Patents by Inventor Stephen C. Rolston

Stephen C. Rolston 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: 5743488
    Abstract: Boundary layer separation at the boundary surface of an intake duct (18) of a turbofan aeroengine nacelle (12) at conditions of high incidence and high engine mass flow arises from shockwave induced pressure gradients in the boundary layer. To control separation, gaseous fluid is withdrawn from a high pressure region of the boundary layer at a downstream region of the boundary surface, conveyed within the intake duct structure (19) and discharged at an upstream region of the boundary surface into a low pressure region of the boundary layer.
    Type: Grant
    Filed: December 5, 1995
    Date of Patent: April 28, 1998
    Assignee: Short Brothers PLC
    Inventors: Stephen C. Rolston, Edward M. Ashford