Patents by Inventor Winnie Tan

Winnie Tan 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).

  • Patent number: 10550303
    Abstract: A hypersonic refractory material, including a refractory leading edge portion for a hypersonic vehicle and a high emissivity oxide coating adhered to the refractory leading edge portion. The high emissivity oxide coating is ZrB2 doped with a cation dopant material selected from the group including Sm, Tm, and mixtures thereof. The cation dopant material is present in a concentration of between 3 mole percent and 8 mole percent.
    Type: Grant
    Filed: June 26, 2017
    Date of Patent: February 4, 2020
    Assignee: Purdue Research Foundation
    Inventors: Rodney Trice, Winnie Tan
  • Publication number: 20190218668
    Abstract: A metallic bond coat Ni16+/?1% Co15+/?1% Cr 8+/?0.5% Al2+/?0.2% Ta0.5+/?0.1% Y: Sicoat 2496 leads to a fusion barrier of titanium into the metallic bond coat so that a substrate is not depleted by titanium.
    Type: Application
    Filed: August 14, 2017
    Publication date: July 18, 2019
    Inventors: WERNER STAMM, ARTURO FLORES RENTERIA, BRITTA STÖHR, WINNIE TAN, APURV JAIN
  • Publication number: 20180127630
    Abstract: A hypersonic refractory material, including a refractory leading edge portion for a hypersonic vehicle and a high emissivity oxide coating adhered to the refractory leading edge portion. The high emissivity oxide coating is ZrB2 doped with a cation dopant material selected from the group including Sm, Tm, and mixtures thereof. The cation dopant material is present in a concentration of between 3 mole percent and 8 mole percent.
    Type: Application
    Filed: June 26, 2017
    Publication date: May 10, 2018
    Inventors: Rodney Trice, Winnie Tan
  • Publication number: 20150132569
    Abstract: A hypersonic refractory material, including a refractory leading edge portion for a hypersonic vehicle and a high emissivity oxide coating adhered to the refractory leading edge portion. The high emissivity oxide coating is selected from the group including Sm2O3, Tm2O3, Yb2O3, Gd2O3, and mixtures thereof, and the refractory leading edge portion includes up to about 15 mole percent of a cation dopant selected from the group including Sm2O3, Tm2O3, Yb2O3, Gd2O3, and mixtures thereof, with the remainder being selected from the group including ZrB2, HfB2, and mixtures thereof. The high emissivity coating is formed by oxidation of cation dopant at elevated temperatures.
    Type: Application
    Filed: September 24, 2012
    Publication date: May 14, 2015
    Inventors: Rodney Trice, Winnie Tan