Gilbert Farmer
31Patents
18h-index
45Co-inventors
77Inventor score
Filing activity: Dec 28, 1994 → Sep 3, 2004
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US5681616A | Thick thermal barrier coating having grooves for enhanced strain tolerance | Emerging Cross-Sectional Technologies | 66 | Expired |
| US6047539A | Method of protecting gas turbine combustor components against water erosion and hot corrosion | Mechanical Engineering; Lighting; Heating | 49 | Expired |
| US6655149B2 | Preferential multihole combustor liner | Emerging Cross-Sectional Technologies | 42 | Expired |
| US5558922A | Thick thermal barrier coating having grooves for enhanced strain tolerance | Emerging Cross-Sectional Technologies | 39 | Expired |
| US6513331B1 | Preferential multihole combustor liner | Emerging Cross-Sectional Technologies | 36 | Expired |
| US6557350B2 | Method and apparatus for cooling gas turbine engine igniter tubes | Mechanical Engineering; Lighting; Heating | 31 | Expired |
| US6672067B2 | Corrugated cowl for combustor of a gas turbine engine and method for configuring same | Mechanical Engineering; Lighting; Heating | 30 | Expired |
| US6655146B2 | Hybrid film cooled combustor liner | Emerging Cross-Sectional Technologies | 29 | Expired |
| US6553767B2 | Gas turbine combustor liner with asymmetric dilution holes machined from a single piece form | Emerging Cross-Sectional Technologies | 26 | Expired |
| US6148600A | One-piece sheet metal cowl for combustor of a gas turbine engine and method of configuring same | Mechanical Engineering; Lighting; Heating | 24 | Expired |
| US6345441B1 | Method of repairing combustion chamber liners | Emerging Cross-Sectional Technologies | 24 | Expired |
| US6655147B2 | Annular one-piece corrugated liner for combustor of a gas turbine engine | Mechanical Engineering; Lighting; Heating | 23 | Expired |
| US6408610B1 | Method of adjusting gas turbine component cooling air flow | Emerging Cross-Sectional Technologies | 22 | Expired |
| US7216485B2 | Adjusting airflow in turbine component by depositing overlay metallic coating | Emerging Cross-Sectional Technologies | 22 | Expired |
| US6663919B2 | Process of removing a coating deposit from a through-hole in a component and component processed thereby | Emerging Cross-Sectional Technologies | 22 | Expired |
| US6568079B2 | Methods for replacing combustor liner panels | Emerging Cross-Sectional Technologies | 19 | Expired |
| US6620457B2 | Method for thermal barrier coating and a liner made using said method | Emerging Cross-Sectional Technologies | 18 | Expired |
| US6725667B2 | Combustor dome for gas turbine engine | Mechanical Engineering; Lighting; Heating | 18 | Expired |
| US6286302A | Venturi for use in the swirl cup package of a gas turbine combustor having water injected therein | Mechanical Engineering; Lighting; Heating | 11 | Expired |
| US6651437B2 | Combustor liner and method for making thereof | Performing Operations; Transporting | 11 | Expired |
| US6908657B2 | Coated component with through-hole having improved surface finish | Emerging Cross-Sectional Technologies | 11 | Expired |
| US6779268B1 | Outer and inner cowl-wire wrap to one piece cowl conversion | Emerging Cross-Sectional Technologies | 10 | Expired |
| US7222488B2 | Fabricated cowl for double annular combustor of a gas turbine engine | Mechanical Engineering; Lighting; Heating | 10 | Expired |
| US6592287B1 | Self-fixtured joint assembly and its preparation | Emerging Cross-Sectional Technologies | 7 | Expired |
| US6254997A | Article with metallic surface layer for heat transfer augmentation and method for making | Emerging Cross-Sectional Technologies | 7 | Expired |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.