Patents Assigned to Goodyear Aerospace Corporation
  • Patent number: 4327467
    Abstract: An inflated shell structure for a curing, embossing, or film winding nip roller having a rubber cover. Fundamentally, the invention includes a mandrel about which a rubber tube is spirally wound. Adhesively secured to the tube and about the mandrel is a bridge composite of plural layers, at least one of which is axially aligned with respect to the mandrel, and at least one of which is circumferentially aligned. Over the bridge network there is maintained a thin rubber cover having a thickness on the order of 0.250-1.0 inch. The tubing can be inflated under a source of gas pressure to give the roll a physical structure of rigidity and consistency. When used as a nip or bonder roller, the forces imparted to the roller are dissipated through the bridge assembly and the inflated tube, greatly limiting the amount of heat generated in the rubber cover.
    Type: Grant
    Filed: May 27, 1980
    Date of Patent: May 4, 1982
    Assignee: Goodyear Aerospace Corporation
    Inventor: Glenn W. Quaint
  • Patent number: 4327413
    Abstract: A circuit incorporated in a braking system for allowing a pilot to select a desired rate of deceleration and to cause the aircraft, upon landing, to achieve and maintain the selected deceleration rate. Fundamentally, the circuit includes a selector switch for selecting the desired rate of deceleration and uses a linear decelerometer signal having an output corresponding to the instantaneous rate of actual deceleration of the aircraft. Comparator circuitry compares the actual and desired rates of deceleration and provides an error signal to high and low rate circuits which charge a storage capacitor which in turn, through a buffer and power drive circuitry, regulates the associated control valve. When the difference between the actual and desired rates exceeds a particular level, the high rate circuit controls the charging of the capacitor.
    Type: Grant
    Filed: September 12, 1979
    Date of Patent: April 27, 1982
    Assignee: Goodyear Aerospace Corporation
    Inventor: Edgar J. Ruof
  • Patent number: 4326755
    Abstract: A deceleration control circuit for limiting the deceleration rate and applied brake pressure at vehicle speeds below a predetermined level. The invention substantially eliminates strut vibrations in aircraft resulting from "grabby" brakes during a braking operation. The invention includes a deceleration detector, operative at vehicle speeds below a particular level, to produce an output signal to the brake valve driver to reduce brake pressure when the deceleration rate exceeds a specific level. The circuitry is adapted to operate in conjunction with an antiskid system and also includes built-in test circuitry for testing the operability of both the antiskid circuitry and the deceleration control circuitry.
    Type: Grant
    Filed: May 11, 1979
    Date of Patent: April 27, 1982
    Assignee: Goodyear Aerospace Corporation
    Inventor: George C. Fretz, III
  • Patent number: 4322462
    Abstract: A splicing unit for integrally joining ends of seal strip material to form a continuous annular seal ring comprises two reinforced elastomeric ply strips with an unreinforced elastomeric gum interposed between them to form an H-section configuration, the length of the unit being substantially the width of the seal strip while the thickness of the gum between the ply strips is substantially the thickness of the seal material to be joined. The ends of the seal strip are inserted between the legs of the H-section on either side of the unreinforced gum and cured to form the integrally spliced seal ring.
    Type: Grant
    Filed: October 17, 1980
    Date of Patent: March 30, 1982
    Assignee: Goodyear Aerospace Corporation
    Inventor: George A. Lucas
  • Patent number: 4314349
    Abstract: A processing element constituting the basic building block of a massively-parallel processor. Fundamentally, the processing element includes an arithmetic sub-unit comprising registers for operands, a sum-bit register, a carry-bit register, a shift register of selectively variable length, and a full adder. A logic network is included with each processing element for performing the basic Boolean logic functions between two bits of data. There is also included a multiplexer for intercommunicating with neighboring processing elements and a register for receiving data from and transferring data to neighboring processing elements. Each such processing element includes its own random access memory which communicates with the arithmetic sub-unit and the logic network of the processing element.
