Improved Thick Wrought 7Xxx Aluminum Alloys, And Methods For Making The Same - EP3294917

The patent EP3294917 was granted to Arconic on Sep 24, 2025. The application was originally filed on May 9, 2016 under application number EP16793338A. The patent is currently recorded with a legal status of "Patent Maintained As Amended".

EP3294917

ARCONIC
Application Number
EP16793338A
Filing Date
May 9, 2016
Status
Patent Maintained As Amended
Aug 22, 2025
Grant Date
Sep 24, 2025
External Links
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C TEC CONSTELLIUM TECHNOLOGY CENTERCONSTELLIUM ISSOIRENov 30, 2022CONSTELLIUM PROPRIETE INDUSTRIELLEADMISSIBLE

Patent Citations (12) New

Patent citations refer to prior patents cited during different phases such as opposition or international search.

Citation PhasePublication NumberPublication Link
DESCRIPTIONCN103233148
DESCRIPTIONUS6972110
INTERNATIONAL-SEARCH-REPORTJP2014198899
INTERNATIONAL-SEARCH-REPORTUS2002150498
INTERNATIONAL-SEARCH-REPORTUS2007029016
INTERNATIONAL-SEARCH-REPORTUS2012000578
INTERNATIONAL-SEARCH-REPORTUS2014209222
OPPOSITIONJPH09279284
OPPOSITIONUS5047092
OPPOSITIONWO9424326
SEARCHCN103233148B
SEARCHUS2007029016

Non-Patent Literature (NPL) Citations (5) New

NPL citations refer to non-patent references such as research papers, articles, or other publications cited during examination or opposition phases.

Citation PhaseReference TextLink
DESCRIPTION- International Alloy Designations and Chemical Composition Limits for Wrought Aluminum and Wrought Aluminum Alloys, The Aluminum Association, (20090000), page 12-
OPPOSITION- ANSI H35.2-
OPPOSITION- A Specimen to Evaluate Susceptibility of Aluminium Alloys to L-S Crack Deviation-
OPPOSITION- International alloy designations and chemical composition limits for wrought aluminum and wrought aluminum allovs-
OPPOSITION- Starke E.A.; Staley J.T., "Application of modern aluminum alloys to aircraft", PROGRESS IN AEROSPACE SCIENCES, OXFORD, GB, GB , (19960101), vol. 32, no. 2, doi:10.1016/0376-0421(95)00004-6, ISSN 0376-0421, pages 131 - 172, XP029212053

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