Patents Assigned to Applied Concepts Aircraft Solutions, Inc.
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Publication number: 20130328327Abstract: A bolt mechanism comprising a backing plate adapted to be mounted on a complementary surface of a flat panel, a bolt assembly housing attached to the backing plate, a sliding bolt assembly carried on the bolt assembly housing one end of which has means adapted to engage and latch to a striker, a spring on said housing for keeping the end of the bolt extending out of the bolt assembly housing, the backing plate having means adapted to enable attachment to and detachment from an actuator housing assembly having complementary means adapted to enable attachment and detachment.Type: ApplicationFiled: August 14, 2013Publication date: December 12, 2013Applicants: Applied Concepts Aircraft Solutions, Inc., The Young Engineers, Inc.Inventor: Manuel Loret de Mola
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Patent number: 8534718Abstract: The combination of an actuator housing assembly and a bolt mechanism assembly adapted to enable attachment and detachment, the assemblies being carried on opposed sides of a panel. The bolt mechanism assembly comprises a sliding bolt assembly one element of which is adapted to latch to a striker.Type: GrantFiled: September 9, 2011Date of Patent: September 17, 2013Assignees: The Young Engineers, Inc., Applied Concepts Aircraft Solutions, Inc.Inventor: Manuel Loret de Mola
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Publication number: 20130168908Abstract: A vibration isolation fastener insert comprising: a rigid cylindrical hub having an externally extending flange and a through longitudinal opening to receive a fastener. An elastomeric bushing around the hub has a slot therein receiving the external flange. An upper housing is disposed around the side of the bushing and has a flange over the top of the bushing. A lower housing is disposed around the external side of the upper housing and has a flange extending below a lower surface of the bushing.Type: ApplicationFiled: January 18, 2013Publication date: July 4, 2013Applicants: APPLIED CONCEPTS AIRCRAFT SOLUTIONS, INC., THE YOUNG ENGINEERS, INC.Inventors: The Young Engineers, Inc., Applied Concepts Aircraft Solutions, Inc.
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Patent number: 8393601Abstract: A vibration isolation fastener insert comprising: a rigid cylindrical hub having an externally extending flange and a through longitudinal opening to receive a fastener. An elastomeric bushing around the hub has a slot therein receiving the external flange. An upper housing is disposed around the side of the bushing and has a flange over the top of the bushing. A lower housing is disposed around the external side of the upper housing and has a flange extending below a lower surface of the bushing.Type: GrantFiled: October 4, 2008Date of Patent: March 12, 2013Assignees: Applied Concepts Aircraft Solutions, Inc., The Young Engineers, Inc.Inventor: Manuel Loret de Mola
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Publication number: 20120080890Abstract: A bolt mechanism comprising a backing plate adapted to be mounted on a flat panel, a bolt assembly housing carried by the backing plate, a sliding bolt assembly carried on the bolt assembly housing one end of which can engage and latch to a striker, and a spring on the housing for keeping the end of the bolt extending out of the bolt assembly housing. An actuator housing assembly comprising a housing having an opening therein, a movable actuator member received in the opening, the actuator member having a front surface and a rear surface and being digitally movable in the opening, and a hammer extending from the rear surface of the movable actuator member. The actuator housing assembly is adapted to enable the attachment to and detachment from the bolt mechanism assembly.Type: ApplicationFiled: December 14, 2011Publication date: April 5, 2012Applicants: The Young Engineers, Inc., Applied Concepts Aircraft Solutions, Inc.Inventor: Manuel Loret de Mola
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Publication number: 20120013134Abstract: A bolt mechanism comprising a backing plate adapted to be mounted on a flat panel, a bolt assembly housing attached to the backing plate, a sliding bolt assembly carried on the bolt assembly housing one end of which can engage and latch to a striker, and a spring on the housing for keeping the end of the bolt extending out of the bolt assembly housing. An actuator housing assembly comprising an actuator housing having an opening therein, a movable actuator member received in the opening, the actuator member having a front surface and a rear surface and being digitally movable in the opening, and a hammer extending from the rear surface of the movable actuator member. The actuator housing assembly is adapted to enable the attachment to and detachment from the bolt mechanism assembly.Type: ApplicationFiled: September 9, 2011Publication date: January 19, 2012Applicants: APPLIED CONCEPTS AIRCRAFT SOLUTIONS, INC., THE YOUNG ENGINEERS, INC.Inventor: Manuel Loret de Mola