Patents Assigned to Goodyear Aerospace Corporation
-
Patent number: 4542809Abstract: 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 ring communicating with the pressure plate. Rotation of the armature causes the drive ring 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: GrantFiled: February 10, 1984Date of Patent: September 24, 1985Assignee: Goodyear Aerospace CorporationInventor: Richard L. Crossman
-
Patent number: 4535957Abstract: A device (10) for venting aircraft tires comprises a fusible plug (42) and a spring-biased piston (30), both plug (42) and piston (30) being positioned within a single bore (B) of the device. The plug (42) is meltable out of the bore when the wheel (12) temperature increases above a specific limit set by the eutectic material which frees the piston (30) to move out of a spring-biased and bore-sealing position within a sealing ring (22) by an overpressure within the tire which overcomes the spring bias. The piston (30) will return to a sealing position when the pressure drops below a value which is insufficient to overcome the spring bias.Type: GrantFiled: July 18, 1983Date of Patent: August 20, 1985Assignee: Goodyear Aerospace CorporationInventors: Andrea L. Bischoff, Robert W. Chin
-
Patent number: 4536824Abstract: This invention provides for the dissipation of heat generated in integrated circuit components mounted on printed circuit boards. High conduction, low thermal resistance cooling channels are mounted between the ICs and the PC board to effect conduction cooling in conjunction with forced air convection cooling of the ICs without adding subtantially to the volume space requirements of the IC component-PC board assemblies.Type: GrantFiled: March 28, 1983Date of Patent: August 20, 1985Assignee: Goodyear Aerospace CorporationInventors: Howard W. Barrett, Paul F. Fledderjohann
-
Patent number: 4529068Abstract: A brake wear adjuster is mounted within the bore of an actuator piston having a snap ring at the entrance of the bore. The adjuster includes a spring holder having a uniquely configured washer that is seated in a groove in the outer surface of the holder. A spring is carried about the holder between the washer and a flange at the opposite end of the holder. A pin having a mounted swage and a deformable swage tube are carried within the bore of the spring holder, the swage tube being movable with the holder while the pin and swage are stationary. Upon hydraulic fluid pressure being applied to the piston, the snap ring engages the washer and it in turn compresses the spring as it moves through the distance established in the groove. An occurrence of disk wear in the brakes causes the piston and holder to move further drawing the swage tube over the swage. Upon release of the pressure, the spring moves the washer and snap ring and thus also the piston to a retracted position to disengage the brake disks.Type: GrantFiled: June 28, 1983Date of Patent: July 16, 1985Assignee: Goodyear Aerospace CorporationInventor: Phillip C. Gallo
-
Patent number: 4529640Abstract: A configuration for a light-weight composite armor comprises an outer layer of high content carbon steel; an inner laminate of multiple plies of ballistic grade fabric; and an intermediate core material interconnecting the outer steel to the fabric laminate in an established spaced relationship to defeat armor piercing projectiles from the outside while providing a reverse offensive threat from the inside.Type: GrantFiled: April 8, 1983Date of Patent: July 16, 1985Assignee: Goodyear Aerospace CorporationInventors: Robert M. Brown, Patrick E. Turner
-
Patent number: 4523282Abstract: An antiskid control circuit for aircraft or other braked vehicles in which a deceleration detector determines the instantaneous rate of deceleration of the vehicle, and provides a deceleration signal to an integrator and lead network, in parallel interconnection. The outputs of the lead network and modulator are applied to an antiskid valve through a summing circuit. The deceleration detector is provided with a selectable gain, such that the gain is greater when the wheel is decelerating than when it is accelerating, allowing the integrator to obtain an average charge as a function of deceleration.Type: GrantFiled: March 8, 1982Date of Patent: June 11, 1985Assignee: Goodyear Aerospace CorporationInventor: Arnold A. Beck
-
Patent number: 4496707Abstract: A method for preparing a polyurethane wherein the components thereof have a long shelf life. The formulation is made by separately preparing a prepolymer solution, a crosslinking solution, and a cement solution. Upon utilization, the solutions are mixed together and applied. The urethane has very good fuel resistance and can be used as a coating in fuel tanks as well as to form integral fuel tanks.Type: GrantFiled: June 9, 1983Date of Patent: January 29, 1985Assignee: Goodyear Aerospace CorporationInventor: Paul E. Liggett
-
Patent number: 4496033Abstract: A pair of axially aligned and nested pistons are mounted in a pressure sealed arrangement within the bore of a pressure housing. A primary piston is moved in response to increasing pressure to provide an actuating output force while a secondary piston simultaneously moves to overcome a reverse bias on it by a tension spring and adds to the actuating force by engaging the primary piston only when the pressure exceeds a specific higher threshold. The primary and secondary pistons thereafter operate in conjunction under the influence of high pressure to provide the output actuating force.Type: GrantFiled: December 28, 1981Date of Patent: January 29, 1985Assignee: Goodyear Aerospace CorporationInventors: John M. Hall, Milan Pantic
-
Patent number: 4487913Abstract: A polyester polyurethane compound is formed by reacting trans-1,4-cyclohexanediisocyanate with a mixed polyester. The mixed polyester can be the copolymerization condensation product of an aliphatic dicarboxylic acid or an aromatic dicarboxylic acid, or a separate physical blend thereof reacted with a polyol. The polyurethane can also contain small amounts of non-extractable epoxies and carbodiimides. The urethane has very good hydrolytic stability in comparison with prior art polyurethane systems and also very good fuel resistance and anti-icing resistance. A preferred area of use is an aircraft fuel tanks and anti-icing components.Type: GrantFiled: March 12, 1984Date of Patent: December 11, 1984Assignee: Goodyear Aerospace CorporationInventor: Daniel A. Chung
-
Patent number: 4474060Abstract: A torque readout sensor for mounting to a bolted interconnection between an aircraft brake assembly and a brake reaction torque limiting apparatus to sense the reaction torque upon the application of braking action comprises a metal body that replaces a bushing at the bolted interconnection and configured such that a deflection of the body is accomplished in the direction of the reaction torque force and at least one pair of strain gauges are affixed to the body at the point of deflection to provide an output electrical signal calibrated to the amount of deflection and thus to the reaction torque experienced by the body.Type: GrantFiled: July 12, 1982Date of Patent: October 2, 1984Assignee: Goodyear Aerospace CorporationInventor: Richard L. Crossman
-
Patent number: 4456496Abstract: A method of making an elastomeric coated fabric container utilizing cured elastomeric coated fabric and adhering the edges of each layer of fabric to the other with an adhesive film and curing the adhesive film under heat and pressure to form said container.Type: GrantFiled: March 1, 1979Date of Patent: June 26, 1984Assignee: Goodyear Aerospace CorporationInventors: Charles A. Suter, Raymond J. Namsick
-
Patent number: 4454201Abstract: 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: GrantFiled: July 1, 1982Date of Patent: June 12, 1984Assignee: Goodyear Aerospace CorporationInventor: John R. Uram, Jr.
