Difference between revisions of "AIRBUS HELICOPTERS Patent Application Trends in 2024"
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[[File:AIRBUS HELICOPTERS Top Technology Areas 2024 - Up to June 2024.png|border|800px|AIRBUS HELICOPTERS Top Technology Areas 2024 - Up to June 2024]] | [[File:AIRBUS HELICOPTERS Top Technology Areas 2024 - Up to June 2024.png|border|800px|AIRBUS HELICOPTERS Top Technology Areas 2024 - Up to June 2024]] | ||
| − | * [[:Category:CPC_B64C25/58|B64C25/58]] ( | + | * [[:Category:CPC_B64C25/58|B64C25/58]] (Arrangements or adaptations of shock-absorbers or springs (shimmy-dampers) |
** Count: 3 patents | ** Count: 3 patents | ||
** Example: [[20240182160. ROTORCRAFT WITH A NON-RETRACTABLE WHEEL-TYPE LANDING GEAR simplified abstract (AIRBUS HELICOPTERS DEUTSCHLAND GMBH)]] | ** Example: [[20240182160. ROTORCRAFT WITH A NON-RETRACTABLE WHEEL-TYPE LANDING GEAR simplified abstract (AIRBUS HELICOPTERS DEUTSCHLAND GMBH)]] | ||
| − | * [[:Category:CPC_B64C2027/8254|B64C2027/8254]] ( | + | * [[:Category:CPC_B64C2027/8254|B64C2027/8254]] (AEROPLANES; HELICOPTERS) |
** Count: 3 patents | ** Count: 3 patents | ||
** Example: [[20240140601. ROTORCRAFT WITH A DUCTED TAIL ROTOR SUPPORTED BY A STATOR simplified abstract (AIRBUS HELICOPTERS DEUTSCHLAND GMBH)]] | ** Example: [[20240140601. ROTORCRAFT WITH A DUCTED TAIL ROTOR SUPPORTED BY A STATOR simplified abstract (AIRBUS HELICOPTERS DEUTSCHLAND GMBH)]] | ||
| − | * [[:Category:CPC_B64C27/82|B64C27/82]] ( | + | * [[:Category:CPC_B64C27/82|B64C27/82]] (AEROPLANES; HELICOPTERS) |
** Count: 3 patents | ** Count: 3 patents | ||
** Example: [[20240140602. ROTORCRAFT WITH A TAIL BOOM HAVING A DUCT-TYPE PORTION simplified abstract (AIRBUS HELICOPTERS DEUTSCHLAND GMBH)]] | ** Example: [[20240140602. ROTORCRAFT WITH A TAIL BOOM HAVING A DUCT-TYPE PORTION simplified abstract (AIRBUS HELICOPTERS DEUTSCHLAND GMBH)]] | ||
| − | * [[:Category:CPC_B64D27/24|B64D27/24]] ( | + | * [[:Category:CPC_B64D27/24|B64D27/24]] (using steam or spring force (jet aircraft) |
** Count: 3 patents | ** Count: 3 patents | ||
** Example: [[20240092188. A ROTORCRAFT WITH AN ENERGY SOURCE STORAGE UNIT simplified abstract (AIRBUS HELICOPTERS DEUTSCHLAND GMBH)]] | ** Example: [[20240092188. A ROTORCRAFT WITH AN ENERGY SOURCE STORAGE UNIT simplified abstract (AIRBUS HELICOPTERS DEUTSCHLAND GMBH)]] | ||
| − | * [[:Category:CPC_B64C27/06|B64C27/06]] ( | + | * [[:Category:CPC_B64C27/06|B64C27/06]] (AEROPLANES; HELICOPTERS) |
** Count: 2 patents | ** Count: 2 patents | ||
** Example: [[20240010472. DOUBLE-LOCKING HOOKING SYSTEM INTENDED FOR TRANSPORTING A LOAD OUTSIDE AN AIRCRAFT simplified abstract (AIRBUS HELICOPTERS)]] | ** Example: [[20240010472. DOUBLE-LOCKING HOOKING SYSTEM INTENDED FOR TRANSPORTING A LOAD OUTSIDE AN AIRCRAFT simplified abstract (AIRBUS HELICOPTERS)]] | ||
| − | * [[:Category:CPC_B64D1/22|B64D1/22]] ( | + | * [[:Category:CPC_B64D1/22|B64D1/22]] (Taking-up articles from earth's surface) |
** Count: 2 patents | ** Count: 2 patents | ||
** Example: [[20240010472. DOUBLE-LOCKING HOOKING SYSTEM INTENDED FOR TRANSPORTING A LOAD OUTSIDE AN AIRCRAFT simplified abstract (AIRBUS HELICOPTERS)]] | ** Example: [[20240010472. DOUBLE-LOCKING HOOKING SYSTEM INTENDED FOR TRANSPORTING A LOAD OUTSIDE AN AIRCRAFT simplified abstract (AIRBUS HELICOPTERS)]] | ||
| − | * [[:Category:CPC_B64C2025/325|B64C2025/325]] ( | + | * [[:Category:CPC_B64C2025/325|B64C2025/325]] (AEROPLANES; HELICOPTERS) |
