Patents by Inventor Shihong G. Song

Shihong G. Song 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: 10247273
    Abstract: A composite wrap is provided for damping vibration in an elongated quill shaft having a cylindrical body. The composite wrap includes interior layering for disposition about a cylindrical body, exterior layering configured to define an exterior composite wrap shape and sequential cured-in-place, vibration damping, fibrous epoxy layers. The sequential cured-in-place, vibration damping, fibrous epoxy layers are radially interposed between the interior and exterior layering to dampen vibrations of and/or to adjust a resonance frequency of the cylindrical body.
    Type: Grant
    Filed: June 13, 2016
    Date of Patent: April 2, 2019
    Assignee: SIKORSKY AIRCRAFT CORPORATION
    Inventors: Jonathan Bremmer, Jeffrey G. Sauer, Robert A. Lacko, Shihong G. Song, John H. Meeson, Jr.
  • Publication number: 20170058990
    Abstract: A composite wrap is provided for damping vibration in an elongated quill shaft having a cylindrical body. The composite wrap includes interior layering for disposition about a cylindrical body, exterior layering configured to define an exterior composite wrap shape and sequential cured-in-place, vibration damping, fibrous epoxy layers. The sequential cured-in-place, vibration damping, fibrous epoxy layers are radially interposed between the interior and exterior layering to dampen vibrations of and/or to adjust a resonance frequency of the cylindrical body.
    Type: Application
    Filed: June 13, 2016
    Publication date: March 2, 2017
    Inventors: Jonathan Bremmer, Jeffrey G. Sauer, Robert A. Lacko, Shihong G. Song, John H. Meeson
  • Publication number: 20160243609
    Abstract: A composite core for forming a passage in an investment casting mold is provided including a generally hollow structural element. The structural element is configured to deform when a force is applied to an end thereof. A rigid shell element is formed about the structural element. The shell element extends beyond both an interior surface and an exterior surface of the structural element. The shell element is configured to shatter when the structural element deforms.
    Type: Application
    Filed: February 23, 2016
    Publication date: August 25, 2016
    Inventors: Shihong G. Song, James S. Giampapa, John H. Meeson, JR.
  • Patent number: 9192985
    Abstract: A composite core for forming a passage in an investment casting mold is provided including a core element. A generally hollow structural element is positioned about an exterior of the core element. The structural element is configured to deform when a force is applied to the structural element. A rigid shell element is integrally formed about the structural element. The shell element is configured to break when the structural element deforms.
    Type: Grant
    Filed: October 7, 2013
    Date of Patent: November 24, 2015
    Assignee: SIKORSKY AIRCRAFT CORPORATION
    Inventors: Jonathan Bremmer, Shihong G. Song, Jeffrey G. Sauer, James S. Giampapa
  • Publication number: 20150096711
    Abstract: A composite core for forming a passage in an investment casting mold is provided including a core element. A generally hollow structural element is positioned about an exterior of the core element. The structural element is configured to deform when a force is applied to the structural element. A rigid shell element is integrally formed about the structural element. The shell element is configured to break when the structural element deforms.
    Type: Application
    Filed: October 7, 2013
    Publication date: April 9, 2015
    Applicant: Sikorsky Aircraft
    Inventors: Jonathan Bremmer, Shihong G. Song, Jeffrey G. Sauer, James S. Giampapa
  • Publication number: 20140202650
    Abstract: A composite core for forming a passage in an investment casting mold is provided including a generally hollow structural element. The structural element is configured to deform when a force is applied to an end thereof. A rigid shell element is formed about the structural element. The shell element extends beyond both an interior surface and an exterior surface of the structural element. The shell element is configured to shatter when the structural element deforms.
    Type: Application
    Filed: January 23, 2013
    Publication date: July 24, 2014
    Applicant: SIKORSKY AIRCRAFT CORPORATION
    Inventors: Shihong G. Song, James S. Giampapa, John H. Meeson, JR.
  • Patent number: 7144649
    Abstract: A fuel cell stack includes a plurality of fuel cells each having an anode layer, an electrolyte layer, and a cathode layer, the fuel cells each having a first effective thermal expansion coefficient; a plurality of bipolar plates positioned between adjacent fuel cells having an anode interconnect, a separator plate, and a cathode interconnect, the bipolar plates being positioned between adjacent fuel cells, wherein the anode interconnect is in electrical communication with the anode layer of one adjacent fuel cell, wherein the cathode interconnect is in electrical communication with the cathode layer of another adjacent fuel cell, and wherein at least one interconnect of the cathode interconnect and the anode interconnect has a second thermal expansion coefficient and is adapted to reduce strain between the at least one interconnect and an adjacent fuel cell due to differences between the first and second thermal expansion coefficients over repeated thermal cycles.
    Type: Grant
    Filed: November 27, 2002
    Date of Patent: December 5, 2006
    Assignee: UTC Fuel Cells, LLC
    Inventors: Jean Yamanis, Sunil G. Warrier, Venkata R. Vedula, Raymond C. Benn, John G. Smeggil, Shihong G. Song, Wayde R. Schmidt
  • Publication number: 20040200187
    Abstract: An interconnect for a solid oxide fuel cell includes a compliant superstructure having a first portion defining a separator plate contact zone and a second portion defining an electrode contact zone, wherein the super structure is porous. In one embodiment, the superstructure is defined by a plurality of compliant substructures provided in a first direction and a plurality of compliant substructures provided in second direction to define a woven structure.
    Type: Application
    Filed: January 16, 2004
    Publication date: October 14, 2004
    Inventors: Sunil G. Warrier, Jean Yamanis, Wayde B. Schmidr, Raymond C. Benn, John G. Smeggil, Shihong G. Song, Venkata R. Vedula
  • Publication number: 20040101733
    Abstract: A fuel cell stack includes a plurality of fuel cells each having an anode layer, an electrolyte layer, and a cathode layer, the fuel cells each having a first effective thermal expansion coefficient; a plurality of bipolar plates positioned between adjacent fuel cells having an anode interconnect, a separator plate, and a cathode interconnect, the bipolar plates being positioned between adjacent fuel cells, wherein the anode interconnect is in electrical communication with the anode layer of one adjacent fuel cell, wherein the cathode interconnect is in electrical communication with the cathode layer of another adjacent fuel cell, and wherein at least one interconnect of the cathode interconnect and the anode interconnect has a second thermal expansion coefficient and is adapted to reduce strain between the at least one interconnect and an adjacent fuel cell due to differences between the first and second thermal expansion coefficients over repeated thermal cycles.
    Type: Application
    Filed: November 27, 2002
    Publication date: May 27, 2004
    Inventors: Jean Yamanis, Sunil G. Warrier, Venkata R. Vedula, Raymond C. Benn, John G. Smeggil, Shihong G. Song, Wayde R. Schmidt