Inventor · disambiguated record
Hazem Kioua
Also filed as: KIOUA HAZEM
11 granted patents·1 pending application·16 citations·filing 2013–2021
82Inventor score
Top patents by PatentIndex Score
12 records- 0186US12037941B2Supersonic speed attenuator of an air intake of an aircraft propulsion assembly comprising a de-icing device and de-icing methodSAFRAN NACELLES·Filed 2021·Granted Jul 16, 2024·2 cites·18 claims
- 0285US12214893B2Air inlet for an aircraft propulsion unit comprising a member for moving a movable upstream portion and method for using such an air inletSAFRAN NACELLES·Filed 2021·Granted Feb 4, 2025·3 cites·20 claims
- 0377US9382814B2Device for connecting a thrust reverser front frame to a fan casing and nacelle incorporating such a deviceAIRCELLE SA·Filed 2013·Granted Jul 5, 2016·8 cites·13 claims
- 0472US10087781B2Assembly centering device for turbojet engine nacelleAIRCELLE SA·Filed 2015·Granted Oct 2, 2018·3 cites·13 claims
- 0546US12246846B2Aircraft propulsion unit comprising a nacelle and a turbomachine independently supported by a wing, fuselage or tail elementSAFRAN NACELLES·Filed 2021·Granted Mar 11, 2025·0 cites·11 claims
- 0644US12037940B2Supersonic air inlet of an aircraft propelling assembly comprising a support arm de-icing device and de-icing methodSAFRAN NACELLES·Filed 2021·Granted Jul 16, 2024·0 cites·18 claims
- 0744US11572188B2Aircraft engine nacelle with asymmetric fan cowlsSAFRAN NACELLES·Filed 2021·Granted Feb 7, 2023·0 cites·18 claims
- 0842US12044168B2Air inlet of a turbomachine nacelle including a circulation conduit of a hot air flow between a movable upstream part and a fixed downstream partSAFRAN NACELLES·Filed 2021·Granted Jul 23, 2024·0 cites·12 claims
- 0942US9341083B2Turbojet engine nacelle with downstream sectionAIRCELLE SA·Filed 2014·Granted May 17, 2016·0 cites·9 claims
- 1040US12110120B2Propulsion unit for an aircraft and method for mounting sameSAFRAN NACELLES·Filed 2021·Granted Oct 8, 2024·0 cites·13 claims
- 1139US12442332B2Propulsion unit for an aircraft comprising a system for sealing between two air intake partsSAFRAN NACELLES·Filed 2021·Granted Oct 14, 2025·0 cites·17 claims
- 1231US2016053720A1Mechanical inhibiting device integrated into a defence line of a thrust reverserAIRCELLE SA·Filed 2015·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →