Patents Represented by Attorney Armand G. Morin
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Patent number: 3983753Abstract: An improved thermistor holder structure is disclosed which facilitates skin-temperature measurement. The device includes a cylindrical plastic housing with tab extensions that permits the apparatus to be held to a skin surface by suitable elastic members or the like. Ventilation openings are provided in the plastic housing to permit air circulation. An adjustable, resilient metal arm with a thermistor holding cup formed at one end is secured to the interior surface of the plastic housing such that the holding cup is located at the center of the housing. A thermistor temperature sensor is inserted into and held in the cup by interference fit.Type: GrantFiled: September 29, 1975Date of Patent: October 5, 1976Assignee: The United States of America as represented by the United States National Aeronautics and Space AdministrationInventors: John E. Greenleaf, Bill A. Williams
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Patent number: 3978364Abstract: High efficiency, multi-dimensional thin film vacuum tubes suitable for use in high temperature, high radiation environments are described. The tubes are fabricated by placing, as by photolithographic techniques, such as are used in solid state integrated circuits, thin film electrode members in selected arrays on facing interior wall surfaces of an alumina substrate envelope. Cathode members are formed using thin films of triple carbonate. The photoresist used in photolithography aids in activation of the cathodes by carbonizing and reacting with the reduced carbonates when heated in vacuum during forming. The finely powdered triple carbonate is mixed with the photoresist used to delineate the cathode locations in the conventional solid state photolithographic manner. Upon high temperature forming (1000.degree. C) the barium, etc. is formed at the surface. Anode and grid members are formed using thin films of refractory metal.Type: GrantFiled: July 24, 1974Date of Patent: August 31, 1976Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: John Dimeff, William J. Kerwin
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Patent number: 3971362Abstract: A miniature, ingestible and encapsulated telemeter device for transmitting information relating to deep-body temperature of a subject comprising a battery source of power, and a free running multivibrator circuit having fixed biasing means connected to oscillator having a predetermind resonant frequency. A thermistor having a negative temperature coefficient of resistance is connected to the battery and the fixed biasing means and is operative to vary the output frequency of the multivibrator circuit in proportion to the temperature of the thermistor, the oscillator being pulsed into alernate states of conduction and non-conduction at the output frequency of the multivibrator to produce an output consisting of bursts of energy at the predetermined resonant frequency, preferably in the range 88 - 108 MHz.Type: GrantFiled: October 27, 1972Date of Patent: July 27, 1976Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventors: Jack M. Pope, Thomas B. Fryer
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Patent number: 3971535Abstract: An aircraft including a single fuselage having a main wing and a horizontal stabilizer airfoil pivotally attached at their centers to the fuselage. The pivotal attachments allow the airfoils to be yawed relative to the fuselage for high speed flight, and to be positioned at right angles with respect to the fuselage during take-off, landing, and low speed flight. The main wing and the horizontal stabilizer are upwardly curved from their center pivotal connections towards their ends to form curvilinear dihedrals.Type: GrantFiled: August 12, 1974Date of Patent: July 27, 1976Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Robert T. Jones
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Patent number: 3972038Abstract: An accelerometer telemetry system incorporated in a finger ring is used for monitoring the motor responses of a subject. The system includes an accelerometer, battery and transmitter and provides information to a remote receiver regarding hand movements of a subject wearing the ring, without the constraints of wires. Possible applications include the detection of fatigue from the hand movements of the wearer.Type: GrantFiled: March 28, 1975Date of Patent: July 27, 1976Inventors: James C. Administrator of the National Aeronautics and Space Administration, with respect to an invention of Fletcher, Eph Konigsberg
