Patents Assigned to Aviation Device & Electronic Components, L.L.C.
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Publication number: 20140312574Abstract: A spacer and gasket assembly is shown for receipt between a static structure having an outer and inner surface and fastener holes therethrough and a removable structure having a base with fastener holes and an upper surface and a lower surface. The static structure and removable structure are engaged through a multiplicity of fasteners having a shaft diameter. The fasteners are adapted to apply a compression on the gasket between the static structure and the removable structure. The static structure and the removable structure have opposed, typically flat, facing walls. The spacer and gasket assembly comprising a substantially non-compressible spacer adapted for receipt between the static structure and the removable structure having a spacer thickness. A gasket has a deformable, flowable, elastomeric body and a skeleton having a skeleton thickness, the skeleton substantially integral with the body. The gasket has an uncompressed gasket thickness.Type: ApplicationFiled: April 29, 2014Publication date: October 23, 2014Applicant: Aviation Devices & Electronic Components, L.L.C.Inventors: Jeff Busby, Matt Boyd
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Publication number: 20140190720Abstract: An elongated, flexible composite gasket member having a knitted wire mesh rope at least partly impregnated with a soft, tacky, flowable, pre-cured polyurethane gel for use in a stuffing tube assembly. The stuffing tube assembly is used in a deck or bulkhead of a ship. The stuffing tube comprises a cable having insulation on a surface thereof, a metallic shielding jacket, and conductors therein, the cable having an exposed section of metallic shielding and non-exposed section; a metallic stuffing tube with an inner cable channel and an at least partly threaded gland nut receiver space, and a constriction between the gland nut receiver space and the inner channel; a gland nut adapted to threadably engage the gland nut receiver space; and a; wherein the cable passes through the gland nut and stuffing tube with the exposed section substantially wrapped in the elongated flexible composite gasket member the gland nut above the elongated flexible composite material and the constriction below.Type: ApplicationFiled: January 9, 2014Publication date: July 10, 2014Applicant: AVIATION DEVICES & ELECTRONIC COMPONENTS, L.L.C.Inventors: Matthew Panfil, Matthew Boyd, Michael Dry, Kent Boomer, Jeff Busby
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Publication number: 20140167367Abstract: A single piece gasket is disclosed having a skeletal member, typically metallic, and a pliable body. The pliable body includes a first portion having a first firmness and a second perimeter portion have a firmer consistency. When such a composite body is placed under compression, the perimeter will tend to limit the flow of the softer inner material past the firmer perimeter region or portion of the gasket. In this manner, creep or overrun of the less firm portion material will be reduced.Type: ApplicationFiled: May 11, 2012Publication date: June 19, 2014Applicant: AVIATION DEVICES & ELECTRONIC COMPONENTS, L.L.C.Inventors: Jeff Busby, Kent Boomer, Matt Boyd, Michael Dry, Doug Smith
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Publication number: 20140015204Abstract: A spacer and gasket assembly is shown for receipt between a static structure having an outer and inner surface and fastener holes therethrough and a removable structure having a base with fastener holes and an upper surface and a lower surface. The static structure and removable structure are engaged through a multiplicity of fasteners having a shaft diameter. The fasteners are adapted to apply a compression on the gasket between the static structure and the removable structure. The static structure and the removable structure have opposed, typically flat, facing walls. The spacer and gasket assembly comprising a substantially non-compressible spacer adapted for receipt between the static structure and the removable structure having a spacer thickness. A gasket has a deformable, flowable, elastomeric body and a skeleton having a skeleton thickness, the skeleton substantially integral with the body. The gasket has an uncompressed gasket thickness.Type: ApplicationFiled: March 11, 2013Publication date: January 16, 2014Applicant: Aviation Devices & Electronic Components, L.L.C.Inventors: Matt Boyd, Michael Dry, Kent Boomer, Jeff Busby
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Publication number: 20040070156Abstract: A novel gasket material. The gasket material has a fabric core. The fabric core is at least partially saturated with a curable polyurethane mix having a tacky side. A durable skin is attached to one side of the polyurethane mix.Type: ApplicationFiled: July 16, 2003Publication date: April 15, 2004Applicant: AVIATION DEVICES AND ELECTRONIC COMPONENTS, L.L.C.Inventors: Lane Smith, Jeff Busby
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Publication number: 20030234498Abstract: A novel gasket material. The gasket material has a foam core. The foam core is at least partially saturated with a curable polyurethane mix.Type: ApplicationFiled: June 26, 2003Publication date: December 25, 2003Applicant: Aviation Devices & Electronic Components; L.L.C.Inventors: Jeff Busby, Lane Smith
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Publication number: 20030047885Abstract: A gasket material for sealing between two members. The gasket material includes a flexible, woven skeletal member. Enclosing the skeletal member is a flexible, compressible resilient body member having a tacky outer surface, the tacky outer surface for engagement between the two members. In a preferred embodiment the flexible skeletal member is closer to a top surface of the resilient body then it is to a bottom surface of the resilient body. The resilient body may be comprised of urethane. The flexible skeletal member may be comprised of a metallic or a non-metallic material.Type: ApplicationFiled: August 5, 2002Publication date: March 13, 2003Applicant: AVIATION DEVICE & ELECTRONIC COMPONENTS, L.L.C.Inventors: Jeff Busby, Lane Smith
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Patent number: 6530577Abstract: A gasket material for sealing between two members, The gasket material includes a flexible, woven skeletal member. Enclosing the skeletal member is a flexible, compressible resilient body member having a tacky outer surface, the tacky outer surface for engagement between the two members. In a preferred embodiment the flexible skeletal member is closer to a top surface of the resilient body then it is to a bottom surface of the resilient body. The resilient body may be comprised of urethane. The flexible skeletal member may be comprised of a metallic or a non-metallic material.Type: GrantFiled: May 12, 2000Date of Patent: March 11, 2003Assignee: Aviation Device & Electronic Components, L.L.C.Inventors: Jeff Busby, Lane Smith