Simpsonville, South Carolina
United States
77
2021-09-02
The entities that hold a legal rights for patent applications filed by inventor Itzel Gary Michael:
Gary Michael Itzel from Simpsonville, US has applied for patents for these inventions. The list has both pending applications and granted patents:
Impingement insert for a gas turbine engine
#2 | 2020-06-11Turbine component and methods of making and cooling a turbine component
#3 | 2020-05-07Turbine airfoil with multiple walls and internal thermal barrier coating
#4 | 2020-02-13Turbine component and methods of making and cooling a turbine component
#5 | 2019-10-10Turbine airfoil multilayer exterior wall
#6 | 2019-06-06Turbine component with tip rail cooling passage
#7 | 2018-11-29Turbomachine rotor blade pocket
#8 | 2018-08-16Gas turbine seals
#9 | 2018-07-05ARTICLE AND MANIFOLD FOR THERMAL ADJUSTMENT OF A TURBINE COMPONENT
#10 | 2018-07-05Components having channels for impingement cooling
#11 | 2018-05-31IMPINGEMENT INSERT FOR A GAS TURBINE ENGINE
#12 | 2018-02-01Turbine components and method for forming turbine components
#13 | 2018-01-18Turbomachine component having impingement heat transfer feature, related turbomachine and storage medium
#14 | 2017-12-07Turbine component and methods of making and cooling a turbine component
#15 | 2017-12-07Turbine component and methods of making and cooling a turbine component
#16 | 2017-12-07Nozzle cooling system for a gas turbine engine
#17 | 2017-12-07Turbine component and methods of making and cooling a turbine component
#18 | 2017-10-05Seal assembly to seal corner leaks in gas turbine
#19 | 2017-09-28Apparatus, turbine nozzle and turbine shroud
#20 | 2017-09-14CERAMIC MATRIX COMPOSITE COMPONENT, GAS TURBINE SEAL ASSEMBLY, AND METHOD OF FORMING CERAMIC MATRIX COMPOSITE COMPONENT
#21 | 2017-08-31Apparatus, turbine nozzle and turbine shroud
#22 | 2017-08-17Rotor Blade Trailing Edge Cooling
#23 | 2017-06-22Cooling circuit for a multi-wall blade
#24 | 2017-06-15ARTICLE AND METHOD OF FORMING AN ARTICLE
#25 | 2017-06-15Article and method of forming an article
#26 | 2017-06-15Article and method of cooling an article
#27 | 2017-05-11ARTICLE, COMPONENT, AND METHOD OF COOLING A COMPONENT
#28 | 2017-04-20Article and method of cooling an article
#29 | 2017-04-13Turbine nozzle with cooling channel coolant distribution plenum
#30 | 2017-04-13Turbine nozzle with cooling channel coolant discharge plenum
#31 | 2017-02-23Article and manifold for thermal adjustment of a turbine component
#32 | 2017-02-02Article, airfoil component and method for forming article
#33 | 2016-12-15Hot gas path component trailing edge having near wall cooling features
#34 | 2016-12-01Article, component, and method of forming an article
#35 | 2016-11-03Turbine airfoil turbulator arrangement
#36 | 2016-10-13TURBINE AIRFOIL
#37 | 2016-03-31TURBINE COMPONENTS WITH STEPPED APERTURES
#38 | 2015-03-05Method and system for controlling gas turbine performance with a variable backflow margin
#39 | 2015-01-08Shroud block segment for a gas turbine
#40 | 2014-11-20Seal system including angular features for rotary machine components
#41 | 2014-09-25Turbine airfoil assembly
#42 | 2014-06-12System and method for removing heat from a turbine
#43 | 2014-04-24Sealing arrangement for a turbine system and method of sealing between two turbine components
#44 | 2014-04-17HOT GAS PATH COMPONENT COOLING FILM HOLE PLATEAU
#45 | 2014-03-13BUCKET ASSEMBLY FOR TURBOMACHINE
#46 | 2014-03-06TURBINE ROTOR BLADE PLATFORM COOLING
#47 | 2014-02-06Systems and apparatus relating to seals for turbine engines
#48 | 2013-08-01Turbomachine passage cleaning system
#49 | 2013-07-04Turbine and method for separating particulates from a fluid
#50 | 2013-05-09Film hole trench
#51 | 2013-05-09Rotating airfoil component of a turbomachine
#52 | 2013-04-18SYSTEM FOR SEALING A SHAFT
#53 | 2013-03-14METHOD OF CONTROLLING TEMPERATURE OF GAS TURBINE COMPONENTS USING A COMPRESSED MOISURIZED COOLANT
#54 | 2013-02-28Bucket assembly treating apparatus and method for treating bucket assembly
#55 | 2012-12-20Hot gas path component
#56 | 2012-07-05Turbomachine airfoil component and cooling method therefor
#57 | 2012-05-10System and method for cooling a turbine bucket
#58 | 2012-03-29Turbine airfoil and method for cooling a turbine airfoil
#59 | 2011-10-27Hot gas path component cooling system
#60 | 2011-09-29Airfoil cooling hole flag region
#61 | 2011-09-29Bimetallic spline seal
#62 | 2011-09-15Apparatus for cooling a platform of a turbine component
#63 | 2011-05-12HEAT SHIELD
#64 | 2010-11-11TURBINE NOZZLE WITH SIDEWALL COOLING PLENUM
#65 | 2010-07-15Turbine bucket angel wing compression seal
#66 | 2010-03-04Turbine bucket for a turbomachine and method of reducing bow wave effects at a turbine bucket
#67 | 2009-10-01FILM COOLING OF TURBINE COMPONENTS
#68 | 2009-04-02Turbine airfoil concave cooling passage using dual-swirl flow mechanism and method
#69 | 2008-12-04Shroud configuration having sloped seal
#70 | 2008-01-17Coated bucket damper pin
#71 | 2007-09-27Steam-cooled gas turbine bucker for reduced tip leakage loss
#72 | 2007-08-16Methods and apparatus for cooling gas turbine rotor blades
#73 | 2007-05-24Gas turbine bucket with cooled platform leading edge and method of cooling platform leading edge
#74 | 2006-12-21Turbine bucket tip cap
#75 | 2006-11-16Coated bucket damper pin and related method
#76 | 2006-05-25Controlled leakage pin and vibration damper for active cooling and purge of bucket slash faces
#77 | 2006-05-25Thermal barrier coating for turbine bucket platform side faces and methods of application
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