Abstract: Disclosed is a fabrication technique for, and the structure of, a flexible self-sealing fuel tank having a preactivated sealant constructed by laying-up over an innerliner, positioned on a form, prefabricated panels having a self-sealant member stitched into a rubber-coated outer wrap.
Type:
Grant
Filed:
October 22, 1981
Date of Patent:
January 11, 1983
Assignee:
The United States of America as represented by the Secretary of the Air Force
Abstract: Disclosed is a fabrication technique for, and the structure of, a flexible self-sealing fuel tank having a preactivated sealant constructed by laying-up over an innerliner, positioned on a form, prefabricated panels having a self-sealant member stitched into a rubber-coated outer wrap.
Type:
Grant
Filed:
March 25, 1980
Date of Patent:
August 24, 1982
Assignee:
The United States of America as represented by the Secretary of the Air Force
Abstract: Disclosed is a lock to lock open the speed brake doors of an aircraft to facilitate servicing the brake mechanism. The lock cooperates with lightening holes in the internal stiffening structure of the speed brake. The lock is adjustable to provide different amounts of brake opening. Surfaces of the lock that contact the aircraft speed brake structure are fabricated of resilient material to protect the aircraft.
Abstract: The injection piston of a regenerative liquid propellant gun is attached to a second piston that has a programmed hydraulic resistance which controls its motion, thus the propellant injection rate from the injection piston and the burning rate of the injected propellants is controlled to provide better propellant pressure-time burning characteristics.
Type:
Grant
Filed:
June 19, 1979
Date of Patent:
August 4, 1981
Assignee:
The United States of America as represented by the Secretary of the Air Force
Abstract: In a first air flow circuit filtered ram air cooperating with an aspirator draws crankcase vapors from the crankcase of an internal combustion engine. Heavy particulate matter in the crankcase vapor is heated and further vaporized by a heat exchanger cooperating with an exhaust manifold of the engine. A second aspirator draws the vaporized particulate matter back into the original vapor steam of the first air flow circuit. The crankcase vapors mixed with the incoming ram air are then directed into the interior cavity of the carburetor air filter. In a second air flow circuit filtered ram air is directed into the crankcase and carburetor air filter cavity and in a third air flow circuit filtered air is drawn through a variable annular orifice and metered in accord with intake manifold pressure and directed into the engine air intake system below the carburetor throttle plate.
Abstract: By angling the propellant fluid inlet to the charging chamber of a liquid propellant gun and having a central vent, the tangential swirling of the entering fluid clears the chamber and the fluid of entrapped gas.
Type:
Grant
Filed:
June 19, 1979
Date of Patent:
May 26, 1981
Assignee:
The United States of America as represented by the Secretary of the Air Force
Abstract: A coaxial line, wide dynamic range, ferrite limiter having optimal frequency selectivity for microwave frequencies is provided by a stepped ferrite rod with disks of varying volumes and dielectric constants controlling the operating frequency and threshold level for each step segment.
Type:
Grant
Filed:
July 6, 1979
Date of Patent:
February 17, 1981
Assignee:
The United States of America as represented by the Secretary of the Air Force
Abstract: The capacitance of an unknown capacitor is determined by counting the cycles of a known frequency contained within a time gate whose time duration is determined by subtracting a gate whose length is equivalent to the stray measuring capacitance from a gate whose length is determined by the capacitance of the unknown capacitor plus the unavoidable stray measuring capacitances.
Abstract: The fabrication of porous cadmium electrodes is disclosed in which high cadmium loading without surface buildup is obtained by using a relatively low current density (approximately 0.2 amperes per square inch of plaque area) and period current reversals of time durations approximately equal to 15% of the forward time durations at a current density substantially equal to the forward current density.
Type:
Grant
Filed:
July 27, 1979
Date of Patent:
December 30, 1980
Assignee:
The United States of America as represented by the Secretary of the Air Force
Inventors:
David H. Fritts, John F. Leonard, Thirumalai G. Palanisamy
Abstract: PIN diodes of decreasing base region thicknesses, wherein the thickest base region diode functions as a quasi-active limiter with turn-on bias supplied by detected RF current in a Schottky barrier diode with a discharge resistor providing fast recovery; and the thinnest base region PIN diode being a zero bias punch-through type, with a dc sensitivity time control, functioning as a passive limiter during transmit and controlled attenuator during receive provides an improved radar receiver protector circuit. The operation of the PIN diode is enhanced by a unique mounting on a gold-plated copper puck in the circuit board and tuning the signal leads to the diode.
Type:
Grant
Filed:
July 6, 1979
Date of Patent:
November 4, 1980
Assignee:
The United States of America as represented by the Secretary of the Air Force
Abstract: Four pulse-repetition-frequency coded laser diode arrays emit four beams in quadrature relationship having a central optical axis coinciding with the missile axis. The returned reflected energy from a target impinges upon an optically centered holographic quadrant selector detection system which provides quadrature output signals. These quadrature output signals are passed through respective pulse-repetition-frequency discriminators corresponding to the quadrature prf coded transmitted beams. The outputs from the discriminators are processed through a null comparison circuit to provide output signals for actuating the servo guidance system of the missile to center the optical axis, which is also the missile axis, on the target so that the missile continuously seeks and eventually flies into the target.
