Patents Represented by Attorney John O. Tresansky
  • Patent number: 4159634
    Abstract: A toggle mechanism pinches a metal tube and maintains the tube in a pinched condition, without fracturing. The toggle mechanism includes a plunger translatable along a longitudinal axis, as well as a pair of links pivoted about a common axis extending through an end of the plunger. One of the links also pivots about a fixed axis. A free end of the other link carries a push link which the other link translates at right angles to the plunger longitudinal axis. First and second sides of the tube bear against a first stop block and are engaged by the push link when a compresson spring, attached to the plunger, is suddenly released to irreversibly drive the plunger along its longitudinal axis so the pivot point of the two links is driven to an over travel position. At over travel, the free end of the push link and the stop block abut against opposite sides of the tube to pinch them together.
    Type: Grant
    Filed: May 19, 1978
    Date of Patent: July 3, 1979
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Edwin O. Stengard
  • Patent number: 4154501
    Abstract: An interleaving device for processing energy signals between various logic devices having a first plurality of spaced energy carrying layer materials. Each of the first layer materials has a plurality of juxtaposed conduits for passing energy signals therethrough. Each of the conduits has a longitudinal axis substantially parallel to a diagonal of each of the first layers. A second plurality of energy carrying materials is arranged between adjacent ones of the spaced first layer materials. Each of the second layer materials has a plurality of juxtaposed conduits for passing the energy signals therethrough. Each of the conduits in the second layer has a longitudinal axis substantially parallel to a diagonal of each of the second layer materials and substantially perpendicular to the axes of the conduits of the first layer materials.
    Type: Grant
    Filed: September 2, 1977
    Date of Patent: May 15, 1979
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: James R. Fischer
  • Patent number: 4142101
    Abstract: A radiation to visible light converter is combined with a visible light intensifier. The converter is a phosphor or scintillator material which is modified to block ambient light. The intensifier includes fiber optics input and output face plates with a photocathode-microchannel plate amplifier-phosphor combination. Incoming radiation is converted to visible light by the converter which is piped into the intensifier by the input fiber optics face plate. The photocathode converts the visible light to electrons which are amplified by a microchannel plate amplifier. The electrons are converted back to light by a phosphor layer and piped out for viewing by the output fiber optics face plate. The converter-intensifier combination may be further combined with it's own radiation source or used with an independent source.
    Type: Grant
    Filed: July 20, 1977
    Date of Patent: February 27, 1979
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Lo I Yin
  • Patent number: 4142119
    Abstract: An electric motor having a low speed shaft that rotates at a speed much slower than the speed of a high speed shaft comprises a stator having a cylindrical bore with a longitudinal axis and a rotor that carries the low speed shaft and rotates in the bore eccentrically about the axis so that there is contact and no magnetic gap between a relatively small portion of the rotor periphery and the periphery of the bore. A magnetic field, rotating at the speed of the high speed shaft, is applied to the periphery of the bore. The field has longitudinally extending magnetic field components of opposite polarity so that around approximately 180.degree. of the bore the field extends in a first direction, while around the other 180.degree. of the bore the field extends in the opposite direction. The rotor includes permanent magnet pole faces at opposite ends of the bore.
    Type: Grant
    Filed: March 21, 1977
    Date of Patent: February 27, 1979
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Jesse M. Madey
  • Patent number: 4140972
    Abstract: Frequency synthesizers at first and second stations that communicate with each other via a transmission link having a constant propagation delay time are started and synchronized by transmitting a tone from the first station to the second station via the link. The output frequencies of the two synthesizers correspond with each other and occur for the same length of time. At the second station, the tone is detected to cause the derivation of a tone burst having a predetermined frequency and duration. At the second station, a predetermined time interval after the derivation of the trailing edge of the tone burst, activation of the synthesizer at that station is initiated. The tone burst and frequencies derived from the synthesizer at the second station are transmitted in sequence from the second station to the first station via the link. At the first station, the tone burst is detected; detection of the trailing edge of the tone burst initiates operation of the synthesizer at the first station.
