Inventor
Norman Bruno Andre Jodet
Inventor
Moissy-Cramayel, FR
Overview
Patents· 17 as inventor
Public. Assignee & technology derived from the patent record. Each patent links to its LexDana page.
F05Dprimary
F05DIndexing scheme for aspects relating to non-positive-displacement machines or engines, gas-turbines or jet-propulsion plants17%
Y02TClimate change mitigation technologies related to transportation15%
B64DEquipment for fitting in or to aircraft14%
F02CGas-turbine plants13%
F01DNon-positive displacement machines or engines, e.g. steam turbines11%
F02KJet-propulsion plants10%
B64CAeroplanes8%
F04DNon-positive-displacement pumps6%
G10KSound-producing devices3%
B26DCutting1%
PatentTitleYear
11,047,303Supply duct of a compressor of a turbine engine202111,000,964Device for perforating an acoustic annular panel for a turbine engine202110,995,702Heating system for convergent-divergent secondary nozzle202110,967,980Turbine engine propelled airplane having an acoustic baffle202110,894,594Aircraft including a wing with improved acoustic treatment202110,787,962Active system generating destructive acoustic interference for an aircraft engine with multiple fan spools202010,723,434Aircraft propulsion unit comprising an unducted-fan turbine engine and an attachment pylon202010,662,876Turbomachine vane comprising an electroacoustic source with improved assembly mode, row of outlet guide vanes and turbomachine comprising such a vane202010,557,417Acoustic absorber cell for a turbojet, and an associated acoustic treatment panel202010,518,869Turboprop201910,370,086Blade for a turbine engine propeller, in particular a propfan engine, propeller, and turbine engine comprising such a blade201910,358,938Undulating stator for reducing the noise produced by interaction with a rotor201910,024,176Rotor blade with reduced acoustic response20189,938,901Attachment pylon for a turbine engine20189,932,897Removable acoustic panels for turbojet engine casing20189,435,214'Turbomachine propeller blade setting device'20168,881,502'Mixer that performs reciprocating rotary motion for a confluent-flow nozzle of a turbine engine, and a method of controlling it'2014Career & activity timeline
Assembled from patent assignee/location history and declaration credentials.
2014–2019Patents assigned to SNECMA (7)· patent assignee history
2014–2018Based in Savigny sur Orge, FR· patent location history
2019–2021Patents assigned to SAFRAN AIRCRAFT ENGINES (12)· patent assignee history
2019–2021Based in Moissy-Cramayel, FR· patent location history
2019–2021Based in Maisons-Alfort, FR· patent location history
2021Based in Mason Alfort, FR· patent location history
Inventor activity
Assignee and location history derived from the patent record.
Assignees
| Assignee | Patents | Span |
|---|---|---|
| SAFRAN AIRCRAFT ENGINES | 12 | 2019–2021 |
| SNECMA | 7 | 2014–2019 |
Locations
| Location | Patents | Span |
|---|---|---|
| Moissy-Cramayel, FR | 6 | 2019–2021 |
| Maisons-Alfort, FR | 5 | 2019–2021 |
| Savigny sur Orge, FR | 5 | 2014–2018 |
| Mason Alfort, FR | 1 | 2021 |