Patents by Inventor Duane Anstead

Duane Anstead 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).

  • Publication number: 20250154879
    Abstract: Bearing assemblies for a turbomachine include a first race statically coupled to a fixed engine housing, a second race coupled to a rotating shaft, a bearing cage disposed between the first race and the second race, and at least one bearing element disposed in the bearing cage. The bearing cage can include inlet channels to allow air to flow into the bearing cage and outlet channels that allow the air and lubricant mixture in the bearing cage to vent into adjacent compartments of the turbomachine. During operation, the inlet channels actively direct an airflow into the bearing cage. In the bearing cage, the air mixes with lubricant, and the air and lubricant mixture is expelled from the bearing cage through the outlet channels, thereby reducing dwell time of lubricant in the bearing assembly.
    Type: Application
    Filed: October 16, 2024
    Publication date: May 15, 2025
    Applicant: General Electric Company
    Inventors: Santosh Kumar Potnuru, Pradeep Sangli, Ravindra Shankar Ganiger, Souvik Math, Duane Anstead, Matthew D. Brothers
  • Publication number: 20060251512
    Abstract: An apparatus for scavenging lubricating oil comprises an integrated slinger/runner rotatable with the turbine engine rotor discourages oil seepage out of an oil sump of a forward bearing for a gas turbine engine during all operating conditions of the gas turbine engine from idle to take-off speeds and during static non-operation. The apparatus includes a runner comprising an axially forward section and a frusto-conical aft section, and a slinger joined coaxially integrally to the aft frusto-conical aft section. The apparatus includes a means for blocking flow of oil from the frusto-conical aft section toward the axially forward section.
    Type: Application
    Filed: May 6, 2005
    Publication date: November 9, 2006
    Inventors: Anant Singh, Stephen Wilton, Duane Anstead, Barry Allmon
  • Publication number: 20060045404
    Abstract: A bearing assembly for a gas turbine engine rotor includes, in an exemplary, an inner race, an outer race assembly, and a rolling element. The outer race assembly includes a body, a plurality of first springs attached to the body, and a plurality of second springs. Each first spring is radially aligned with a corresponding second spring forming a spring pair. The outer race assembly also includes a plurality of connecting members. Each connecting member extends between and connects a first end of the first spring and a first end of the second spring of said spring pair. The outer race assembly further includes a flange with each second spring attached to the flange.
    Type: Application
    Filed: August 27, 2004
    Publication date: March 2, 2006
    Inventors: Barry Allmon, Richard Riffle, Jerry Cabe, Duane Anstead