Patents by Inventor James L. Smialek
James L. Smialek has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).
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Patent number: 7261783Abstract: A nickel-base superalloy article for use in turbines has increased creep resistance and lower density. The superalloy article includes, as measured in % by weight, 6.0-12.0% Mo, 5.5-6.5% Al, 3.0-7.0% Ta, 0-15% Co, 2.0-6.0% Cr, 1.0-4.0% Re, 0-1.5% W, 0-1.5% Ru, 0-2.0%-Ti, 0-3.0% Nb, 0-0.2% Hf, 0-0.02% Y, 0.001-0.005% B, 0.01-0.04% C, and a remainder including nickel plus impurities.Type: GrantFiled: September 22, 2004Date of Patent: August 28, 2007Assignee: The United States of America as Represented by the Administrator of NASAInventors: Rebecca A. MacKay, Timothy P. Gabb, James L Smialek, Michael V. Nathal
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Patent number: 6410148Abstract: A barrier layer for a silicon containing substrate which inhibits the formation of gaseous species of silicon when exposed to a high temperature aqueous environment comprises a barium-strontium alumino silicate.Type: GrantFiled: April 15, 1999Date of Patent: June 25, 2002Assignees: General Electric Co., United Technologies Corp., The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Harry Edwin Eaton, Jr., William Patrick Allen, Nathan S. Jacobson, Nanottam P. Bansal, Elizabeth J. Opila, James L. Smialek, Kang N. Lee, Irene T. Spitsberg, Hongyu Wang, Peter Joel Meschter, Krishan Lal Luthra
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Patent number: 6387456Abstract: A barrier layer for a silicon containing substrate which inhibits the formation of gaseous species of silicon when exposed to a high temperature aqueous environment comprises a barium-strontium alumino silicate.Type: GrantFiled: September 5, 2000Date of Patent: May 14, 2002Assignees: General Electric Company, United Technologies Corporation, The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Harry Edwin Eaton, Jr., William Patrick Allen, Nathan S. Jacobson, Narottam P. Bansal, Elizabeth J. Opila, James L. Smialek, Kang N. Lee, Irene T. Spitsberg, Hongyu Wang, Peter Joel Meschter, Krishan Lal Luthra
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Patent number: 6316078Abstract: An article coated with a thermal barrier coating system, and method for preparation of a coated article. The article has a macro-segmented thermal barrier coating due to the presence of a pattern of three-dimensional features. The features may be a series of raised ribs formed on the substrate surface and being spaced from 0.05 inches to 0.30 apart. The ribs have a width W ranging from 0.005 inches to 0.02 inches, and a height R ranging from 25% to 100% of the thickness of the barrier coating. Alternately, the features may be a similar pattern of grooves formed in the surface of the substrate. Other embodiments provide segmentation by grooves or ribs in the bond coat or alternately grooves formed in the thermal barrier layer.Type: GrantFiled: March 14, 2000Date of Patent: November 13, 2001Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: James L. Smialek
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Patent number: 6312763Abstract: A barrier layer for a silicon containing substrate which inhibits the formation of gaseous species of silicon when exposed to a high temperature aqueous environment comprises a yttrium silicate.Type: GrantFiled: November 16, 2000Date of Patent: November 6, 2001Assignees: United Technologies Corporation, General Electric Co., NASAInventors: Harry Edwin Eaton, Jr., William Patrick Allen, Nathan S. Jacobson, Kang N. Lee, Elizabeth J. Opila, James L. Smialek, Hongyu Wang, Peter Joel Meschter, Krishan Lal Luthra
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Patent number: 6296941Abstract: A barrier layer for a silicon containing substrate which inhibits the formation of gaseous species of silicon when exposed to a high temperature aqueous environment comprises a yttrium silicate.Type: GrantFiled: April 15, 1999Date of Patent: October 2, 2001Assignees: General Electric Company, United Technologies Corporation, NASAInventors: Harry Edwin Eaton, Jr., William Patrick Allen, Nathan S. Jacobson, Kang N. Lee, Elizabeth J. Opila, James L. Smialek, Hongyu Wang, Peter Joel Meschter, Krishan Lal Luthra
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Patent number: 6296942Abstract: A barrier layer for a silicon containing substrate which inhibits the formation of gaseous species of silicon when exposed to a high temperature aqueous environment comprises a calcium alumino silicate.Type: GrantFiled: April 15, 1999Date of Patent: October 2, 2001Assignees: General Electric Company, United Technologies Corporation, NASAInventors: Harry Edwin Eaton, Jr., William Patrick Allen, Robert Alden Miller, Nathan S. Jacobson, James L. Smialek, Elizabeth J. Opila, Kang N. Lee, Bangalore A. Nagaraj, Hongyu Wang, Peter Joel Meschter, Krishan Lal Luthra
