11
Ronald W Boscaljon, Ronald A Rossway, David E Jewell, Eric Hazelwood: Lightweight positive lock coupling. Stanley Aviation Corporation, Fields and Johnson P C, June 13, 2000: US06073973 (28 worldwide citation)

In the first embodiment, a coupling assembly is provided wherein the inner peripheral diameter of an annular spring is sized to be threadably received over the threads of a coupler and is held in a recess formed by the ends of threads and the edge of a shoulder. This structure minimizes the diameter ...


12
Gerald D Lilja, Frank Fowler, Robert F Hatch: Jet aircraft engine transport apparatus. Stanley Aviation Corporation, Fields & Johnson P C, October 6, 1998: US05816367 (28 worldwide citation)

A jet aircraft engine transport apparatus is disclosed which utilizes three major subcomponents. The first subcomponent is a shipping stand which enables a jet aircraft engine to be configured for transport in either a truck transport mode or air transport mode. The second subcomponent is a fan doll ...


13
Todd A Eyster, Albert B Olsen: Fluid conduit coupling. Stanley Aviation Corporation, Fields & Johnson P C, April 15, 1997: US05620210 (27 worldwide citation)

A coupling assembly for connecting adjacent ends of conduits, primarily used for aircraft fuel, water and oxygen lines having redundant locking features is provided. This coupling can be manipulated with one hand and includes laterally spaced locking tines which engage a mating channel for locking t ...


14
Richard R Runkles, John A Dyer: Conduit coupling device with redundancy features. Stanley Aviation Corporation, Fields Lewis Pittenger & Rost, February 13, 1990: US04900070 (26 worldwide citation)

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 secu ...


15
Edwin J Gale, Albert B Olsen: Coupler with combination locking and bonding ring. Stanley Aviation Corporation, Fields Lewis Pittenger & Rost, February 28, 1989: US04808117 (25 worldwide citation)

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 ...


16
Ronald W Boscaljon, Ronald A Rossway, David E Jewell: Positive lock coupling. Stanley Aviation Corporation, Fields and Johnson P C, February 16, 1999: US05871239 (24 worldwide citation)

A threaded coupling assembly is provided for interconnecting the ends of first and second fluid-carrying conduit members in fixed releasably locking relationship. First and second coupling members are circumferentially engageable with the ends of the conduit members to hold them in fluid communicati ...


17
Ronald A Rossway, Robert F Hatch, Behzad B Suroosh: Method of installing and removing jet aircraft engine. Stanley Aviation Corporation, Sheridan Ross P C, September 25, 2001: US06292999 (20 worldwide citation)

An aircraft engine shipping system includes a frame assembly for supporting the aircraft engine, and a cradle assembly mounted on the frame assembly for securing the aircraft engine to the frame assembly. The frame assembly includes shock absorbers to provide continual shock absorption to an aircraf ...


18
Ronald W Boscaljon, Ronald A Rossway, David E Jewell: Positive lock coupling. Stanley Aviation Corporation, Fields and Johnson P C, April 18, 2000: US06050609 (20 worldwide citation)

A first coupling member has a peripheral facing surface with a pair of annular slots, each of a different length and width. A second coupling member has a lock ring longitudinally slidable thereon with a facing surface having a pair of annular raised locking tabs sized to correspond to the respectiv ...


19
Clifton P Breay, Thomas B Darby, Daniel E Keenan, Anthony W Vaughan: Positive locking fitting assembly. Stanley Aviation Corporation, Sheridan Ross PC, April 26, 2005: US06883836 (18 worldwide citation)

A positive locking fitting assembly is provided for interconnecting two adjacent structures, such as two modular components of an aircraft. The fitting assembly includes a pair of couplers which attach to the respective modular components, and a transfer tube which interconnects the couplers. Each c ...


20
Edwin J Gale, Albert B Olsen, John C Dinsmoor: Coupler with combination locking and bonding ring. Stanley Aviation Corporation, Fields Lewis Pittenger & Rost, May 22, 1990: US04928202 (18 worldwide citation)

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 ...