Patents Represented by Attorney P. E. Milliken
  • Patent number: 4383594
    Abstract: A unique configuration for a torque tube assembly associated with a disk type brake comprises separable and replaceable keys and a separable and replaceable brake disk backplate. The keys are mounted in anti-rotation slots at the inboard and outboard ends of the torque tube and bolted to the barrel portion of the torque tube and are characterized by a radial extension that supports the separable backplate. The torque tube is a formed wrought metal tube that is mounted to the stationary portion of the brake housing via bolts that thread into the inboard end of the keys. In this configuration, the occurrence of a defective key and/or backplate does not require replacement of the total torque tube assembly.
    Type: Grant
    Filed: June 8, 1981
    Date of Patent: May 17, 1983
    Assignee: Goodyear Aerospace Corporation
    Inventors: Harold E. Correll, Richard L. Crossman
  • Patent number: 4382832
    Abstract: A process for providing a low haze, high transparent, high heat-resistant laminate by forming a preform laminate of a high heat-resistant layer covered on both surfaces by a non-glass protective layer with at least one said layer being an as-cast acrylic layer. This combination can be readily stored for long periods of time or used immediately after the formation thereof by peeling off one of the as-cast acrylic layers and applying a transparent flexible adhesive layer thereto. The transparent material can be added to the adhesive layer. Many other combinations and laminates can be formed from the preform high heat-resistant laminate since during the preparation thereof, haze is not introduced to the transparency via moisture, and contact with haze-forming release coatings is avoided.
    Type: Grant
    Filed: September 28, 1981
    Date of Patent: May 10, 1983
    Assignee: Goodyear Aerospace Corporation
    Inventor: John Uram, Jr.
  • Patent number: 4381049
    Abstract: Apparatus for electrically controlling the application and release of aircraft brakes. In one embodiment, the invention includes a slurry clutch controlling a reciprocating member which is operatively connected to the pressure plate. In another embodiment of the invention, a torque motor is adapted to have an armature which comprises a ball screw, the ball screw being in engagement with a longitudinal drive rod interconnected with the pressure plate. Rotation of the armature causes the drive rod to move the pressure plate into forceful engagement with the brake disk stack or to retract the same. In yet another embodiment of the invention, a plurality of torque motors are interconnected with a bull gear which is operative for driving the pressure plate.
    Type: Grant
    Filed: July 30, 1979
    Date of Patent: April 26, 1983
    Assignee: Goodyear Aerospace Corporation
    Inventor: Richard L. Crossman
  • Patent number: 4373645
    Abstract: A resilient liner for mounting within a hopper type receptacle which receives and discharges flowable bulk particulate material. The liner is comprised of one or more resilient panels each having a fluid tight envelope with a top and bottom sheet held in substantially spaced parallel relationship by a series of internal transverse seams or walls or by a layer of open celled foam when the internal pressure of the envelope is at least slightly higher than the ambient pressure outside the envelope. The panels are sufficiently resilient, that particles or chunks of material passing through the hopper striking the top of the envelope cause undulation of the top of the envelope which aids in maintaining the constant flow of particulate material through the receptacle. The panels may be protected by a wear resistant cover loosely covering the panels or integral with the panels.
    Type: Grant
    Filed: March 30, 1981
    Date of Patent: February 15, 1983
    Assignee: Goodyear Aerospace Corporation
    Inventor: Hugh Boyd
  • Patent number: 4372533
    Abstract: A pneumatic pad comprises reinforcement fabrics of parallel cords pre-formed to a specific radius through the edges of the pad and press-molded to a very flat pre-pressurized configuration. At least two orthogonally oriented reinforcement fabrics are embedded in elastomer and have lapped ends positioned in opposite covers of the pad such that each cover comprises at least three cord reinforcement plies two of which are oriented orthogonally with respect to the other.
    Type: Grant
    Filed: March 12, 1982
    Date of Patent: February 8, 1983
    Assignee: Goodyear Aerospace Corporation
    Inventors: Ernest Knaus, Paul E. Liggett, Raymond J. Namsick
  • Patent number: 4360124
    Abstract: A flexible, fabric-reinforced, complex-shaped container comprises a fabric reinforcement material and at least one facing layer of a polymeric or elastomeric material, said fabric comprised of yarns capable of changing their effective lengths upon being shaped to a complex mold configuration and thereafter maintained in that shaped condition by curing of the composite material. The method of the invention comprises applying a differential pressure to the fabric reinforced composite in a concave mold having the desired complex configuration to move the composite into the mold cavities as the effective length of the yarns change to conform to the mold and thereafter curing of the composite so as to set the composite to the mold shape.
    Type: Grant
    Filed: October 6, 1980
    Date of Patent: November 23, 1982
    Assignee: Goodyear Aerospace Corporation
    Inventors: Ernest Knaus, Raymond J. Namsick, Herbert D. Smith
  • 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: 4350231
    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 thereof 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: September 15, 1980
    Date of Patent: September 21, 1982
    Assignee: Goodyear Aerospace Corporation
    Inventors: Richard L. Crossman, Richard L. Kirk
  • 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: 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: 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: 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: 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: 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.