Timothy Warner
26Patents
8h-index
32Co-inventors
75Inventor score
Filing activity: Aug 15, 1994 → Sep 13, 2022
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US7294213B2 | Aircraft structural member made of an Al-Cu-Mg alloy | Emerging Cross-Sectional Technologies | 21 | Expired |
| US5858134A | Process for producing alsimgcu alloy products with improved resistance to intercrystalline corrosion | Chemistry; Metallurgy | 21 | Expired |
| US7087317B2 | Composite laminated aluminum-glass fiber sandwich panels | Emerging Cross-Sectional Technologies | 17 | Expired |
| US6569542B2 | Aircraft structure element made of an Al-Cu-Mg alloy | Emerging Cross-Sectional Technologies | 14 | Expired |
| US7229508B2 | Al—Cu—Mg—Ag—Mn-alloy for structural applications requiring high strength and high ductility | Chemistry; Metallurgy | 12 | Expired |
| US6602361B2 | Product made of an AlCuMg alloy for aircraft structural elements | Chemistry; Metallurgy | 11 | Expired |
| US7550110B2 | Al-Zn-Mg-Cu alloys and products with improved ratio of static mechanical characteristics to damage tolerance | Chemistry; Metallurgy | 10 | Expired |
| US7452429B2 | Products made of Al-Zn-Mg-Cu alloys with an improved compromise between static mechanical characteristics and damage tolerance | Chemistry; Metallurgy | 8 | Expired |
| US7490752B2 | Manufacturing method for friction welded aluminum alloy parts | Emerging Cross-Sectional Technologies | 8 | Expired |
| US5643372A | Process for the desensitisation to intercrystalline corrosion of 2000 and 6000 series Al alloys and corresponding products | Chemistry; Metallurgy | 8 | Expired |
| US7744704B2 | High fracture toughness aluminum-copper-lithium sheet or light-gauge plate suitable for use in a fuselage panel | Chemistry; Metallurgy | 6 | Active |
| US7135077B2 | Thick products made of heat-treatable aluminum alloy with improved toughness and process for manufacturing these products | Chemistry; Metallurgy | 5 | Expired |
| US7252723B2 | AlCuMg alloys with high damage tolerance suitable for use as structural members in aircrafts | Chemistry; Metallurgy | 4 | Expired |
| US8771441B2 | High fracture toughness aluminum-copper-lithium sheet or light-gauge plates suitable for fuselage panels | Chemistry; Metallurgy | 4 | Active |
| US7763128B2 | Process for manufacturing structural components by machining plates | Chemistry; Metallurgy | 4 | Active |
| US7704333B2 | Al-Cu-Mg-Ag-Mn alloy for structural applications requiring high strength and high ductility | Chemistry; Metallurgy | 4 | Active |
| US8277580B2 | Al-Zn-Cu-Mg aluminum base alloys and methods of manufacture and use | Chemistry; Metallurgy | 4 | Active |
| US7837808B2 | Process for manufacturing structural components by machining plates | Chemistry; Metallurgy | 4 | Expired |
| US6692589B2 | Aircraft structure element made of an Al-Cu-Mg- alloy | Emerging Cross-Sectional Technologies | 3 | Expired |
| US9945010B2 | Aluminum-copper-lithium alloy with improved impact resistance | Emerging Cross-Sectional Technologies | 3 | Active |
| US7993474B2 | Aircraft structural member made of an Al-Cu-Mg alloy | Emerging Cross-Sectional Technologies | 2 | Active |
| US10196722B2 | Method for manufacturing a structural element having a variable thickness for aircraft production | Chemistry; Metallurgy | 1 | Active |
| US11111562B2 | Aluminum-copper-lithium alloy with improved mechanical strength and toughness | Chemistry; Metallurgy | 0 | Active |
| US12024765B2 | AlMgMn alloy product with improved corrosion resistance | Chemistry; Metallurgy | 0 | Active |
| US12421578B2 | Al—Zn—Cu—Mg alloys with high strength and method of fabrication | Chemistry; Metallurgy | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.