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Patent number: 3964306Abstract: A system for measuring momentum flux in a turbulently flowing fluid including a sensing apparatus for dynamically sensing the mainstream and the cross velocity components of the fluid, a transducer operative to provide two electrical output signals representative of the velocity components in the mainstream and in the cross direction, and signal processors to derive the Reynolds stress wave and the Reynolds stress.Type: GrantFiled: January 29, 1975Date of Patent: June 22, 1976Inventors: James C. Administrator of the National Aeronautics and Space Administration, with respect to an invention of Fletcher, Dah Yu Cheng
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Patent number: 3965096Abstract: A new class of polymers is provided, namely, poly (diarylsiloxy) arylazines. These novel polymers have a basic chemical composition which has the property of stabilizing the optical and physical properties of the polymer against the degradative effect of ultraviolet light and high temperatures. This stabilization occurs at wavelengths including those shorter than found on the surface of the earth and in the absence or presence of oxygen, making the polymers of the present invention useful for high performance coating applications in extraterrestrial space as well as similar applications in terrestrial service. The invention also provides novel aromatic azines which are useful in the preparation of polymers such as those of the present invention.Type: GrantFiled: November 8, 1973Date of Patent: June 22, 1976Assignee: The United States of America as represented by the Administrator of the United States National Aeronautics and Space AdministrationInventors: Ronald F. Reinisch, Hermilo R. Gloria, Ronald E. Goldsberry, Michael J. Adamson
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Patent number: 3956833Abstract: An aircraft simulator for affording practice in landing maneuvers and the like. A cathode ray tube (CRT) produces an image corresponding to the runway which image changes in response to the trainee's manipulation of controls. The CRT image is projected along an optical path to a screen that is visually accessible to the trainee. Interposed in the optical path are optical elements such as mirrors which are spaced from one another along the optical path so as to create virtual images on the screen that appear to be at different distances from the trainee. The optical elements are sequentially interposed in the path and circuits are provided for synchronizing the production of the CRT image with one of the optical elements so that the image on the screen appears to the trainee to have a range corresponding to the environment being simulated by the CRT image.Type: GrantFiled: September 13, 1974Date of Patent: May 18, 1976Assignee: The United States of America as represented by the United States National Aeronautics and Space AdministrationInventor: Wendell D. Chase
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Patent number: 3957037Abstract: The invention comprises of a pair of readout ring electrodes which are used in conjunction with apparatus for measuring the electrical impedance between different points in the body of a living animal to determine the amount of blood flow therebetween. The readout electrodes have independently adjustable diameters to permit attachment around different parts of the body between which it is desired to measure electric impedance. The axial spacing between the electrodes is adjusted by a pair of rods which have a first pair of ends fixedly attached to one electrode and a second pair of ends slidably attached to the other electrode. Indicia are provided on the outer surface of the ring electrodes and on the surface of the rods to permit measurement of the circumference and spacing between the ring electrodes. The ring electrodes are electrically isolated from each other.Type: GrantFiled: February 24, 1975Date of Patent: May 18, 1976Inventors: James C. Administrator of the National Aeronautics and Space Administration, with respect to an invention of Fletcher, Leslie D. Montgomery, Dwight L. Moody, Jr.
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Patent number: 3953734Abstract: A non-dispersive gas analyzing apparatus is described having a first chamber for containing a first gas, the density of which it is desired to determine. A source of radiant energy is provided for passing radiant energy through the first chamber. Modulation means are provided for modulating the radiant energy passing through the first chamber by modulating the volume of the chamber at the acoustic resonance frequency of the first gas and the chamber. Signal generating means including a second chamber for containing a gas which is heated by radiant energy emerging from the first chamber and a microphonic means responsive to the resulting pressurization in the second chamber is provided for generating a signal having a frequency and amplitude corresponding to the modulation of the radiant energy in the first chamber.Type: GrantFiled: November 22, 1974Date of Patent: April 27, 1976Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: John Dimeff
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Patent number: 3952083Abstract: A reusable silica surface insulation (RSI) material is provided by bonding amorphous silica fibers with colloidal silica at an elevated temperature. The surface insulation is ordinarily manufactured in the form of blocks (i.e., tiles).Type: GrantFiled: December 26, 1973Date of Patent: April 20, 1976Inventors: James C. Administrator of the National Aeronautics and Space Administration, with respect to an invention of Fletcher, Howard E. Goldstein, Marnell Smith, Daniel Leiser
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Patent number: 3948102Abstract: A capacitive transducer and circuit especially suited for making measurements in a high-temperature environment. The transducer includes two capacitive electrodes and a shield electrode. As the temperature of the transducer rises, the resistance of the insulation between the capacitive electrode decreases and a resistive current attempts to interfere with the capacitive current between the capacitive electrodes. The shield electrode and the circuit coupled thereto reduces the resistive current in the transducer. A bridge-type circuit coupled to the transducer ignores the resistive current and measures only the capacitive current flowing between the capacitive electrodes.Type: GrantFiled: July 17, 1975Date of Patent: April 6, 1976Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space AdministrationInventor: Grant W. Coon
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Patent number: 3943368Abstract: A method and apparatus is described for compensating for reflection losses in an optical path length modulated absorption-absorption gas analyzer used for determining the density of a reference gas in an unknown gas sample. The apparatus comprises a first chamber for containing a first gas including a reference gas at a known partial density and a second chamber for containing a second gas including a sample of the reference gas at an unknown partial density. A source of radiant energy is provided for passing radiant energy through the first and second chambers. Means are provided for modulating the path length of the radiant energy in the chambers. Additionally, a chopper wheel comprising a plurality of gas cells containing a sample of the reference gas is interspersed by a plurality of gas cells containing a gas excluding the reference gas.Type: GrantFiled: October 15, 1974Date of Patent: March 9, 1976Assignee: The United States of America as represented by the United States National Aeronautics and Space Administration Office of General Counsel-Code GPInventor: John Dimeff
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Patent number: 3938956Abstract: In a hydrogen flame detector there is provided a means for modulating the density of a gas stream prior to its introduction into the detector flame. A detector, responsive to the resulting modulation of the flame, is provided for producing an output signal having a component fluctuating at the frequency of modulation. A cross-correlator, responsive to the output signal and a signal at the frequency of modulation, is provided for producing a resultant signal proportional to the cross-correlation between its two input signals. A means is further provided for recording or otherwise utilizing the resultant signal thus produced.Type: GrantFiled: June 28, 1974Date of Patent: February 17, 1976Assignee: The United States of America as represented by the National Aeronautics and Space Administration Office of General Counsel-Code GPInventor: John Dimeff
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Patent number: 3938035Abstract: A flask having a threaded neck and a cap adapted for threaded engagement on the neck. A laminated disc between the cap and the neck forms a gas tight seal and the cap has a central opening that exposes a medial region of the disc. Piercing the disc through the opening are two electrodes, the inner ends of which contact the sample within the flask and the outer ends of which afford connection of test equipment thereto. Cylindric glass tubes are fitted over the external portion of the electrodes to provide physical support therefor; silicone rubber or the like serves to retain the glass cylinders in place and form a gas tight seal between the cylinders and the electrodes. Shrinkable tubing is shrunk over the glass tubes to afford further mechanical support and sealing. A final relatively large diameter shrinkable tube is shrunk over both electrodes and their associated glass cylinders.Type: GrantFiled: July 16, 1974Date of Patent: February 10, 1976Inventors: James C. Administrator of the National Aeronautics and Space Administration, with respect to an invention of Fletcher, William P. Gilbreath, Michael J. Adamson, Alexander G. Fassbender
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Patent number: RE28921Abstract: An automated visual examination apparatus for measuring visual sensitivity and mapping blind spot location including a projection system for displaying to a patient a series of visual stimuli, a response switch enabling him to indicate his reaction to the stimuli, and a recording system responsive to both the visual stimuli per se and the patient's responses, the recording system thereby providing a correlated permanent record of both stimuli and response from which a substantive and readily apparent visual evaluation can be made.Type: GrantFiled: March 19, 1974Date of Patent: August 3, 1976Assignee: The United States of America as represented by the administrator of the National Aeronautics and Space AdministrationInventors: Richard F. Haines, James W. Fitzgerald, Salvadore A. Rositano