** Count: 2 patents | ** Count: 2 patents | ||
** Example: [[20240182160. ROTORCRAFT WITH A NON-RETRACTABLE WHEEL-TYPE LANDING GEAR simplified abstract (AIRBUS HELICOPTERS DEUTSCHLAND GMBH)]] | ** Example: [[20240182160. ROTORCRAFT WITH A NON-RETRACTABLE WHEEL-TYPE LANDING GEAR simplified abstract (AIRBUS HELICOPTERS DEUTSCHLAND GMBH)]] | ||
| − | * [[:Category:CPC_B64C25/06|B64C25/06]] ( | + | * [[:Category:CPC_B64C25/06|B64C25/06]] (AEROPLANES; HELICOPTERS) |
** Count: 2 patents | ** Count: 2 patents | ||
** Example: [[20240182161. ROTORCRAFT WITH A NON-RETRACTABLE WHEEL-TYPE LANDING GEAR simplified abstract (AIRBUS HELICOPTERS DEUTSCHLAND GMBH)]] | ** Example: [[20240182161. ROTORCRAFT WITH A NON-RETRACTABLE WHEEL-TYPE LANDING GEAR simplified abstract (AIRBUS HELICOPTERS DEUTSCHLAND GMBH)]] | ||
| − | * [[:Category:CPC_B64C1/1407|B64C1/1407]] ( | + | * [[:Category:CPC_B64C1/1407|B64C1/1407]] ({Doors; surrounding frames}) |
** Count: 2 patents | ** Count: 2 patents | ||
** Example: [[20240183202. LATCHING AND LOCKING SYSTEM FOR AN ACTUATABLE DOOR simplified abstract (AIRBUS HELICOPTERS DEUTSCHLAND GMBH)]] | ** Example: [[20240183202. LATCHING AND LOCKING SYSTEM FOR AN ACTUATABLE DOOR simplified abstract (AIRBUS HELICOPTERS DEUTSCHLAND GMBH)]] | ||
| − | * [[:Category:CPC_G01G19/07|G01G19/07]] ( | + | * [[:Category:CPC_G01G19/07|G01G19/07]] (WEIGHING (sorting by weighing) |
** Count: 2 patents | ** Count: 2 patents | ||
** Example: [[20240005207. METHOD FOR TRAINING AT LEAST ONE ARTIFICIAL INTELLIGENCE MODEL FOR ESTIMATING THE WEIGHT OF AN AIRCRAFT DURING FLIGHT BASED ON USE DATA simplified abstract (AIRBUS HELICOPTERS)]] | ** Example: [[20240005207. METHOD FOR TRAINING AT LEAST ONE ARTIFICIAL INTELLIGENCE MODEL FOR ESTIMATING THE WEIGHT OF AN AIRCRAFT DURING FLIGHT BASED ON USE DATA simplified abstract (AIRBUS HELICOPTERS)]] | ||
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** Count: 1 patents | ** Count: 1 patents | ||
** Example: [[20240025552. AIRCRAFT COMPRISING AT LEAST TWO TURBOSHAFT ENGINES AND DEVICE CONFIGURED TO BE CONNECTED TO ONE OF THE TURBOSHAFT ENGINES AND METHOD FOR CONTROLLING SUCH AN AIRCRAFT simplified abstract (AIRBUS HELICOPTERS)]] | ** Example: [[20240025552. AIRCRAFT COMPRISING AT LEAST TWO TURBOSHAFT ENGINES AND DEVICE CONFIGURED TO BE CONNECTED TO ONE OF THE TURBOSHAFT ENGINES AND METHOD FOR CONTROLLING SUCH AN AIRCRAFT simplified abstract (AIRBUS HELICOPTERS)]] | ||
| − | * [[:Category:CPC_F02C7/268|F02C7/268]] ( | + | * [[:Category:CPC_F02C7/268|F02C7/268]] (Starting drives for the rotor {, acting directly on the rotor of the gas turbine to be started}) |
** Count: 1 patents | ** Count: 1 patents | ||
** Example: [[20240025552. AIRCRAFT COMPRISING AT LEAST TWO TURBOSHAFT ENGINES AND DEVICE CONFIGURED TO BE CONNECTED TO ONE OF THE TURBOSHAFT ENGINES AND METHOD FOR CONTROLLING SUCH AN AIRCRAFT simplified abstract (AIRBUS HELICOPTERS)]] | ** Example: [[20240025552. AIRCRAFT COMPRISING AT LEAST TWO TURBOSHAFT ENGINES AND DEVICE CONFIGURED TO BE CONNECTED TO ONE OF THE TURBOSHAFT ENGINES AND METHOD FOR CONTROLLING SUCH AN AIRCRAFT simplified abstract (AIRBUS HELICOPTERS)]] | ||
| − | * [[:Category:CPC_F01D15/10|F01D15/10]] ( | + | * [[:Category:CPC_F01D15/10|F01D15/10]] (Adaptations for driving, or combinations with, electric generators) |
