Inventor
Melvin Robert Jackson
Inventor
Niskayuna, NY, US
Overview
168→
Patents
1977–2012
Patent span
General tagging of new technological developments
Primary field (CPC Y)
Patents· 168 as inventor
Public. Assignee & technology derived from the patent record. Each patent links to its LexDana page.
Y10Tprimary
Y10TTechnical subjects covered by former us classification17%
C22CAlloys14%
C23CCoating metallic material10%
Y02TClimate change mitigation technologies related to transportation10%
F01DNon-positive displacement machines or engines, e.g. steam turbines9%
F05DIndexing scheme for aspects relating to non-positive-displacement machines or engines, gas-turbines or jet-propulsion plants7%
B23PMetal-working not otherwise provided for5%
B23KSoldering or unsoldering4%
B22DCasting of metals3%
B22FWorking metallic powder3%
PatentTitleYear
8,153,052'High-temperature composite articles and associated methods of manufacture'20127,931,759'Metal alloy compositions and articles comprising the same'20117,910,158'Method for fabricating an array of electrode and electrolyte materials for use in solid oxide fuel cells'20117,811,396'Method for HVOF or LPPS restoration coating repair of a nickel-base superalloy article'20107,745,029'Ferritic steels for solid oxide fuel cells and other high temperature applications'20107,727,318'Metal alloy compositions and articles comprising the same'20107,722,729'Method for repairing high temperature articles'20107,704,335'Refractory metal intermetallic composites based on niobium-silicides, and related articles'20107,654,734'Methods and devices for evaluating the thermal exposure of a metal article'20107,651,023'Nickel-based braze alloy compositions and related processes and articles'20107,622,150'Oxidation resistant coatings for molybdenum silicide-based composite articles'20097,575,042'Methods for the formation of refractory metal intermetallic composites, and related articles and compositions'20097,494,619'High temperature alloys, and articles made and repaired therewith'20097,392,927'Combinatorial production of material compositions from a single sample'20087,360,437'Devices for evaluating material properties, and related processes'20087,358,674'Structure having electrodes with metal core and coating'20087,351,290'Robotic pen'20087,332,123'Method for manufacturing composite articles and the articles obtained therefrom'20087,329,471'Methods and apparatus for assembling solid oxide fuel cells'20087,189,459'Turbine blade for extreme temperature conditions'20077,004,622'Systems and methods for determining conditions of articles and methods of making such systems'20066,982,123'Method for repair of a nickel-base superalloy article using a thermally densified coating'20066,982,059'Rhodium, platinum, palladium alloy'20066,974,636'Protective coating for turbine engine component'20056,921,586'Ni-Base superalloy having a coating system containing a diffusion barrier layer'20056,913,655'Niobium-silicide based composities resistant to high temperature oxidation'20056,908,288'Repair of advanced gas turbine blades'20056,905,559'Nickel-base superalloy composition and its use in single-crystal articles'20056,861,157'Article for high temperature service and method for manufacture'20056,849,299'Apparatus and method for introducing small amounts of refractory elements into a vapor deposition coating'20056,838,190'Article with intermediate layer and protective layer, and its fabrication'20056,837,687'Foil formed structure for turbine airfoil'20056,767,653'Coatings, method of manufacture, and the articles derived therefrom'20046,746,782'Diffusion barrier coatings, and related articles and processes'20046,726,444'Hybrid high temperature articles and method of making'20046,720,088'Materials for protection of substrates at high temperature, articles made therefrom, and method for protecting substrates'20046,689,199'Apparatus and method for introducing small amounts of refractory elements into a vapor deposition coating'20046,676,381'Method and apparatus for casting near-net shape articles'20046,644,917'Smart coating system with chemical taggants for coating condition assessment'20036,645,560'Oxidation resistant coatings for niobium-based silicide composites'20036,640,546'Foil formed cooling area enhancement'20036,634,860'Foil formed structure for turbine airfoil tip'20036,623,692'Rhodium-based alloy and articles made therefrom'20036,616,410'Oxidation resistant and/or abrasion resistant squealer tip and method for casting same'20036,615,470'System and method for repairing cast articles'20036,609,894'Airfoils with improved oxidation resistance and manufacture and repair thereof'20036,607,847'Bonded niobium silicide and molybdenum silicide composite articles using brazes'20036,586,118'Bonded niobium silicide and molybdenum silicide composite articles using semi-solid brazes'20036,582,534'High-temperature alloy and articles made therefrom'20036,575,702'Airfoils with improved strength and manufacture and repair thereof'20036,565,680'Superalloy weld composition and repaired turbine engine component'20036,565,989'Bonded niobium silicide and molybdenum silicide composite articles using germanium and silicon based