Patents by Inventor Adrial Kirchen

Adrial Kirchen 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: 11215418
    Abstract: An in-weapon sensor enables electronic measurement of the firing pin indent force of a weapon system. The in-weapon sensor measures, either directly or indirectly, the indent force of the firing pin and communicates the information outside of the weapon to a data capture device. The data capture device provides a visual indication as to whether the firing pin indent force is sufficient or insufficient.
    Type: Grant
    Filed: August 30, 2019
    Date of Patent: January 4, 2022
    Assignee: The United States of America as Represented by the Secretary of the Army
    Inventors: Thomas C. Grego, Christopher Gandy, Brian Donovan, Adrial Kirchen, Jeffrey Kinsberg, Andrew Orsini
  • Patent number: 10513330
    Abstract: A blade damper with a magnetic contaminants trap includes, a housing defining a cavity, a piston in operable communication with the housing dividing the cavity into at least a first chamber and a second chamber, a passageway in operable communication with the cavity configured to allow fluid within the cavity to move between the first chamber and the second chamber through the passageway, and at least one magnet in operable communication with fluid in at least one of the cavity and the passageway, such that magnetic contaminants are prevented from freely moving about within the fluid after having been attracted toward the at least one magnet by a magnetic field of the at least one magnet.
    Type: Grant
    Filed: August 3, 2015
    Date of Patent: December 24, 2019
    Assignee: SIKORSKY AIRCRAFT CORPORATION
    Inventors: Adrial Kirchen, James Orbon
  • Patent number: 10301015
    Abstract: A linkage assembly configured for use on a rotor blade having a first section and a second section, the second section being configured to rotate about a blade fold axis between an aligned position and a rotated position relative to the first section is provided. The linkage assembly includes a bracket having a first portion rotatably coupled to the first section about the blade fold axis and a second portion mounted to the second section. A spacer assembly is positioned between the bracket and an adjacent wall of the second section. The overall thickness of the spacer assembly is adjustable to control a distance between the second section and the bracket to adjust the rotated position.
    Type: Grant
    Filed: June 19, 2015
    Date of Patent: May 28, 2019
    Assignee: SIKORSKY AIRCRAFT CORPORATION
    Inventors: Adrial Kirchen, Jonathon Crim, Steven M. Capelle, Stephen V. Poulin
  • Patent number: 10247218
    Abstract: A fastener assembly includes a first component having a back face and a first mating face opposing the back face, and a second component having a front face and a second mating face opposing the front face. The first component and the second component arranged such that the first mating face is closest to the second mating face. A bushing is installed through the first component, an outer surface of the bushing having frictional engagement with the first component to retain the bushing thereat. A threaded fastener extends through the bushing and the second component, and transmits a load into the bushing. A nut is secured to the fastener at the second component to retain the second component at the first component and which induces the load into the fastener. The frictional engagement between the bushing and the first component is configured to resist the load applied to the fastener.
    Type: Grant
    Filed: January 8, 2016
    Date of Patent: April 2, 2019
    Assignee: SIKORSKY AIRCRAFT CORPORATION
    Inventors: Adrial Kirchen, Richard T. Bourque, Kristin Elizabeth Mailhot
  • Publication number: 20180229836
    Abstract: A blade damper with a magnetic contaminants trap includes, a housing defining a cavity, a piston in operable communication with the housing dividing the cavity into at least a first chamber and a second chamber, a passageway in operable communication with the cavity configured to allow fluid within the cavity to move between the first chamber and the second chamber through the passageway, and at least one magnet in operable communication with fluid in at least one of the cavity and the passageway, such that magnetic contaminants are prevented from freely moving about within the fluid after having been attracted toward the at least one magnet by a magnetic field of the at least one magnet.
    Type: Application
    Filed: August 3, 2015
    Publication date: August 16, 2018
    Inventors: Adrial Kirchen, James Orbon
  • Publication number: 20170217580
    Abstract: A linkage assembly configured for use on a rotor blade having a first section and a second section, the second section being configured to rotate about a blade fold axis between an aligned position and a rotated position relative to the first section is provided. The linkage assembly includes a bracket having a first portion rotatably coupled to the first section about the blade fold axis and a second portion mounted to the second section. A spacer assembly is positioned between the bracket and an adjacent wall of the second section. The overall thickness of the spacer assembly is adjustable to control a distance between the second section and the bracket to adjust the rotated position.
    Type: Application
    Filed: June 19, 2015
    Publication date: August 3, 2017
    Inventors: Adrial Kirchen, Jonathon Crim, Steven M. Capelle, Stephen V. Poulin
  • Publication number: 20160265577
    Abstract: A fastener assembly includes a first component having a back face and a first mating face opposing the back face, and a second component having a front face and a second mating face opposing the front face. The first component and the second component arranged such that the first mating face is closest to the second mating face. A bushing is installed through the first component, an outer surface of the bushing having frictional engagement with the first component to retain the bushing thereat. A threaded fastener extends through the bushing and the second component, and transmits a load into the bushing. A nut is secured to the fastener at the second component to retain the second component at the first component and which induces the load into the fastener. The frictional engagement between the bushing and the first component is configured to resist the load applied to the fastener.
    Type: Application
    Filed: January 8, 2016
    Publication date: September 15, 2016
    Inventors: Adrial Kirchen, Richard T. Bourque, Kristin Elizabeth Mailhot