Patents Assigned to Space
  • Patent number: 6629449
    Abstract: Method and apparatus are provided for a non-invasive bubble measuring instrument operable for detecting, distinguishing, and counting gaseous embolisms such as bubbles over a selectable range of bubble sizes of interest. A selected measurement volume in which bubbles may be detected is insonified by two distinct frequencies from a pump transducer and an image transducer, respectively. The image transducer frequency is much higher than the pump transducer frequency. The relatively low-frequency pump signal is used to excite bubbles to resonate at a frequency related to their diameter. The image transducer is operated in a pulse-echo mode at a controllable repetition rate that transmits bursts of high-frequency ultrasonic signal to the measurement volume in which bubbles may be detected and then receives the echo. From the echo or received signal, a beat signal related to the repetition rate may be extracted and used to indicate the presence or absence of a resonant bubble.
    Type: Grant
    Filed: March 26, 2002
    Date of Patent: October 7, 2003
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Robert Kline-Schoder, Patrick J. Magari
  • Patent number: 6631325
    Abstract: A computer implemented physical signal analysis method is includes two essential steps and the associated presentation techniques of the results. All the steps exist only in a computer: there are no analytic expressions resulting from the method. The first step is a computer implemented Empirical Mode Decomposition to extract a collection of Intrinsic Mode Functions (IMF) from nonlinear, nonstationary physical signals based on local extrema and curvature extrema. The decomposition is based on the direct extraction of the energy associated with various intrinsic time scales in the physical signal. Expressed in the IMF's, they have well-behaved Hilbert Transforms from which instantaneous frequencies can be calculated. The second step is the Hilbert Transform. The final result is the Hilbert Spectrum. Thus, the invention can localize any event on the time as well as the frequency axis. The decomposition can also be viewed as an expansion of the data in terms of the IMF's.
    Type: Grant
    Filed: May 21, 1998
    Date of Patent: October 7, 2003
    Assignee: The United States as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Norden Eh Huang, Zheng Shen
  • Patent number: 6628941
    Abstract: An airborne constellation is disclosed with a plurality of individual lighter-than-air platforms spaced apart above a contiguous geographic area within a predetermined altitude range so that ubiquitous line of sight coverage of the geographic area is provided. Each of the plurality of platforms include an enclosure holding a regulated volume of low density gas for buoyancy of the platforms. Each of the plurality of platforms further includes a signal transmitting device attached to the enclosure by which signals from the platform may be transmitted to the contiguous geographic area.
    Type: Grant
    Filed: June 29, 1999
    Date of Patent: September 30, 2003
    Assignee: Space Data Corporation
    Inventors: Gerald M. Knoblach, Eric A. Frische
  • Patent number: 6627065
    Abstract: Coating compositions and methods of their use are described herein for the reduction of corrosion in imbedded metal structures. The coatings are applied as liquids to an external surface of a substrate in which the metal structures are imbedded. The coatings are subsequently allowed to dry. The liquid applied coatings provide galvanic protection to the imbedded metal structures. Continued protection can be maintained with periodic reapplication of the coating compositions, as necessary, to maintain electrical continuity. Because the coatings may be applied using methods similar to standard paints, and because the coatings are applied to external surfaces of the substrates in which the metal structures are imbedded, the corresponding corrosion protection may be easily maintained. The coating compositions are particularly useful in the protection of metal-reinforced concrete.
    Type: Grant
    Filed: October 15, 2001
    Date of Patent: September 30, 2003
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics & Space Administration
    Inventors: Louis G. MacDowell, Joseph J. Curran
  • Patent number: 6626792
    Abstract: A gear bearing having a first gear and a second gear, each having a plurality of teeth. Each gear operates on two non-parallel surfaces of the opposing gear teeth to perform both gear and bearing functions simultaneously. The gears are moving at substantially the same speed at their contact points. The gears may be roller gear bearings or phase-shifted gear bearings, and may be arranged in a planet/sun system or used as a transmission.
