Patents by Inventor Michael Scott Just

Michael Scott Just 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: 10190537
    Abstract: A turbofan engine having a fan, a fan casing surrounding the fan and having a first radial flange, a thrust reverser having a second radial flange, and a band clamp coupling the first and second radial flanges to connect the thrust reverser and the fan casing. The band clamp may be a segmented band clamp.
    Type: Grant
    Filed: July 2, 2013
    Date of Patent: January 29, 2019
    Assignee: MRA Systems, Inc.
    Inventors: Antony Brett Scarr, Thomas Joseph Weir, Allen Madsen Woolley, Brian Kelby Clegg, Michael Scott Just, Robert Paul Klingele, David Solberg
  • Publication number: 20160146154
    Abstract: A turbofan engine having a fan, a fan casing surrounding the fan and having a first radial flange, a thrust reverser having a second radial flange, and a band clamp coupling the first and second radial flanges to connect the thrust reverser and the fan casing. The band clamp may be a segmented band clamp.
    Type: Application
    Filed: July 2, 2013
    Publication date: May 26, 2016
    Inventors: Antony Brett SCARR, Thomas Joseph WEIR, Allen Madsen WOOLLEY, Brian Kelby CLEGG, Michael Scott JUST, Robert Paul KLINGELE, David SOLBERG
  • Patent number: 9238511
    Abstract: A pylon structure for mounting an aircraft engine to a wing. The pylon structure comprises a torque box having a wing mount on the aft portion, a first engine mount on the fore portion and second engine mount on the aft portion.
    Type: Grant
    Filed: March 4, 2014
    Date of Patent: January 19, 2016
    Assignee: MRA SYSTEMS, INC.
    Inventors: Allen Madsen Woolley, Brian Kelby Clegg, Michael Scott Just, Rameshchandra Dahyabhai Patel
  • Publication number: 20150251768
    Abstract: A pylon structure for mounting an aircraft engine to a wing. The pylon structure comprises a torque box having a wing mount on the aft portion, a first engine mount on the fore portion and second engine mount on the aft portion.
    Type: Application
    Filed: March 4, 2014
    Publication date: September 10, 2015
    Applicant: MRA Systems, Inc.
    Inventors: Allen Madsen Woolley, Brian Kelby Clegg, Michael Scott Just, Rameshchandra Dahyabhai Patel