Patents Assigned to Stanley Aviation Corporation
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Patent number: 5160176Abstract: 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: GrantFiled: November 18, 1991Date of Patent: November 3, 1992Assignee: Stanley Aviation CorporationInventor: Edwin J. Gale
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Patent number: 4982860Abstract: 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: GrantFiled: May 14, 1990Date of Patent: January 8, 1991Assignee: Stanley Aviation CorporationInventors: John C. Dinsmoor, Barry Van Everen
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Patent number: 4936476Abstract: 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: GrantFiled: April 20, 1989Date of Patent: June 26, 1990Assignee: Stanley Aviation CorporationInventors: John C. Dinsmoor, Barry V. Everen
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Patent number: 4928202Abstract: 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: GrantFiled: December 12, 1988Date of Patent: May 22, 1990Assignee: Stanley Aviation CorporationInventors: Edwin J. Gale, Albert B. Olsen, John C. Dinsmoor
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Patent number: 4900070Abstract: 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: GrantFiled: February 21, 1989Date of Patent: February 13, 1990Assignee: Stanley Aviation CorporationInventors: Richard R. Runkles, John A. Dyer
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Patent number: 4881760Abstract: 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: GrantFiled: November 7, 1988Date of Patent: November 21, 1989Assignee: Stanley Aviation CorporationInventors: Richard R. Runkles, John A. Dyer, Jack W. Beyer
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Patent number: 4808117Abstract: 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: GrantFiled: September 8, 1987Date of Patent: February 28, 1989Assignee: Stanley Aviation CorporationInventors: Edwin J. Gale, Albert B. Olsen
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Patent number: 4625999Abstract: 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: GrantFiled: November 19, 1981Date of Patent: December 2, 1986Assignee: Stanley Aviation CorporationInventors: Gordon A. Valentine, Edwin J. Gale
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Patent number: 4621840Abstract: 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: GrantFiled: October 31, 1983Date of Patent: November 11, 1986Assignee: Stanley Aviation CorporationInventor: Frank L. Foster
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Patent number: 4522433Abstract: 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: GrantFiled: May 14, 1982Date of Patent: June 11, 1985Assignee: Stanley Aviation CorporationInventors: Gordon A. Valentine, Edwin J. Gale
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Patent number: 4478439Abstract: 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: GrantFiled: March 26, 1982Date of Patent: October 23, 1984Assignee: Stanley Aviation CorporationInventor: Jack A. Arnold
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Patent number: 4438959Abstract: 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: GrantFiled: December 2, 1981Date of Patent: March 27, 1984Assignee: Stanley Aviation CorporationInventor: Gordon A. Valentine
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Patent number: 4429905Abstract: 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: GrantFiled: December 29, 1981Date of Patent: February 7, 1984Assignee: Stanley Aviation CorporationInventor: Gordon A. Valentine
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Patent number: 4349357Abstract: 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: GrantFiled: June 23, 1980Date of Patent: September 14, 1982Assignee: Stanley Aviation CorporationInventor: George K. Russell
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Patent number: 4008937Abstract: 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: GrantFiled: September 20, 1974Date of Patent: February 22, 1977Assignee: Stanley Aviation CorporationInventor: Ernest A. Filippi
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Patent number: D315819Type: GrantFiled: April 20, 1989Date of Patent: March 26, 1991Assignee: Stanley Aviation CorporationInventors: John C. Dinsmoor, Barry Van Everen