Phoenix, Arizona
United States
94
2021-12-02
The entities that hold a legal rights for patent applications filed by inventor Morris Mark C.:
Mark C. Morris from Phoenix, US has applied for patents for these inventions. The list has both pending applications and granted patents:
TURBINE NOZZLE WITH REDUCED LEAKAGE FEATHER SEALS
#2 | 2021-07-29Engine components with cooling holes having tailored metering and diffuser portions
#3 | 2021-06-10Turbine vane with dust tolerant cooling system
#4 | 2021-06-10Turbine vane with dust tolerant cooling system
#5 | 2020-12-03Turbine blade with dust tolerant cooling system
#6 | 2020-10-08Turbine nozzle with reduced leakage feather seals
#7 | 2020-07-30Gas turbine engines including tangential on-board injectors and methods for manufacturing the same
#8 | 2020-05-07Methods for processing bonded dual alloy rotors including differential heat treatment processes
#9 | 2020-02-13Prime surface heat exchanger with contoured separator members
#10 | 2020-01-16Turbine blade with dust tolerant cooling system
#11 | 2020-01-16Turbine vane with dust tolerant cooling system
#12 | 2019-12-19Heat exchanger with interspersed arrangement of cross-flow structures
#13 | 2019-08-22METHODS FOR ADDITIVELY MANUFACTURING TURBINE ENGINE COMPONENTS VIA BINDER JET PRINTING WITH GAMMA PRIME PRECIPITATION HARDENED NICKEL-BASED SUPERALLOYS
#14 | 2019-08-22METHODS FOR ADDITIVELY MANUFACTURING TURBINE ENGINE COMPONENTS VIA BINDER JET PRINTING WITH TITANIUM ALUMINIDE ALLOYS
#15 | 2019-08-15METHODS FOR ADDITIVELY MANUFACTURING TURBINE ENGINE COMPONENTS VIA BINDER JET PRINTING WITH NICKEL-CHROMIUM-TUNGSTEN-MOLYBDENUM ALLOYS
#16 | 2019-06-20Gas turbine engines with airfoils having improved dust tolerance
#17 | 2019-03-28Prime surface heat exchanger with contoured separator members
#18 | 2019-03-28Heat exchanger with interspersed arrangement of cross-flow structures
#19 | 2018-12-06NICKEL-BASED SUPERALLOY COMPONENTS AND ADDITIVE MANUFACTURING PROCESSES USING NICKEL-BASED SUPERALLOYS
#20 | 2018-12-06ADDITIVE MANUFACTURING PROCESSES USING NICKEL-BASED SUPERALLOYS
#21 | 2018-12-06Surface improvement of additively manufactured articles produced with aluminum alloys
#22 | 2018-12-06Surface improvement of additively manufactured articles produced with aluminum alloys
#23 | 2018-03-01Methods for directionally recrystallizing additively-manufactured metallic articles by heat treatment with a gradient furnace
#24 | 2017-11-23Engine components with cooling holes having tailored metering and diffuser portions
#25 | 2017-09-21Methods for processing bonded dual alloy rotors including differential heat treatment processes
#26 | 2017-06-15Heat exchanger designs using variable geometries and configurations
#27 | 2017-05-11Surface improvement of additively manufactured articles produced with aluminum alloys
#28 | 2017-01-26Hybrid bonded turbine rotors and methods for manufacturing the same
#29 | 2017-01-12Turbine engine couplings and methods for manufacturing turbine engine couplings
#30 | 2016-12-01NICKEL-BASED SUPERALLOYS AND ADDITIVE MANUFACTURING PROCESSES USING NICKEL-BASED SUPERALLOYS
#31 | 2016-05-26HYBRID BONDED TURBINE ROTORS AND METHODS FOR MANUFACTURING THE SAME
#32 | 2016-02-25Methods for producing alloy forms from alloys containing one or more extremely reactive elements and for fabricating a component therefrom
#33 | 2015-12-17HEAT EXCHANGER DESIGNS USING VARIABLE GEOMETRIES AND CONFIGURATIONS
#34 | 2015-12-10Engine systems and methods for removing particles from turbine air
#35 | 2015-10-22Methods for forming ceramic reinforced titanium alloys
#36 | 2015-05-28Methods and systems for manufacturing components from articles formed by additive-manufacturing processes
#37 | 2015-04-30Counter-flow heat exchange systems
#38 | 2015-04-16Turbine rotor blades with tip portion parapet wall cavities
#39 | 2015-04-16Turbine rotor blades with improved tip portion cooling holes
#40 | 2015-04-02Methods for forming oxide dispersion-strengthened alloys
#41 | 2015-03-26Gas turbine engines with turbine airfoil cooling
#42 | 2015-03-19Gas turbine engines with turbine rotor blades having improved platform edges
