Inventor · disambiguated record
Mrinal Munshi
Also filed as: MUNSHI MRINAL
12 granted patents·9 pending applications·81 citations·filing 2010–2016
90Inventor score
Top patents by PatentIndex Score
21 records- 0188US9630277B2Airfoil having built-up surface with embedded cooling passageLEE CHING-PANG·Filed 2010·Granted Apr 25, 2017·12 cites·18 claims
- 0287US8608443B2Film cooled component wall in a turbine engineLEE CHING-PANG·Filed 2010·Granted Dec 17, 2013·11 cites·20 claims
- 0386US10094285B2Gas turbine outer case active ambient cooling including air exhaust into sub-ambient cavityMUNSHI MRINAL·Filed 2013·Granted Oct 9, 2018·13 cites·18 claims
- 0485US9186757B2Method of providing a turbine blade tip repairMUNSHI MRINAL·Filed 2012·Granted Nov 17, 2015·13 cites·20 claims
- 0583US9181819B2Component wall having diffusion sections for cooling in a turbine engineLEE CHING-PANG·Filed 2010·Granted Nov 10, 2015·9 cites·18 claims
- 0683US8894359B2Gas turbine engine with outer case ambient external cooling systemMUNSHI MRINAL·Filed 2011·Granted Nov 25, 2014·10 cites·20 claims
- 0776US8939717B1Vane outer support ring with no forward hook in a compressor section of a gas turbine engineLEE CHING-PANG·Filed 2013·Granted Jan 27, 2015·4 cites·15 claims
- 0864US9206700B2Outer vane support ring including a strong back plate in a compressor section of a gas turbine engineLEE CHING-PANG·Filed 2013·Granted Dec 8, 2015·3 cites·18 claims
- 0963US9664062B2Gas turbine engine with multiple component exhaust diffuser operating in conjunction with an outer case ambient external cooling systemMUNSHI MRINAL·Filed 2013·Granted May 30, 2017·3 cites·10 claims
- 1052US9102014B2Method of servicing an airfoil assembly for use in a gas turbine engineGEORGIEVA PETYA M·Filed 2010·Granted Aug 11, 2015·1 cites·19 claims
- 1148US9470102B2Crack resistant turbine vane and method for vane containment cap attachmentSIEMENS ENERGY INC·Filed 2014·Granted Oct 18, 2016·1 cites·19 claims
- 1245US2013302166A1Turbine blade with chamfered squealer tip formed from multiple components and convective cooling holesLEE CHING-PANG·Filed 2012·Application pending·0 cites
- 1343US2015044046A1Manufacturing method for strut shield collar of gas turbine exhaust diffuserSHTEYMAN YEVGENIY·Filed 2013·Application pending·0 cites
- 1442US2015275682A1Sprayed haynes 230 layer to increase spallation life of thermal barrier coating on a gas turbine engine componentSIEMENS ENERGY INC·Filed 2014·Application pending·0 cites
- 1541US2015040393A1Manufacturing method for exhaust diffuser shell with strut shield collar and joint flangeSHTEYMAN YEVGENIY·Filed 2013·Application pending·0 cites
- 1640US2016131045A1Emissions control system for a gas turbine engineSIEMENS ENERGY INC·Filed 2014·Application pending·0 cites
- 1739US9458737B2Adjustable bracing apparatus and assembly method for gas turbine exhaust diffuserROTH DOUGLAS R·Filed 2013·Granted Oct 4, 2016·1 cites·15 claims
- 1838US2015301510A1Controlling a Target SystemDÜLL SIEGMUND·Filed 2014·Application pending·0 cites
- 1938US2015044039A1Exhaust diffuser shell with flange and manufacturing methodSHTEYMAN YEVGENIY·Filed 2013·Application pending·0 cites
- 2037US2013149107A1Gas turbine outer case active ambient cooling including air exhaust into a sub-ambient region of exhaust flowMUNSHI MRINAL·Filed 2013·Application pending·0 cites
- 2136US2017038750A1Method, controller, and computer program product for controlling a target systemSIEMENS AG·Filed 2016·Application pending·0 cites
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