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ZODIAC AERO ELECTRIC

Overview
  • Total Patents
    236
  • GoodIP Patent Rank
    6,413
  • Filing trend
    ⇩ 15.0%
About

ZODIAC AERO ELECTRIC has a total of 236 patent applications. It decreased the IP activity by 15.0%. Its first patent ever was published in 2011. It filed its patents most often in France, United States and China. Its main competitors in its focus markets electrical machinery and energy, transport and computer technology are GE AVIAT SYSTEMS LTD, ASTRONICS ADVANCED ELECTRONIC SYSTEMS CORP and AMERICAN POWER CONV CORP.

Patent filings per year

Chart showing ZODIAC AERO ELECTRICs patent filings per year from 1900 to 2020

Top inventors

# Name Total Patents
#1 Tsao Christian 34
#2 Pradier Jean-Clair 31
#3 Deshayes Olivier 30
#4 Balbinot Jean-Pierre 16
#5 Andreoletti Remi 13
#6 Giron Julien 13
#7 De Truchis Maxime 12
#8 De Bossoreille Romain 12
#9 Bonnefous Edouard 12
#10 Doule Claude 12

Latest patents

Publication Filing date Title
FR3100663A1 Reinforcement element for battery cell assembly intended for an aircraft
FR3100391A1 Electrical assembly comprising a concealed electrical component providing the electrical connection between a conductive element and a communication card
FR3100374A1 Coil comprising a set of asymmetric conductive turns
FR3099262A1 Graphic data processing system
US2020028361A1 Power switching device for an electrical power distribution system, in particular for an aircraft, with metering of the consumed electrical power
FR3098619A1 Retractable touchscreen interface
FR3098005A1 Device for protecting a load in a power electronic circuit
FR3098034A1 MODULAR WIRING SUPPORT
US2019393774A1 Device for transforming and for rectifying polyphase voltage
FR3097084A1 Removable switching assembly for electrical power distribution connection
FR3096804A1 Semi-spherical touch interface
FR3095895A1 Battery box
FR3086079A1 MULTI-KEY TOUCH DEVICE WITH CAPACITIVE DETECTION
FR3084169A1 METHOD FOR DETERMINING THE OPERATING STATE OF A BATTERY AND BATTERY IMPLEMENTING SUCH A METHOD
FR3084211A1 POWER ELECTRICAL CONNECTION KIT FOR THE CONNECTION OF ELECTRIC CABLES TO AN AIRCRAFT ELECTRIC CORE AND CORRESPONDING POWER ELECTRICAL SYSTEM
FR3084171A1 Method and device for determining a time limit for use of a battery
FR3084170A1 Method for determining a covariance state noise matrix for setting a battery charge observer and device thereof
FR3083374A1 Holding piece, housing and related method
FR3083007A1 Cooling and heating device for battery and battery incorporating such a device
CN108872738A For detecting the device and method of electrical load