Patents by Inventor Richard Alan Schwartz

Richard Alan Schwartz 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: 10393766
    Abstract: An angle of attack sensor includes a housing having an open first end and a closed second end, a heated chassis positioned within the open first end of the housing, a mounting plate positioned on the heated chassis adjacent the open first end of the housing such that an internal chamber is formed between the heated chassis and the mounting plate, a transducer compartment between the heated chassis and the closed second end of the housing, and a water management system located adjacent the internal chamber and the transducer compartment. The water management system includes an annular chamber positioned in the internal chamber, a first tube at a first end of the annular chamber, and a second tube at a second end of the annular chamber. The first tube has a hole such that the first tube is in fluid communication with the annular chamber and the internal chamber, and the second tube is in fluid communication with the annular chamber and the transducer compartment.
    Type: Grant
    Filed: August 17, 2017
    Date of Patent: August 27, 2019
    Assignee: Rosemount Aerospace Inc.
    Inventors: Carlos Alcaya, Alexander N. Reid, Richard Alan Schwartz, William B. Krueger, Timothy DeAngelo, Kenneth Freeman
  • Publication number: 20190100327
    Abstract: An angle of attack sensor includes a housing, a heated chassis positioned at least partially within the housing and defining a pocket, a mounting plate positioned adjacent the heated chassis and having a circular opening, an external surface facing away from the housing, and an internal surface facing toward the housing, and a vane assembly extending through the circular opening of the mounting plate. The vane assembly includes a vane extending from a root to a tip and a vane base connected to the root of the vane and positioned within the pocket of the heated chassis such that the vane base is offset inwardly from the external surface toward the housing.
    Type: Application
    Filed: September 29, 2017
    Publication date: April 4, 2019
    Inventors: William B. Krueger, Kenneth Freeman, Richard Alan Schwartz, Alexander N. Reid, Timothy DeAngelo
  • Publication number: 20190056424
    Abstract: An angle of attack sensor includes a housing having an open first end and a closed second end, a heated chassis positioned within the open first end of the housing, a mounting plate positioned on the heated chassis adjacent the open first end of the housing such that an internal chamber is formed between the heated chassis and the mounting plate, a transducer compartment between the heated chassis and the closed second end of the housing, and a water management system located adjacent the internal chamber and the transducer compartment. The water management system includes an annular chamber positioned in the internal chamber, a first tube at a first end of the annular chamber, and a second tube at a second end of the annular chamber. The first tube has a hole such that the first tube is in fluid communication with the annular chamber and the internal chamber, and the second tube is in fluid communication with the annular chamber and the transducer compartment.
    Type: Application
    Filed: August 17, 2017
    Publication date: February 21, 2019
    Inventors: Carlos Alcaya, Alexander N. Reid, Richard Alan Schwartz, William B. Krueger, Timothy DeAngelo, Kenneth Freeman
  • Publication number: 20190056425
    Abstract: An angle of attack sensor includes a vane assembly and a multi-piece faceplate adjacent the vane assembly. The faceplate includes a heated chassis defining a pocket and a mounting plate positioned adjacent the heated chassis and having an opening. The vane assembly has a portion that is positioned in the pocket of the heated chassis and extends through the opening of the mounting plate.
    Type: Application
    Filed: November 28, 2017
    Publication date: February 21, 2019
    Inventors: Alexander N. Reid, Richard Alan Schwartz, William B. Krueger, Timothy DeAngelo, Kenneth Freeman
  • Publication number: 20180136249
    Abstract: An angle of attack sensor includes a vane that is freely rotatable to align with a direction of an oncoming airflow over the vane. The airfoil includes a root proximate a vane hub that connects to a rotatable shaft, a tip opposite the root, a leading edge, a trailing edge opposite the leading edge, a first lateral face, a second lateral face, and a heating element disposed within the airfoil between the first and second lateral faces proximate the leading edge. The first lateral face extends from the leading edge to the trailing edge. The second lateral face is opposite the first lateral face and extends from the leading edge to the trailing edge. The first and second lateral faces are symmetric about a chord of the airfoil and each have an outer surface profile that is nonlinear and geometrically convex from the leading edge to the trailing edge.
    Type: Application
    Filed: November 14, 2016
    Publication date: May 17, 2018
    Inventors: William B. Krueger, Alexander N. Reid, Richard Alan Schwartz, Kenneth Freeman
  • Publication number: 20180079525
    Abstract: The bearings of aircraft angle of attack (AOA) vanes are susceptible to lightning strike damage, which causes fluting on the inner and outer races of the bearings and causes the bearings to generate friction, noise, and vibrations. To prevent the bearings from experiencing damage due to lightning strikes, the bearings, the shaft, and/or the mounting plate are configured to create an electric isolator to prevent the electric current from the lightning strike from passing through the bearings, thereby preventing the bearings from incurring lightning strike damage.
    Type: Application
    Filed: September 16, 2016
    Publication date: March 22, 2018
    Inventors: William B. Krueger, Richard Alan Schwartz, Kenneth Freeman
  • Patent number: 9702783
    Abstract: An air data probe includes a stationary housing assembly, an air data measurement unit, and a fluid sensing unit disposed proximate to an interface between the housing assembly and the air data measurement unit. The air data measurement unit is rotatable about a longitudinal axis of the air data probe, relative to the stationary housing assembly. The fluid sensing unit includes a second electrically conductive sensing surface physically and dielectrically spaced from a first sensing surface.
    Type: Grant
    Filed: August 1, 2014
    Date of Patent: July 11, 2017
    Assignee: Rosemount Aerospace Inc.
    Inventors: Timothy J. DeAngelo, Richard Alan Schwartz, Curt A. Dykstra
  • Publication number: 20160033356
    Abstract: An air data probe includes a stationary housing assembly, an air data measurement unit, and a fluid sensing unit disposed proximate to an interface between the housing assembly and the air data measurement unit. The air data measurement unit is rotatable about a longitudinal axis of the air data probe, relative to the stationary housing assembly. The fluid sensing unit includes a second electrically conductive sensing surface physically and dielectrically spaced from a first sensing surface.
    Type: Application
    Filed: August 1, 2014
    Publication date: February 4, 2016
    Inventors: Timothy J. DeAngelo, Richard Alan Schwartz, Curt A. Dykstra
  • Patent number: 6098474
    Abstract: The present invention relates to a enclosure for a control surface position transmitter used on aerospace vehicles. The enclosure has improved capability for protecting the components of the position transmitter from damage caused by moisture-induced corrosion. The enclosure is a can-shaped structure that includes separate compartments for its mechanical and electronic components. A series of channels and passageways allow air to circulate freely in and out of the mechanical component compartment, and the electronic component compartment includes a low power heater to keep the electronic components dry and moisture-free.
    Type: Grant
    Filed: September 9, 1997
    Date of Patent: August 8, 2000
    Assignee: Rosemont Aerospace Inc.
    Inventors: Brian Earl Sartain, Richard Alan Schwartz
  • Patent number: D774583
    Type: Grant
    Filed: March 15, 2013
    Date of Patent: December 20, 2016
    Assignee: Rosemount Aerospace Inc.
    Inventors: Kevin John Benning, Jonathan L. Boer, Wallace Johnson, Eric L. Lovaasen, Richard Alan Schwartz
  • Patent number: D829257
    Type: Grant
    Filed: November 10, 2016
    Date of Patent: September 25, 2018
    Assignee: Rosemount Aerospace Inc.
    Inventors: Kevin J. Benning, Jonathan L. Boer, Wallace Johnson, Eric L. Lovaasen, Richard Alan Schwartz