Airbus Operations Gmbh Patent Portfolio Statistics

Airbus Operations Gmbh

Profile Summary

This article summarizes the perfomance of the assignee in the recent years. The overall statistics for this portfolio help to analyze the areas where the assignee is performing well. The filing trend, perfomance across the tech centers and the perfomance of the recent applications has been mentioned below. All the stats are calculated based on the perfomance in USPTO.

How does the overall patent portfolio of Airbus Operations Gmbh look like?

Assignee Art Units
Total Applications: 3,238 2,258,072
Granted Patents: 2,568 1,392,011
Grant Index 85.12% 75.27%
Abandoned/Rejected Applications: 449 (14.88%) 457,302 (24.73%)
In-Process Applications: 215 408,759
Average Grant Time: 3.25 Years 2.6 Years
Average Office Actions: 1.98 1.49

Which Technology Area Airbus Operations Gmbh is filing most patents in? (Last 10 years)

Art Unit Definition Total Applications
3644 Aeronautics, Agriculture, Fishing, Trapping, Vermin Destroying, Plant and Animal Husbandry, Weaponry, Nuclear Systems, and License and Review 483
3647 Aeronautics, Agriculture, Fishing, Trapping, Vermin Destroying, Plant and Animal Husbandry, Weaponry, Nuclear Systems, and License and Review 198
3642 Aeronautics, Agriculture, Fishing, Trapping, Vermin Destroying, Plant and Animal Husbandry, Weaponry, Nuclear Systems, and License and Review 144
3643 Aeronautics, Agriculture, Fishing, Trapping, Vermin Destroying, Plant and Animal Husbandry, Weaponry, Nuclear Systems, and License and Review 97
3744 Refrigeration, Vaporization, Ventilation, AndCombustion 87

How many patents are Airbus Operations Gmbh filing every year?

Year Total Applications Predicted
2022 0* 730
2021 49* 679
2020 64 590
2019 167 167
2018 191
2017 187
2016 193
2015 208
2014 245
2013 263

*The drop in the number of applications filed in last two years compared to previous years is because applications can take up to 18 months to get published

Recently filed patent applications of Airbus Operations Gmbh in USPTO?

Publication number: US20220190410A1
Application number: 17/550,922

Abstract:
With the measures described herein, a structural composite laminate is provided that includes a structural fuel cell, a structural supercondensator and a structural battery. Each of these components is configured in a self-supporting manner, such that aircraft parts, like exterior panels, may be manufactured from the laminate. The aircraft parts are capable of generating electrical energy by means of the structural fuel cell and distribute the electrical energy over the whole aircraft without cabling. Furthermore, short power demand peaks can be absorbed by the structural supercondensator, whereas the basic load is supplied by the structural battery.

Publication date: 2022-06-16
Applicant: Airbus Operations Gmbh
Inventors: Linde Peter


Publication number: US20220186051A1
Application number: 17/550,865

Abstract:
A coating material for a lightning-prone object includes a base color substance and an additive admixed with the base color substance. The additive comprises rigid hollow beads filled with an inert gas. At least a portion of the hollow beads have an electrically conductive coating.

Publication date: 2022-06-16
Applicant: Airbus Operations Gmbh
Inventors: Kaste Michael


Publication number: US20220191634A1
Application number: 17/538,267

Abstract:
A method for testing an audio signal system having multiple audio component connection sockets, each socket having at least one audio signal interface connected to a ground interface of the socket via a series circuit including a resistor and a capacitor, including feeding, via a signal processing device, a time domain reflectometry test signal into a wired network of the audio signal system, in which the sockets are connected to the signal processing device via differently lengthed electrical lines, detecting in a temporally resolved manner, via the signal processing device, test return signals reflected at the multiple sockets, comparing the detected test return signals with a temporally resolved reference pattern for test return signals, which reference pattern was created under predefined boundary conditions, and determining a faulty connection of a socket if comparing the detected test return signals with the reference pattern reveals a deviation above a predefined threshold value.

Publication date: 2022-06-16
Applicant: Airbus Operations Gmbh
Inventors: Frank Khelfa


How are Airbus Operations Gmbh’s applications performing in USPTO?

Application Number Title Status Art Unit Examiner
17/550,922 Structural Composite Laminate Structure For An Aircraft Part, Aircraft Part Manufactured With Such A Laminate And Aircraft OPAP Central, Docket
17/550,865 Coating Material For A Lightning-Prone Object OPAP Central, Docket
17/538,267 Method For Testing An Audio Signal System And Aircraft Comprising An Audio Signal System OPAP Central, Docket
17/615,074 Flow Body For An Aircraft Having An Integrated De-Icing System Docketed New Case – Ready for Examination OPAP Central, Docket
17/535,885 Method For Producing A Torsion Box For A Structure Of An Airplane And A Torsion Box For A Structure Of An Airplane Docketed New Case – Ready for Examination OPAP Central, Docket