Bruno Schuermans
32Patents
9h-index
53Co-inventors
74Inventor score
Filing activity: Jan 30, 2002 → May 30, 2018
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US6981358B2 | Reheat combustion system for a gas turbine | Mechanical Engineering; Lighting; Heating | 121 | Expired |
| US8029273B2 | Burner | Mechanical Engineering; Lighting; Heating | 73 | Active |
| US7198483B2 | Burner unit and method for operation thereof | Mechanical Engineering; Lighting; Heating | 18 | Expired |
| US7457710B2 | Apparatus and method for testing combustion | Physics | 17 | Expired |
| US8991185B2 | Combustion device for a gas turbine configured to suppress thermo-acoustical pulsations | Mechanical Engineering; Lighting; Heating | 15 | Active |
| US10546070B2 | Simultaneous broadband damping at multiple locations in a combustion chamber | Mechanical Engineering; Lighting; Heating | 15 | Active |
| US7484352B2 | Combustor for a gas turbine | Mechanical Engineering; Lighting; Heating | 12 | Active |
| US8931589B2 | Damper arrangement and method for designing same | Mechanical Engineering; Lighting; Heating | 10 | Active |
| US8727070B2 | Helmholtz damper and method for regulating the resonance frequency of a Helmholtz damper | Emerging Cross-Sectional Technologies | 9 | Active |
| US10228138B2 | System and apparatus for gas turbine combustor inner cap and resonating tubes | Mechanical Engineering; Lighting; Heating | 8 | Active |
| US8839624B2 | Combustion device of a gas turbine including a plurality of passages and chambers defining helmholtz resonators | Mechanical Engineering; Lighting; Heating | 6 | Active |
| US7137809B2 | Method for the production of a burner unit | Mechanical Engineering; Lighting; Heating | 6 | Expired |
| US7901203B2 | Combustion chamber | Mechanical Engineering; Lighting; Heating | 5 | Active |
| US10221769B2 | System and apparatus for gas turbine combustor inner cap and extended resonating tubes | Mechanical Engineering; Lighting; Heating | 5 | Active |
| US9285123B2 | Burner system with staged fuel injection | Mechanical Engineering; Lighting; Heating | 5 | Active |
| US10330319B2 | Sequential combustion with dilution gas mixer | Emerging Cross-Sectional Technologies | 4 | Active |
| US8205714B2 | Method for adjusting a Helmholtz resonator and an adjustable Helmholtz resonator | Mechanical Engineering; Lighting; Heating | 3 | Active |
| US9970659B2 | Damper for combustion oscillation damping in a gas turbine | Mechanical Engineering; Lighting; Heating | 3 | Active |
| US9857079B2 | Combustion device for a gas turbine | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US7424804B2 | Premix burner | Mechanical Engineering; Lighting; Heating | 2 | Expired |
| US9068512B2 | Method for protecting a gas turbine engine against high dynamical process values and gas turbine engine for conducting the method | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US9528898B2 | Probe for measuring pressure oscillations in the combustor of a gas turbine | Physics | 1 | Active |
| US11041625B2 | Fuel nozzle with narrow-band acoustic damper | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US10145558B2 | Method for determining the temperature inside a combustor | Emerging Cross-Sectional Technologies | 1 | Active |
| US10247420B2 | Axially staged mixer with dilution air injection | Mechanical Engineering; Lighting; Heating | 1 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.