Patents by Inventor Richard A B McCall

Richard A B McCall 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: 11923131
    Abstract: A product includes an array of cold spray-formed structures. Each of the structures is characterized by having a defined feature size in at least one dimension of less than 100 microns as measured in a plane of deposition of the structure, at least 90% of a theoretical density of a raw material from which the structure is formed, and essentially the same functional properties as the raw material. A product includes a cold spray-formed structure characterized by having a defined feature size in at least one dimension of less than 100 microns as measured in a plane of deposition of the structure, at least 90% of a theoretical density of a raw material from which the structure is formed, and essentially the same functional properties as the raw material.
    Type: Grant
    Filed: November 12, 2020
    Date of Patent: March 5, 2024
    Inventors: Alexander Baker, Scott K. McCall, Harry B. Radousky, Nathan Woollett, Richard Thuss
  • Patent number: 6264428
    Abstract: A hollow cooled aerofoil blade (10) is provided with a central, lengthways extending plenum (16) and has pressure and suction flanks (20,15). The suction flank (15) has lengthways extending passages (21) therein that direct cooling air from the root region (13) into the central plenum (16). From the central plenum, the cooling air flows through a first set of apertures (27) into lengthways extending passages (28) in the pressure flank (20). The cooling air then flows through a second set of apertures (30) in the pressure flank to provide film cooling of the pressure flank (20) external surface.
    Type: Grant
    Filed: January 11, 2000
    Date of Patent: July 24, 2001
    Assignee: Rolls-Royce plc
    Inventors: Geoffrey M Dailey, Peter A Evans, Richard A B McCall
  • Patent number: 6116612
    Abstract: An annular seal is provided between a turbine rotor disc and the adjacent static structure. The seal comprises rotor fins extending from the turbine disc for rotation therewith and an abradable honeycomb layer radially outward of the rotor fins. The abradable honeycomb layer is located on the inner diameter of a sealing ring attached to the static structure. The sealing ring is moveable in an axial direction so that in operation the honeycomb has one axial position for transient conditions and an alternative axial position for stabilized running. The seal clearance can thus be optimised at the two axial positions reducing the leakage flow through the seal.
    Type: Grant
    Filed: August 17, 1998
    Date of Patent: September 12, 2000
    Assignee: Rolls-Royce plc
    Inventors: Mark A Halliwell, Richard A B McCall