    Type: Grant
    Filed: December 31, 1979
    Date of Patent: February 2, 1982
    Assignee: Goodyear Aerospace Corporation
    Inventor: Kenneth E. Batcher
  • Patent number: 4294886
    Abstract: A highly heat resistant transparency of epoxy resins cured with adducts of trimethoxyboroxine and benzyl alcohol is disclosed. This transparency may exist in a composite with other layers of transparent material known to those skilled in the art. The epoxy resin having the trimethoxyboroxine and benzyl alcohol may also have triphenyl phosphite which further increases the resistance to intense heat for these transparencies in their use on military and industrial hardware.
    Type: Grant
    Filed: August 28, 1979
    Date of Patent: October 13, 1981
    Assignee: Goodyear Aerospace Corporation
    Inventor: John R. Uram, Jr.
  • Patent number: 4286694
    Abstract: Brake discs of carbon or other porous material in which the opposed faces of the discs are provided with shallow grooves extending between the inner and outer circumferences to vent steam and other gases generated during braking. The grooves of the stationary discs may be at different angles relative to the radii than are the grooves of the rotating discs.
    Type: Grant
    Filed: May 16, 1979
    Date of Patent: September 1, 1981
    Assignee: Goodyear Aerospace Corporation
    Inventors: Roy R. Wiseman, Jr., James J. Kovac
  • Patent number: 4282508
    Abstract: A conductor for transmitting an electrical signal from a signal generator on a rotating member to a signal detector on a relatively stationary member across the motion interface between the two members comprises at least one solid carbon graphite ring mounted coaxially between the two members and having a first annular surface in intimate contact with a mating conductive surface on the signal generator and having a second annular surface in intimate contact with a mating conductive surface on the stationary member that is electrically connected to the signal detector, said carbon graphite ring functioning as an electrical interconnection between the two members.
    Type: Grant
    Filed: April 28, 1980
    Date of Patent: August 4, 1981
    Assignee: Goodyear Aerospace Corporation
    Inventors: Bernard D. Raffel, John M. Bowyer
  • Patent number: 4279333
    Abstract: A friction pad configuration and a method and apparatus for fastening said pads to a disk core member wherein the base of the pad is formed with a plurality of extended tabs that are inserted in slots in the core and secured to the tabs of a pad on the opposite surface of the core by a clip that draws the base-to-base mounted pads together on the core. Alternatively, and for mounting on a single face surface of the core, U-clips are mounted on the tabs and inserted through the core to the opposite surface therof and the ends of the U-clips are bent down into annular grooves in the face surface of the core to securely mount the pads to the core.
    Type: Grant
    Filed: June 4, 1979
    Date of Patent: July 21, 1981
    Assignee: Goodyear Aerospace Corporation
    Inventors: Richard L. Crossman, Richard L. Kirk
  • Patent number: 4278153
    Abstract: A brake disk frictional module is provided, composed of sintered metallic material reinforced throughout its entire volume by a grid system of pure metal or metallic alloy. The friction module may be manufactured by sintering the metallic material with the grid reinforcement in either a mold or within the brake disk cup. The internal reinforcement of the frictional module prevents spalling weight loss, friction coefficient decay, or other physical defect as caused by frictional strain during use. The reinforcement material reduces the overall temperature of the disk during use, and aids frictional coefficient of the disk because of the metallic compatibility of the metallic material and grid system.
    Type: Grant
    Filed: November 24, 1978
    Date of Patent: July 14, 1981
    Assignee: Goodyear Aerospace Corporation
    Inventor: Doulatabad A. Venkatu
  • Patent number: 4276969
    Abstract: In a friction component for brakes, clutches and the like, a core member is adapted for carrying a plurality of friction pads or cups on either or both of its surfaces. According to this invention a cylindrical metal bushing is positioned in an aperture through the core member to contact the bottoms of friction pads on the opposite surfaces of the core. The bushing has annular projections at the ends that make contact with the bottoms of the friction pads and passage of an electrical welding current through the assembly affects welding of the bushing projections to the bottoms of the pads and rigidly secures them to the core member.
