Patents Represented by Attorney L A Germain
-
Patent number: 4683930Abstract: A split retaining ring for locking a separable tire bead flange on a wheel rim has inboard and outboard facing portions and two circumferentially aligned terminal ends, each terminal end characterized by an outboard facing tab having a drilled-through bore. A buckle member having a pair of apertures is mounted on the retaining ring such that each tab passes through a respective aperture and the buckle functions to maintain the terminal ends of the retaining ring in a specific orientation when it is mounted on a wheel rim. A wire fastener is positioned through each drilled bore in a tab to retain the buckle member on the split retaining ring.Type: GrantFiled: October 31, 1985Date of Patent: August 4, 1987Assignee: Goodyear Aerospace CorporationInventors: Paul A. Elam, Jack W. Keller
-
Patent number: 4683824Abstract: A cartridge launched spin stabilized disk for deploying chaff (radar countermeasure dipoles) or other expendable materials or substances from a moving aircraft. The disk, containing the expendable material is ejected from the aircraft at some elevation angle and at an angle in azimuth off of the aircraft line-of-flight and dispenses the expendable material in a more or less uniform fashion for a brief period of time as it travels away from the aircraft.Type: GrantFiled: October 29, 1984Date of Patent: August 4, 1987Inventor: Robert L. Gibbs
-
Patent number: 4676167Abstract: An airborne spin dispensing apparatus (100,101) and method of dispensing a plurality of sub-units (60) such that the ground plane impact pattern of the plurality of sub-units substantially corresponds to a particular geometric ground target. An onboard microprocessor (24) which receives flight data (26) and a selected target data (28) also has a program store of sub-unit ejection sequences each of which corresponds to a particular target impact geometry. The microprocessor (24) selects an appropriate sub-unit ejection sequence in accordance with the flight and selected target data and effects a release of the sub-units (60) from the spinning apparatus such that their ground impact pattern substantially matches the geometry of the ground target.Type: GrantFiled: January 31, 1986Date of Patent: June 30, 1987Assignee: Goodyear Aerospace CorporationInventors: Joseph C. Huber, Jr., Bellur L. Nagabhushan
-
Patent number: 4655398Abstract: A spray nozzle extension is affixed to the output of a conventional spray gun apparatus to allow an operator to spray a polymeric elastomer into enclosed spaces of an integral fuel tank cavity such as to form an in situ tank within the cavity. The nozzle tip is extended from the spray gun by a flexible hose and the complete unit includes variously arranged in-line filter and swivel connectors to achieve dispersion of lumps in the spray material and axial, yaw, and pitch rotation of the nozzle tip respectively.Type: GrantFiled: December 16, 1985Date of Patent: April 7, 1987Assignee: Goodyear Aerospace CorporationInventor: Paul E. Liggett
-
Patent number: 4653403Abstract: Apparatus for ejecting and dispersing a payload of passive radiation interference material into the near vicinity of a tactical aircraft comprises a cartridge case adapted for carrying and launching at least one cylindrical payload disk, the cartridge case having a lineal length of rack teeth within its bore and the payload disk having at least a portion of its exterior circumferential extent with matching gear teeth such that upon explosively pressurizing the cartridge case the payload disk is ejected exhibiting high linear and rotational velocities. The payload disk has tapered bore wall surfaces which confine the payload material and upon being ejected the spin-stabilized payload disk disperses the payload substantially uniformly within the first few milliseconds after leaving the cartridge case.Type: GrantFiled: March 1, 1985Date of Patent: March 31, 1987Inventor: Robert L. Gibbs
-
Patent number: 4648647Abstract: A long beam having designated forward and rearward ends includes a mounted load trolley for carrying and moving a load along a portion of its length, which beam is adapted for being carried aloft in a substantially horizontal attitude by a high lift crane. The beam also carries a standing leg apparatus at its forward end and the load is carried by the trolley from a rearward stopped position that is axially aligned with the center of gravity of the apparatus to a forward off-loading position. The trolley is maintained at the rearward center of gravity position while the high lift crane carries the apparatus and the load aloft to a delivery location and the standing leg apparatus is lowered to a substantially vertical position with respect to the horizontal attitude of the beam to take the weight of the load when the trolley is moved off of the center of gravity position for delivery and off-loading of the load at the forward end of the beam.Type: GrantFiled: June 15, 1983Date of Patent: March 10, 1987Inventor: Charles W. Patton
-
Patent number: 4635695Abstract: A split retaining ring 60 locking a separable tire bead flange 14 on a wheel rim 10 has inboard 60a and outboard 60b facing portions and circumferentially aligned terminal ends 40, 50, each terminal end characterized by a drilled-through bore 46, 56 extending in the axial direction of the ring from the inboard facing portion to the outboard facing portion. A lockwire 70 is positioned through each drilled bore 46, 56 to retain the terminal ends 40, 50 of the split ring in a predetermined circumferential spaced-apart relationship.Type: GrantFiled: October 31, 1985Date of Patent: January 13, 1987Assignee: Goodyear Aerospace CorporationInventors: Richard J. Frank, Donald H. Smith
-
Patent number: 4628953Abstract: A fusible thermally responsive device (20) for mounting in a bore (12) provided for it in a wheel (10) to vent an overpressure condition caused by heat generated in an aircraft wheel and brake assembly comprises a rod-shaped length of a thermally activated virgin eutectic alloy (34) exhibiting a tolerance within .+-.1.degree. F. of a specific melt temperature established for the alloy, which rod-shaped eutectic alloy in its virgin solid form has one end (34b) machined to a self-holding taper such as to be press-fit into a mating bore (28,48) having the same self-holding taper (28b,48b) in a cylindrical carrier member (22,42). The carrier is mounted in the wheel bore, either from the inside (22) or the outside (42) of the wheel, and a pair of O-ring type seals (32,52,62) provide a positive sealing relationship between the virgin eutectic (34) and the carrier (22,42) and between the carrier (22,42) and the wheel (10).Type: GrantFiled: February 11, 1985Date of Patent: December 16, 1986Assignee: Goodyear Aerospace CorporationInventors: Harold E. Correll, William P. Fulmer, James P. Jones, Jr.
-
Patent number: 4596316Abstract: A reciprocating drive for operative axial communication with a brake disk stack through a pressure plate to compress the disk stack for braking of a rotatable wheel comprises: a relatively stationary annular housing; an annular ram member mounted coaxially within the housing and adapted for axial movement and contacting engagement with the pressure plate to effect compression of the brake disk stack; a relatively rotatable annular ring gear member mounted coaxially between the housing and the ram member; a plurality of rollers operative between the rotatable ring gear and ram members to effect an axial movement of the ram member when interacting with the rotatable ring gear member; and at least two high torque motors mounted within the housing and having pinion drives for operative engagement with the ring gear member to rotate the member in response to an electrical signal.Type: GrantFiled: July 1, 1985Date of Patent: June 24, 1986Assignee: Goodyear Aerospace CorporationInventor: Richard L. Crossman
-
Patent number: 4573508Abstract: A flexible and collapsible storage tank (10) for holding large volumes of material is fabricated in a rectangular shape from long lengths of a rubberized square-woven fabric. The lengths of fabric are oriented with overlapping adjacent edges to form inner (122) and outer (124) envelope structures which are integrally vulcanized into a homogeneous tank body (20). The inner envelope (122) is formed by longitudinally oriented fabric plies (22) having overlapping adjacent edges (22a) while the outer envelope (124) is formed by edge plies of fabric (26) folded about the peripheral edges of the inner envelope (122) and orthogonally oriented fabric plies (24) positioned on either side of the inner envelope (122). The tank (10) includes an air vent valve (40) mounted in its top and a closure (30) which clamps and seals a corner exposure (20a) of the tank body (20) and provides access and communication into the tank for filling and emptying.Type: GrantFiled: April 4, 1985Date of Patent: March 4, 1986Assignee: Goodyear Aerospace CorporationInventor: Ernest Knaus