brazes'20036,565,990'Bonded niobium silicide and molybdenum silicide composite articles and method of manufacture'20036,562,483'Method for improving the oxidation-resistance of metal substrates coated with thermal barrier coatings'20036,554,920'High-temperature alloy and articles made therefrom'20036,551,063'Foil formed structure for turbine airfoil trailing edge'20036,521,356'Oxidation resistant coatings for niobium-based silicide composites'20036,497,968'Oxidation resistant coatings for molybdenum silicide-based composite articles'20026,475,642'Oxidation-resistant coatings, and related articles and processes'20026,468,367'Superalloy weld composition and repaired turbine engine component'20026,468,040'Environmentally resistant squealer tips and method for making'20026,465,755'Manufacture of repair material and articles repaired with the material'20026,447,623'Creep resistant Nb-silicide based two-phase composites'20026,444,331'Roughened bond coats for a thermal barrier coating system and method for producing'20026,428,910'Nb-based silicide composite compositions'20026,419,765'Niobium-silicide based composites resistant to low temperature pesting'20026,413,650'Method for repairing superalloy castings using a metallurgically bonded tapered plug'20026,409,848'Creep resistant Nb-silicide based multiphase composites'20026,387,193'Repair material, process of repairing using the repair material, and article repaired'20026,372,299'Method for improving the oxidation-resistance of metal substrates coated with thermal barrier coatings'20026,368,727'Roughened bond coat for a thermal barrier coating system and method for producing'20026,361,878'Roughened bond coat and method for producing using a slurry'20026,354,799'Superalloy weld composition and repaired turbine engine component'20026,321,449'Method of forming hollow channels within a component'20016,306,524'Diffusion barrier layer'20016,302,649'Superalloy weld composition and repaired turbine engine component'20016,300,588'Manufacture of repair material and articles repaired with the material'20016,287,644'Continuously-graded bond coat and method of manufacture'20016,264,766'Roughened bond coats for a thermal barrier coating system and method for producing'20016,242,050'Method for producing a roughened bond coat using a slurry'20016,214,248'Method of forming hollow channels within a component'20016,210,635'Repair material'20016,199,746'Method for preparing superalloy castings using a metallurgically bonded tapered plug'20016,190,467'Repair alloy compositions'20016,168,871'Method of forming high-temperature components and components formed thereby'20016,136,453'Roughened bond coat for a thermal barrier coating system and method for producing'20006,027,584'Repair alloy compositions'20006,001,492'Graded bond coat for a thermal barrier coating system'19995,960,249'Method of forming high-temperature components and components formed thereby'19995,942,055'Silicide composite with niobium-based metallic phase and silicon-modified Laves-type phase'19995,932,033'Silicide composite with niobium-based metallic phase and silicon-modified laves-type phase'19995,933,699'Method of making double-walled turbine components from pre-consolidated assemblies'19995,912,087'Graded bond coat for a thermal barrier coating system'19995,904,201'Solidification of an article extension from a melt using a ceramic mold'19995,900,283'Method for providing a protective coating on a metal-based substrate and related articles'19995,858,558'Nickel-base sigma-gamma in-situ intermetallic matrix composite'19995,833,773'Nb-base composites'19985,822,852'Method for replacing blade tips of directionally solidified and single crystal turbine blades'19985,822,853'Method for making cylindrical structures with cooling channels'19985,820,337'Double wall turbine parts'19985,778,960'Method for providing an extension on an end of an article'19985,759,380'Method of preparing oxidation resistant coatings'19985,743,322'Method for forming an article extension by casting using a ceramic mold'19985,724,816'Combustor for a gas turbine with cooling structure'19985,721,061'Oxidation-resistant coating for niobium-base alloys'19985,699,401'Anode assembly for use in x-ray tubes, and related articles of manufacture'19975,676,191'Solidification of an article extension from a melt using an integral mandrel and ceramic mold'19975,673,744'Method for forming an article extension by melting of a mandrel in a ceramic mold'19975,673,745'Method for forming an article extension by melting of an alloy preform in a ceramic mold'19975,666,643'High temperature braze material'19975,655,000'Target/rotor connection for use in x-ray tubes'19975,640,767'Method for making a double-wall airfoil'19975,626,462'Double-wall airfoil'19975,597,967'Aluminum-silicon alloy foils'19975,577,093'Target/stem connection for x-ray tube anode assemblies'19965,571,304'Oxide dispersion strengthened alloy foils'19965,548,628'Target/rotor connection for use in x-ray tube rotating anode assemblies'19965,547,410'Method of making an improved target/stem connection for x-ray tube anode assemblies'19965,530,733'Target/stem connection utilizing a diffusion enhancer for