·3 cites·13 claims
- 0476US11105210B2Blade comprising a leading edge shield and method for producing the bladeSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Aug 31, 2021·2 cites·19 claims
- 0575US11773733B2Fibrous texture for turbine engine blade made of composite materialSAFRAN AIRCRAFT ENGINES·Filed 2021·Granted Oct 3, 2023·1 cites·12 claims
- 0674US10240463B2Blade made of organic matrix composite material provided with a metal strip, and a method of fastening a metal strip on a blade fiber preformSNECMA·Filed 2016·Granted Mar 26, 2019·1 cites·11 claims
- 0762US10883374B2Blade comprising a folded leading edge shield and method of manufacturing the bladeSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Jan 5, 2021·1 cites·11 claims
- 0860US10533574B2Composite blade, comprising a leading-edge reinforcement made of another materialSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Jan 14, 2020·1 cites·10 claims
- 0958US11795825B2Inter-blade platform with a sacrificial box sectionSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Oct 24, 2023·0 cites·20 claims
- 1053US10689996B2Turbomachine blade fitted with an elastomer gasketSAFRAN AIRCRAFT ENGINES·Filed 2017·Granted Jun 23, 2020·0 cites·8 claims
- 1149US11377973B2Sealing arrangement between two ring-shaped walls of an aircraft engineSAFRAN AIRCRAFT ENGINES·Filed 2019·Granted Jul 5, 2022·0 cites·9 claims
- 1249US2021372428A1Hybridization of the fibres of the fibrous reinforcement of a bladeSAFRAN AIRCRAFT ENGINES·Filed 2019·Application pending·0 cites
- 1345US10570757B2Rotary assembly of a turbomachine equipped with an axial retention system of a bladeSAFRAN AIRCRAFT ENGINES·Filed 2017·Granted Feb 25, 2020·0 cites·9 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →