Inventor · disambiguated record
Tewfik Boudebiza
Also filed as: BOUDEBIZA TEWFIK
18 granted patents·1 pending application·37 citations·filing 2014–2022
89Inventor score
Top patents by PatentIndex Score
19 records- 0195US10557415B2Turbo-engine including two separate ventilation flowsSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Feb 11, 2020·18 cites·12 claims
- 0285US10584641B2Turbine engine with a pair of contrarotating propellers placed upstream of the gas generatorSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Mar 10, 2020·8 cites·14 claims
- 0382US10174634B2Device and method for lubricating a turbomachine rolling bearingSAFRAN AIRCRAFT ENGINES·Filed 2015·Granted Jan 8, 2019·4 cites·12 claims
- 0477US10850859B2Aircraft with a propulsion unit with offset fanSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Dec 1, 2020·3 cites·13 claims
- 0569US10006539B2Epicyclic reduction gear with fluid transfer pipes, and propeller turbomachine for an aircraft with such a reduction gearSNECMA·Filed 2014·Granted Jun 26, 2018·2 cites·11 claims
- 0668US11225317B2Radial shaft device for controlling the pitch of fan blades of a turbine engine having an un-ducted fanSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Jan 18, 2022·2 cites·7 claims
- 0758US11692512B2Fan module equipped with an electrical machine for an aircraft turbine engineSAFRAN AIRCRAFT ENGINES·Filed 2019·Granted Jul 4, 2023·0 cites·13 claims
- 0857US12305579B2Aircraft turbomachine comprising an electric machineSAFRAN AIRCRAFT ENGINES·Filed 2022·Granted May 20, 2025·0 cites·7 claims
- 0950US11371432B2Aircraft engine intake arrangement comprising a mechanical decouplerSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Jun 28, 2022·0 cites·13 claims
- 1049US10495005B2Epicyclic reduction device for the rotational drive of blade sets of a reduction turbomachineSAFRAN AIRCRAFT ENGINES·Filed 2014·Granted Dec 3, 2019·0 cites·10 claims
- 1147US11015521B2Aircraft propulsion assembly equipped with a main fan and with at least one offset fanSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted May 25, 2021·0 cites·12 claims
- 1246US11174781B2Aircraft propulsion assembly equipped with a main fan and with a least one offset fanSAFRAN AIRCRAFT ENGINES·Filed 2016·Granted Nov 16, 2021·0 cites·15 claims
- 1345US2020240641A1Turbomachine, such as an aircraft turbojet engineSAFRAN AIRCRAFT ENGINES·Filed 2020·Application pending·0 cites
- 1444US11499439B2Double flow turbojet including an intermediate flow path dedicated to supplying with air via radial arms an exhaust casing of this turbojetSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Nov 15, 2022·0 cites·6 claims
- 1543US11772778B2System for controlling the cyclic setting of bladesSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Oct 3, 2023·0 cites·9 claims
- 1643US11187107B2Turbojet with bearing architecture optimised for the support of a low pressure shaftSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Nov 30, 2021·0 cites·18 claims
- 1742US9903230B2Device for securing and retaining at least one electrical harness in a turbomachineSNECMA·Filed 2014·Granted Feb 27, 2018·0 cites·9 claims
- 1840US10077113B2Engine cowl incorporating an equipment ventilation circuitSAFRAN AIRCRAFT ENGINES·Filed 2014·Granted Sep 18, 2018·0 cites·7 claims
- 1937US9926070B2Turbine engine having a pair of propellers for an aircraftSNECMA·Filed 2015·Granted Mar 27, 2018·0 cites·10 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →