Patents Assigned to Stanley Aviation Corporation
  • Patent number: 5160176
    Abstract: In accordance with this invention, an adjustable coupling device for releasably interconnecting confronting ends of first and second fluid carrying conduits is provided. A bell flange is attached to the confronting end of one of the conduits. This bell flange has an arcuate internal sealing surface adjacent the lip thereof and a recess extending inwardly longitudinally from the arcuate sealing surface. A sealing flange is attached to the confronting end of the other of the conduits and is sized to be received within the bell flange. It also includes a peripheral abutment spaced from the outer end thereof. A sleeve is mounted on the end of the sealing flange and has a curved outer surface and an inner surface engageable with the abutment to limit the inward movement thereof. A sealing ring is mounted on the sealing flange adjacent the sleeve and is engageable with the arcuate sealing surface of the bell flange when the flanges are drawn together.
    Type: Grant
    Filed: November 18, 1991
    Date of Patent: November 3, 1992
    Assignee: Stanley Aviation Corporation
    Inventor: Edwin J. Gale
  • Patent number: 4982860
    Abstract: An extrusion is provided which includes an upper double sidewall and a lower bulbous portion forming an integral pallet structure. This extrusion can be cut to suitable lengths and welded at the corners to form a sealed rectangular container bottom. A bottom panel is welded around its peripheral edge to the extrusion lengths. Reinforcing I-beams can be placed across the bottom and laterally spaced openings can be cut in the ends and sides of the bottom portions for receiving fork-lift tines. These cut-out portions can be reinforced by tubes or channel members, as required. This structure minimizes the critical welding required to make a sealed container bottom, since only the corner welds and the bottom panel welds are located where air leakage can occur.
    Type: Grant
    Filed: May 14, 1990
    Date of Patent: January 8, 1991
    Assignee: Stanley Aviation Corporation
    Inventors: John C. Dinsmoor, Barry Van Everen
  • Patent number: 4936476
    Abstract: An extrusion is provided which includes an upper double sidewall and a lower bulbous portion forming an integral pallet structure. This extrusion can be cut to suitable lengths and welded at the corners to form a sealed rectangular container bottom. A bottom panel is welded around its peripheral edge to the extrusion lengths. Reinforcing I-beams can be placed across the bottom and laterally spaced openings can be cut in the ends and sides of the bottom portions for receiving fork-lift tines. These cut-out portions can be reinforced by tubes or channel members, as required. This structure minimizes the critical welding required to make a sealed container bottom, since only the corner welds and the bottom panel welds are located where air leakage can occur.
    Type: Grant
    Filed: April 20, 1989
    Date of Patent: June 26, 1990
    Assignee: Stanley Aviation Corporation
    Inventors: John C. Dinsmoor, Barry V. Everen
  • Patent number: 4928202
    Abstract: A bonding jumper is mounted on one facing surface of first and second coupling means which are threadably interconnected. The bonding jumper has a plurality of resilient detent members for bearing against the facing surface of the other coupling means to establish a redundant electrical bond between the first and second coupling means when the facing surfaces are axially drawn toward each other. A plurality of recesses is provided in the second surface for coating with the detent means to yieldably resist opposing relative rotation in the unthreading direction.
    Type: Grant
    Filed: December 12, 1988
    Date of Patent: May 22, 1990
    Assignee: Stanley Aviation Corporation
    Inventors: Edwin J. Gale, Albert B. Olsen, John C. Dinsmoor
  • Patent number: 4900070
    Abstract: A coupling assembly for connecting adjacent ends of conduits, primarily used for aircraft fuel lines having redundant locking features is provided. This coupling can be manipulated with one hand and includes laterally spaced locking tines which engage raised elements for locking the coupling in secured relationship. The coupling assembly can be manipulated with one hand and has viewing ports to be sure that all parts are in place. Also, the tines and guide members are configured to create a force between the two with a longitudinal component tending to open the assembly.
    Type: Grant
    Filed: February 21, 1989
    Date of Patent: February 13, 1990
    Assignee: Stanley Aviation Corporation
    Inventors: Richard R. Runkles, John A. Dyer
  • Patent number: 4881760
    Abstract: A coupling assembly for connecting adjacent ends of conduits, primarily used for aircraft fuel lines having redundant locking features is provided. This coupling can be manipulated with one hand and includes a central tine and laterally spaced locking tines which engage a mating channel for locking the coupling in secured relationship. Indicia is provided across the locking tines which is not visible when the coupling assembly is completely and securely closed. The coupling assembly can be manipulated with one hand and has viewing ports to be sure that all parts are in place. Also, the tines and guide members are configured to create a force between the two with a longitudinal component tending to open the assembly.
    Type: Grant
    Filed: November 7, 1988
    Date of Patent: November 21, 1989
    Assignee: Stanley Aviation Corporation
    Inventors: Richard R. Runkles, John A. Dyer, Jack W. Beyer
  • Patent number: 4808117
    Abstract: A bonding jumper is mounted on one facing surface of first and second coupling means which are threadably interconnected. The bonding jumper has a plurality of resilient detent members for bearing against the facing surface of the other coupling means to establish a redundant electrical bond between the first and second coupling means when the facing surfaces are axially drawn toward each other. A plurality of recesses is provided in the second surface for coacting with the detent means to yieldably resist opposing relative rotation in the unthreading direction.
