Inventor
Nicholas Joseph Kray
Inventor
Mason, OH, US
Overview
Patents· 89 as inventor
Public. Assignee & technology derived from the patent record. Each patent links to its LexDana page.
F01Dprimary
F01DNon-positive displacement machines or engines, e.g. steam turbines20%
F05DIndexing scheme for aspects relating to non-positive-displacement machines or engines, gas-turbines or jet-propulsion plants18%
Y02TClimate change mitigation technologies related to transportation15%
F04DNon-positive-displacement pumps12%
F02CGas-turbine plants4%
B29CShaping or joining of plastics4%
Y10TTechnical subjects covered by former us classification4%
F02KJet-propulsion plants3%
B29LIndexing scheme associated with subclass b29c, relating to particular articles2%
B63HMarine propulsion or steering2%
PatentTitleYear
11,131,247Additively manufactured rotating shaft202111,111,815Frangible gas turbine engine airfoil with fusion cavities202111,052,982Apparatus for dovetail chord relief for marine propeller202111,053,848Additively manufactured booster splitter with integral heating passageways202111,047,058Method for manufacturing leading edge guard202110,938,328Harvesting energy from composite aircraft engine components202110,927,703Circumferentially varying thickness composite fan casing202110,920,607Metallic compliant tip fan blade202110,920,595Turbine component having multiple controlled metallic grain orientations, apparatus and manufacturing method thereof202110,837,457Composite blade root stress reducing shim202010,837,286Frangible gas turbine engine airfoil with chord reduction202010,830,067Mechanical airfoil morphing with internal mechanical structures202010,815,798Turbine engine blade with leading edge strip202010,815,795Pre-tension and retention structure for composite fan blade202010,815,816Containment case active clearance control structure202010,788,053Noise reducing gas turbine engine airfoil202010,760,428Frangible gas turbine engine airfoil202010,751,958Composite woven outlet guide vane with optional hollow airfoil202010,746,045Frangible gas turbine engine airfoil including a retaining member202010,738,630Platform apparatus for propulsion rotor202010,724,376Airfoil having integral fins202010,703,452Apparatus and system for propeller blade aft retention202010,704,414Airfoil containment structure including a notched and tapered inner shell202010,697,470Containment case trench filler layer and method of containing releasable components from rotatable machines202010,689,073Apparatus and system for marine propeller blade dovetail stress reduction202010,677,260Turbine engine and method of manufacturing202010,677,259Apparatus and system for composite fan blade with fused metal lead edge202010,677,261Turbine engine and containment assembly for use in a turbine engine202010,662,813Turbine engine and containment assembly for use in a turbine engine202010,633,067Method and system for improving flow characteristics in marine propellers202010,612,560Composite airfoil with fuse architecture202010,589,475Braided blades and vanes having dovetail roots202010,557,350I beam blade platform202010,546,078Turbofan case for controlling blade deflection202010,539,025Airfoil assembly with leading edge element202010,519,788Composite airfoil metal patch201910,502,086System and method for actuating gas turbine engine components using integrated jamming devices201910,486,785Propeller assembly and method of assembling201910,450,870Frangible gas turbine engine airfoil201910,436,061Tapered composite backsheet for use in a turbine engine containment assembly201910,422,348Unsymmetrical turbofan abradable grind for reduced rub loads201910,422,340Composite booster spool with separable composite blades201910,371,097Non-Newtonian materials in aircraft engine airfoils201910,328,639Method and system for variable heat sources for composite fiber placement201910,323,532Flow discourager and method of making same201910,196,898Turbine airfoil with passive morphing structure201910,145,382Method and system for separable blade platform retention clip201810,125,619Rotor assembly for use in a turbofan