Inventor · disambiguated record
Frédéric Paul Eichstadt
Also filed as: EICHSTADT FREDERIC · EICHSTADT FREDERIC P · EICHSTADT FREDERIC PAUL · EICHSTADT FRÉDÉRIC PAUL
11 granted patents·1 pending application·68 citations·filing 1993–2021
86Inventor score
Top patents by PatentIndex Score
12 records- 0186US11035294B2Turbomachine with double flow and its lubricant reservoirSAFRAN AIRCRAFT ENGINES·Filed 2018·Granted Jun 15, 2021·5 cites·9 claims
- 0282US7347672B2Rotor disk balancing device, disk fitted with such a device and rotor with such a diskSNECMA MOTEURS·Filed 2005·Granted Mar 25, 2008·23 cites·32 claims
- 0376US7290988B2Device for blocking a ring for axially retaining a blade, associated rotor disk and retaining ring, and rotor and aircraft engine comprising themSNECMA·Filed 2006·Granted Nov 6, 2007·16 cites·19 claims
- 0469US10562638B2Cradle for a turbopropeller engine with integrated air inlet ductSAFRAN AIRCRAFT ENGINES·Filed 2017·Granted Feb 18, 2020·2 cites·10 claims
- 0547US11572833B2Aircraft engine assembly with a supply path to an inter-flow compartment tank of turbine engineSAFRAN AIRCRAFT ENGINES·Filed 2019·Granted Feb 7, 2023·0 cites·10 claims
- 0645US12018628B2Turbojet engine rear part comprising a nozzle having flaps comprising levers that are movable by means of upstream and downstream bearing wallsSAFRAN AIRCRAFT ENGINES·Filed 2021·Granted Jun 25, 2024·0 cites·8 claims
- 0742US5795128AControl device for a pivot integrated in a manifoldSNECMA·Filed 1997·Granted Aug 18, 1998·19 cites·6 claims
- 0840US10077113B2Engine cowl incorporating an equipment ventilation circuitSAFRAN AIRCRAFT ENGINES·Filed 2014·Granted Sep 18, 2018·0 cites·7 claims
- 0939US8037687B2Bypass turbomachine with reduction of jet noiseSNECMA·Filed 2008·Granted Oct 18, 2011·0 cites·5 claims
- 1034US2018134402A1Bipartite cradle with slide for turbomachineHELLEGOUARCH ANTOINE ELIE·Filed 2017·Application pending·0 cites
- 1133US11713730B2Convergent-divergent flap pair for a variable-geometry turbojet engine nozzle comprising cooling air circulation ducts connected through contact surfacesSAFRAN AIRCRAFT ENGINES·Filed 2020·Granted Aug 1, 2023·0 cites·9 claims
- 1231US5269138AVariable geometry flame trap device for use in an after-burner device of a gas turbineSNECMA·Filed 1993·Granted Dec 14, 1993·3 cites·7 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →