Inventor · disambiguated record
Baghdad Achbari
Also filed as: ACHBARI BAGHDAD
8 granted patents·13 citations·filing 2013–2022
78Inventor score
Top patents by PatentIndex Score
8 records- 0179US9399952B2Method for assembling a nozzle and an exhaust case of a turbomachineSNECMA·Filed 2013·Granted Jul 26, 2016·7 cites·9 claims
- 0273US11746706B2Air-sealing device intended to be inserted between an aircraft dual-flow turbine engine casing element, and a nacelle elementSAFRAN AIRCRAFT ENGINES·Filed 2019·Granted Sep 5, 2023·2 cites·12 claims
- 0364US9897011B2Gas turbine engine comprising an exhaust cone attached to the exhaust casingSNECMA·Filed 2013·Granted Feb 20, 2018·3 cites·8 claims
- 0460US11851200B2Fire resistance device designed to be placed between one end of a mounting strut for an aircraft turbomachine and a cowling of said turbomachine delimiting an inter-flow compartmentSAFRAN AIRCRAFT ENGINES·Filed 2019·Granted Dec 26, 2023·1 cites·10 claims
- 0552US12104498B2Inlet cone for an aircraft turbomachineSAFRAN AIRCRAFT ENGINES·Filed 2022·Granted Oct 1, 2024·0 cites·14 claims
- 0643US9732885B2Cooling device for the casing of an aircraft jet engine comprising a supporting deviceSNECMA·Filed 2014·Granted Aug 15, 2017·0 cites·16 claims
- 0737US11480107B2Fire resistance device intended to be interposed between an upstream end of an aircraft turbine engine mounting structure and a cowling of the turbine engine delimiting an inter-flow compartmentSAFRAN AIRCRAFT ENGINES·Filed 2019·Granted Oct 25, 2022·0 cites·18 claims
- 0832US11585292B2Outer shroud of an intermediate casing for a dual flow turbine engine for an aircraft, comprising improved air-sealing and fire-resistance devicesSAFRAN AIRCRAFT ENGINES·Filed 2019·Granted Feb 21, 2023·0 cites·11 claims
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