Patents by Inventor Daniel B. DeBra

Daniel B. DeBra 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: 6550720
    Abstract: The excess space and weight capacity that is typical of a launch of large satellites to high-energy orbits, such as a geosynchronous orbit, is used to deploy small satellites at a substantially lower-energy orbit, such as a low-earth orbit. An orbit-transfer vehicle provides the navigation, propulsion, and control systems required to transport a payload satellite from a geosynchronous-transfer orbit (GTO) to a predetermined low-earth orbit (LEO). Depending upon the particular configuration, upon achieving the low-earth orbit, the orbit transfer vehicle either releases the payload satellite, or remains attached to the payload satellite to provide support services, such as power, communications, and navigation, to the payload satellite. To reduce the fuel requirements for this deployment via the orbit-transfer vehicle, the orbit-transfer vehicle employs aerobraking to bring the satellite into a low-earth orbit.
    Type: Grant
    Filed: August 9, 2001
    Date of Patent: April 22, 2003
    Assignee: AeroAstro
    Inventors: Richard Fleeter, Daniel B. DeBra, Paul Gloyer, Zeno Wahl, David Goldstein
  • Publication number: 20020190160
    Abstract: The excess space and weight capacity that is typical of a launch of large satellites to high-energy orbits, such as a geosynchronous orbit, is used to deploy small satellites at a substantially lower-energy orbit, such as a low-earth orbit. An orbit-transfer vehicle provides the navigation, propulsion, and control systems required to transport a payload satellite from a geosynchronous-transfer orbit (GTO) to a predetermined low-earth orbit (LEO). Depending upon the particular configuration, upon achieving the low-earth orbit, the orbit transfer vehicle either releases the payload satellite, or remains attached to the payload satellite to provide support services, such as power, communications, and navigation, to the payload satellite. To reduce the fuel requirements for this deployment via the orbit-transfer vehicle, the orbit-transfer vehicle employs aerobraking to bring the satellite into a low-earth orbit.
    Type: Application
    Filed: August 9, 2001
    Publication date: December 19, 2002
    Inventors: Richard Fleeter, Daniel B. DeBra, Paul Gloyer, Zeno Wahl, David Goldstein
  • Patent number: 5304888
    Abstract: An improved electron or ion gun support structure includes a hollow cylinder for rigidly connecting the source assembly to the source-motion ring, with the source cathode and associated lens extending into the hollow portion of the cylinder. The gun is thus made very stable and less susceptible to outside vibrations.
    Type: Grant
    Filed: January 24, 1992
    Date of Patent: April 19, 1994
    Assignee: ETEC Systems, Inc.
    Inventors: Mark A. Gesley, Daniel B. DeBra
  • Patent number: 5209402
    Abstract: A laminar flow diffuser has a plurality of round, thin, stacked plates. A central bore penetrates all the plates with the exception of the bottom plate. The diffuser is secured to the vacuum chamber port. When gas enters the port, it enters the central bore and then flows radially outward through the interplate spaces to the outer circumference of the plates and subsequently into the periphery of the chamber. The diffuser thereby provides a controlled laminar flow which prevents turbulence in the chamber and hence, reduces the possibility of contamination to the workpiece in the chamber. The laminar flow diffuser is easily cleaned, both during its initial assembly and later after use, because it chiefly has flat surfaces which do not harbor dirt or gas.
    Type: Grant
    Filed: May 24, 1991
    Date of Patent: May 11, 1993
    Assignee: Etec System, Inc.
    Inventors: Daniel B. DeBra, William A. Eckes