-
Patent number: 4568863Abstract: A control circuit for regulating the application and release of brake force in an electric brake. A pulse width modulator presents an output signal of regulatable duty cycle to power drivers connected to the electric motors of the brake. A control circuit regulates the direction of current flow through the motors to achieve either brake application or brake release. The output of the pulse width modulator is set by the position of the brake pedal or by a signal which is a function of the correlation betwen brake torque and the position of the brake pedal, whichever is larger.Type: GrantFiled: June 27, 1984Date of Patent: February 4, 1986Assignee: Goodyear Aerospace CorporationInventor: Edgar J. Ruof
-
Patent number: 4567967Abstract: 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: December 15, 1983Date of Patent: February 4, 1986Assignee: Goodyear Aerospace CorporationInventor: Richard L. Crossman
-
Patent number: 4566237Abstract: An armored panel construction for a shelter to defeat ballistic fragment and thermal radiation threats comprises an inner structural panel of aluminum alloy sheets bonded to a honeycomb core and an outer face panel of an aramid fiber fabric in a multi-ply resin matrix laminate. The face panel is in a specific spaced relationship to the inner structural panel such that the energy of an impacting projectile is distributed over a large area and the face panel is allowed to flex inwardly in the absorption of such energy.Type: GrantFiled: April 8, 1983Date of Patent: January 28, 1986Assignee: Goodyear Aerospace CorporationInventor: Patrick E. Turner
-
Patent number: 4565729Abstract: A plurality of polyurethane layers, some of which have a contrasting color with respect to an adjacent layer is formed into a laminate. During preparation, each layer is separately formed, as by spraying, and the contrasting color ensures that the preceding layer can be fully covered. The laminate can be utilized to cover areas or objects which are otherwise difficult to ensure that it has a continuous or complete coating. The invention is suitable for use as a coating and for the preparation of various in situ articles or enclosures, for example a fuel tank, such as commercial and military aircraft.Type: GrantFiled: June 9, 1983Date of Patent: January 21, 1986Assignee: Goodyear Aerospace CorporationInventors: Paul E. Liggett, David L. Braun
-
Patent number: 4557356Abstract: A friction brake disk is formed having a plurality of T-shaped slots extending through a peripheral edge thereof from one braking face surface to the other and each slot carries a keyslot reinforcement comprised of a metallic insert member having the same T-shaped configuration such as to be easily inserted in the slot in the axial direction of the disk but restrained from being removed in the radial direction. Each insert member is locked within the slot in the axial direction by at least one retaining clip that is fastened to the insert member and extends beyond the slot into the face surface of the disk.Type: GrantFiled: April 30, 1984Date of Patent: December 10, 1985Assignee: Goodyear Aerospace CorporationInventor: Don W. Petersen
-
Patent number: 4555450Abstract: A transparent moisture-resistant mercaptan composition is made utilizing an amino-titanate catalyst. The composition can be utilized in association with high heat-resistant transparent compositions containing a boroxine compound.Type: GrantFiled: May 1, 1984Date of Patent: November 26, 1985Assignee: Goodyear Aerospace CorporationInventor: John R. Uram, Jr.
-
Patent number: 4552194Abstract: A retaining ring (30) for use in combination with a wheel rim (10) having a separable bead flange (14) to secure the separable bead flange on the rim in the absence of a properly inflated tire is characterized by an inboard facing portion (30a) and an outboard facing portion (30b) and a split in the ring defining terminal ends, (32,33) each terminal end having a circumferentially oriented first bore (36,37) in the inboard facing portion (30a) and a second bore (38,39) in the outboard facing portion (30b) at an angular relationship with respect to the first bore.Type: GrantFiled: June 11, 1984Date of Patent: November 12, 1985Assignee: Goodyear Aerospace CorporationInventors: Richard P. Brown, Harold E. Correll
-
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