Patents by Inventor Aaron Hrdlichka

Aaron Hrdlichka 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: 9657844
    Abstract: A valve unit for an aircraft is provided. The valve unit includes valve assembly; and a servo controller coupled to the valve assembly and configured to control operation of the valve assembly. At least a portion of at least one of the valve assembly or servo controller is formed by a high temperature aluminum alloy.
    Type: Grant
    Filed: April 5, 2012
    Date of Patent: May 23, 2017
    Assignee: HONEYWELL INTERNATIONAL INC.
    Inventors: Aaron Hrdlichka, Robbie Joseph Adams, Rich Hopkins, Eric Holtz, Steve Patterson
  • Patent number: 9625053
    Abstract: The subject matter of this specification can be embodied in, among other things, an apparatus that includes a valve with a valve housing having an axial bore, a first inlet port, a first outlet port, and a piston located within the axial bore and having a first fluid passage and configured to allow reciprocal axial movement of the piston within the axial bore between a first position in which the first fluid passage aligns axially with the first inlet port and the first outlet port to form a first fluidic circuit, and a second position in which the piston blocks at least one of the first inlet port and the first outlet port. The apparatus also includes a lockout assembly configurable to fix the piston into a selected position in a first configuration, and not interfere with reciprocal axial movement of the piston in a second configuration.
    Type: Grant
    Filed: October 14, 2014
    Date of Patent: April 18, 2017
    Assignee: Woodward, Inc.
    Inventors: Brian Hoemke, Shawn Justin Pollock, Adam J. Kurzynski, Aaron Hrdlichka
  • Publication number: 20160102778
    Abstract: The subject matter of this specification can be embodied in, among other things, an apparatus that includes a valve with a valve housing having an axial bore, a first inlet port, a first outlet port, and a piston located within the axial bore and having a first fluid passage and configured to allow reciprocal axial movement of the piston within the axial bore between a first position in which the first fluid passage aligns axially with the first inlet port and the first outlet port to form a first fluidic circuit, and a second position in which the piston blocks at least one of the first inlet port and the first outlet port. The apparatus also includes a lockout assembly configurable to fix the piston into a selected position in a first configuration, and not interfere with reciprocal axial movement of the piston in a second configuration.
    Type: Application
    Filed: October 14, 2014
    Publication date: April 14, 2016
    Inventors: Brian Hoemke, Shawn Justin Pollock, Adam J. Kurzynski, Aaron Hrdlichka
  • Publication number: 20150369372
    Abstract: A valve unit for an aircraft is provided. The valve unit includes valve assembly; and a servo controller coupled to the valve assembly and configured to control operation of the valve assembly. At least a portion of at least one of the valve assembly or servo controller is formed by a high temperature aluminum alloy.
    Type: Application
    Filed: April 5, 2012
    Publication date: December 24, 2015
    Applicant: HONEYWELL INTERNATIONAL INC.
    Inventors: Aaron Hrdlichka, Robbie Joseph Adams, Rich Hopkins, Eric Holtz, Steve Patterson