Patents by Inventor Rolf Sondergaard

Rolf Sondergaard 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: 8629978
    Abstract: Three-dimensional surface illumination using curved laser sheets is described for optical flow measurements over conformal curved surfaces. The illumination method is applicable to many different optical-based flow visualization and measurement techniques, particularly for particle image velocimetry. An alignment sheet increases the accuracy of determining the position and movement of particles used in optical-base fluid flow techniques.
    Type: Grant
    Filed: January 5, 2011
    Date of Patent: January 14, 2014
    Assignee: The United States of America as represented by the Secretary of the Air Force
    Inventors: Jordi Estevadeordal, Christopher Marks, Rolf Sondergaard, James M. Wolff
  • Patent number: 6397577
    Abstract: A gas turbine engine structure is described wherein the compressor region and the turbine region of the engine are disposed substantially concentrically of each other between fixed inner and outer casings, with the combustor disposed at one common end of the compressor and turbine, and wherein the rotor components of the engine include one or more rings, bands, housings or casings with the turbine blades and compressor blades mounted respectively on the inner and outer surface thereof, and wherein the compressor and turbine stator components are mounted respectively on the inner surface of the outer casing and the outer surface of the inner casing, or, alternatively, wherein the turbine and compressor stator components are mounted respectively on the inner surface of the outer casing and the outer surface of the inner casing, which structure geometries eliminate much of the weight associated with the disks and interconnecting shafts that characterize conventional engines.
    Type: Grant
    Filed: April 2, 2001
    Date of Patent: June 4, 2002
    Assignee: The United States of America as represented by the Secretary of the Air Force
    Inventor: Rolf Sondergaard
  • Patent number: 6139268
    Abstract: A turbine blade having an extensible tail is described. The extensible tail is selectively positionable during engine operation, enabling fine-tuning for maximum power and efficiency during engine operation. During periods of operation exhibiting low Reynolds number flows, the extensible tail is projected out from the trailing edge of the turbine blade, into the gas path. As Reynolds number flows increase, the extensible tail is retracted back into the turbine blade, maximizing turbine engine efficiency.
    Type: Grant
    Filed: March 19, 1999
    Date of Patent: October 31, 2000
    Assignee: The United States of America as represented by the Secretary of the Air Force
    Inventors: Christopher G. Murawski, Rolf Sondergaard