    Type: Grant
    Filed: March 3, 2001
    Date of Patent: September 30, 2003
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: John M. Vranish
  • Patent number: 6627894
    Abstract: Microcalorimeters are arranged in a n×m matrix, and plural element groups are composed of the microcalorimeters. Each element group is composed of n calorimeters arranged in a column. AC biases having different frequencies are applied to their respective element groups. The elements produce output signals in response to given external information. The output signals from corresponding elements belonging to their respective different element groups are superimposed on their respective AC biases and added with signal adders. A multiplex signal of the thus added output signals can be taken out on one signal line and read. Each microcalorimeter is placed in a bridge-type circuit to cancel out the AC bias in the output in the absence of a signal in the microcalorimeter.
    Type: Grant
    Filed: January 15, 2002
    Date of Patent: September 30, 2003
    Assignee: The Institute of Space and Astronautical Science
    Inventors: Kazuhisa Mitsuda, Toshiyuki Miyazaki
  • Patent number: 6628567
    Abstract: An acoustic monitoring device has at least two acoustic sensors with a triggering mechanism and a multiplexing circuit. After the occurrence of a triggering event at a sensor, the multiplexing circuit allows a recording component to record acoustic emissions at adjacent sensors. The acoustic monitoring device is attached to a solid medium to detect the occurrence of damage.
    Type: Grant
    Filed: June 15, 1999
    Date of Patent: September 30, 2003
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: William H. Prosser, Daniel F. Perey, Michael R. Gorman, Edgar F. Scales
  • Patent number: 6622472
    Abstract: A multi-lobed, low friction vane, thrust vector controller is disclosed. Low friction vanes are independently movable into and out of the thrust of the exhaust of a jet engine. All vanes may be used together to adjust exhaust surface area to maximize thrust and fuel efficiency in varying conditions. Vanes also move independently to impart directional force to roll, pitch and yaw traditional aircraft and hover VTOL aircraft. A bleed air pressure actuator for moving the vanes is disclosed.
    Type: Grant
    Filed: October 17, 2001
    Date of Patent: September 23, 2003
    Assignee: Gateway Space Transport, Inc.
    Inventor: William Henry Plumpe, Jr.
  • Patent number: 6623642
    Abstract: Phosphate-contaminated water passes through a domestic sewage treatment system, in which oxidation of the ammonium progresses far enough to cause a lowering of the pH to 5 or less. The water is passed over sand grains coated with aluminum hydroxide (gibbsite). Enough Al3+ ions enter solution, at the low pH, to cause all the phosphate-P to precipitate as aluminum phosphate, and nothing else precipitates other than the aluminum phosphate.
    Type: Grant
    Filed: March 8, 2001
    Date of Patent: September 23, 2003
    Assignee: Centre for Research in Earth and Space Technology
    Inventor: William Dean Robertson
  • Patent number: 6623826
    Abstract: Thermal apparatus that reduces passive intermodulation products generated on a satellite or other spaceborne vehicle. Exemplary passive intermodulation free thermal blankets comprise a reflector stack including multiple polyimide layers with metallized film on one side thereof, a binding layer that secures the reflector stack together, and an outer cover layer that wraps around the binding layer and reflector stack to cover an outer surface of the thermal blanket and form a hem on an inner surface of the thermal blanket. Multiple small thermal blankets or patches may be bound together using grounding inserts and polyimide tape to form a quilt-like assembly. The quilt-like assembly is enclosed by an outer cover layer that wraps around the multiple patches to cover one surface thereof and form a hem on an opposite surface thereof.
    Type: Grant
    Filed: October 29, 2001
    Date of Patent: September 23, 2003
    Assignee: Space Systems/Loral
    Inventors: Mark Hasegawa, Mary Owings
  • Publication number: 20030173874
    Abstract: An electro-active transducer for sonic applications includes a ferroelectric material sandwiched by first and second electrode patterns to form a piezo-diaphragm coupled to a mounting frame. When the device is used as a sonic actuator, the first and second electrode patterns are configured to introduce an electric field into the ferroelectric material when voltage is applied to the electrode patterns. When the device is used as a sonic sensor, the first and second electrode patterns are configured to introduce an electric field into the ferroelectric material when the ferroelectric material experiences deflection in a direction substantially perpendicular thereto.