-
Patent number: 4449616Abstract: A brake adjuster, including a pin interconnecting a brake pressure plate at one end and a metal swage at the opposite end and oriented within a deformable tube such as to radially deform the tube to the shape of the swage as the swage moves into the tube bore in response to brake wear, is rendered non-reversible to loading in the reverse direction by a washer mounted on the pin, relative to the swage, and having the circumferential geometric configuration of the tube bore such as to move easily within the bore in the swaging direction but stopped from movement in the opposite direction by the deformed portion of the tube. In alternative embodiments a tube is mounted on the pin or the pin diameter is increased to approximate the bore diameter of the deformable tube. The trailing edges of the tube or the pin adjacent the leading edge of the swage abut the deformed portion of the tube in the reverse direction to prevent motion in that direction.Type: GrantFiled: December 3, 1979Date of Patent: May 22, 1984Assignee: Goodyear Aerospace CorporationInventors: Lester W. Musser, Jr., Lee A. Germain
-
Patent number: 4450202Abstract: 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: GrantFiled: July 1, 1982Date of Patent: May 22, 1984Assignee: Goodyear Aerospace CorporationInventor: John R. Uram, Jr.
-
Patent number: 4435240Abstract: 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: GrantFiled: September 22, 1982Date of Patent: March 6, 1984Assignee: Goodyear Aerospace CorporationInventors: Ernest Knaus, Raymond J. Namsick, Herbert D. Smith
-
Patent number: 4434021Abstract: A manufacturing process for reverse building complex-shaped vehicle fuel tanks using complementary female mold halves which, when joined together about their mating peripheral edges, exactly duplicate the vehicle body cavity into which the completed tanks are to be mounted. Plies of a urethane elastomer are spray-coated into the molds and nylon fabric reinforcement is applied in two steps to complete the composite which forms the tank structure. Upon completion of forming of the composite, the mold halves are joined and a splice is completed from the inside of the tank by laying in reinforcement fabric at the butt joined sections of the composite and sealing it with urethane elastomer.Type: GrantFiled: July 2, 1982Date of Patent: February 28, 1984Assignee: Goodyear Aerospace CorporationInventors: Keith D. Robinson, George P. Smitley
-
Patent number: 4433758Abstract: 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: GrantFiled: August 14, 1978Date of Patent: February 28, 1984Assignee: Goodyear Aerospace CorporationInventor: Richard L. Crossman
-
Patent number: 4432440Abstract: 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: GrantFiled: February 11, 1982Date of Patent: February 21, 1984Assignee: Goodyear Aerospace CorporationInventor: Richard L. Crossman
-
Patent number: 4423832Abstract: An inflatable liner for mounting within a hopper type receptacle or container which receives and discharges flowable bulk particulate material. The liner is comprised of one or more inflatable members such as inflatable fabric bags or tubular members loosely supported by sling members at spaced locations along the interior surface of the walls of the container in such manner that each inflatable member is capable of limited miltidirectional movement with respect to the adjacent container wall and a flexible wear resistant cover sheet loosely covering the wall and the inflatable members. The slings may be attached to either the container wall or to the bottom side of the cover sheet. Alternate inflatable members are inflated and deflated in any desired sequence to cause the cover sheet to undulate and thereby set up a continuous cyclic wave motion which serves to maintain the continuous flow of particulate material through the container.Type: GrantFiled: July 29, 1981Date of Patent: January 3, 1984Assignee: Goodyear Aerospace CorporationInventors: Hugh Boyd, John J. Kane
-
Patent number: RE31898Abstract: An inflatable-deflatable flexible structural component comprising a flexible foam core portion having a fabric covering, the fabric being sealed against loss of air by a flexible elastomeric coating.Type: GrantFiled: May 17, 1984Date of Patent: May 28, 1985Assignee: Goodyear Aerospace CorporationInventor: Charles A. Suter