A computer docking station devised to save desktop space while also eliminating the presence of permanent cables that can clutter the work surface is disclosed. The computer docking station utilizes a split design, with a lower dock subassembly positioned beneath the work surface for housing the permanent cables necessary for the computer workstation to operate and an upper dock subassembly comprising one or more data ports positioned on top of the work surface. A monitor arm mount can be attached to, or integrated into, the upper dock subassembly, thereby alleviating the need for a separate monitor arm mount without negatively impacting the docking station's footprint.

Configurations for rack connection systems are disclosed. In at least one embodiment, an adapter for a component plug includes a rotation component to enable rotation of at least a portion of the component plug about at least two axes.

A holder for an electronic rack includes a pivot point and a first end of the holder having a first blind-mate connector to be coupled to a second blind-mate connector at a first engagement interface. The first blind-mate connector and the second blind-mate connector are coupled in response to the holder moving to the second position in response to contact with the electronic rack. The holder additionally includes a second end of the holder having a third blind-mate connector to be coupled to a fourth blind-mate connector at a second engagement interface. The third blind-mate connector and the fourth blind-mate connector are coupled in response to the holder moving to the second position in response to contact with the electronic rack.

An electrical connection assembly including two complementary connectors, each including a mutually parallel electrically insulating plates each comprising one face carrying signal transport contacts and an opposite face carrying at least one shielding sheet in such a manner that, when the connectors are connected together, the plates are interleaved between one another so that the contacts are pressed against one another and the shielding sheets are pressed against each other.

A method electrically insulates an electronic device including a housing having a first face provided with a first opening closed by a PCB and a second face provided with a second opening extending facing at least a portion of at least one connection interface in which at least one first connector is connected. The method includes the steps of forming a mold around the connection interface, and while the device is placed in a vacuum enclosure, pouring a liquid resin into the mold in order to form a layer of electrically insulating material between the connector and the connection interface. A device is obtained by performing the method.

An electronic component system includes a chassis that includes a body, an electrically isolated portion, and an insulator disposed between the electrically isolated portion and the body, wherein the insulator is comprised of a first electrically insulating material. The electronic component system further includes a first electronic component mounted to the electrically isolated portion, and a second electronic component mounted to the body and electrically connected to the first electronic component.

A power distribution panel with a backplane, an insulating panel covering the backplane, and at least one electronic component mounted to the insulating panel. A set of feet can be mounted to the insulating panel and configured to absorb stress applied to the insulating panel where the set of feet are located in the same plane as the backplane.

Disclosed is a computer case with I/O panels on opposite sides of the case, and a method for providing the case. The case includes a top, a bottom, a back side that is opposite a front side, and a right side that is opposite a left side. The case also includes a front I/O opening formed in the front side that receives a front I/O panel. The computer case also includes a rear I/O opening in the back side that receives a rear I/O panel.

Ruggedized avionics assemblies for use on kinetically launched space vehicles are disclosed. The avionic assemblies are able to maintain structural integrity and functionality under high acceleration forces generated during kinetic launch, including acceleration forces of >5,000 times Earth's gravity in a single direction of loading. The avionics assembly is ruggedized to withstand this level of acceleration force during launch via a plurality of constraining elements to constrain a plurality of printed circuit boards aligned in parallel to an acceleration vector. Further, a high specific strength and stiffness composition of the plurality of constraining elements aids in supporting the printed circuit boards and preventing them from bending and dislodging electronic components mounted to the printed circuit boards.

A scalable system for high-power computer, comprising a plurality of motherboard chassis, inserted in a computer rack mounting kit, each motherboard chassis, being configured to receive at least one motherboard module, said plurality of inner chassis forming a stack of inner chassis, the stack being configured to receive an outer floating bracket chassis, said outer chassis being inserted by a second longitudinal end of each inner chassis forming the stack of inner chassis, each said outer floating bracket chassis being configured to accommodate at least one double floating bracket being configured to house a cable box capable of connecting the connectors of a plurality of motherboard modules, arranged in said inner chassis of the stack, to each other, the system being characterized in that the double floating bracket comprises at least several floating attachment means.