Patents by Inventor Robert L. Pons

Robert L. Pons 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: 4566432
    Abstract: A structure (47) is rotatable 360.degree. about a vertical azimuth axis and 90.degree. or more about an orthogonal elevation axis. The structure (47) is mounted upon a rotating turret (6) in the general shape of an inverted pyramid, with a vertical generally cylindrical torque tube (11) protruding from the bottom of the turret (6). A drive wheel (12) is attached to the bottom of the tube (11) and provides a mechanical advantage for azimuthal rotation because it is larger than the wheel (25, 26, 30) connecting the top of the tube (11) with the bottom of the turret (6). The turret (6) rotatably turns about tripod base (46) by means of wheels (29) mounted beneath the rim (30) of said upper wheel (25, 26, 30). Elevational motion is provided by means of a lead screw (16) connecting rotating turret (6) with structure (47), which can be a modular mass-producible solar radiation reflector consisting of many identical reflective panels (1), each having the shape of a portion of the surface of a sphere.
    Type: Grant
    Filed: April 6, 1984
    Date of Patent: January 28, 1986
    Assignee: Ford Aerospace & Communications Corporation
    Inventors: Isidore F. Sobczak, William C. Cleveland, Jr., Robert L. Pons
  • Patent number: 4535961
    Abstract: A structure (47) is rotatable 360.degree. about a vertical azimuth axis and 90.degree. or more about an orthogonal elevation axis. The structure (47) is mounted upon a rotating turret (6) in the general shape of an inverted pyramid, with a vertical generally cylindrical torque tube (11) protruding from the bottom of the turret (6). A drive wheel (12) is attached to the bottom of the tube (11) and provides a mechanical advantage for azimuthal rotation because it is larger than the wheel (25, 26, 30) connecting the top of the tube (11) with the bottom of the turret (6). The turret (6) rotatably turns about tripod base (46) by means of wheels (29) mounted beneath the rim (30) of said upper wheel (25, 26, 30). Elevational motion is provided by means of a lead screw (16) connecting rotating turret (6) with structure (47) which can be a modular mass-producible solar radiation reflector consisting of many identical reflective panels (1), each having the shape of a portion of the surface of a sphere.
    Type: Grant
    Filed: March 8, 1982
    Date of Patent: August 20, 1985
    Assignee: Ford Aerospace & Communications Corporation
    Inventors: Isidore F. Sobczak, William C. Cleveland, Jr., Robert L. Pons
  • Patent number: 4463749
    Abstract: A modular solar radiation concentrator consists of many identical reflective panels (1), each having the shape of a portion of the surface of a sphere. The panels (1) are mass produced, mounted between a pair of horizontal beams (2) so they can partially rotate about two orthogonal axes, and aligned as part of multi-beam (2) modules (3) on a test fixture so that all panels (1) reflect distant radiation upon a small aperture (36). Spaced occur between all panels (1) when mounted in the concentrator. The reflector support structure (4) has a finite number of identically angled bends so that the overall reflector (47) approximates the surface of a sphere. A solar radiation receiver (34) is hingedly suspended to the support structure (4) at the focal point of each of the panels (1). The reflector (47) is mounted upon an azimuth/elevation mount (6, 46), which rotates reflector (47) 360.degree. about a vertical azimuth axis and 90.degree. or more about an orthogonal elevation axis.
    Type: Grant
    Filed: March 8, 1982
    Date of Patent: August 7, 1984
    Assignee: Ford Aerospace & Communications Corporation
    Inventors: Isidore F. Sobczak, William C. Cleveland, Jr., Robert L. Pons
  • Patent number: 4457297
    Abstract: A modular solar radiation concentrator consists of many identical reflective panels (1), each having the shape of a portion of the surface of a sphere. The panels (1) are mass produced, mounted between a pair of horizontal beams (2) so they can partially rotate about two orthogonal axes, and aligned as part of multi-beam (2) modules (3) on a test fixture so that all panels (1) reflect distant radiation upon a small aperture (36). Spaces occur between all panels (1) when mounted in the concentrator. The reflector support structure (4) has a finite number of identically angled bends so that the overall reflector (47) approximates the surface of a sphere. A solar radiation receiver (34) is hingedly suspended to the support structure (4) at the focal point of each of the panels (1). The reflector (47) is mounted upon an azimuth/elevation mount (6, 46), which rotates reflector (47) 360.degree. about a vertical azimuth axis and 90.degree. or more about an orthogonal elevation axis.
    Type: Grant
    Filed: September 6, 1983
    Date of Patent: July 3, 1984
    Assignee: Ford Aerospace & Communications Corp.
    Inventors: Isidore F. Sobczak, William C. Cleveland, Jr., Robert L. Pons
  • Patent number: 4335578
    Abstract: A solar converter is disclosed which has particular applicability at the focal point of a parabolic concentrator. The converter absorbs solar thermal radiation in a cavity type receiver and transports the heat via a secondary fluid to a heat exchanger which contains a primary (i.e., working) fluid used for process heating or to power a heat engine employing either Stirling, Rankine, or Brayton thermodynamic cycles. The secondary fluid is boiled within the receiver by the trapped solar radiation and the released vapor rises along an elevated path to the heat exchanger. The vapor condenses on the surfaces of the heat exchanger, thereby transferring heat to the engine working fluid. The condensed liquid then flows by means of gravity back to the solar receiver. The walls of the cavity receiver are typically comprised of two concentric cylinders joined at one end in a half toroid and at the other end in concentric half spheres.
    Type: Grant
    Filed: May 30, 1980
    Date of Patent: June 22, 1982
    Assignee: Ford Aerospace & Communications Corporation
    Inventors: Douglas B. Osborn, Robert L. Pons