Harris Shafique
28Patents
10h-index
26Co-inventors
75Inventor score
Filing activity: Oct 29, 1997 → Sep 30, 2019
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US6141968A | Fuel nozzle for gas turbine engine with slotted fuel conduits and cover | Mechanical Engineering; Lighting; Heating | 45 | Expired |
| US6289676A | Simplex and duplex injector having primary and secondary annular lud channels and primary and secondary lud nozzles | Mechanical Engineering; Lighting; Heating | 44 | Expired |
| US7481248B2 | Flexible heat shields and method | Mechanical Engineering; Lighting; Heating | 27 | Active |
| US7028484B2 | Nested channel ducts for nozzle construction and the like | Mechanical Engineering; Lighting; Heating | 26 | Expired |
| US7654088B2 | Dual conduit fuel manifold for gas turbine engine | Mechanical Engineering; Lighting; Heating | 18 | Expired |
| US8099227B2 | Control of gas turbine engine | Emerging Cross-Sectional Technologies | 16 | Active |
| US6823677B2 | Stress relief feature for aerated gas turbine fuel injector | Mechanical Engineering; Lighting; Heating | 15 | Expired |
| US7533531B2 | Internal fuel manifold with airblast nozzles | Mechanical Engineering; Lighting; Heating | 15 | Active |
| US7559202B2 | Reduced thermal stress fuel nozzle assembly | Mechanical Engineering; Lighting; Heating | 13 | Active |
| US7721436B2 | Method of manufacturing a metal injection moulded combustor swirler | Emerging Cross-Sectional Technologies | 12 | Active |
| US7530231B2 | Fuel conveying member with heat pipe | Mechanical Engineering; Lighting; Heating | 10 | Active |
| US7658339B2 | Modular fuel nozzle air swirler | Mechanical Engineering; Lighting; Heating | 10 | Active |
| US8167572B2 | Dynamically tuned turbine blade growth pocket | Emerging Cross-Sectional Technologies | 9 | Active |
| US8074452B2 | Nested channel ducts for nozzle construction and the like | Mechanical Engineering; Lighting; Heating | 8 | Active |
| US7738694B2 | Calibration of optical patternator spray parameter measurements | Physics | 7 | Active |
| US7559201B2 | Redundant fuel manifold sealing arrangement | Mechanical Engineering; Lighting; Heating | 7 | Active |
| US7716933B2 | Multi-channel fuel manifold | Mechanical Engineering; Lighting; Heating | 7 | Active |
| US7497012B2 | Gas turbine fuel nozzle manufacturing | Emerging Cross-Sectional Technologies | 7 | Active |
| US8886438B2 | Control of gas turbine engine | Emerging Cross-Sectional Technologies | 6 | Active |
| US7937926B2 | Integral heater for fuel conveying member | Mechanical Engineering; Lighting; Heating | 5 | Active |
| US8038411B2 | Compressor turbine blade airfoil profile | Emerging Cross-Sectional Technologies | 4 | Active |
| US9382849B2 | Control of gas turbine engine | Emerging Cross-Sectional Technologies | 3 | Active |
| US7565807B2 | Heat shield for a fuel manifold and method | Mechanical Engineering; Lighting; Heating | 3 | Active |
| US8538658B2 | Control of gas turbine engine | Emerging Cross-Sectional Technologies | 3 | Active |
| US8276387B2 | Gas turbine engine fuel conveying member | Mechanical Engineering; Lighting; Heating | 2 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.