Patents by Inventor Philip A. Simpson

Philip A. Simpson 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: 9064068
    Abstract: Partially opaque intellectual property (IP) includes source code providing the IP functionality. Meta-comments (pragmas or attributes) are provided with the source code to enable visibility of one or more nodes in the IP. Aliasing of the visibility-enabled nodes may also be provided for using meta-comments in the IP source code. The visibility-enabled nodes may be used by system designers in debugging a system design in either a software simulation environment and/or in debugging of a hardware device implementing the partially opaque IP.
    Type: Grant
    Filed: July 7, 2008
    Date of Patent: June 23, 2015
    Assignee: Altera Corporation
    Inventors: Jeffrey R. Fox, Philip A. Simpson
  • Patent number: 7409652
    Abstract: Partially opaque intellectual property (IP) includes source code providing the IP functionality. Meta-comments (pragmas or attributes) are provided with the source code to enable visibility of one or more nodes in the IP. Aliasing of the visibility-enabled nodes may also be provided for using meta-comments in the IP source code. The visibility-enabled nodes may be used by system designers in debugging a system design in either a software simulation environment and/or in debugging of a hardware device implementing the partially opaque IP.
    Type: Grant
    Filed: June 4, 2004
    Date of Patent: August 5, 2008
    Assignee: Altera Corporation
    Inventors: Jeffrey R. Fox, Philip A. Simpson
  • Patent number: 4537066
    Abstract: Measurements of net thrust of an aeroengine on a thrust balance in a test cell must be corrected to gross thrust and it is also advantageous to detect changes in the airflows into and through the test cell of a magnitude sufficient to alter significantly the thrust correction factor. The invention can accomplish both these objectives by obtaining measures of the static pressures p.sub.i and p.sub.e in planes i and e respectively of the test cell using pressure probes 29 and 31, and utilizing the measures of p.sub.i and p.sub.e(a) in a function of the formD=f(p.sub.i, p.sub.e)where D is the thrust correction necessary to convert the net thrust reading on the thrust balance to gross thrust, and(b) to monitor variations of p.sub.i and p.sub.e with respect to the net thrust and detect such of these variations as are outside predetermined limits of variation, such detection indicating the occurence of changes in the characteristics of the airflows sufficient to alter significantly the value of D.
    Type: Grant
    Filed: October 12, 1983
    Date of Patent: August 27, 1985
    Assignee: Rolls-Royce Limited
    Inventor: Philip A. Simpson