** Count: 1 patents | ** Count: 1 patents | ||
** Example: [[20240025552. AIRCRAFT COMPRISING AT LEAST TWO TURBOSHAFT ENGINES AND DEVICE CONFIGURED TO BE CONNECTED TO ONE OF THE TURBOSHAFT ENGINES AND METHOD FOR CONTROLLING SUCH AN AIRCRAFT simplified abstract (AIRBUS HELICOPTERS)]] | ** Example: [[20240025552. AIRCRAFT COMPRISING AT LEAST TWO TURBOSHAFT ENGINES AND DEVICE CONFIGURED TO BE CONNECTED TO ONE OF THE TURBOSHAFT ENGINES AND METHOD FOR CONTROLLING SUCH AN AIRCRAFT simplified abstract (AIRBUS HELICOPTERS)]] | ||
| − | * [[:Category:CPC_B64D29/08|B64D29/08]] ( | + | * [[:Category:CPC_B64D29/08|B64D29/08]] (Inspection panels for power plants) |
** Count: 1 patents | ** Count: 1 patents | ||
** Example: [[20240150030. AIRCRAFT PROVIDED WITH AN EXHAUST DUCT COUPLED TO A STABILIZATION SYSTEM simplified abstract (AIRBUS HELICOPTERS)]] | ** Example: [[20240150030. AIRCRAFT PROVIDED WITH AN EXHAUST DUCT COUPLED TO A STABILIZATION SYSTEM simplified abstract (AIRBUS HELICOPTERS)]] | ||
| − | * [[:Category:CPC_B64D33/02|B64D33/02]] ( | + | * [[:Category:CPC_B64D33/02|B64D33/02]] (of combustion air intakes (air intakes for gas-turbine plants or jet-propulsion plants per se) |
** Count: 1 patents | ** Count: 1 patents | ||
** Example: [[20240150030. AIRCRAFT PROVIDED WITH AN EXHAUST DUCT COUPLED TO A STABILIZATION SYSTEM simplified abstract (AIRBUS HELICOPTERS)]] | ** Example: [[20240150030. AIRCRAFT PROVIDED WITH AN EXHAUST DUCT COUPLED TO A STABILIZATION SYSTEM simplified abstract (AIRBUS HELICOPTERS)]] | ||
| − | * [[:Category:CPC_F01N1/00|F01N1/00]] ( | + | * [[:Category:CPC_F01N1/00|F01N1/00]] (Silencing apparatus characterised by method of silencing {(by cooling) |
** Count: 1 patents | ** Count: 1 patents | ||
** Example: [[20240084748. METHOD OF OPTIMIZING THE NOISE GENERATED IN FLIGHT BY A ROTORCRAFT simplified abstract (AIRBUS HELICOPTERS)]] | ** Example: [[20240084748. METHOD OF OPTIMIZING THE NOISE GENERATED IN FLIGHT BY A ROTORCRAFT simplified abstract (AIRBUS HELICOPTERS)]] | ||
| − | * [[:Category:CPC_B64D31/06|B64D31/06]] ( | + | * [[:Category:CPC_B64D31/06|B64D31/06]] (EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT) |
** Count: 1 patents | ** Count: 1 patents | ||
** Example: [[20240084748. METHOD OF OPTIMIZING THE NOISE GENERATED IN FLIGHT BY A ROTORCRAFT simplified abstract (AIRBUS HELICOPTERS)]] | ** Example: [[20240084748. METHOD OF OPTIMIZING THE NOISE GENERATED IN FLIGHT BY A ROTORCRAFT simplified abstract (AIRBUS HELICOPTERS)]] | ||
| − | * [[:Category:CPC_B64D27/10|B64D27/10]] ( | + | * [[:Category:CPC_B64D27/10|B64D27/10]] (of gas-turbine type (jet aircraft) |
** Count: 1 patents | ** Count: 1 patents | ||
** Example: [[20240084748. METHOD OF OPTIMIZING THE NOISE GENERATED IN FLIGHT BY A ROTORCRAFT simplified abstract (AIRBUS HELICOPTERS)]] | ** Example: [[20240084748. METHOD OF OPTIMIZING THE NOISE GENERATED IN FLIGHT BY A ROTORCRAFT simplified abstract (AIRBUS HELICOPTERS)]] | ||
Latest revision as of 16:32, 20 July 2024
Contents
AIRBUS HELICOPTERS Patent Filing Activity
AIRBUS HELICOPTERS patent applications in 2024
Top 10 Technology Areas
- B64C25/58 (Arrangements or adaptations of shock-absorbers or springs (shimmy-dampers)
- B64C2027/8254 (AEROPLANES; HELICOPTERS)
- B64C27/82 (AEROPLANES; HELICOPTERS)
- B64D27/24 (using steam or spring force (jet aircraft)
- B64C27/06 (AEROPLANES; HELICOPTERS)
- B64D1/22 (Taking-up articles from earth's surface)
- B64C2025/325 (AEROPLANES; HELICOPTERS)
- B64C25/06 (AEROPLANES; HELICOPTERS)
- B64C1/1407 ({Doors; surrounding frames})
- G01G19/07 (WEIGHING (sorting by weighing)
Emerging Technology Areas
- F05D2260/85 (No explanation available)
- F05D2220/76 (No explanation available)
- F05D2220/329 (No explanation available)
- F02C7/268 (Starting drives for the rotor {, acting directly on the rotor of the gas turbine to be started})
- F01D15/10 (Adaptations for driving, or combinations with, electric generators)
- B64D29/08 (Inspection panels for power plants)
- B64D33/02 (of combustion air intakes (air intakes for gas-turbine plants or jet-propulsion plants per se)
- F01N1/00 (Silencing apparatus characterised by method of silencing {(by cooling)
- B64D31/06 (EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT)
- B64D27/10 (of gas-turbine type (jet aircraft)
Top Inventors
- Axel FINK (3 patents)
- Didier BERTIN (3 patents)
- Rupert PFALLER (3 patents)
- Tobias RIES (3 patents)
- Guillaume LEGRAS (3 patents)
- Aurelien ACHARD (2 patents)
- Aurelien VAYSSIERE (2 patents)
- Pierre FRUITET (2 patents)
- Philippe PINTO (2 patents)
- Marc GAZZINO (1 patent)
Patent Categories
Geographical Distribution of Inventors
Geographical Distribution of US Inventors
Categories:
- Pages with broken file links
- AIRBUS HELICOPTERS
- Companies
- CPC F02C9/00
- CPC F02C6/206
- CPC H02P9/08
- CPC H02P2101/25
- CPC F16H57/01
- CPC G01N33/2858
- CPC B64D2045/0085
- CPC B66C1/36
- CPC B64C27/06
- CPC B66D1/54
- CPC B64D1/22
- CPC B64C25/36
- CPC B64C25/58
- CPC B64C2025/325
- CPC B64C25/06
- CPC B64C25/34
- CPC E05B81/06
- CPC E05B81/14
- CPC B64C1/1407
- CPC E05C3/045
- CPC E05C3/004
- CPC B64C1/1438
- CPC G06N20/00
- CPC B64D45/00
- CPC G01G19/414
- CPC G01G19/07
- CPC E05D15/00
- CPC B64C1/1461
- CPC E05Y2900/502
- CPC G01S17/933
- CPC B64D45/08
- CPC G01S7/4815
- CPC G01S17/89
- CPC G06T7/70
- CPC G06T15/00
- CPC G06T17/05
- CPC G08G5/0021
- CPC G08G5/0086
- CPC G08G5/045
- CPC G06T2207/30261
- CPC B64C27/48
- CPC F01D5/30
- CPC F01D25/06
- CPC F05D2220/90
- CPC F05D2240/30
- CPC F05D2260/96
- CPC B64C27/54
- CPC B64C2027/8254
- CPC B64C27/82
- CPC G08G5/0034
- CPC G08G5/006
- CPC G06N5/003
- CPC G08G5/0039
- CPC B64C2027/8272
- CPC B64C2027/8281
- CPC G01G19/14
- CPC B64D47/06
- CPC B64C27/463
- CPC F21K2/00
- CPC G08G5/0026
- CPC B60L50/60
- CPC B64C1/062
- CPC B64D27/24
- CPC B60L2200/10
- CPC H02J15/008
- CPC E05B77/38
- CPC B64C27/04
- CPC B64C25/60
- CPC B64C25/26
- CPC B64C25/20
- CPC B64D33/04
- CPC B64F5/10
- CPC A62C3/06
- CPC A62C3/08
- CPC F02D35/0007
- CPC B64D27/02
- CPC B64D27/10
- CPC B64D31/06
- CPC F01N1/00
- CPC B64D2027/026
- CPC B64D33/02
- CPC B64D29/08
- CPC F01D15/10
- CPC F02C7/268
- CPC F05D2220/329
- CPC F05D2220/76
- CPC F05D2260/85
- Patent Trends by Company in 2024
