Inventor
CAROLINE MARIE FRANTZ
Inventor
FR
Overview
Patents· 27 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 plants20%
F01DNon-positive displacement machines or engines, e.g. steam turbines17%
F02CGas-turbine plants14%
Y02TClimate change mitigation technologies related to transportation12%
F02KJet-propulsion plants10%
F04DNon-positive-displacement pumps8%
B64CAeroplanes7%
B64DEquipment for fitting in or to aircraft3%
H02KDynamo-electric machines2%
F16HGearing2%
PatentTitleYear
12,480,427Turbomachine module equipped with variable pitch vanes and an annular interface shroud202512,460,550Fan module equipped with an oil transfer device202512,365,444Module for an aircraft turbine engine202512,365,445Hydraulic assembly for an aircraft engine202512,330,769Electrohydraulic pitch setting with reversible pump202512,313,081Module for mounting a turbomachine fan blade202512,281,581Module for an aircraft turbine engine202512,110,845Aeronautic propulsion system with improved propulsion efficiency202412,104,504Device for setting the pitch of blades for a turbine engine, and turbine engine comprising same202412,092,029Fan module equipped with an oil transfer device202412,078,126Aeronautic propulsion system with improved propulsion efficiency202412,060,807Aircraft turbine engine equipped with an electrical machine202411,913,385Aeronautical propulsion system with improved propulsive efficiency202411,891,967Turbofan comprising a power supply device to drive the compressor202411,802,515Aeronautic propulsion system with low leakage rate and improved propulsion efficiency202311,725,592Aeronautical propulsion system having a low leakage flow rate and improved propulsion efficiency202311,692,512Fan module equipped with an electrical machine for an aircraft turbine engine202311,692,453Aircraft turbine engine equipped with an electrical machine202311,649,765Method for operating an air intake of a turbojet engine nacelle during a thrust phase and during a reverse thrust phase202311,643,944Turbine shaft of a turbomachine and method for protecting against overspeed of said shaft202311,643,941Aircraft turbine engine provided with an electrical machine202311,591,987Turbomachine with electric machine comprising a rotor ring attached to the fan202311,572,889Blade pivot of adjustable orientation and of reduced bulk for a turbomachine fan hub202311,560,809Electric module for an aircraft fan comprising blades with improved attachment202311,512,615Device for supplying an oil tank from a second tank202211,466,697Fan module comprising variable-pitch blades202211,293,300Aircraft turbine engine with at least two bodies and means for drawing power2022Career & activity timeline
Assembled from patent assignee/location history and declaration credentials.
2022–2025Patents assigned to SAFRAN AIRCRAFT ENGINES (27)· patent assignee history
2022–2025Based in FR· patent location history
2023–2024Patents assigned to SAFRAN TRANS SYSTEMS (5)· patent assignee history
2025Patents assigned to SAFRAN LANDING SYSTEMS (1)· patent assignee history
Inventor activity
Assignee and location history derived from the patent record.
Assignees
| Assignee | Patents | Span |
|---|---|---|
| SAFRAN AIRCRAFT ENGINES | 27 | 2022–2025 |
| SAFRAN TRANS SYSTEMS | 5 | 2023–2024 |
| SAFRAN LANDING SYSTEMS | 1 | 2025 |
Locations
| Location | Patents | Span |
|---|---|---|
| FR | 27 | 2022–2025 |