Patents by Inventor Timothy Nowak

Timothy Nowak 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).

  • Modular Device with Solar Power Supply
    Publication number: 20220109321
    Abstract: Various modular systems including a power unit are shown. In one example, a power unit includes a solar panel, a power storage device and one or more power outlet interfaces. One of the surfaces of the power unit includes a coupling mechanism that permits that power unit to couple with modular storage units. In one embodiment, the modular system includes a frame and wheels coupled to the frame to permit the power unit to be more easily transported.
    Type: Application
    Filed: October 1, 2021
    Publication date: April 7, 2022
    Inventors: Donald J. Truettner, Kyle C. Fassbender, Joseph Marco, Timothy Nowak, Sean Roberts, Steven Zipparro, Samuel Feldner, Caleb Nathaniel Hille
  • Bimetallic turbine shroud and method of fabricating
    Patent number: 9416671
    Abstract: A bimetallic ring for use as a turbine shroud in a gas turbine engine. The bimetallic ring forms a sealing surface as a hot gas flow path boundary in the engine. The ring is comprised of two materials. The first material, a wrought, oxidation resistant metal alloy comprises a first portion, which is the hot gas flow path sealing surface. The second material, a low cost low alloy steel, comprises a second portion that may be at least a pair of supporting side plates. A dissimilar weld joint joins the sealing surface to the second portion, the at least pair of supporting side plates.
    Type: Grant
    Filed: October 4, 2012
    Date of Patent: August 16, 2016
    Assignee: General Electric Company
    Inventors: Bill Damon Johnston, Daniel Anthony Nowak, Srikanth Chandrudu Kottilingam, Melbourne J Myers, Joe Timothy Nowak
  • BIMETALLIC TURBINE SHROUD AND METHOD OF FABRICATING
    Publication number: 20140099194
    Abstract: A bimetallic ring for use as a turbine shroud in a gas turbine engine. The bimetallic ring forms a sealing surface as a hot gas flow path boundary in the engine. The ring is comprised of two materials. The first material, a wrought, oxidation resistant metal alloy comprises a first portion, which is the hot gas flow path sealing surface. The second material, a low cost low alloy steel, comprises a second portion that may be at least a pair of supporting side plates. A dissimilar weld joint joins the sealing surface to the second portion, the at least pair of supporting side plates.
    Type: Application
    Filed: October 4, 2012
    Publication date: April 10, 2014
    Applicant: GENERAL ELECTRIC COMPANY
    Inventors: Bill Damon JOHNSTON, Daniel Anthony NOWAK, Srikanth Chandrudu KOTTILINGAM, Melbourne J. MYERS, Joe Timothy NOWAK