Type:
Grant
Filed:
July 9, 1975
Date of Patent:
November 4, 1980
Assignee:
The United States of America as represented by the Secretary of the Air Force
Abstract: An anti-G valve and control system for providing a multivariable, multi-profile, pressurization of aircrew anti-G garments are disclosed. The ramp characteristic, the ramp onset level, a step onset, the step level, a limit pressure, are all controllable over the normal operating range. In addition, an optional ready pressure control is provided to just fill the anti-G suit volume and greatly decrease inflation time required to reach higher pressures.
Type:
Grant
Filed:
October 6, 1978
Date of Patent:
August 26, 1980
Assignee:
The United States of America as represented by the Secretary of the Air Force
Abstract: A leak-tight joint between a Kovar ceramic feed-through and an aluminum housing is obtained by electron beam welding a short length of the outside surface of the Kovar cylindrical shell of the feedthrough to a region of nickel deposited on a thin wall cylindrical tube of aluminum formed in the aluminum housing.
Type:
Grant
Filed:
June 30, 1978
Date of Patent:
July 15, 1980
Assignee:
The United States of America as represented by the Secretary of the Air Force
Abstract: The video outputs of the correlators of a conventional IFM receiver are split by capacitors to obtain (1) pulse signals only and (2) pulse plus cw signals. Combining these signals in differential amplifiers, frequency readings are provided in the normal manner with the improvement that the individual frequency readings of simultaneously received pulse and cw signals are provided.
Type:
Grant
Filed:
December 22, 1978
Date of Patent:
March 18, 1980
Assignee:
The United States of America as represented by the Secretary of the Air Force
Abstract: The indications of attitude indicators at two different indicating locations that are indicating the same parameter but actuated from different sources, are monitored for the same indication by electrically interconnecting two transolvers that are mechanically coupled to the respective attitude indicator at each location. A monitor, at one indicating location, furnishes the excitation for the transolver at the other location and by the magnitudes of the sine and cosine outputs of the local transolver furnishes flag indication of any system defects of either indicator at each location.
Type:
Grant
Filed:
June 15, 1978
Date of Patent:
March 11, 1980
Assignee:
The United States of America as represented by the Secretary of the Air Force
Abstract: Two sectoral radial resonators coupled at their centers of radii by a strip transmission line and doubly loaded with opposing ferrimagnetic spheres between the said strip transmission line and the ground planes provides a frequency selective power limiter.
Type:
Grant
Filed:
May 2, 1978
Date of Patent:
March 11, 1980
Assignee:
The United States of America as represented by the Secretary of the Air Force
Inventors:
Philip S. Carter, Steven N. Stitzer, Harry Goldie
Abstract: In a surface channel charge transfer device noise due to the presence of surface states is minimized by ion implanting the charge coupled device propagation channel so as to provide a narrow potential trough which confines the charge to the center of the CCD channel.
Type:
Grant
Filed:
August 3, 1978
Date of Patent:
January 22, 1980
Assignee:
The United States of America as represented by the Secretary of the Air Force
Abstract: Disclosed is an analog tuning circuit, suitable for multiplexing, having a field-effect transistor connected to the output of an operational amplifier with the drain connected in a feedback loop to the inverting input of the amplifier.
Type:
Grant
Filed:
July 7, 1978
Date of Patent:
January 15, 1980
Assignee:
The United States of America as represented by the Secretary of the Air Force
Abstract: In a porous electrode primary battery a sensing grid is positioned in a cell on or near the surface of the porous cathode facing the separator and anode. The voltage measured between this sensing grid and the conventional cathode current collector grid is a function of the current distribution within the electrode which is continuously changing as the battery discharges, thus the measured voltage is indicative of the state of charge of the particular cell having the sensing grid and for a battery containing cooperatively connected cells, the state of the battery in general.
Type:
Grant
Filed:
April 17, 1978
Date of Patent:
December 25, 1979
Assignee:
The United States of America as represented by the Secretary of the Air Force
Abstract: Electrolyte, lost from the stack to the case in a sealed electrochemical cell, is returned to the stack by a zirconium oxide based ceramic deposited on the inside wall of the pressure vessel, wicking by capillary action, the electrolyte from regions external to the stack to the stack components. The ceramic wick is also used to transfer electrolyte from one separator and/or reservoir to another within the stack, replacing an interior stack wick in a recirculating design. The wall wick is also effective in a back-to-back type cell design.
Type:
Grant
Filed:
December 19, 1978
Date of Patent:
December 4, 1979
Assignee:
The United States of America as represented by the Secretary of the Air Force