Patents by Inventor Roger S. Hollister

Roger S. Hollister 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: 6557258
    Abstract: A cutter, for cutting various surfaces having various curvatures, having a blade assembly and a housing. The blade assembly includes a first blade and a second blade, each having an inner edge and an outer edge, and a guide mounted between the first blade and second blade adjacent to the inner edges thereof. The first blade has a first cutting surface and the second blade has a second cutting surface which are each oriented toward the guide. The first cutting surface is convex toward the guide and the second cutting surface is concave toward the guide, wherein the user may cut concave or convex surfaces by selectively using one of the blades.
    Type: Grant
    Filed: October 18, 1999
    Date of Patent: May 6, 2003
    Inventors: Elizabeth M. Roberts, Roger S. Hollister
  • Patent number: 5477107
    Abstract: Lossy slabs are provided in linear-beam tubes such as coupled-cavity TWTs and klystrons to produce a more level tube response over its full operating band, and to eliminate oscillations at the upper cut-off frequency in the TWTs. The slab thicknesses are selected to produce a substantially non-resonant field of about one-quarter wavelength within the slab when the tube is operated within its passband. The slabs are formed from a dielectric material with a conductive mixture of at least about 15%.
    Type: Grant
    Filed: December 21, 1993
    Date of Patent: December 19, 1995
    Assignee: Hughes Aircraft Company
    Inventors: Ivo Tammaru, Christine G. Thoma, Roger S. Hollister, Robert G. Ripley
  • Patent number: 5051656
    Abstract: In a travelling-wave tube (20), a cylindrically-shaped slow-wave circuit cavity-defining member (34) is supported by and is thermomechanically bonded to a tubularly-configured vacuum wall member (32). The bonded joint comprises a pair of arcuate grooves (52) extending lengthwise of the slow-wave circuit and positioned diametrically opposite one another about the axis of the tube. A helical or wavy spring (54, 58) lies in each groove and is resiliently biased in intimate mechanical and thermal contact between the groove and the vacuum wall. The helical spring, in particular, can be used as a conduit for exhaust of gases from the travelling-wave tube during its fabrication.
    Type: Grant
    Filed: September 5, 1989
    Date of Patent: September 24, 1991
    Assignee: Hughes Aircraft Company
    Inventors: Sunder S. Rajan, Roger S. Hollister, Thomas P. Carlisle