Patents by Inventor Rollo G. Smethers, Jr.

Rollo G. Smethers, Jr. 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: 4797680
    Abstract: An airborne antenna platform is disclosed capable of providing near-continuous spherical coverage of the volume surrounding the airborne platform.
    Type: Grant
    Filed: September 16, 1985
    Date of Patent: January 10, 1989
    Assignee: Lockheed Corporation
    Inventor: Rollo G. Smethers, Jr.
  • Patent number: 4379533
    Abstract: An airplane features one basic airframe capable of carrying passengers or cargo such as intermodal containers or vehicles. It consists of a basic structure containing the cockpit, wings, engines and empennage. The cockpit and empennage portions are connected by an open, flat section (similar to a flatbed truck) on which the payload is placed. The payload thus forms and constitutes the fuselage shape and may be comprised of a passenger pod, cargo containers or outsized and vehicular equipment. Loading and unloading of such payloads is facilitated by a removable forward section to permit front end access and by laterally disposed vertical tails for aft end access.
    Type: Grant
    Filed: March 23, 1981
    Date of Patent: April 12, 1983
    Assignee: Lockheed Corporation
    Inventors: Edward W. Caldwell, Rollo G. Smethers, Jr.
  • Patent number: 4040334
    Abstract: A mechanism rapidly and repetitively launches missiles from inside an aircraft during flight. One or more missiles are carried and launched through a tube protruding through the front of the aircraft thus obviating the necessity for bomb bay or other sizeable, open doors. The aircraft interior may be used as a large accumulator so that pressurized internal air is utilized as the propellant when admitted to a breech. Thus, a "cold" launch is achieved negating the possibility of a "hang fire". Multiple missiles can be carried in revolving chambers which are capable of rapid rotation into firing position. The advantages of the system include the ability to launch at high aircraft altitudes and speeds with the missile moving toward the target.
    Type: Grant
    Filed: April 20, 1976
    Date of Patent: August 9, 1977
    Assignee: Lockheed Aircraft Corporation
    Inventor: Rollo G. Smethers, Jr.
  • Patent number: D269669
    Type: Grant
    Filed: September 11, 1980
    Date of Patent: July 12, 1983
    Assignee: Lockheed Corporation
    Inventors: John P. Hancock, Rollo G. Smethers, Jr.
  • Patent number: D298227
    Type: Grant
    Filed: September 16, 1985
    Date of Patent: October 25, 1988
    Assignee: Lockheed Corporation
    Inventor: Rollo G. Smethers, Jr.