Patents Represented by Attorney E. W. Oldham
  • Patent number: 4554299
    Abstract: A method for preparing a polyurethane which has good long term flexibility, solvent resistance and resistance to hydrolysis, said method comprising mixing three components just prior to curing said components comprising a prepolymer solution, a cement solution and a crosslinking solution, said crosslinking solution comprising a solvent, an aromatic diamine and the ketimine of an aliphatic diamine.
    Type: Grant
    Filed: April 12, 1985
    Date of Patent: November 19, 1985
    Assignee: Goodyear Aerospace Corporation
    Inventor: Paul E. Liggett
  • Patent number: 4554300
    Abstract: A method for preparing a polyurethane suitable for lining fuel tanks, said polyurethane having good, fuel resistance and improved hydrolysis resistance by using a ketimine of an aliphatic diamine as a curing agent in a three-component system composed of a prepolymer solution, a cement solution and a curing agent solution.
    Type: Grant
    Filed: April 12, 1985
    Date of Patent: November 19, 1985
    Assignee: Goodyear Aerospace Corporation
    Inventors: Paul E. Liggett, Daniel A. Chung
  • Patent number: 4454201
    Abstract: A high heat resistant transparency of epoxy resins cured with adducts of trimethoxyboroxine and benzyl alcohol is disclosed to resist intense heat for these transparencies in their use on military and industrial hardware. Additionally, the transparency may include phosphite or phosphate compounds to improve heat resistance, with the phosphate compound in sufficient concentrations to delay gel times such that the phenyl substituted alkyl alcohol may be eliminated from the composition. This transparency may exist in a composite with other layers of transparent material known to those skilled in the art. The epoxy tranparency layer is bound to the other transparent layers, in a variety of configurations, using an interlayer of mercaptan terminated resins. These resins greatly improve resistance to moisture permeability in and about the edges of the entire transparency.
    Type: Grant
    Filed: July 1, 1982
    Date of Patent: June 12, 1984
    Assignee: Goodyear Aerospace Corporation
    Inventor: John R. Uram, Jr.
  • Patent number: 4450202
    Abstract: A high heat resistant transparency of epoxy resins cured with adducts of trimethoxyboroxine and benzyl alcohol is disclosed to resist intense heat for these transparencies in their use on military and industrial hardware. Additionally, the transparency may include phosphite or phosphate compounds to improve heat resistance, with the phosphate compound in sufficient concentrations to delay gel times such that the phenyl substituted alkyl alcohol may be eliminated from the composition. This transparency may exist in a composite with other layers of transparent material known to those skilled in the art. The epoxy transparency layer is bound to the other transparent layers, in a variety of configurations, using an interlayer of mercaptan terminated resins. These resins greatly improve resistance to moisture permeability in and about the edges of the entire transparency.
    Type: Grant
    Filed: July 1, 1982
    Date of Patent: May 22, 1984
    Assignee: Goodyear Aerospace Corporation
    Inventor: John R. Uram, Jr.
  • Patent number: 4433758
    Abstract: A brake adjuster wherein a solid or fluted rod is connected between the return mechanism and the pressure plate of a brake assembly. The rod passes through a draw ring of slightly less diameter than the major diameter of the rod. The draw ring may be part and parcel of, or operatively connected to, the spring follower. The rod is drawn through the draw ring under force imparted by the pressure plate on brake wear action, the draw ring swaging and reshaping the rod as the rod extends to compensate for brake wear. The rod may be either a smooth, solid one, or it may be fluted or ribbed.
    Type: Grant
    Filed: August 14, 1978
    Date of Patent: February 28, 1984
    Assignee: Goodyear Aerospace Corporation
    Inventor: Richard L. Crossman
  • Patent number: 4359732
    Abstract: 1. In a terrain contour mapping system in an aircraft, the combination ofa dipole radar antenna consisting of two vertically spaced fan beam antenna poles mounted on the aircraft,means to transmit radar signals at a depressed angle from the antenna in directions normal to the flight path of the aircraft,means to measure and record the phase difference in the radar signals received at the two poles of the antenna when the signals are reflected from the earth,an inertial system to measure and record airborne platform orientation and position,means to combine the orientation and position information with the recorded radar information, andground stationed means adapted to receive the combined information to provide a three coordinate output signal which determines points on a map representing the contour of the terrain flown over by the aircraft.