    Type: Grant
    Filed: September 8, 1987
    Date of Patent: February 28, 1989
    Assignee: Stanley Aviation Corporation
    Inventors: Edwin J. Gale, Albert B. Olsen
  • Patent number: 4625999
    Abstract: A remotely-operable connector comprising a pair of female end fittings, each adapted to be permanently fixed one to each of a pair of pipes to be coupled together, and a jumper assembly having a jumper pipe terminating at opposite ends in male end fittings which are received one in each of the female end fittings. Each mating pair of male and female fittings is received in a pivot housing which is mounted for universal articulation on the female fitting for enabling the housing to be angularly aligned with the end of the male fitting which is received in the female fitting.
    Type: Grant
    Filed: November 19, 1981
    Date of Patent: December 2, 1986
    Assignee: Stanley Aviation Corporation
    Inventors: Gordon A. Valentine, Edwin J. Gale
  • Patent number: 4621840
    Abstract: A retention for male and female structural members, including a self-locking selectively releasable locking spring wire or clip received in opposing grooves on the male and female members for locking the two members together, and interengaged threaded formations on the two members for absorbing a major portion of any force tending to axially separate the two members.
    Type: Grant
    Filed: October 31, 1983
    Date of Patent: November 11, 1986
    Assignee: Stanley Aviation Corporation
    Inventor: Frank L. Foster
  • Patent number: 4522433
    Abstract: Flexible fluid couplings incorporating spherical seats which permit the interconnected pipe section to move axially and/or articulate relative to each other. O-ring seals in the coupling are protected against pressure induced extrusion. The center of articulation is located in a plane which passes close to the O-ring seals.
    Type: Grant
    Filed: May 14, 1982
    Date of Patent: June 11, 1985
    Assignee: Stanley Aviation Corporation
    Inventors: Gordon A. Valentine, Edwin J. Gale
  • Patent number: 4478439
    Abstract: A fluid-conveying coupling assembly in which a plurality of torsionally deflectable seal rings establish a redundant seal between interconnected coupling structures and in which each seal ring is torsionally deflected to its seal-establishing condition by engagement with just one pair of formations on the coupling structure.
    Type: Grant
    Filed: March 26, 1982
    Date of Patent: October 23, 1984
    Assignee: Stanley Aviation Corporation
    Inventor: Jack A. Arnold
  • Patent number: 4438959
    Abstract: A fluid-receiving assembly having a pair of relatively axially displaceable structures, a torsionally deflectable seal ring for establishing a seal between the structures, and a pair of formations engaging diagonally opposite corner edges of the seal ring to torsionally deflect it to its seal establishing condition, one of the formations being formed on one of the structures and the other of the formations being formed in part by the other structure and in part by an adapter ring.
    Type: Grant
    Filed: December 2, 1981
    Date of Patent: March 27, 1984
    Assignee: Stanley Aviation Corporation
    Inventor: Gordon A. Valentine
  • Patent number: 4429905
    Abstract: A fluid-conveying coupling assembly in which a pair of torsionally deflectable seal rings establish a redundant seal between interconnected coupling structures and in which the seal rings are oriented and deflected in such a manner that they impose non-cumulative radially directed forces on the interconnected structures.
    Type: Grant
    Filed: December 29, 1981
    Date of Patent: February 7, 1984
    Assignee: Stanley Aviation Corporation
    Inventor: Gordon A. Valentine
  • Patent number: 4349357
    Abstract: A heatless fractionating apparatus and method wherein a pressurized gaseous mixture, such as air, is alternately passed through first and second adsorbent beds for adsorbing at least a first component but not a second component of the gaseous mixture, and wherein each adsorbent bed is purged of the adsorbed component during the intervals in which the gaseous mixture is not passed through it. A valve system for each adsorbent bed comprises a pressure-responsive valve which responds to the delivery of the pressurized gaseous mixture through an electrically operated valve to deliver the gaseous mixture to its associated adsorbent bed. The pressure-responsive valve also operates to vent purge and other gases from its associated adsorbent bed when the electrically operated valve is closed to block delivery of the pressurized gaseous mixture to the pressure-responsive valve.
    Type: Grant
    Filed: June 23, 1980
    Date of Patent: September 14, 1982
    Assignee: Stanley Aviation Corporation
    Inventor: George K. Russell
  • Patent number: 4008937
    Abstract: A pipe or conduit coupling assembly having a pair of confronting, fluid-conveying members, a longitudinally split coupler removably circumferentially surrounding the fluid-conveying members to limit displacement of the fluid-conveying members away from each other, and at least one electrically conductive spring metal jumper mounted exteriorly on the coupler to complete an electrical circuit between the fluid-conveying members. A special retainer and toggle clamp assembly extends circumferentially around the split sections of the coupler and has a special toggle clamp which is incapable of being improperly latched to releasably secure the split sections of the coupler in place. A special safety lock is provided to prevent inadvertent release of the toggle clamp.
    Type: Grant
    Filed: September 20, 1974
    Date of Patent: February 22, 1977
    Assignee: Stanley Aviation Corporation
    Inventor: Ernest A. Filippi
  • Patent number: D315819
    Type: Grant
    Filed: April 20, 1989
    Date of Patent: March 26, 1991
    Assignee: Stanley Aviation Corporation
    Inventors: John C. Dinsmoor, Barry Van Everen