Patents by Inventor Robert E. Chaney

Robert E. Chaney 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: 5715163
    Abstract: An aircraft navigation control system includes a flight management system control display unit (12), a navigation display unit (40), logic circuitry (60) and a cursor control input device (70). The flight management system control display unit (12) includes a keyboard (30) to allow desired route waypoint modification via keyboard entries. These entries appear on a display (20) which provides a text listing of the selected waypoints. The navigation display (40) produces a graphical depiction of the selected waypoints as provided on the flight management system control display unit (12). In addition, the user may modify or create a new desired route by movement of a cursor (4) on the navigation display (40) to thereby highlight and select various waypoints as depicted on the display (40). By use of this graphical interface via a cursor control device (70) and the cursor (74) on the navigation display (40), a user may create, by a connect the dot approach, a new desired navigation route.
    Type: Grant
    Filed: August 22, 1995
    Date of Patent: February 3, 1998
    Assignee: The Boeing Company
    Inventors: Eric S. Bang, John L. Groce, deceased, Robert E. Chaney
  • Patent number: 5523949
    Abstract: An improvement to an autopilot flight director system allows the flight crew to make a late runway change without disengaging the autopilot. The improved system allows a transition to a new runway assignment if radio altitude is greater than 1500 feet. Control logic determines whether or not localizer and/or glideslope have been captured and enters predetermined modes as a function thereof to effect a transition to the new approach while enabling instrument landing system retuning while maintaining autopilot engagement. Flight crew workload during approach is significantly reduced as a result of implementation of the improved system.
    Type: Grant
    Filed: August 5, 1994
    Date of Patent: June 4, 1996
    Assignee: The Boeing Company
    Inventors: Robert M. Agate, Ronald J. Bloom, John E. Cashman, Robert E. Chaney, John C. Griffin, III, Charles A. Hovland, Ronald Lilischkies, Joseph M. MacDonald, Timothy C. McRoberts, Frank P. Santoni, Jr.
  • Patent number: 4172883
    Abstract: A method wherein a quartz tube is charged with chunks of metallurgical grade silicon and/or a mixture of such chunks and high purity quartz sand, and impurities from a class including aluminum, boron, and the like, as well as certain transition metals including nickel, iron, manganese and the like. The tube is then evacuated and heated to a temperature within a range of 800.degree. C. to 1400.degree. C., whereupon a stream of gas comprising a reactant, such as silicon tetrafluoride, continuously is delivered at low pressures through the charge for causing a metathetical reaction of impurities of the silicon and the reactant to occur for forming a volatile halide and leaving a residue of silicon of an improved purity. Additionally, the reactant may include carbon monoxide gas, whereby impurites such as iron and nickel react therewith to form volatile carbonyls.
    Type: Grant
    Filed: June 23, 1978
    Date of Patent: October 30, 1979
    Inventors: Robert A. Administrator of the National Aeronautics and Space Administration, with respect to an invention by Frosch, William M. Ingle, Stephen W. Thompson, Robert E. Chaney