Michael James Weimer
52Patents
13h-index
68Co-inventors
87Inventor score
Filing activity: Jun 20, 1994 → Jul 20, 2021
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US7449075B2 | Method for producing a beta-processed alpha-beta titanium-alloy article | Chemistry; Metallurgy | 42 | Expired |
| US6465040B2 | Method for refurbishing a coating including a thermally grown oxide | Emerging Cross-Sectional Technologies | 20 | Expired |
| US5634992A | Method for heat treating gamma titanium aluminide alloys | Chemistry; Metallurgy | 18 | Expired |
| US6283714A | Protection of internal and external surfaces of gas turbine airfoils | Emerging Cross-Sectional Technologies | 18 | Expired |
| US6497920B1 | Process for applying an aluminum-containing coating using an inorganic slurry mix | Emerging Cross-Sectional Technologies | 16 | Expired |
| US7364801B1 | Turbine component protected with environmental coating | Emerging Cross-Sectional Technologies | 16 | Active |
| US8579013B2 | Casting mold composition with improved detectability for inclusions and method of casting | Chemistry; Metallurgy | 15 | Active |
| US6274193A | Repair of a discrete selective surface of an article | Emerging Cross-Sectional Technologies | 15 | Expired |
| US6532657B1 | Pre-service oxidation of gas turbine disks and seals | Emerging Cross-Sectional Technologies | 15 | Expired |
| US6607789B1 | Plasma sprayed thermal bond coat system | Emerging Cross-Sectional Technologies | 14 | Expired |
| US6571472B2 | Restoration of thickness to load-bearing gas turbine engine components | Emerging Cross-Sectional Technologies | 14 | Expired |
| US7582133B2 | Methods for reducing carbon contamination when melting highly reactive alloys | Mechanical Engineering; Lighting; Heating | 14 | Active |
| US6800376B1 | Gas turbine engine component having a refurbished coating including a thermally grown oxide | Emerging Cross-Sectional Technologies | 14 | Expired |
| US6921251B2 | Aluminide or chromide coating of turbine engine rotor component | Emerging Cross-Sectional Technologies | 13 | Expired |
| US8062581B2 | Refractory crucibles capable of managing thermal stress and suitable for melting highly reactive alloys | Emerging Cross-Sectional Technologies | 13 | Active |
| US6755924B2 | Method of restoration of mechanical properties of a cast nickel-based super alloy for serviced aircraft components | Emerging Cross-Sectional Technologies | 13 | Expired |
| US7790101B2 | Articles for use with highly reactive alloys | Emerging Cross-Sectional Technologies | 13 | Active |
| US7761969B2 | Methods for making refractory crucibles | Emerging Cross-Sectional Technologies | 13 | Active |
| US6926928B2 | Protection of a gas turbine component by a vapor-deposited oxide coating | Emerging Cross-Sectional Technologies | 10 | Expired |
| US6905730B2 | Aluminide coating of turbine engine component | Emerging Cross-Sectional Technologies | 9 | Expired |
| US6869508B2 | Physical vapor deposition apparatus and process | Chemistry; Metallurgy | 8 | Expired |
| US6305077A | Repair of coated turbine components | Emerging Cross-Sectional Technologies | 8 | Expired |
| US7314674B2 | Corrosion resistant coating composition, coated turbine component and method for coating same | Emerging Cross-Sectional Technologies | 8 | Expired |
| US7754342B2 | Strain tolerant corrosion protecting coating and spray method of application | Emerging Cross-Sectional Technologies | 7 | Active |
| US6533875B1 | Protecting a surface of a nickel-based article with a corrosion-resistant aluminum-alloy layer | Emerging Cross-Sectional Technologies | 7 | Expired |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.