    Type: Application
    Filed: March 12, 2003
    Publication date: September 18, 2003
    Applicant: USA as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Robert G. Bryant, Robert L. Fox
  • Publication number: 20030173873
    Abstract: A fluid-control electro-active device includes a piezo-diaphragm made from a ferroelectric material sandwiched by first and second electrode patterns configured to introduce an electric field into the ferroelectric material when voltage is applied thereto. The electric field originates at a region of the ferroelectric material between the first and second electrode patterns, and extends radially outward from this region of the ferroelectric material and substantially parallel to the plane of the ferroelectric material. The piezo-diaphragm deflects symmetrically about this region in a direction substantially perpendicular to the electric field. An annular region coupled to and extending radially outward from the piezo-diaphragm perimetrically borders the piezo-diaphragm. A housing is connected to the annular region and defines at least one fluid flow path therethrough with the piezo-diaphragm disposed therein.
    Type: Application
    Filed: March 13, 2003
    Publication date: September 18, 2003
    Applicant: National Aeronautics and Space Administration
    Inventors: Robert G. Bryant, Dennis C. Working
  • Publication number: 20030173872
    Abstract: An electro-active transducer includes a ferroelectric material sandwiched by first and second electrode patterns. When the device is used as an actuator, the first and second electrode patterns are configured to introduce an electric field into the ferroelectric material when voltage is applied to the electrode patterns. When the device is used as a sensor, the first and second electrode patterns are configured to introduce an electric field into the ferroelectric material when the ferroelectric material experiences deflection in a direction substantially perpendicular thereto. In each case, the electrode patterns are designed to cause the electric field to: i) originate at a region of the ferroelectric material between the first and second electrode patterns, and ii) extend radially outward from the region of the ferroelectric material (at which the electric field originates) and substantially parallel to the ferroelectric material's plane.
    Type: Application
    Filed: January 16, 2003
    Publication date: September 18, 2003
    Applicant: Administrator of the National Aeronautics and Space Administration
    Inventors: Robert G. Bryant, Robert L. Fox
  • Patent number: 6619322
    Abstract: A fast-acting valve includes an annular valve seat that defines an annular valve orifice between the edges of the annular valve seat, an annular valve plug sized to cover the valve orifice when the valve is closed, and a valve-plug holder for moving the annular valve plug on and off the annular valve seat. The use of an annular orifice reduces the characteristic distance between the edges of the valve seat. Rather than this distance being equal to the diameter of the orifice, as it is for a conventional circular orifice, the characteristic distance equals the distance between the inner and outer radii (for a circular annulus). The reduced characteristic distance greatly reduces the gap required between the annular valve plug and the annular valve seat for the valve to be fully open, thereby greatly reducing the required stroke and corresponding speed and acceleration of the annular valve plug.
    Type: Grant
    Filed: July 27, 2000
    Date of Patent: September 16, 2003
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Bogdan V. Wojciechowski, Robert J. Pegg
  • Patent number: 6617146
    Abstract: A method and system are provided for automatically positioning specimen containers and culture medium containers and transferring specimen samples from the containers to the culture medium. The samples are positioned at predetermined locations, and a sample is automatically streaked in a pattern on the culture medium after deposition of the sample. A means is also provided for establishing the predetermined locations by recording a position of a deposit location in a memory as deposit location data. Biological specimens such as a sample of bacteria are used in the method and system.
    Type: Grant
    Filed: December 9, 1999
    Date of Patent: September 9, 2003
    Assignee: Canadian Space Agency
    Inventors: Frank Naccarato, Anne M. C. Bornath, Georgeta Mazilu
  • Patent number: 6615609
    Abstract: The present invention provides an accumulator 21 for evaporating and condensing a refrigerant in a pressure vessel 22 thereof to control pressure or the like in a closed-loop type controlled unit. The accumulator comprises liquid-phase refrigerant holding means 23 for holding the refrigerant in liquid phase, heating means 25 for heating and evaporating the refrigerant in liquid-phase, cooling means 24 for cooling and condensing the refrigerant in vapor-phase, and a connection port 28 in fluid communication with the controlled unit. The liquid-phase refrigerant holding means 23 includes a vane 32 made of a material capable of absorbing the refrigerant in liquid phase, and the end 35 of the vane 32 has a shape in contact with the inner surface of the pressure vessel 22.
