Average Co-Inventor Count = 2.89
ph-index = 9
The patent ph-index is calculated by counting the number of publications for which an author has been cited by other authors at least that same number of times.
Company Filing History:
1. Airbus Operations (s.a.s.) (34 from 2,279 patents)
2. Airbus France (4 from 458 patents)
3. Airbus Operations Gmbh (1 from 3,623 patents)
4. Creuzet Aeronautique (1 from 3 patents)
5. Airbus Corporation (140 patents)
39 patents:
1. 12134982 - Strip-form acoustic material having an integrated flange, and internal wall of an aircraft air intake made with this material
2. 12054275 - Resistive skin shell incorporating perforated metal bands, and acoustic inner wall of an aircraft air intake formed from such resistive skin shells
3. 12030659 - Anterior part of a nacelle for an aircraft propulsion assembly, whose front frame is connected to an outer wall without penetrating it
4. 12023879 - Method for manufacturing deicing acoustic skin for an aircraft acoustic panel, using a fiber spacing device
5. 12014714 - Cellular sound insulation structure including a diaphragm provided with a tube configured to treat different acoustic frequencies, method for manufacturing such a cellular sound insulation structure, and associated tool
6. 11952136 - Method for manufacturing an acoustic panel having a capsular skin, and acoustic panel incorporating such a skin
7. 11945596 - Method for producing an alveolar soundproofing structure including a diaphragm, and alveolar soundproofing structure obtained
8. 11745887 - Multifrequency absorption acoustic panel for an aircraft nacelle
9. 11731381 - Method for manufacturing two soundproof panels in the same mold using two mold cavities
10. 11685507 - Sound-absorbing panel with a cellular core and a de-icing system
11. 11655045 - Anterior part of the nacelle of an aircraft propulsion assembly whose air intake lip is linked to the outer panel by nesting
12. 11649063 - Acoustic panel for an aircraft nacelle air inlet with castellated resistive skin, propulsion unit and aircraft fitted with such acoustic panels
13. 11649062 - Forward part of an aircraft propulsion unit nacelle comprising a main propagation path for forces between an air intake lip and a back skin of an acoustic panel
14. 11518526 - Aircraft engine nacelle comprising an anti-icing protection system
15. 11459950 - Sound attenuation panel for aircraft having a combination of acoustic attenuation properties