MIKRO SYSTEMS, INC.
57Patents
56Active
57Granted
58Portfolio score
Filing activity: Dec 3, 2002 → Oct 4, 2021 · 10 expiring within 5 years
Most-cited patents
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US7141812B2 | Devices, methods, and systems involving castings | Performing Operations; Transporting | 191 | Expired |
| US9315663B2 | Systems, devices, and/or methods for manufacturing castings | Emerging Cross-Sectional Technologies | 176 | Active |
| US7785098B1 | Systems for large area micro mechanical systems | Performing Operations; Transporting | 101 | Active |
| US7893413B1 | Systems, devices, and methods for large area micro mechanical systems | Performing Operations; Transporting | 59 | Active |
| US9206309B2 | Systems, devices, and/or methods for manufacturing castings | Emerging Cross-Sectional Technologies | 46 | Active |
| US8752386B2 | Air/fuel supply system for use in a gas turbine engine | Mechanical Engineering; Lighting; Heating | 42 | Active |
| US9208916B2 | Methods for manufacturing three-dimensional devices and devices created thereby | Emerging Cross-Sectional Technologies | 25 | Active |
| US8813824B2 | Systems, devices, and/or methods for producing holes | Emerging Cross-Sectional Technologies | 25 | Active |
| US8049193B1 | Systems, devices, and methods for large area micro mechanical systems | Performing Operations; Transporting | 25 | Active |
| US9057277B2 | Systems, devices, and/or methods for producing holes | Emerging Cross-Sectional Technologies | 25 | Active |
| US8196640B1 | Self supporting core-in-a-core for casting | Performing Operations; Transporting | 21 | Active |
| US8813812B2 | Turbine component casting core with high resolution region | Performing Operations; Transporting | 21 | Active |
| US8936068B2 | Method of casting a component having interior passageways | Emerging Cross-Sectional Technologies | 21 | Active |
| US9387533B1 | Systems, devices, and methods involving precision component castings | Mechanical Engineering; Lighting; Heating | 19 | Active |
| US9555470B1 | Systems, devices, and methods involving precision component castings | Mechanical Engineering; Lighting; Heating | 18 | Active |
| US8840363B2 | Trailing edge cooling system in a turbine airfoil assembly | Mechanical Engineering; Lighting; Heating | 17 | Active |
| US9366143B2 | Cooling module design and method for cooling components of a gas turbine system | Mechanical Engineering; Lighting; Heating | 17 | Active |
| US8940114B2 | Hybrid manufacturing process and product made using laminated sheets and compressive casing | Emerging Cross-Sectional Technologies | 14 | Active |
| US9017027B2 | Component having cooling channel with hourglass cross section | Mechanical Engineering; Lighting; Heating | 13 | Active |
| US8714926B2 | Turbine component cooling channel mesh with intersection chambers | Mechanical Engineering; Lighting; Heating | 12 | Active |
| US10022790B2 | Turbine airfoil cooling system with leading edge impingement cooling system turbine blade investment casting using film hole protrusions for integral wall thickness control | Mechanical Engineering; Lighting; Heating | 12 | Active |
| US9017025B2 | Serpentine cooling circuit with T-shaped partitions in a turbine airfoil | Mechanical Engineering; Lighting; Heating | 9 | Active |
| US8764394B2 | Component cooling channel | Mechanical Engineering; Lighting; Heating | 9 | Active |
| US9878369B1 | Systems, devices, and methods involving precision component castings | Mechanical Engineering; Lighting; Heating | 9 | Active |
| US8894367B2 | Compound cooling flow turbulator for turbine component | Mechanical Engineering; Lighting; Heating | 9 | Active |
Source: USPTO / EPO open patent data. Counts and citation impact are objective bibliographic measures.