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Airbus Operations (S.A.S.) Patent Application Trends in 2024

From WikiPatents

Airbus Operations (S.A.S.) Patent Filing Activity

Airbus Operations (S.A.S.) patent applications in 2024

Top 10 Technology Areas

B64F5/10 (No explanation available)
- Count: 5 patents
- Example: 20240109672. METHOD FOR ASSEMBLING A FUSELAGE PORTION USING WELDING, WITH IMPROVED FLEXIBILITY, AND FUSELAGE PORTION AND AIRCRAFT THUS OBTAINED simplified abstract (AIRBUS OPERATIONS (S.A.S.))
B64D2221/00 (No explanation available)
- Count: 2 patents
- Example: 20240083593. METHOD FOR ANALYZING AN AIRCRAFT ELECTRICAL STRUCTURE BY SEARCHING FOR EQUIPOTENTIALS IN EMBEDDED GRAPHS simplified abstract (AIRBUS OPERATIONS (S.A.S.))
B64C1/068 (No explanation available)
- Count: 2 patents
- Example: 20240025561. SYSTEM FOR HANDLING A SIDE SHELL OF AN AIRCRAFT WITH A VIEW TO ASSEMBLING A FUSELAGE BARREL OF THE AIRCRAFT AND METHOD FOR ASSEMBLING A FUSELAGE BARREL OF AN AIRCRAFT simplified abstract (AIRBUS OPERATIONS (S.A.S.))
B64D29/06 (No explanation available)
- Count: 1 patents
- Example: 20240124148. AIRCRAFT ENGINE NACELLE PROVIDED WITH A THRUST REVERSER HAVING A MOBILE EJECTION STRUCTURE simplified abstract (Airbus Operations (S.A.S.))
F02K1/763 (No explanation available)
- Count: 1 patents
- Example: 20240124148. AIRCRAFT ENGINE NACELLE PROVIDED WITH A THRUST REVERSER HAVING A MOBILE EJECTION STRUCTURE simplified abstract (Airbus Operations (S.A.S.))
B64D2033/0206 (No explanation available)
- Count: 1 patents
- Example: 20240124148. AIRCRAFT ENGINE NACELLE PROVIDED WITH A THRUST REVERSER HAVING A MOBILE EJECTION STRUCTURE simplified abstract (Airbus Operations (S.A.S.))
B64D27/26 (No explanation available)
- Count: 1 patents
- Example: 20240002064. REINFORCED LATTICE STRUCTURE AND AIRCRAFT COMPRISING AT LEAST ONE SUCH STRUCTURE simplified abstract (AIRBUS OPERATIONS (S.A.S.))
F01D25/28 (No explanation available)
- Count: 1 patents
- Example: 20240002064. REINFORCED LATTICE STRUCTURE AND AIRCRAFT COMPRISING AT LEAST ONE SUCH STRUCTURE simplified abstract (AIRBUS OPERATIONS (S.A.S.))
B64D2027/266 (No explanation available)
- Count: 1 patents
- Example: 20240002064. REINFORCED LATTICE STRUCTURE AND AIRCRAFT COMPRISING AT LEAST ONE SUCH STRUCTURE simplified abstract (AIRBUS OPERATIONS (S.A.S.))
F05D2240/90 (No explanation available)
- Count: 1 patents
- Example: 20240002064. REINFORCED LATTICE STRUCTURE AND AIRCRAFT COMPRISING AT LEAST ONE SUCH STRUCTURE simplified abstract (AIRBUS OPERATIONS (S.A.S.))