    Type: Grant
    Filed: April 11, 1977
    Date of Patent: February 20, 1979
    Inventors: James C. Administrator of the National Aeronautics and Space Administration with respect to an invention of Fletcher, Edward A. Enriquez, Ronald E. Gookin
  • Patent number: 4134447
    Abstract: The wave length of an infrared, semiconductor laser diode having an output frequency that is dependent on the diode temperature is maintained substantially constant by maintaining the diode temperature constant. The diode is carried by a cold tip of a closed cycle helium refrigerator. The refrigerator has a tendency to cause the temperature of the cold tip to oscillate. A heater diode and a sensor diode are placed on a thermal heat sink that is the only highly conductive thermal path between the laser diode and the cold tip. The heat sink has a small volume and low thermal capacitance so that the sensing diode is at substantially the same temperature as the heater diode and substantially no thermal lag exists between them. The sensor diode is connected in a negative feedback circuit with the heater diode so that the tendency of the laser diode to thermally oscillate is virtually eliminated.
    Type: Grant
    Filed: September 30, 1977
    Date of Patent: January 16, 1979
    Inventors: Robert A. Administrator of the National Aeronautics and Space Administration, with respect to an invention of Frosch, Donald E. Jennings, John J. Hillman
  • Patent number: 4132599
    Abstract: Method for the quick determination of the susceptibilities of various unidentified bacteria contained in an aqueous physiological fluid sample, particularly urine, to one or more antibiotics. A bacterial adenosine triphosphate (ATP) assay is carried out after the elimination of non-bacterial ATP to determine whether an infection exists. If an infection does exist, a portion of the sample is further processed, including subjecting parts of the portion to one or more antibiotics. Growth of the bacteria in the parts are determined, again by an ATP assay, to determine whether the unidentified bacteria in the sample are susceptible to the antibiotic or antibiotics under test.
    Type: Grant
    Filed: April 23, 1976
    Date of Patent: January 2, 1979
    Inventors: James C. Administrator of the National Aeronautics and Space Administration, with respect to an invention of Fletcher, Grace L. Picciolo, Emmett W. Chappelle, Jody W. Deming, Christian G. Shrock, Hillar Vellend, Michael J. Barza, Louis Weinstein
  • Patent number: 4129357
    Abstract: A birefringent filter module comprises, in seriatum, an entrance polarizer, a first birefringent crystal responsive to optical energy exiting the entrance polarizer, a partial polarizer responsive to optical energy exiting the first polarizer, a second birefringent crystal responsive to optical energy exiting the partial polarizer, and an exit polarizer. The first and second birefringent crystals have fast axes disposed .+-. 45.degree. from the high transmitivity direction of the partial polarizer. Preferably, the second crystal has a length 1/2 that of the first crystal and the high transmitivity direction of the partial polarizer is nine times as great as the low transmitivity direction. To provide tuning, the polarizations of the energy entering the first crystal and leaving the second crystal are varied by either rotating the entrance and exit polarizers, or by sandwiching the entrance and exit polarizers between pairs of half wave plates that are rotated relative to the polarizers.
    Type: Grant
    Filed: August 11, 1977
    Date of Patent: December 12, 1978
    Inventors: Robert A. Administrator of the National Aeronautics and Space Administration, with respect to an invention of Frosch, Alan M. Title
  • Patent number: 4128814
    Abstract: A maser functioning as a frequency standard stable to one part in 10.sup.14 includes a variable volume, constant surface area storage bulb having a fixed volume portion located in a resonant cavity from which the frequency standard is derived. A variable volume portion of the bulb, exterior to the resonant cavity, has a maximum volume on the same order of magnitude as the fixed volume bulb portion. The cavity has a length to radius ratio of at least 3:1 so that the operation is attained without the need for a feedback loop. A baffle plate, between the fixed and variable volume bulb portions, includes apertures for enabling hydrogen atoms to pass between the two bulb portions and is an electromagnetic shield that prevents coupling of the electromagnetic field of the cavity into the variable volume bulb portion. The maser is operated so that the zero wall shift frequency thereof can be determined by being operated at first and second very accurately controlled temperatures for identical small and large volumes.
    Type: Grant
    Filed: November 30, 1977
    Date of Patent: December 5, 1978
    Inventors: Robert A. Administrator of the National Aeronautics and Space Administration, with respect to an invention of Frosch, Victor S. Reinhardt, Peter O. Cervenka
  • Patent number: 4119996
    Abstract: A high speed CMOS formed on a single semiconductor substrate includes a DMOS having an asymmetric channel and a VMOS with a relatively short channel length. The short channel length of the VMOS is achieved by: (1) forming a double diffusion along one edge of a V groove, or (2) ion implanting boron into the apex of the V groove and diffusing a single layer to a relatively deep depth along both edges of the groove.
    Type: Grant
    Filed: July 20, 1977
    Date of Patent: October 10, 1978
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Murzban D. Jhabvala
  • Patent number: 4119964
    Abstract: The presence, frequency and amplitude of radio frequency interference superimposed on communication links originating from a terrestrial region and including a relay in a geostationary spacecraft are determined by pointing a narrow beam antenna on the satellite at the terrestrial region. The level of noise radiated from the region, in a predetermined frequency band of interest, to the antenna is measured at a terrestrial station that is usually remote from the region. Many of the measurements are performed in each of a plurality of frequency bands across the spectrum. Calibrating radio signals having a plurality of predetermined EIRP's (Effective Isotropic Radiated Power) and frequencies in the spectrum are transmitted from the region through the spacecraft narrow beam antenna back to the station. At the station, the levels of the received calibrating signals are separately measured for each of the frequency bands and EIRP's.
    Type: Grant
    Filed: October 28, 1976
    Date of Patent: October 10, 1978
    Inventors: James C. Administrator of the National Aeronautics and Space Administration, with respect to an invention of Fletcher, Klaus G. Johannsen, Samuel Sabaroff, Varice F. Henry
  • Patent number: 4117881
    Abstract: Blood cells, blood marrow, and other similar biological tissue is frozen while in a polyethylene bag placed in abutting relationship against opposed walls of a pair of heaters. The bag and tissue are cooled with refrigerating gas at a time programmed rate at least equal to the maximum cooling rate needed at any time during the freezing process. The temperature of the bag, and hence of the tissue, is compared with a time programmed desired value for the tissue temperature to derive an error indication. The heater is activated in response to the error indication so that the temperature of the tissue follows the desired value for the time programmed tissue temperature. The tissue is heated to compensate for excessive cooling of the tissue as a result of the cooling by the refrigerating gas. In response to the error signal, the heater is deactivated while the latent heat of fusion is being removed from the tissue while the tissue is changing phase from liquid to solid.
    Type: Grant
    Filed: June 14, 1977
    Date of Patent: October 3, 1978
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Thomas E. Williams, Thomas A. Cygnarowicz
  • Patent number: 4118665
    Abstract: The phase and/or period stability of a device being tested is determined by connecting the device in one orthogonal arm of a phase detector having a mixer. In the other arm is an adjustable, variable phase shift device, such as a line stretcher. The output of the mixer is fed through an active low pass filter to derive a DC voltage indicative of the phase shift of the tested device. Initially, the variable phase device is adjusted so that the DC voltage is approximately zero to nullify the phase shift of the tested device under normal conditions. The DC voltage level is converted into a time interval indicative of the phase change of the tested device by determining when the level equals the amplitude of a low frequency ramp voltage that functions similar to a beat frequency output of a prior art dual mixer detector.
    Type: Grant
    Filed: December 8, 1977
    Date of Patent: October 3, 1978
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Victor S. Reinhardt
  • Patent number: 4111851
    Abstract: A coating characterized by low thermal absorption, high thermal emittance and high electrical conductivity comprises:(a) a fired oxide pigment comprising a minor amount of aluminum oxide and a major amount of zinc oxide;(b) a vehicle-binder comprising an alkali metal silicate; and(c) sufficient water to provide a mixture suitable for application to a substrate.The fired oxide pigment may further include a minor amount of cobalt oxide. The resulting coating is particularly useful for coating the surfaces of spacecraft and similar objects.
    Type: Grant
    Filed: October 21, 1977
    Date of Patent: September 5, 1978
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Michael Charles Shai
  • Patent number: 4093354
    Abstract: A method of forming two diverging beams of energy from a single beam of energy including the steps of splitting the single beam of energy into an externally reflected beam and an internally transmitted beam at a first surface on a wedge shaped energy beam splitting device; splitting the internally transmitted beam into an internally reflected beam and an externally transmitted beam at a second surface of the wedge shaped energy beam splitting device, and substantially totally reflecting the internally reflected beam between the first and second surfaces until the internally reflected beam reaches an end of the wedge shaped energy beam splitting device. The above method may further include steps paralleling the above steps wherein two diverging beams of energy are formed from a second beam of energy impinging on the second surface and then combining the two diverging beams with the two diverging beams formed from the beam of energy split by the first surface, to form first and second combined beams.