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Patent number: 6284325Abstract: A barrier layer for a silicon containing substrate which inhibits the formation of gaseous species of silicon when exposed to a high temperature aqueous environment comprises a calcium alumino silicate.Type: GrantFiled: November 16, 2000Date of Patent: September 4, 2001Assignees: General Electric Company, United Technologies Corporation, The United States of America as represented by the United States National Aeronautics and Space AdministrationInventors: Harry Edwin Eaton, Jr., William Patrick Allen, Robert Alden Miller, Nathan S. Jacobson, James L. Smialek, Elizabeth J. Opila, Kang N. Lee, Bangalore A. Nagaraj, Hongyu Wang, Peter Joel Meschter, Krishan Lal Luthra
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Patent number: 5837387Abstract: A coating for protecting titanium aluminide alloys, including the TiAl .gamma.+Ti.sub.3 Al (.alpha..sub.2) class, from oxidative attack and interstitial embrittlement at temperatures up to at least 1000.degree. C. is disclosed. This protective coating consists essentially of titanium, aluminum, and chromium in the following approximate atomic ratio:Ti(41.5-34.5)Al(49-53)Cr(9.5-12.Type: GrantFiled: July 3, 1996Date of Patent: November 17, 1998Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Michael P. Brady, James L. Smialek, William J. Brindley
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Patent number: 5776617Abstract: A diffusion barrier to help protect titanium aluminide alloys, including the coated alloys of the TiAl.gamma.+Ti.sub.3 Al (.alpha..sub.2) class, from oxidative attack and interstitial embrittlement at temperatures up to at least 1000.degree. C. is disclosed. The coating may comprise FeCrAlX alloys. The diffusion barrier comprises titanium, aluminum, and iron in the following approximate atomic percent:Ti-(50-55)Al-(9-20)Fe.This alloy is also suitable as an oxidative or structural coating for such substrates.Type: GrantFiled: October 21, 1996Date of Patent: July 7, 1998Assignee: The United States of America Government as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Michael P. Brady, James L. Smialek, William J. Brindley
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Patent number: 5275670Abstract: A thermocouple having an electropositive leg formed of a noble metal-Al alloy and an electronegative leg electrically joined at respective ends thereof to form a thermocouple junction. The thermocouple provides for accurate and reproducible measurement of high temperatures (600.degree.-1300.degree. C.) in inert, oxidizing, or reducing environments, gases or vacuum. Furthermore, the thermocouple circumvents the need for expensive, strategic precious metals such as rhodium as a constituent component. Selective oxidation of rhodium is also thereby precluded.Type: GrantFiled: July 6, 1993Date of Patent: January 4, 1994Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: James L. Smialek, Michael G. Gedwill
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Patent number: 5116690Abstract: An oxidation resistant coating for titanium alloys and titanium alloy matrix composites comprises an MCrAlX material. M is a metal selected from nickel, cobalt, and iron. X is an active element selected from Y, Yb, Zr and Hf.Type: GrantFiled: April 1, 1991Date of Patent: May 26, 1992Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: William J. Brindley, James L. Smialek, Carl J. Rouge
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Patent number: 5049539Abstract: A ceramic superconductivity part, such as a wire 10, is produced through the partial oxidation of a specially formulated copper alloy in a core 12. The alloys contain low level quantities of rare earth and alkaline earth dopant elements. Upon oxidation at high temperature, superconducting oxide phases are formed as a thin film 14.Type: GrantFiled: January 31, 1989Date of Patent: September 17, 1991Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: James L. Smialek
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Patent number: 4535035Abstract: An oxidation resistant coating is produced on carbon-base materials, and the same processing step effects an infiltration of the substrate with silicon containing material. The process comprises making a slurry of nickel and silicon powders in a nitrocellulose lacquer, spraying onto the graphite or carbon-carbon substrate, and sintering in vacuum to form a fused coating that wets and covers the surface as well as penetrates into the pores of the substrate.Optimum wetting and infiltration occurs in the range of Ni-60 w/o Si to Ni-90 w/o Si with deposited thicknesses of 25-100 mg/cm.sup.2. Sintering temperatures of about 1200.degree. C. to about 1400.degree. C. are used, depending on the melting point of the specific coating composition.The sintered coating results in Ni-Si intermetallic phases and SiC, both of which are highly oxidation resistant. The final coating composition can be further controlled by the length of the sintering time.Type: GrantFiled: January 17, 1984Date of Patent: August 13, 1985Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: James L. Smialek, George C. Rybicki