#43 | 2015-02-19Vibration isolator assemblies and methods for the manufacture thereof
#44 | 2014-12-11Unitary heat exchangers having integrally-formed compliant heat exchanger tubes and heat exchange systems including the same
#45 | 2014-09-25Spring assemblies for use in gas turbine engines and methods for their manufacture
#46 | 2014-09-18Methods for forming dispersion-strengthened aluminum alloys
#47 | 2014-07-17Gas turbine engine components and methods for their manufacture using additive manufacturing techniques
#48 | 2014-04-10Gas turbine engine components with lateral and forward sweep film cooling holes
#49 | 2014-04-03Cooled turbine airfoil structures
#50 | 2014-03-27Gas turbine engine components with blade tip cooling
#51 | 2014-03-20Turbine stator airfoil assemblies and methods for their manufacture
#52 | 2014-03-06Non-destructive evaluation methods for aerospace components
#53 | 2014-02-27METHANE CONVERSION APPARATUS AND PROCESS USING A SUPERSONIC FLOW REACTOR
#54 | 2014-02-27METHANE CONVERSION APPARATUS AND PROCESS USING A SUPERSONIC FLOW REACTOR
#55 | 2014-02-27Methane Conversion Apparatus and Process Using a Supersonic Flow Reactor
#56 | 2014-02-06Methods for manufacturing titanium aluminide components from articles formed by consolidation processes
#57 | 2013-11-28Methods for manufacturing components from articles formed by additive-manufacturing processes
#58 | 2013-09-19Turbine blade tip cooling
#59 | 2013-09-12Tubular heat exchange systems
#60 | 2013-08-22Turbine stator airfoils with individual orientations
#61 | 2013-08-01Multi-material turbine components
#62 | 2013-03-21Methods for manufacturing components from articles formed by additive-manufacturing processes
#63 | 2013-03-21TURBINE BLADES AND METHODS OF FORMING MODIFIED TURBINE BLADES AND TURBINE ROTORS
#64 | 2013-03-14Gas turbine engines with improved trailing edge cooling arrangements
#65 | 2013-03-07Gas turbine engines with abradable turbine seal assemblies
#66 | 2013-01-03Methods for manufacturing engine components with structural bridge devices
#67 | 2012-09-06Methods for repairing turbine components
#68 | 2012-06-14TURBINE ROTOR DISKS AND TURBINE ASSEMBLIES
#69 | 2012-04-19Turbine blades and turbine rotor assemblies
#70 | 2012-01-05Turbine nozzles and methods of manufacturing the same
#71 | 2011-12-22Methods for manufacturing turbine components
#72 | 2011-12-08Impeller backface shroud for use with a gas turbine engine
#73 | 2011-06-09Method of fabricating turbine components for engines
#74 | 2011-05-26Seal plates for directing airflow through a turbine section of an engine and turbine sections
#75 | 2011-01-13Method of making turbine stator airfoils with individual orientations
#76 | 2010-11-11Turbine blades and methods of forming modified turbine blades and turbine rotors
#77 | 2010-09-16Turbine blade platform
#78 | 2010-05-27Method for detecting deviation in crystallographic orientation in a metal structure
#79 | 2010-05-20Turbine nozzles and methods of manufacturing the same
#80 | 2010-05-06Spacers and turbines
#81 | 2010-02-11Gas turbine engine assemblies with vortex suppression and cooling film replenishment
#82 | 2010-01-14Gas turbine engine assemblies with recirculated hot gas ingestion
#83 | 2009-12-24Gas turbine engine with improved thermal isolation
#84 | 2008-07-10Cooled turbine blade cast tip recess
#85 | 2008-03-06High effectiveness cooled turbine blade
#86 | 2008-01-03Method to modify an airfoil internal cooling circuit
#87 | 2007-10-11Diffuser particle separator
#88 | 2007-08-30Method to augment heat transfer using chamfered cylindrical depressions in cast internal cooling passages
#89 | 2006-04-13Method for modifying gas turbine nozzle area
#90 | 2005-12-13High effectiveness cooled turbine vane or blade
#91 | 2005-10-27Gas turbine engine including a low pressure sump seal buffer source and thermally isolated sump
#92 | 2005-06-23Variable turbine cooling flow system
#93 | 2005-06-16Gas turbine high temperature turbine blade outer air seal assembly
#94 | 2005-06-09Gas turbine cooled shroud assembly with hot gas ingestion suppression
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