Inventor · disambiguated record
Imon-Kalyan Bagchi
Also filed as: BAGCHI IMON KALYAN
10 granted patents·5 pending applications·51 citations·filing 2008–2022
86Inventor score
Files withROLLS ROYCE PLC9BAGCHI IMON-KALYAN2RACKWITZ LEIF2ROLLS ROYCE DEUTSCHLAND1ROLLS ROYCE DEUTSCHLAND LTD & CO KG1
Top patents by PatentIndex Score
15 records- 0195US11353215B1Lean burn combustorROLLS ROYCE PLC·Filed 2021·Granted Jun 7, 2022·5 cites·19 claims
- 0294US8646275B2Gas-turbine lean combustor with fuel nozzle with controlled fuel inhomogeneityRACKWITZ LEIF·Filed 2012·Granted Feb 11, 2014·25 cites·18 claims
- 0392US11402099B2Combustor with improved aerodynamicsROLLS ROYCE PLC·Filed 2021·Granted Aug 2, 2022·2 cites·20 claims
- 0492US11339970B1Combustor with improved aerodynamicsROLLS ROYCE PLC·Filed 2021·Granted May 24, 2022·2 cites·20 claims
- 0589US9335048B2Combustion chamber of a gas turbineROLLS ROYCE DEUTSCHLAND·Filed 2015·Granted May 10, 2016·6 cites·15 claims
- 0674US11280493B2Fuel spray nozzle for gas turbine engineROLLS ROYCE PLC·Filed 2019·Granted Mar 22, 2022·2 cites·13 claims
- 0774US8943829B2Lean premix burner of a gas-turbine engine provided with a flow-guiding elementBAGCHI IMON-KALYAN·Filed 2011·Granted Feb 3, 2015·6 cites·11 claims
- 0873US11339967B2Fuel injectorROLLS ROYCE PLC·Filed 2020·Granted May 24, 2022·1 cites·12 claims
- 0972US11603993B2Combustor with improved aerodynamicsROLLS ROYCE PLC·Filed 2022·Granted Mar 14, 2023·0 cites·20 claims
- 1059US8943828B2Lean premix burner of a gas-turbine engine provided with a concentric annular central bodyBAGCHI IMON-KALYAN·Filed 2011·Granted Feb 3, 2015·2 cites·7 claims
- 1159US2009139240A1Gas-turbine lean combustor with fuel nozzle with controlled fuel inhomogeneityRACKWITZ LEIF·Filed 2008·Application pending·0 cites
- 1246US2023015929A1Lean burn injector with supply line switchingROLLS ROYCE PLC·Filed 2022·Application pending·0 cites
- 1346US2014360202A1Fuel injector and a combustion chamberROLLS ROYCE PLC·Filed 2014·Application pending·0 cites
- 1444US2017299183A1Method for operating a lean premix burner of an aircraft gas turbine and device for carrying out the methodROLLS ROYCE DEUTSCHLAND LTD & CO KG·Filed 2013·Application pending·0 cites
- 1537US2017356653A1Combustion chamberROLLS ROYCE PLC·Filed 2017·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →