Inventor · disambiguated record
Bruno Alexandre Didier Jacon
Also filed as: JACON BRUNO ALEXANDRE DIDIER
10 granted patents·4 citations·filing 2018–2022
78Inventor score
Files withSAFRAN AIRCRAFT ENGINES10
Top patents by PatentIndex Score
10 records- 0173US11746706B2Air-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
- 0265US10598037B2Air-fire seal and assembly comprising such a sealSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Mar 24, 2020·1 cites·17 claims
- 0360US11851200B2Fire 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
- 0454US11098607B2Air-fire seal and assembly comprising such a sealSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Aug 24, 2021·0 cites·14 claims
- 0553US11649769B2Airtight seal for bleed valve door of a turbomachineSAFRAN AIRCRAFT ENGINES·Filed 2019·Granted May 16, 2023·0 cites·12 claims
- 0651US12319401B2Sealing arrangement for a rolling bearing subjected to centrifugal forcesSAFRAN AIRCRAFT ENGINES·Filed 2022·Granted Jun 3, 2025·0 cites·15 claims
- 0749US11920519B2Fire resistance device designed to be placed between one end of a mounting strut for an aircraft turbomachine and a cowling of the turbomachine delimiting an inter-flow compartmentSAFRAN AIRCRAFT ENGINES·Filed 2019·Granted Mar 5, 2024·0 cites·13 claims
- 0848US11629611B2Seal for an intermediate turbomachine casingSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Apr 18, 2023·0 cites·13 claims
- 0937US11480107B2Fire 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
- 1032US11585292B2Outer 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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