Inventor · disambiguated record
Laurent Cazeaux
Also filed as: CAZEAUX LAURENT
14 granted patents·9 pending applications·5 citations·filing 2014–2024
83Inventor score
Top patents by PatentIndex Score
23 records- 0192US12053915B2Method for manufacturing a door of a thrust reversal systemAIRBUS OPERATIONS SAS·Filed 2022·Granted Aug 6, 2024·1 cites·13 claims
- 0277US11187190B2Turbofan comprising a cam actuating a set of rotatable blades for blocking off the bypass flow ductAIRBUS OPERATIONS SAS·Filed 2020·Granted Nov 30, 2021·2 cites·6 claims
- 0374US11187189B2Aircraft propulsion system comprising a mobile articulated cowlAIRBUS OPERATIONS SAS·Filed 2019·Granted Nov 30, 2021·2 cites·11 claims
- 0461US2025108551A1Method for manufacturing an intermediate resistive membrane of an acoustic coatingAIRBUS OPERATIONS SAS·Filed 2024·Application pending·0 cites
- 0559US2024253802A1Alveolar structure of an acoustic damping panel comprising at least one partition configured for vibrating at a desired frequency, method for producing said alveolar structureAIRBUS SAS·Filed 2024·Application pending·0 cites
- 0659US2024253803A1Alveolar structure of an acoustic damping panel comprising at least one attached element configured for vibrating at a desired frequency, method for producing said alveolar structureAIRBUS SAS·Filed 2024·Application pending·0 cites
- 0759US2025108544A1Method for manufacturing an intermediate resistive membrane of an acoustic linerAIRBUS OPERATIONS SAS·Filed 2024·Application pending·0 cites
- 0858US12397921B2Internal fixed structure for an aircraft nacelleAIRBUS OPERATIONS SAS·Filed 2024·Granted Aug 26, 2025·0 cites·10 claims
- 0956US11746705B2Method for manufacturing an acoustic element of a sound absorption structure from at least one sheet of materialAIRBUS OPERATIONS SAS·Filed 2019·Granted Sep 5, 2023·0 cites·21 claims
- 1054US11486335B2Turbofan engine comprising a set of rotatable blades for blocking off the bypass flow ductAIRBUS OPERATIONS SAS·Filed 2021·Granted Nov 1, 2022·0 cites·7 claims
- 1153US11773806B2Assembly for an aircraft propulsion system comprising a hinged structure supporting the fan cowl and the thrust reverserAIRBUS OPERATIONS SAS·Filed 2022·Granted Oct 3, 2023·0 cites·9 claims
- 1251US12486698B2Locking mechanism for at least one movable element situated in a first zone and comprising a component that can be adjusted from a second zone, and aircraft comprising at least one such locking mechanismAIRBUS OPERATIONS SAS·Filed 2023·Granted Dec 2, 2025·0 cites·8 claims
- 1351US11511875B2Acoustic absorption structure comprising at least one rotationally-indexed acoustic element and aircraft propulsion assembly comprising said acoustic absorption structureAIRBUS OPERATIONS SAS·Filed 2019·Granted Nov 29, 2022·0 cites·12 claims
- 1451US10900517B2Dry friction slide with inclined contact surfacesAIRBUS OPERATIONS SAS·Filed 2019·Granted Jan 26, 2021·0 cites·19 claims
- 1550US11473528B2Aircraft turbofan having a cowl articulated in rotation and a system for deploying said cowlAIRBUS OPERATIONS SAS·Filed 2021·Granted Oct 18, 2022·0 cites·8 claims
- 1649US2025188851A1Propulsion assembly for an aircraft comprising a fluid-cooling circuit with quick-fit nacelle/engine couplings and aircraft provided with such an assemblyAIRBUS OPERATIONS SAS·Filed 2024·Application pending·0 cites
- 1747US11499504B2Propulsion assembly for an aircraft, having a maneuverable thrust reverserAIRBUS OPERATIONS SAS·Filed 2020·Granted Nov 15, 2022·0 cites·7 claims
- 1843US11572189B2Acoustic absorption structure comprising a liquid drainage system and propulsive assembly comprising such an acoustic absorption structureAIRBUS OPERATIONS SAS·Filed 2019·Granted Feb 7, 2023·0 cites·13 claims
- 1942US2021049993A1Double-enclosure acoustic element of small size, in particular for an aircraft acoustic panelAIRBUS OPERATIONS SAS·Filed 2020·Application pending·0 cites
- 2041US2020072161A1Low-frequency-sound-absorbing structure for a primary nozzle of a turbomachine of an aircraftAIRBUS OPERATIONS SAS·Filed 2019·Application pending·0 cites
- 2133US2020256282A1Turbojet comprising a thrust reverser drive mechanismAIRBUS OPERATIONS SAS·Filed 2020·Application pending·0 cites
- 2232US11193450B2Nacelle of a turbojet comprising a blocking door and a system for deployment of the blocking doorAIRBUS OPERATIONS SAS·Filed 2020·Granted Dec 7, 2021·0 cites·9 claims
- 2332US2015367947A1Aircraft propulsion assembly comprising at least one brush seal resistant to high-temperatureAIRBUS OPERATIONS SAS·Filed 2014·Application pending·0 cites
Join the waitlist — get patent alerts
Get an alert when Laurent Cazeaux files or is granted a new patent.
We store only your email — no account needed. See our privacy policy.
Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →