Patents by Inventor Peter Henry Calder

Peter Henry Calder 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: 3955782
    Abstract: A gas turbine turbojet engine for a supersonic aircraft which fits into a nacelle having a substantially square cross-section. Air flow passing between the square section of the nacelle and the circular section of the engine is compressed by an auxiliary compressor driven by a compressor of the turbojet. The auxiliary compressor is housed within a diameter not greater than the maximum diameter of the turbojet, thus enhancing the engine performance particularly at take-off.
    Type: Grant
    Filed: July 10, 1974
    Date of Patent: May 11, 1976
    Assignee: Rolls-Royce (1971) Limited
    Inventors: Peter Henry Calder, Neil Milner Evans