Patents by Inventor Mackenzie Whalen

Mackenzie Whalen 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: 20230073840
    Abstract: An angle of attack sensor includes a housing having an open end and a closed end, a faceplate positioned on the open end of the housing, the faceplate comprising a periphery at an outer edge of the faceplate, a central opening, and an exterior surface extending from the periphery to the central opening, and a vane assembly extending through the central opening of the faceplate. The exterior surface of the faceplate has a sloped profile from the periphery to the central opening.
    Type: Application
    Filed: February 25, 2021
    Publication date: March 9, 2023
    Inventors: Mackenzie Whalen, Aaron A. Cusher, Armando Valdes Chavez, Daniel Hanson, Richard Alan Schwartz, Wallace Johnson, William B. Krueger, Kaleb Anderson
  • Patent number: 11142323
    Abstract: A wall for a heated faceplate includes a base and tines protruding from the base and spaced from each another. The tines are configured to accumulate ice in a manner which promotes shedding of small ice formations to prevent large accumulations of ice father aft on the faceplate.
    Type: Grant
    Filed: January 2, 2019
    Date of Patent: October 12, 2021
    Assignee: Rosemount Aerospace Inc.
    Inventor: Mackenzie Whalen
  • Patent number: 10564173
    Abstract: An air data probe includes a housing and a probe head with a body, total pressure and alpha chambers, total pressure and alpha ports, and alpha drain ports. The total pressure chamber extends through a radial center of the body. The alpha chambers are disposed radially outward from the total pressure chamber. The total pressure port is disposed in a distal end of the body is collinear with a centerline axis of the body. The total pressure chamber is in fluid communication with the total pressure port and with the housing. The alpha ports are disposed downstream of the total pressure port and upstream of the housing. The alpha chambers are in fluid communication with the alpha ports. The alpha drain ports are disposed downstream from the alpha port and upstream from the housing. The alpha drain ports fluidly communicate with the alpha chamber.
    Type: Grant
    Filed: May 9, 2018
    Date of Patent: February 18, 2020
    Assignee: Rosemount Aerospace, Inc.
    Inventors: Mackenzie Whalen, James Barron Egberg, Paul Robert Johnson
  • Publication number: 20190346476
    Abstract: An air data probe includes a housing and a probe head with a body, total pressure and alpha chambers, total pressure and alpha ports, and alpha drain ports. The total pressure chamber extends through a radial center of the body. The alpha chambers are disposed radially outward from the total pressure chamber. The total pressure port is disposed in a distal end of the body is collinear with a centerline axis of the body. The total pressure chamber is in fluid communication with the total pressure port and with the housing. The alpha ports are disposed downstream of the total pressure port and upstream of the housing. The alpha chambers are in fluid communication with the alpha ports. The alpha drain ports are disposed downstream from the alpha port and upstream from the housing. The alpha drain ports fluidly communicate with the alpha chamber.
    Type: Application
    Filed: May 9, 2018
    Publication date: November 14, 2019
    Inventors: Mackenzie Whalen, James Barron Egberg, Paul Robert Johnson
  • Patent number: 10416188
    Abstract: An air data probe includes a probe body and an air data sensing port disposed in the probe body. The probe body includes a barrel region, a tapered head region extending forward from the barrel region, and a tip at a forward-most end of the tapered head region. The air data sensing port is disposed in the probe body at a port location aft of the tip. The probe body has a turbulence-producing geometry originating at the tip that produces a turbulent boundary layer of airflow that extends from the tip to the port location.
    Type: Grant
    Filed: July 14, 2017
    Date of Patent: September 17, 2019
    Assignee: Rosemount Aerospace Inc.
    Inventors: Charles Jae Doolittle, Mackenzie Whalen, James Barron Egberg, Aaron A. Cusher, Brian Daniel Matheis
  • Publication number: 20190210734
    Abstract: A wall for a heated faceplate includes a base and tines protruding from the base and spaced from each another. The tines are configured to accumulate ice in a manner which promotes shedding of small ice formations to prevent large accumulations of ice father aft on the faceplate.
    Type: Application
    Filed: January 2, 2019
    Publication date: July 11, 2019
    Inventor: Mackenzie Whalen
  • Publication number: 20180017591
    Abstract: An air data probe includes a probe body and an air data sensing port disposed in the probe body. The probe body includes a barrel region, a tapered head region extending forward from the barrel region, and a tip at a forward-most end of the tapered head region. The air data sensing port is disposed in the probe body at a port location aft of the tip. The probe body has a turbulence-producing geometry originating at the tip that produces a turbulent boundary layer of airflow that extends from the tip to the port location.
    Type: Application
    Filed: July 14, 2017
    Publication date: January 18, 2018
    Inventors: Charles Jae Doolittle, Mackenzie Whalen, James Barron Egberg, Aaron A. Cusher, Brian Daniel Matheis
  • Patent number: 9696187
    Abstract: A device is disclosed for measuring total pressure of a fluid flow comprises a tubular member having an inlet chamber with an inlet opening at a first end of the tubular member. The tubular member also comprises an outlet chamber having an outlet opening at a second end of the tubular member. The inlet opening has a diameter transverse to the longitudinal axis and the outlet opening has a second diameter transverse to the longitudinal axis. The ratio of the first diameter to the second diameter is from 3:1 to 10:1. The tubular member also includes a transitional chamber between the inlet chamber and the outlet chamber. Total pressure can be measured in the inlet chamber.
    Type: Grant
    Filed: July 1, 2015
    Date of Patent: July 4, 2017
    Assignee: ROSEMOUNT AEROSPACE INC.
    Inventors: Mackenzie Whalen, Brian Daniel Matheis
  • Publication number: 20170003151
    Abstract: A device is disclosed for measuring total pressure of a fluid flow comprises a tubular member having an inlet chamber with an inlet opening at a first end of the tubular member. The tubular member also comprises an outlet chamber having an outlet opening at a second end of the tubular member. The inlet opening has a diameter transverse to the longitudinal axis and the outlet opening has a second diameter transverse to the longitudinal axis. The ratio of the first diameter to the second diameter is from 3:1 to 10:1. The tubular member also includes a transitional chamber between the inlet chamber and the outlet chamber. Total pressure can be measured in the inlet chamber.
    Type: Application
    Filed: July 1, 2015
    Publication date: January 5, 2017
    Inventors: Mackenzie Whalen, Brian Daniel Matheis