    Type: Grant
    Filed: April 2, 1979
    Date of Patent: July 7, 1981
    Assignee: Goodyear Aerospace Corporation
    Inventors: Robert W. Chin, Walter J. Krause
  • Patent number: 4275932
    Abstract: An improved aircraft wheel configuration obviates the hazard of wheel failure during take-off and landing situations when tire deflation occurs and the wheel accepts full loading on its flanges. The wheel is configured to provide a differential flange height between the inboard and outboard flanges such that the total load applied to the wheel is distributed equally between the flanges. Alternatively, and/or in addition the flanges are restructured to provide an increased section modulus and the inboard flange is designed to provide a wider contact surface.
    Type: Grant
    Filed: June 8, 1979
    Date of Patent: June 30, 1981
    Assignee: Goodyear Aerospace Corporation
    Inventors: Roy W. Baird, Robert E. Berger, Richard L. Kirk
  • Patent number: 4275376
    Abstract: A signal communicator for transmitting an electrical signal from one member rotating relative to another member is in the configuration of a journal bearing and comprises at least one conically shaped annular graphite ring supported by inner and outer electrically conductive races. While one race is insulatively mounted on the rotating member and electrically connected to a condition sensor, the other race is insulatively mounted on the relatively stationary member and electrically connected to a signal detector, and the graphite ring is an electrical conductor interconnecting the sensor and detector via the two races. Alternatively, two opposing and contacting graphite rings are mounted in nonconducting carriers, one of the carriers keyed for rotation with the sensor while the other is mounted on the relatively stationary member.
    Type: Grant
    Filed: April 28, 1980
    Date of Patent: June 23, 1981
    Assignee: Goodyear Aerospace Corporation
    Inventors: William C. Alexander, Richard L. Kirk, Kenneth A. Thomsen
  • Patent number: 4269455
    Abstract: An antiskid brake control system for a wheeled vehicle having a second order lead network in parallel connection with a deceleration detector. The deceleration detector includes both a current threshold level and a voltage threshold level, the deceleration rate of a wheel having to exceed both thresholds to result in a brake control signal to the modulator and brake control valves. The lead network, deceleration detector, and a modulator all feed a summing circuit which includes a switching circuit providing the system with two distinct characteristic gains. Also included is a circuit for linearly discharging certain capacitors in the system. Also included are locked wheel, touchdown protection, and low speed drop-out circuitry to regulate the application and release of antiskid control and touchdown and upon the occurrence of preselected vehicle activities.
    Type: Grant
    Filed: August 14, 1978
    Date of Patent: May 26, 1981
    Assignee: Goodyear Aerospace Corporation
    Inventors: Arnold A. Beck, Edgar J. Ruof
  • Patent number: 4262378
    Abstract: A buoyant capsule depth controller is presented for positioning and maintaining a capsule within the ocean waters for establishing an observation or defense station. A bouyant capsule is connected to a weight assembly by means of explosive fittings which detonate at a predetermined depth to separate the two. The buoyant capsule and weight assembly are then held together by means of a short line of fixed length until a second predetermined depth is reached, at which time a pressure-actuated release mechanism releases the short line and a cable wound within the weight assembly is payed out to the buoyant capsule below a preset depth as the weight assembly sinks to the ocean floor. The paying out of the cable rotates a shaft within the weight assembly which in turn drives an hydraulic pump, the output of the pump being controlled by a valve to regulate the amount of drag which the pump exerts upon the shaft thus controlling the rate of cable pay out.
    Type: Grant
    Filed: June 8, 1979
    Date of Patent: April 21, 1981
    Assignee: Goodyear Aerospace Corporation
    Inventors: Charles A. Phillips, John A. Pitrone, Edward W. McGraw
  • Patent number: 4257837
    Abstract: A splicing unit for integrally joining ends of seal strip material to form a continuous annular seal ring comprises two reinforced elastomeric ply strips with an unreinforced elastomeric gum interposed between them to form an H-section configuration, the length of the unit being substantially the width of the seal strip while the depth of the gum between the ply strips is substantially the thickness of the seal material to be joined. The ends of the seal strip are inserted between the legs of the H-section on either side of the unreinforced gum and cured to form the integrally spliced seal ring.