    Type: Grant
    Filed: February 28, 2002
    Date of Patent: September 9, 2003
    Assignee: National Space Development Agency of Japan
    Inventors: Haruo Kawasaki, Shin'ichi Toyama
  • Patent number: 6616218
    Abstract: A device for controlling drag on a ground vehicle. The device consists of a porous skin or skins mounted on the trailing surface and/or aft portions of the ground vehicle. The porous skin is separated from the vehicle surface by a distance of at least the thickness of the porous skin. Alternately, the trailing surface, sides, and/or top surfaces of the ground vehicle may be porous. The device minimizes the strength of the separation in the base and wake regions of the ground vehicle, thus reducing drag.
    Type: Grant
    Filed: September 13, 2001
    Date of Patent: September 9, 2003
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Steven X. S. Bauer, Richard M. Wood
  • Patent number: 6618010
    Abstract: System and methods are disclosed for passively determining the location of a moveable transmitter utilizing a pair of phase shifts at a receiver for extracting a direction vector from a receiver to the transmitter. In a preferred embodiment, a phase difference between the transmitter and receiver is extracted utilizing a noncoherent demodulator in the receiver. The receiver includes an antenna array with three antenna elements, which preferably are patch antenna elements spaced apart by one-half wavelength. Three receiver channels are preferably utilized for simultaneously processing the received signal from each of the three antenna elements. Multipath transmission paths for each of the three receiver channels are indexed so that comparisons of the same multipath component are made for each of the three receiver channels. The phase difference for each received signal is determined by comparing only the magnitudes of received and stored modulation signals to determine a winning modulation symbol.
    Type: Grant
    Filed: November 14, 2001
    Date of Patent: September 9, 2003
    Assignee: United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: G. Dickey Arndt, Phong H. Ngo, Henry A. Chen, Chau T. Phan, Brian A. Bourgeois, John Dusl, Brent W. Hill
  • Patent number: 6611737
    Abstract: A navigation controller and method for performing navigation control are provided. According to the method, a time varying prediction model is determined based on a predictor having a model component and a correlation processor component. The time varying linear prediction model is then used to formulate a predictive controller or to update the controller in use. The controller is then used to control navigation. Because of the correlation processor, the predictor is better adapted to compensate for shortcomings in the model thus making the automated navigation control superior. In use, the method controls vessel navigation in any of a number of predefined modes such as cruising and turning modes. Moreover, through the selection of the operational scenario, the controller can be made to adapt to differing control objectives—for example tight tracking or increased operational efficiency of the vessel.
    Type: Grant
    Filed: December 20, 2001
    Date of Patent: August 26, 2003
    Assignee: Canadian Space Agency
    Inventors: Mona El-Tahan, Hussein El-Tahan, Kevin Tuer, Mauro Rossi
  • Patent number: 6611329
    Abstract: An optical path switch divides sample path radiation into a time series of alternating first polarized components and second polarized components. The first polarized components are transmitted along a first optical path and the second polarized components along a second optical path. A first gasless optical filter train filters the first polarized components to isolate at least a first wavelength band thereby generating first filtered radiation. A second gasless optical filter train filters the second polarized components to isolate at least a second wavelength band thereby generating second filtered radiation. A beam combiner combines the first and second filtered radiation to form a combined beam of radiation. A detector is disposed to monitor magnitude of at least a portion of the combined beam alternately at the first wavelength band and the second wavelength band as an indication of the concentration of the substance in the sample path.
    Type: Grant
    Filed: November 10, 1999
    Date of Patent: August 26, 2003
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Glen W. Sachse