x-ray tube anode assemblies'19965,498,187'Method of making an improved target/stem assembly - rotor body assembly connection for x-ray tubes'19965,498,186'Method of making an improved target/stem connection for x-ray tube anode assemblies'19965,480,468'Ni-base alloy foils'19965,474,809'Evaporation method'19955,472,794'Composite structure with NbTiAlHfCrV or NbTiAlHfCrVZrC allow matrix and niobium base metal reinforcement'19955,427,735'Superalloy foils by hot isostatic pressing'19955,426,001'Clad structural member with NbTiAl low Hf alloy cladding and niobium base metal core'19955,405,708'Clad structural member with NbTiHf alloy cladding and niobium base metal core'19955,366,565'NbTiAlCrHf alloy and structures'19945,320,911'Clad structural member with NBTIALCR alloy cladding and niobium base metal core'19945,318,859'Clad structural member with NbTiAl alloy cladding and niobium base metal core'19945,316,865'Composite structure with NbTiAl low Hf alloy matrix and niobium base metal reinforcement'19945,306,570'Clad structural member with NbTiAl high Hf alloy cladding and niobium base metal core'19945,304,427'Composite structure with NBTIA1CRHF alloy matrix and niobium base metal reinforcement'19945,296,309'Composite structure with NbTiAlCr alloy matrix and niobium base metal reinforcement'19945,277,990'Composite structure with NbTiAl and high Hf alloy matrix and niobium base metal reinforcement'19945,273,831'Clad structural member with NbTiAlCr HF alloy cladding and niobium base metal core'19935,270,122'Composite structure with NbTiAl alloy matrix and niobium base metal reinforcement'19935,264,293'Composite structure with NbTiHf alloy matrix and niobium base metal'19935,159,619'High performance metal x-ray tube target having a reactive barrier layer'19925,035,958'Nickel-base superalloys especially useful as compatible protective environmental coatings for advanced superaloys'19915,026,522'Nb-Ti-Hf high temperature alloys'19915,019,334'Low density high strength alloys of Nb-Ti-Al for use at high temperatures'19915,006,307'Hafnium containing niobium, titanium, aluminum high temperature alloy'19915,000,913'Hafnium containing high temperature Nb-Al alloy'19914,990,308'Chromium containing high temperature Nb--Ti--Al alloy'19914,983,356'Ruthenium bearing iron base high temperature structural alloys'19914,980,244'Protective alloy coatings comprising Cr-Al-Ru containing one or more of Y, Fe, Ni and Co'19904,956,144'Hafnium containing Nb-Ti-Al high temperature alloy'19904,931,254'Nb-Ti-Al-Hf-Cr alloy'19904,904,546'Material system for high temperature jet engine operation'19904,877,576'Low density high strength alloys of Nb-Ti-Al for use at high temperatures'19894,726,962'Alternating segment ring structure'19884,669,212'Gun barrel for use at high temperature'19874,657,823'Alternating segment ring structure'19874,603,568'Method of fabricating bimetal variable exhaust nozzle flaps and seals'19864,589,937'Carbide reinforced nickel-base superalloy eutectics having improved resistance to surface carbide formation'19864,577,431'Wear resistant gun barrel and method of forming'19864,537,742'Method for controlling dimensions of RSPD articles'19854,522,664'Phase stable carbide reinforced nickel-base superalloy eutectics having improved high temperature stress-rupture strength and improved resistance to surface carbide formation'19854,447,466'Process for making plasma spray-cast components using segmented mandrels'19844,418,124'Plasma spray-cast components'19834,298,816'Molybdenum substrate for high power density tungsten focal track X-ray targets'19814,292,076'Transverse ductile fiber reinforced eutectic nickel-base superalloys'19814,237,193'Oxidation corrosion resistant superalloys and coatings'19804,117,179'Oxidation corrosion resistant superalloys and coatings'19784,055,447'Directionally solidified eutectic .gamma.-.gamma.\' nickel-base superalloys'19774,054,469'Directionally solidified eutectic .gamma.+.beta. nickel-base superalloys'19774,045,255'Directionally solidified eutectic .gamma.+.beta. nickel-base superalloys'1977Career & activity timeline
Assembled from patent assignee/location history and declaration credentials.
1977–2012Patents assigned to GEN ELECTRIC (165)· patent assignee history
1977Patents assigned to NASA (2)· patent assignee history
1977–1998Based in Schenectady, NY, US· patent location history
1981–2012Based in Niskayuna, NY, US· patent location history
2008–2011Based in Corea, ME, US· patent location history
2012Patents assigned to BEWLAY BERNARD PATRICK (1)· patent assignee history
2012Patents assigned to JACKSON MELVIN ROBERT (1)· patent assignee history
2012Patents assigned to MARTE JUDSON SLOAN (1)· patent assignee history
Inventor activity
Assignee and location history derived from the patent record.
Assignees
| Assignee | Patents | Span |
|---|---|---|
| GEN ELECTRIC | 165 | 1977–2012 |
| NASA | 2 | 1977 |
| BEWLAY BERNARD PATRICK | 1 | 2012 |
| JACKSON MELVIN ROBERTself | 1 | 2012 |
| MARTE JUDSON SLOAN | 1 | 2012 |
Locations
| Location | Patents | Span |
|---|---|---|
| Niskayuna, New York, US | 121 | 1981–2012 |
| Schenectady, New York, US | 37 | 1977–1998 |
| Corea, ME, US | 10 | 2008–2011 |