    Type: Grant
    Filed: November 21, 1963
    Date of Patent: November 16, 1982
    Assignee: Goodyear Aerospace Corporation
    Inventor: Gregory L. Martin
  • Patent number: 4352848
    Abstract: A high heat resistant transparency of epoxy resins cured with adducts of trimethoxyboroxine and benzyl alcohol is disclosed to resist intense heat for these transparencies in their use on military and industrial hardware. This transparency may exist in a composite with other layers of transparent material known to those skilled in the art. The epoxy transparency layer is bound to the other transparent layers, in a variety of configurations, using an interlayer of mercaptan terminated resins. These resins greatly improve resistance to moisture permeability in and about the edges of the entire transparency.
    Type: Grant
    Filed: November 6, 1980
    Date of Patent: October 5, 1982
    Assignee: Goodyear Aerospace Corporation
    Inventor: John R. Uram, Jr.
  • Patent number: 4343928
    Abstract: A high heat resistant transparency of epoxy resins cured with adducts of trimethoxyboroxine and benzyl alcohol is disclosed to resist intense heat for these transparencies in their use on military and industrial hardware. Additionally, the transparency may include phosphite or phosphate compounds to improve heat resistance, with the phosphate compound in sufficient concentrations to delay gel times such that the phenyl substituted alkyl alcohol may be eliminated from the composition. This transparency may exist in a composite with other layers of transparent material known to those skilled in the art. The epoxy transparency layer is bound to the other transparent layers, in a variety of configurations, using an interlayer of mercaptan terminated resins. These resins greatly improve resistance to moisture permeability in and about the edges of the entire transparency.
    Type: Grant
    Filed: February 5, 1981
    Date of Patent: August 10, 1982
    Assignee: Goodyear Aerospace Corporation
    Inventor: John R. Uram, Jr.
  • Patent number: 4343857
    Abstract: A coating for optical members such as acrylic or polycarbonate comprising prehydrozyled alkyl silicate, polysilicic acid and monocarboxylic acid dispersed in an aqueous vinyl interpolymer and an epoxy binder containing a filler of fumed silica or aluminum oxide and a silane.
    Type: Grant
    Filed: August 23, 1978
    Date of Patent: August 10, 1982
    Assignee: Goodyear Aerospace Corporation
    Inventor: John Uram, Jr.
  • Patent number: 4338370
    Abstract: A chemically resistant coated fabric laminate in which a rubber layer is adhered to one side of a fabric which has been dipped in a blend solution of a rubber and an adhesive. To the remaining side of the impregnated fabric is applied a rubber layer which has thereon a chemically resistant preformed film. The rubber layer containing the preformed film has a dry adhesive compound incorporated therein.
    Type: Grant
    Filed: April 7, 1980
    Date of Patent: July 6, 1982
    Assignee: Goodyear Aerospace Corporation
    Inventor: Charles A. Suter
  • Patent number: 4336592
    Abstract: An antiskid control system is presented which includes variable gains to compensate for brakes which exhibit large changes in lining friction coefficient. Fundamentally, the invention includes a pressure transducer and associated amplifier which presents an output signal corresponding to brake pressure. An accelerometer is connected to a second amplifier which presents an output signal analogous to brake torque. These two signals are combined in a summing circuit and the function obtained therefrom is used to modify the control signal from the antiskid control circuit. Effectively, this function provides a modification of antiskid system gain.
    Type: Grant
    Filed: June 23, 1980
    Date of Patent: June 22, 1982
    Assignee: Goodyear Aerospace Corporation
    Inventor: Arnold A. Beck
  • Patent number: 4327948
    Abstract: An antiskid brake control wherein sensitive deceleration detectors present output signals to a valve driver for releasing brake pressure. The deceleration detector output is also passed to a modulator which acts as a memory circuit to keep the average brake pressure near the skid level and also provides for a controlled reapplication of brake pressure following the release. A constant current discharge circuit is connected to the modulator to provide a linear discharge of the modulator capacitor. A fast recovery circuit is interconnected between the deceleration detector and modulator to rapidly discharge the modulator capacitor in the event that no outputs from the deceleration detector have been sensed for a predetermined period of time. The control system includes gain control circuitry to provide for at least three distinct system gains.
    Type: Grant
    Filed: August 14, 1978
    Date of Patent: May 4, 1982
    Assignee: Goodyear Aerospace Corporation
    Inventors: Arnold A. Beck, Edgar J. Ruof
  • 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: 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: 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: 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