    Type: Grant
    Filed: February 25, 1980
    Date of Patent: March 24, 1981
    Assignee: Goodyear Aerospace Corporation
    Inventor: George A. Lucas
  • Patent number: 4252014
    Abstract: A circuit incorporated with an antiskid system for testing the operability of the system. A multivibrator may be actuated to energize converter circuitry with a signal indicative of a particular wheel speed. The entire antiskid system is then caused to function as though the vehicle wheels are actually spinning and the vehicle is moving. The major subcircuits of the antiskid system are connected to logic circuitry which senses their operation and produces an output signal to a lamp which is illuminated when the subcircuits are properly operative. When the multivibrator operation is ceased, changes in operation of the various subcircuits is again sensed by the logic circuitry which, if such subcircuits are operating properly, deenergizes the lamp.
    Type: Grant
    Filed: May 2, 1979
    Date of Patent: February 24, 1981
    Assignee: Goodyear Aerospace Corporation
    Inventor: Edgar J. Ruof
  • Patent number: 4244029
    Abstract: A digital video correlator wherein a reference image and a live image are digitized and compared against each other in a shifting network to determine the correlation or degrees thereof existing between the two images. Fundamentally, the invention includes a video digitizer which divides live and real images from various sources into picture elements and digitizes those elements to fixed voltage levels. The digitized live image is passed to a dynamic memory consisting of a plurality of interconnected shift registers while the digitized reference image is maintained within a first set of shift registers comprising a portion of a processor. A second set of shift registers within the processor maintain therein a mask function. Yet a third set of shift registers within the processor are interconnected in parallel to the dynamic memory to receive, under control of a clock, the digitized data of the live image.
    Type: Grant
    Filed: December 12, 1977
    Date of Patent: January 6, 1981
    Assignee: Goodyear Aerospace Corporation
    Inventors: James J. Hogan, Charles O. Lambert, Gene A. Wallace
  • Patent number: 4243940
    Abstract: A circuit for converting AC signals from a wheel speed transducer to a varying DC level indicative of the instantaneous rotational speed of the wheel of a vehicle. The invention includes a squaring circuit receiving a sinusoidal input from a wheel speed transducer and producing a fixed amplitude square wave of a frequency equivalent to that of the sinusoidal input. A pulsing circuit receives the square wave signal and produces a series of fixed duration pulses of a frequency double that of the sinusoidal signal. These pulses are applied to an integrator which produces a DC output of an amplitude characteristic of the frequency of the sinusoidal input. The integrator has a characteristic phase lag associated therewith resulting in a tendency of the phase of the superimposed AC output, caused by cyclic changes in the frequency of the transducer output, to lag the phase of the associated wheel speed change.
    Type: Grant
    Filed: December 7, 1978
    Date of Patent: January 6, 1981
    Assignee: Goodyear Aerospace Corporation
    Inventor: Edgar J. Ruof
  • Patent number: 4237445
    Abstract: Devices for transmitting signals from a rotatable tire to a stationary receiver which correspond to the internal pressure of the tire. In one embodiment, a Bourdon tube communicates with internal tire pressure to regulate the magnetic gap of an electromagnetic induction configuration. Changes in the magnetic gap result in corresponding changes in an output signal strength. In another embodiment of the invention, a bellows is provided in communication with tire pressure for regulating the position of the core of an LVDT. The core position and, accordingly, the output of the LVDT corresponds to tire pressure. In yet another embodiment, strain gauges or other appropriate electrical signal generators are connected to the tire and interconnected with a rotating race. A plurality of ball bearings are maintained in a preloaded condition between the rotating race and a stationary race, the latter race communicating signals to a tire pressure meter or the like.
    Type: Grant
    Filed: July 30, 1979
    Date of Patent: December 2, 1980
    Assignee: Goodyear Aerospace Corporation
    Inventor: Richard L. Crossman