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SAFRAN NACELLES

Overview
  • Total Patents
    585
  • GoodIP Patent Rank
    2,750
  • Filing trend
    ⇧ 47.0%
About

SAFRAN NACELLES has a total of 585 patent applications. It increased the IP activity by 47.0%. Its first patent ever was published in 2008. It filed its patents most often in France, EPO (European Patent Office) and WIPO (World Intellectual Property Organization). Its main competitors in its focus markets engines, pumps and turbines, transport and environmental technology are ROHR INC, AIRCELLE SA and TODOROVIC PREDRAG.

Patent filings per year

Chart showing SAFRAN NACELLESs patent filings per year from 1900 to 2020

Top inventors

# Name Total Patents
#1 Boileau Patrick 89
#2 Desjoyeaux Bertrand 79
#3 Gonidec Patrick 57
#4 Caruel Pierre 57
#5 Kerbler Olivier 45
#6 Versaevel Marc 43
#7 Maalioune Hakim 37
#8 Delehouze Arnaud 30
#9 Peyron Vincent 30
#10 Provost Benjamin 29

Latest patents

Publication Filing date Title
WO2020115424A1 Thrust reverser provided with a lightweight thrust reverser flap
WO2020114988A1 Air intake and method for de-icing an air intake of a nacelle of an aircraft jet engine
FR3102511A1 Flap thrust reverser controlled by a mechanism fitted with aeronautical horns
WO2020084245A1 Upper axial retention for a cascade-type thrust reverser with sliding vanes of d-shaped structure
FR3102080A1 Repair process for an air inlet lip
FR3101853A1 OFFSET PLANE FLUSHING THE WAKE OF THE WING
FR3101808A1 Repair by suture of a sandwich panel
FR3101723A1 Acoustic attenuation panel for low frequency waves
FR3101569A1 Automatic lay-up and compaction machine
FR3100745A1 Repair process for thermal protection of a nacelle structure
FR3100845A1 External nozzle member for turbomachine
FR3100918A1 ACOUSTIC PANEL FOR AN AIRCRAFT PROPELLER ASSEMBLY, AND ITS MANUFACTURING PROCESS
FR3100796A1 Turbojet engine nacelle air inlet, containing in its volume a multilayer weave fabric
FR3100466A1 Method of brazing a powertrain panel using different input alloys
FR3100570A1 Structural and / or acoustic panel comprising a U-shaped closing flange oriented towards the interior of the panel, and method of manufacturing such a panel
FR3100475A1 Method and machine for cutting draping elements
FR3100576A1 Thrust reverser comprising primary locks offset with respect to a plane of symmetry of the movable cowl
FR3100578A1 Thrust reverser with cable kinematics for scooping shutters
FR3100577A1 Thrust reverser comprising a single movable cowl control cylinder
FR3099912A1 Air inlet of a nacelle of an aircraft turbomachine