Patents Assigned to The United States of America respresented by the Administrator of National Aeronautics and Space Administration
  • Patent number: 5637477
    Abstract: A process has been developed for recombinant production of selected polypeptides using transformed insect cells cultured in a horizontally rotating culture vessel modulated to create low shear conditions. A metabolically transformed insect cell line is produced using the culture procedure regardless of genetic transformation. The recombinant polypeptide can be produced by an alternative process using virully infected or stably transformed insect cells containing a gene encoding the described polypeptide. The insect cells can also be a host for viral production.
    Type: Grant
    Filed: August 16, 1994
    Date of Patent: June 10, 1997
    Assignee: The United States of America as respresented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Glenn F. Spaulding, Thomas J. Goodwin, Kim C. O'Connor, Karen M. Francis, Angela D. Andrews, Tacey L. Prewett
  • Patent number: 5248421
    Abstract: A fluid separator for separating particulate matter such as contaminates is provided which includes a series of spiral tubes of progressively decreasing cross sectional area connected in series. Each tube has an outlet on the outer curvature of the spiral. As fluid spirals down a tube, centrifugal force acts to force the heavier particulate matter to the outer wall of the tube, where it exits through the outlet. The remaining, and now cleaner, fluid reaches the next tube, which is smaller in cross sectional area, where the process is repeated. The fluid which comes out the final tube is diminished of particulate matter.
    Type: Grant
    Filed: October 9, 1992
    Date of Patent: September 28, 1993
    Assignee: The United States of America as respresented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Glen A. Robertson
  • Patent number: 5241866
    Abstract: A method and apparatus for directly measuring the time-averaged streamwise momentum in a turbulent stream use a probe which has total head response which varies as the cosine-squared of the angle of incidence. The probe has a nose with a slight indentation on its front face for providing the desired response. The method of making the probe incorporates unique design features. Another probe may be positioned in a side-by-side relationship to the first probe to provide a direct measurement of the total pressure. The difference between the two pressures yields the sum of the squares of the cross-stream components of the turbulence level.
    Type: Grant
    Filed: February 21, 1991
    Date of Patent: September 7, 1993
    Assignee: The United States of America respresented by the Administrator of National Aeronautics and Space Administration
    Inventor: Vernon J. Rossow
  • Patent number: 4564787
    Abstract: The object of the invention is to provide a traveling wave tube with increased linearity to avoid intermodulation of signals being amplified. In a traveling wave tube 10, as shown in FIG. 1, the slow wave structure is a helix (18) including a sever (21). A dynamic velocity taper is provided by gradually reducing the spacing (26) between the repeating elements of the slow wave structure which are the windings of helix (18). The reduction takes place between Zo indicated by line 23 and Z.sub.s which coincides with the output point of helix (18) as indicated by the line (22). The spacing (26) begins to decrease at Z.sub.o and is decreased by up to about 5% at Z.sub.s. The spacing (26) between the repeating elements of the slow wave structure is ideally at an exponential rate because the curve (27), as shown in FIG. 3, increases from Z.sub.o to Zs the point of maximum efficiency and power, at an exponential rate. FIG. 3 shows a coupled cavity traveling wave tube having cavities 32 through 37.
    Type: Grant
    Filed: March 20, 1985
    Date of Patent: January 14, 1986
    Assignee: The United States of America as respresented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Henry G. Kosmahl