    Type: Grant
    Filed: December 23, 1975
    Date of Patent: June 6, 1978
    Inventors: James C. Administrator of the National Aeronautics and Space Administration, with respect to an invention of Fletcher, Walter Robert Leeb
  • Patent number: 4092874
    Abstract: An actuator mechanism having a frame, a shaft rotatably supported in the frame, a positioning mechanism coupled to the shaft for rotating the shaft in two rotary positions disposed approximately 180.degree. apart, and a pair of plungers coupled to the shaft each of which is responsive to a control signal for applying bi-directional rotation to the shaft respectively.
    Type: Grant
    Filed: December 6, 1976
    Date of Patent: June 6, 1978
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: William C. Stange
  • Patent number: 4092617
    Abstract: A substantially constant power level is derived over a predetermined frequency band, in each of a plurality of relatively widely spaced power ranges, from a microwave load having a predetermined amplitude versus frequency response, such as an antenna. A microwave source of substantially constant amplitude drives a forward path connected between the source and the load. The forward path includes a voltage controlled, PIN diode, variable microwave attenuator. A feedback path responsive to the microwave power level in the forward path derives a control voltage for the PIN attenuator. The feedback path includes a microwave equalizer attenuator having an amplitude versus frequency response corresponding substantially with the amplitude versus frequency response of the load. The equalizer attenuator drives a linear, crystal amplitude detector.
    Type: Grant
    Filed: March 29, 1977
    Date of Patent: May 30, 1978
    Inventors: James C. Administrator of the National Aeronautics and Space Administration, with respect to an invention of Fletcher, Leo E. Titus
  • Patent number: 4092606
    Abstract: A received, suppressed carrier, quadraphase shift key modulated (QPSK) signal is demodulated with a phase locked loop including a variable frequency, coherent reference that drives first and second channels also responsive to the QPSK signal. The channels respectively derive first and second replicas of binary signals that modulated the suppressed carrier. The replicas are combined to derive a variable amplitude error signal for controlling the coherent reference frequency. The frequency of the coherent reference is dithered at a low rate so that there is derived a relatively low level tracking error phase from the locked loop. The frequency of the coherent reference is swept when the phase of the error signal differs from the dithering phase by a predetermined value that is appreciably less than 90.degree..
    Type: Grant
    Filed: June 21, 1977
    Date of Patent: May 30, 1978
    Inventors: Alan M. Acting Administrator of the National Aeronautics and Space Administration, with respect to an invention of Lovelace, Carl R. Ryan
  • Patent number: 4091329
    Abstract: A circuit deriving an output voltage that is proportional to the logarithm of a DC input voltage susceptible to wide variations in amplitude includes a constant current source which forward biases a diode so that the diode operates in the exponential portion of its voltage versus current characteristic, above its saturation current. The constant current source includes first and second, cascaded feedback, DC operational amplifiers connected in a negative feedback circuit. An input terminal of the first amplifier is responsive to the input voltage. A circuit shunting the first amplifier output terminal includes a resistor in series with the diode. The voltage across the resistor is sensed at the input of the second DC operational feedback amplifier.
    Type: Grant
    Filed: February 16, 1977
    Date of Patent: May 23, 1978
    Inventors: James C. Administrator of the National Aeronautics and Space Administration, with respect to the invention of Fletcher, Paris H. Wiley, Eugene A. Manus
  • Patent number: 4077678
    Abstract: An energy storage device comprises a flywheel rotor in the form of a spokeless ring of filamentary, composite material rotating around a ring-shaped stator. Along the inner rim of the rotor, there is a layer of magnetically soft iron that forms homopolar, salient pole pairs. An ironless armature winding mounted on the stator extends into an air gap formed between the pole pairs. To bring the rotor up to speed, alternating current is supplied to the armature winding using electronic commutation. The armature current interacts with flux in the air gap to create a force acting to rotate the rotor. During coast down, current may be tapped from the rotor using commutation diodes. The rotor and stator are maintained in axial alignment to each other by magnetic flux produced by a permanent magnet in the stator. An electromagnet incorporated in the stator modulates permanent magnet flux to compensate for any eccentricity between the stator and the rotor that may develop during rotation.
    Type: Grant
    Filed: July 30, 1976
    Date of Patent: March 7, 1978
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Philip A. Studer, Harold E. Evans