Patents by Inventor Matthew Peter Basiletti

Matthew Peter Basiletti 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).

  • Gas turbine engine component including a compliant layer
    Patent number: 10487670
    Abstract: A blade for a gas turbine engine comprises a blade portion having a first end and a second end and an engagement portion including a first surface coupled to the second end of the blade portion and a second surface coupled to the second end of the blade portion, the first and second surfaces arranged to extend divergently away from one another. The engagement portion is adapted for coupling to a wheel included in a gas turbine engine wheel.
    Type: Grant
    Filed: December 23, 2013
    Date of Patent: November 26, 2019
    Assignees: Rolls-Royce Corporation, Rolls-Royce North American Technologies Inc.
    Inventors: David J. Thomas, Richard C. Uskert, Adam L. Chamberlain, Matthew Peter Basiletti
  • GAS TURBINE ENGINE COMPONENT INCLUDING A COMPLIANT LAYER
    Publication number: 20150050158
    Abstract: A blade for a gas turbine engine comprises a blade portion having a first end and a second end and an engagement portion including a first surface coupled to the second end of the blade portion and a second surface coupled to the second end of the blade portion, the first and second surfaces arranged to extend divergently away from one another. The engagement portion is adapted for coupling to a wheel included in a gas turbine engine wheel.
    Type: Application
    Filed: December 23, 2013
    Publication date: February 19, 2015
    Inventors: David J. Thomas, Richard C. Uskert, Adam L. Chamberlain, Matthew Peter Basiletti
  • Bladed disk assembly
    Patent number: 8753090
    Abstract: A bladed disk assembly includes a disk, a blade, and a retaining clip. The disk is centered on an axis. The disk has at least one groove extending along the axis. The blade is received in the groove. The retaining clip contacts the blade and limits movement of the blade along the axis. The retaining clip is engaged with the disk through a snap-fit.
    Type: Grant
    Filed: November 24, 2010
    Date of Patent: June 17, 2014
    Assignee: Rolls-Royce Corporation
    Inventors: Matthew Peter Basiletti, Richard Christopher Uskert, Michelle Lynn Tucker
  • BLADED DISK ASSEMBLY
    Publication number: 20120128498
    Abstract: A bladed disk assembly is disclosed herein. The bladed disk assembly includes a disk centered on an axis. The disk has at least one groove extending along the axis. The bladed disk assembly also includes a blade received in the groove. The bladed disk assembly also includes a retaining clip contacting the blade and limiting movement of the blade along the axis. The retaining clip is engaged with the disk through a snap-fit.
    Type: Application
    Filed: November 24, 2010
    Publication date: May 24, 2012
    Inventors: Matthew Peter Basiletti, Richard Christopher Uskert, Michelle Lynn Tucker