Patents by Inventor Ernest C. Montesanto

Ernest C. Montesanto 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: 4623858
    Abstract: A waveguide coupler for quickly, easily, and reliably coupling and decoupling two waveguide sections (1A, 1B). The ends (17A, 17B) of the waveguide sections (1A, 1B) are translationally aligned by means of closely fitting coaxial cylindrical shells (41, 21) surrounding the waveguide ends (17A, 17B, respectively). The ends (17A, 17B) are recessed within the shells (41, 21, respectively). A freely rotatable cylindrical sleeve (31) is axially positioned around one of the waveguide ends (17B) by means of a retaining means (13). Less than one revolution of the sleeve (31) is sufficient to effectuate coupling or decoupling of the waveguide sections (1A, 1B), by means of a set of substantially identical helical grooves (34) within the inner surface of the sleeve (31) engaging pins (49) protruding from one of the shells (41).
    Type: Grant
    Filed: January 15, 1985
    Date of Patent: November 18, 1986
    Assignee: Ford Aerospace & Communications Corporation
    Inventors: Ernest C. Montesanto, Joseph K. Martin
  • Patent number: 4500170
    Abstract: An actuator (1) for mechanically supporting a structure such as an optical or radio telescope reflector (3). The actuator (1) is free to precess about a pivot point (C) which is fixed with respect to the supporting cell structure (9). This can be accomplished by gimballing the actuator (1) using vertical (13) and horizontal (17) trunnions. This gimballing arrangement permits radial and axial excursions of each actuator ball (29) to compensate for gravity vector variations as the reflector (3) is moved to point towards its target, and to compensate for thermal expansion variations between the reflector (3) and cell (9). Fine axial position adjustments are accomplished by a rotating nut (43) or a rotating screw (63) configuration in conjunction with a stepper motor (47 or 67). Motor (47 or 67) can receive its commands from a real-time closed loop system sensitive to axial position or axial load.
    Type: Grant
    Filed: June 14, 1982
    Date of Patent: February 19, 1985
    Assignee: Ford Aerospace & Communications Corporation
    Inventor: Ernest C. Montesanto