Patents by Inventor Calvin W. Gillard

Calvin W. Gillard 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: 5221363
    Abstract: An array of solar cells for supplying electrical energy to a building (e.g., for operating air-conditioning equipment) is mounted in a window fitting, which comprises a pair of transparent glass panes between which a window blind (e.g., of the venetian blind type) is mounted. Solar cells are secured to slats of the window blind so as to be exposed to sunlight incident thereon.
    Type: Grant
    Filed: August 27, 1992
    Date of Patent: June 22, 1993
    Assignee: Lockheed Missiles & Space Company, Inc.
    Inventor: Calvin W. Gillard
  • Patent number: 5200758
    Abstract: An antenna system is provided having a plurality of individual antenna elements located on a foldable platform. The antenna elements are appropriately phased to yield a desired radiation pattern. The platform has a plurality of light-emitting devices mounted at predetermined locations on the platform. Light from each of the light-emitting devices passes through a corresponding window assembly on a hub. A biconical reflector within the hub directs rays of light from all the light-emitting devices through a telescope and a system of mirrors which focus the rays so as to form images on photodetector arrays. The images formed by the focused optical signals relate to the actual configuration of the platform.
    Type: Grant
    Filed: March 9, 1990
    Date of Patent: April 6, 1993
    Assignee: Lockheed Missiles & Space Company, Inc.
    Inventor: Calvin W. Gillard
  • Patent number: 5090803
    Abstract: An optical coordinate transfer assembly provides angular correlation between spatially separated objects. In a particular embodiment of the invention, roll, pitch and yaw of a second directional device 12 relative to a first directional device 11 can be measured (and correction and/or compensation therefor can be made) using an optical alignment sensor 20 mounted on the first directional device 11 and a rooftop-mirror/lens assembly 21 mounted on the second directional device 12. Light beams projected from the optical alignment sensor 20 are reflected by reflector devices 35 and 36 on the rooftop-mirror/lens assembly 21 to linear arrays 69, 70 and 78 of photodetectors, which generate electronic signals indicating angular discrepancies between the orientations of the first and second directional devices 11 and 12 in three degrees of freedom to sub-microradian accuracy over a wide range of measurements.
    Type: Grant
    Filed: September 21, 1990
    Date of Patent: February 25, 1992
    Assignee: Lockheed Missiles & Space Company, Inc.
    Inventors: Lawrence L. Ames, Calvin W. Gillard, Neal E. Buholz
  • Patent number: 5047788
    Abstract: The figure of an unfurled antenna comprising a radio-frequency reflective fabric (10) is mapped and controlled by a system comprising a plurality of light-emitting devices (14, 15) mounted at precisely specified locations on ribs (11), which support the fabric (10). Light from each of the light-emitting devices (14, 15) passes through a corresponding window assembly (16) on a hub (12), which support the ribs (11) and also houses a telescope of the Schmidt-Cassegrain type. A biconical reflector (27) mounted within the hub (12) directs rays of light from all the light-emitting devices (14, 15) to a primary mirror (21) of the telescope, from which the rays are reflected to a secondary mirror (22), which focuses the rays so as to form images on photodetector arrays (31) and (32). The images formed on the photodetector arrays (31) and (32) are swaths of light, which cross the photodetector arrays (31) and (32) at positions determined by the actual positions of the light-emitting devices (14, 15).
    Type: Grant
    Filed: October 5, 1989
    Date of Patent: September 10, 1991
    Assignee: Lockheed Missiles & Space Company, Inc.
    Inventor: Calvin W. Gillard
  • Patent number: 4611915
    Abstract: The improved Absolute Distance Sensor has achieved presently a resolution of about 0.03 .mu.m (RMS) for measurements over long distances. A two-color, synthetic Michelson interferometer employing a CO.sub.2 source is designed to sequentially switch between four sets of R and P line pairs and thereby provide a basis for forming simultaneous equations which are employed to greatly reduce the half wavelength ambiguity typical of single wavelength interferometers.
    Type: Grant
    Filed: June 7, 1983
    Date of Patent: September 16, 1986
    Assignee: The United States of America as represented by the Secretary of the Air Force
    Inventors: Calvin W. Gillard, Neal E. Buholz, William M. Wells, III