engine and method of assembling201810,099,434Composite airfoil structures201810,062,202System and methods of generating a computer model of a composite component201810,047,763Rotor assembly for use in a turbofan engine and method of assembling201810,041,354Blade and method for manufacturing blade20189,976,429Composite disk20189,885,244'Metal leading edge protective strips for airfoil components and method therefor'20189,868,259'Fiber placement machine roller with vacuum assisted tow handling'20189,797,257'Attachment of composite article'20179,777,579'Attachment of composite article'20179,777,593'Hybrid metal and composite spool for rotating machinery'20179,745,851'Metal leading edge on composite blade airfoil and shank'20179,682,756'System for composite marine propellers'20179,475,218'Apparatus and method for forming flanges on components'20169,399,922'Non-integral fan blade platform'20169,297,257'Spinner assembly with removable fan blade leading edge fairings'20169,239,062'Low radius ratio fan for a gas turbine engine'20169,121,294'Fan blade with composite core and wavy wall trailing edge cladding'20159,085,989'Airfoils including compliant tip'20159,040,138'Composite article including composite to metal interlock and method of fabrication'20158,974,656'Method for roughening metal surfaces and article manufactured thereby'20158,905,719'Composite rotor and vane assemblies with integral airfoils'20148,777,576'Metallic fan blade platform'20148,763,753'Acoustic panel and method of forming'20148,662,834'Method for reducing tip rub loading'20148,657,570'Rotor blade with reduced rub loading'20148,632,327'Apparatus to apply a variable surface texture on an airfoil'20148,457,937'Method of optimizing volume utilization of an autoclave'20138,240,210'Method and system for multimodal inspection with a coordinate measuring device'20128,205,500'Systems and methods for inspecting an object using ultrasound'20128,179,132'Method and system for integrating eddy current inspection with a coordinate measuring device'20128,123,463'Method and system for manufacturing a blade'20128,020,308'Non-destructive inspection system having self-aligning probe assembly'20118,011,877'Fiber composite reinforced aircraft gas turbine engine drums with radially inwardly extending blades'20117,976,694'Apparatus and method for hybrid machining a contoured, thin-walled workpiece'20117,972,109'Methods and apparatus for fabricating a fan assembly for use with turbine engines'20117,921,575'Method and system for integrating ultrasound inspection (UT) with a coordinate measuring machine (CMM)'20117,780,410'Method and apparatus for gas turbine engines'20106,773,234'Methods and apparatus for facilitating preventing failure of gas turbine engine blades'20046,290,465'Rotor blade'20015,435,694'Stress relieving mount for an axial blade'19955,310,318'Asymmetric axial dovetail and rotor disk'1994Career & activity timeline
Assembled from patent assignee/location history and declaration credentials.
1994–2021Patents assigned to GEN ELECTRIC (89)· patent assignee history
1994–2018Based in Cincinnati, OH, US· patent location history
2001–2018Based in Blue Ash, OH, US· patent location history
2012–2018Patents assigned to KRAY NICHOLAS JOSEPH (15)· patent assignee history
2012Patents assigned to WU YANYAN (3)· patent assignee history
2012Patents assigned to BATZINGER THOMAS JAMES (2)· patent assignee history
2014–2015Patents assigned to SHIM DONG-JIN (3)· patent assignee history
2014–2021Based in Mason, OH, US· patent location history
2019–2021Based in West Chester, OH, US· patent location history
Inventor activity
Assignee and location history derived from the patent record.
Assignees
| Assignee | Patents | Span |
|---|---|---|
| GEN ELECTRIC | 89 | 1994–2021 |
| KRAY NICHOLAS JOSEPHself | 15 | 2012–2018 |
| SHIM DONG-JIN | 3 | 2014–2015 |
| WU YANYAN | 3 | 2012 |
| BATZINGER THOMAS JAMES | 2 | 2012 |
Locations
| Location | Patents | Span |
|---|---|---|
| Mason, OH, US | 61 | 2014–2021 |
| Blue Ash, OH, US | 11 | 2001–2018 |
| Cincinnati, OH, US | 9 | 1994–2018 |
| West Chester, OH, US | 8 | 2019–2021 |