Patents by Inventor Frank A. Hewitt

Frank A. Hewitt 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: 8317126
    Abstract: An aircraft having a lift/propulsion unit which includes a power unit such as a turboshaft engine which drives a fan through a transmission mechanism. The fan discharges to vectoring nozzles which can be independently swivelled to provide lift or propulsion thrust. An output shaft of the transmission mechanism serves as the main shaft of a motor/generator of modular form. The motor/generator can act as a generator to charge an electrical storage device such as a battery, or as a motor to drive the fan, either alone or to supplement the output of engine. Reaction control nozzles are provided at extremities of the aircraft to provide stabilizing thrust. The aircraft is capable of vertical take off and hovering, with the vectoring nozzles swivelled to a lift position, and forward thrust with the vectoring nozzles swivelled to a propulsion position.
    Type: Grant
    Filed: April 15, 2010
    Date of Patent: November 27, 2012
    Assignee: Rolls-Royce PLC
    Inventors: Paul J. H. Harris, Frank A. Hewitt, Martin C. Johnson, Christopher Wright
  • Publication number: 20100301158
    Abstract: An aircraft having a lift/propulsion unit which includes a power unit such as a turboshaft engine which drives a fan through a transmission mechanism. The fan discharges to vectoring nozzles which can be independently swivelled to provide lift or propulsion thrust. An output shaft of the transmission mechanism serves as the main shaft of a motor/generator of modular form. The motor/generator can act as a generator to charge an electrical storage device such as a battery, or as a motor to drive the fan, either alone or to supplement the output of engine. Reaction control nozzles are provided at extremities of the aircraft to provide stabilising thrust. The aircraft is capable of vertical take off and hovering, with the vectoring nozzles swivelled to a lift position, and forward thrust with the vectoring nozzles swivelled to a propulsion position.
    Type: Application
    Filed: April 15, 2010
    Publication date: December 2, 2010
    Applicant: ROLLS-ROYCE PLC
    Inventors: Paul J.H. HARRIS, Frank A. Hewitt, Martin C. Johnson, Christopher Wright
  • Patent number: 4385914
    Abstract: The process involves the steps of:spraying droplets of an aqueous alcohol input solution through spray-bars into a heat transfer fluid contained within a refrigerated process vessel and allowing the droplets to fall through the heat transfer fluid so that some of the water separates out as ice in the droplets;collecting the droplets as a slurry of ice and concentrated solution at the bottom of the process vessel andsubsequently removing the ice to produce a concentrated output solution from the process.The process can be repeated in subsequent process stages up to a limiting concentration of 92% by weight of alcohol in the case of ethanol. The invention includes apparatus in which the process can be performed. Means by which the efficiency of the process may be optimized are also included.
    Type: Grant
    Filed: November 20, 1981
    Date of Patent: May 31, 1983
    Assignee: Rolls-Royce Limited
    Inventors: Frank A. Hewitt, Keith G. Tillen