Patents by Inventor Michael D. Runyan

Michael D. Runyan 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: 9413049
    Abstract: A rotary joint includes a contactless electrical connection that has an annular shape, not extending into a central region surrounded and defined by the annular contactless electrical connection. The annular shape of the electrical connection portions allows other uses for the central region, such as for passing an optical signal through the rotary joint. Feeds are coupled to annular waveguide structures in both halves of the rotary joint, for input and output of signals. The feeds may provide connections to the annular waveguide structures at regularly-spaced circumferential intervals around the waveguide structures, such as at about every half-wavelength of the incoming (and outgoing) signals. The annular waveguide structures propagate signals in an axial direction, parallel to the axis of rotation of the rotary joint. The signals propagate contactlessly (non-electrically-conductively) across a gap in the axial direction between the two annular waveguides.
    Type: Grant
    Filed: March 24, 2014
    Date of Patent: August 9, 2016
    Assignee: Raytheon Company
    Inventors: John J Wootan, Clifton Quan, Chad E Patterson, Michael D Runyan
  • Publication number: 20150270671
    Abstract: A rotary joint includes a contactless electrical connection that has an annular shape, not extending into a central region surrounded and defined by the annular contactless electrical connection. The annular shape of the electrical connection portions allows other uses for the central region, such as for passing an optical signal through the rotary joint. Feeds are coupled to annular waveguide structures in both halves of the rotary joint, for input and output of signals. The feeds may provide connections to the annular waveguide structures at regularly-spaced circumferential intervals around the waveguide structures, such as at about every half-wavelength of the incoming (and outgoing) signals. The annular waveguide structures propagate signals in an axial direction, parallel to the axis of rotation of the rotary joint. The signals propagate contactlessly (non-electrically-conductively) across a gap in the axial direction between the two annular waveguides.
    Type: Application
    Filed: March 24, 2014
    Publication date: September 24, 2015
    Applicant: Raytheon Company
    Inventors: John J. Wootan, Clifton Quan, Chad E. Patterson, Michael D Runyan
  • Patent number: 5685071
    Abstract: A method of manufacturing an environmentally robust electronic module for aircraft avionics or other military or commercial electronic systems. The method produces a sealed chip-on-board electronic module and comprises the following steps. A printed wiring board is provided having an electrical interconnection circuit printed thereon. Bare integrated circuit chips directly mounted and wirebonded to the printed wiring board. Solderable components are then mounted and conductively connected to the printed wiring board to produce a chip-on-board electronic module. The chip-on-board electronic module is then passivated with silicon nitride to produce a sealed chip-on-board electronic module. The electronic module is passivated by applying a coating of silicon nitride using a plasma enhanced chemical vapor deposition process at a temperature near room temperature so that no stress is induced in the integrated circuit chips or wirebonds of the electronic module.
    Type: Grant
    Filed: June 5, 1995
    Date of Patent: November 11, 1997
    Assignee: Hughes Electronics
    Inventors: Louis E. Gates, Jr., Michael D. Runyan
  • Patent number: 5250845
    Abstract: The hermetic module (10) has a frame 12 with an integral heat sink panel (20) extending thereacross between the side walls (14, 16). High-density integrated circuit electronics are mounted on the heat sink panel by hybrid assembly techniques. Covers (36, 38) are welded to the walls to achieve closure. Feedthrough 74 includes connector block (84) extending through an opening in front bulkhead (76). The front bulkhead is Kovar clad, and seal is achieved by means of a Kovar flexible seal extending between the Kovar side of the front bulkhead and the Kovar ring on the connector block.
    Type: Grant
    Filed: November 30, 1990
    Date of Patent: October 5, 1993
    Assignee: Hughes Aircraft Company
    Inventor: Michael D. Runyan
  • Patent number: 4980635
    Abstract: A carrier for an integrated circuit package is disclosed which comprises a base (30) suitable for receiving an integrated circuit package with unformed leads (20') or formed leads (20), a cover (60), flexible material (66), such as an elastomer, disposed between the cover (60) and base (30) surfaces, and pressure is maintained across the cover (60) and base (30) by way of finger (44) on a clip (40) on the base (30) engaging latching edges (68) of cover (60). The leads (22) of the integrated circuit package (20, 20') are thereby secured in position by the elastomeric material (66) which forms itself partially around each of the leads in response to pressure applied across the base (30) and cover (60) as hereinabove described. The disclosed invention eliminates the need for separate grooves or nests in the base (30) of the carrier for each lead of the integrated circuit package.
    Type: Grant
    Filed: December 26, 1984
    Date of Patent: December 25, 1990
    Assignee: Hughes Aircraft Company
    Inventors: R. Thomas Walton, James A. Hathaway, Michael D. Runyan, Michael L. Turnage