Emerging Technology Areas

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B64F5/50 (No explanation available)
- Count: 1 patents
- Example: 20240025560. REFERENTIAL POSITIONING DEVICE INTENDED TO POSITION RELATIVE TO EACH OTHER AT LEAST ONE CABIN FLOOR GRID AND ONE SIDE SHELL OF AN AIRCRAFT IN ORDER TO ASSEMBLE A FUSELAGE BARREL OF THE AIRCRAFT simplified abstract (AIRBUS OPERATIONS (S.A.S.))
H02J3/46 (No explanation available)
- Count: 1 patents
- Example: 20240025557. ELECTRICAL SUPPLY SYSTEM OF AN AIRCRAFT simplified abstract (AIRBUS OPERATIONS (S.A.S.))
B64D41/00 (No explanation available)
- Count: 1 patents
- Example: 20240025557. ELECTRICAL SUPPLY SYSTEM OF AN AIRCRAFT simplified abstract (AIRBUS OPERATIONS (S.A.S.))
F17C2270/0189 (No explanation available)
- Count: 1 patents
- Example: 20240150032. FASTENING SYSTEM FOR AN AIRCRAFT INTENDED TO FASTEN AT LEAST ONE TANK INTENDED TO CONTAIN LIQUID HYDROGEN, ALLOWING EASY ACCESS TO THE TANK simplified abstract (Airbus Operations (S.A.S.))
F17C2205/0103 (No explanation available)
- Count: 1 patents
- Example: 20240150032. FASTENING SYSTEM FOR AN AIRCRAFT INTENDED TO FASTEN AT LEAST ONE TANK INTENDED TO CONTAIN LIQUID HYDROGEN, ALLOWING EASY ACCESS TO THE TANK simplified abstract (Airbus Operations (S.A.S.))
F17C13/08 (No explanation available)
- Count: 1 patents
- Example: 20240150032. FASTENING SYSTEM FOR AN AIRCRAFT INTENDED TO FASTEN AT LEAST ONE TANK INTENDED TO CONTAIN LIQUID HYDROGEN, ALLOWING EASY ACCESS TO THE TANK simplified abstract (Airbus Operations (S.A.S.))
B64D37/30 (No explanation available)
- Count: 1 patents
- Example: 20240150032. FASTENING SYSTEM FOR AN AIRCRAFT INTENDED TO FASTEN AT LEAST ONE TANK INTENDED TO CONTAIN LIQUID HYDROGEN, ALLOWING EASY ACCESS TO THE TANK simplified abstract (Airbus Operations (S.A.S.))
B64D37/04 (No explanation available)
- Count: 1 patents
- Example: 20240150032. FASTENING SYSTEM FOR AN AIRCRAFT INTENDED TO FASTEN AT LEAST ONE TANK INTENDED TO CONTAIN LIQUID HYDROGEN, ALLOWING EASY ACCESS TO THE TANK simplified abstract (Airbus Operations (S.A.S.))
B64D45/00 (No explanation available)
- Count: 1 patents
- Example: 20240083593. METHOD FOR ANALYZING AN AIRCRAFT ELECTRICAL STRUCTURE BY SEARCHING FOR EQUIPOTENTIALS IN EMBEDDED GRAPHS simplified abstract (AIRBUS OPERATIONS (S.A.S.))
E05C9/00 (No explanation available)
- Count: 1 patents
- Example: 20240083568. AIRCRAFT FUSELAGE DOOR COMPRISING AN INTERNAL PANEL AND AN EXTERNAL PANEL, AND AIRCRAFT FUSELAGE PART COMPRISING SUCH A DOOR simplified abstract (Airbus Operations (S.A.S.))

Top Inventors

Jean-Marc DATAS (4 patents)
Thomas CARTEREAU (4 patents)
Jacques BOURIQUET (4 patents)
André AQUILA (4 patents)
Nicolas DARBONVILLE (4 patents)
Thomas AUTRET (4 patents)
Joël BARBOULE (4 patents)
Sébastien BAYONNE (4 patents)
Patrick GUERIN (4 patents)
Sjoerd VAN DER VEEN (4 patents)

Patent Categories

Geographical Distribution of Inventors

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Geographical Distribution of US Inventors

Airbus Operations (S.A.S.) Inventor States 2024 - Up to June 2024

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