Conductively coated fastening systems are disclosed herein. An apparatus includes a fastening system and a structural assembly. The structural assembly comprises a first structural element made of an electrically conductive fiber reinforced plastic and a second structural element. The first structural element comprises a first hole and the second structural element comprises a second hole. The first and second holes are separately pre-formed prior to assembly of the structural assembly. The structural assembly further comprises an electrically conductive gap filler applied to a first structural element sidewall of the first hole of the first structural element. The fastening system comprises a fastener comprising a head and a shank extending from the head. The shank is configured to be inserted into the first hole and the second hole.

A mezzanine power pin includes a dual layer pin body extending between a pin top having an upper power interface and a pin bottom having a lower power interface. The dual layer pin body has a base metal core and an outer metal oxide layer combined with the base metal core defining an outermost layer of the dual layer pin body. The mezzanine power pin includes an upper fastener coupled to the pin top to mechanically and electrically connect an upper component to the upper power interface. The mezzanine power pin includes a lower fastener coupled to the pin bottom to mechanically and electrically connect a lower component to the lower power interface. The base metal core is configured to electrically connect the upper component and the lower component through the base metal core.

Method of manufacturing a ground apparatus and ground apparatus comprising an aluminum nut (16) having an internal thread and adapted to clamp an eyelet (28) of an electrical conductor on a corresponding contact area of the stud (12), wherein the nut (16) has at least one coating (30) which contains at least zinc, characterized in that the coating further comprises tin, in that the coating consists of an acid tin-zinc electroplating on the aluminum nut (16) and is such that the tin is between 60 and 80% by weight of the coating and the tin-zinc coating forms a layer with an average thickness of from about 5 to 16 microns

A power electronic arrangement has a power converter module including a switching device with a substrate with a first and a second DC voltage conductor track and a first and a second DC voltage terminal element connected in an electrically conducting manner with the correct polarity, and has a first and a second DC voltage connection element. The first DC voltage terminal element is connected to the first DC voltage connection element in an electrically conducting manner with the correct polarity by means of a first materially-bonded connection. The second DC voltage terminal element is connected to the second DC voltage connection element in an electrically conducting manner with the correct polarity by means of a second materially-bonded connection. The second DC voltage terminal element or the second DC voltage connection element has a continuous welding cavity in the region of the first connection.

A conduit nipple grounding bushing to connect between two electrical enclosures or an electrical enclosure and a conduit body, comprising a body having a first portion and a second portion forming a hollow cylindrical interior for the passage of conductors therethrough, the body having a first opening at a first end of the body and a second opening at a second end of the body, the first portion having an outer surface with one or more mounting pads along a circumferential area, each of said one or more mounting pads configured for receipt of a grounding lug, and an end surface dimensioned to contact an electrical box about a knockout hole thereof, and wherein the second portion has exterior threads configured to pass through a knockout hole of an electrical box and dimensioned for receipt of a locknut if the conduit nipple grounding bushing is connected between two electrical boxes or for threaded engagement with a threaded hub of a conduit body if the conduit nipple grounding bushing is connected between an electrical box and a conduit body; and a grounding lug dimensioned for securement to one of the mounting pads by a screw, wherein the mounting pad includes a threaded bore for receipt of said screw.

A bus bar connector with a replaceable fuse are provided. A first terminal assembly inside the casing includes a first connecting element and plural first resilient contacts electrically connected with the first connecting element. A second terminal assembly inside the casing includes a second connecting element and plural second resilient contacts. An end of the second connecting element is electrically connected with the plural second resilient contacts, and another end of the second connecting element extends to form a cable connecting portion. The first cable assembly includes a first cable body extending from at least one of the left and right sides of the casing, and a cable connection portion connected to one side of the first cable body. The fuse element is connected in series between the cable connection portion and the first connecting element. The second cable assembly is electrically connected to the cable connecting portion.

An electrical switching device includes a connection section for fastening and contacting an electrical conductor. The connection section has a fastening element for fastening the electrical conductor, a current-carrying element spaced apart from the fastening element and including a contact point, and an electrically conductive contacting element extending from the fastening element to the contact point of the current-carrying element and into an inner section of the electrical switching device.

Aircraft wing composite ribs having electrical grounding paths are described. An example composite rib includes a carbon fiber reinforced plastic (CFRP) panel, a metallic rib post, a metallic fitting, and a metallic grounding member. The metallic rib post is coupled to the CFRP panel and configured to be coupled to a spar of an aircraft wing, the spar being coupled to a current return network (CRN) cable. The metallic fitting is coupled to the CFRP panel and configured to be coupled to a skin panel of the aircraft wing. The metallic grounding member is positioned between the CFRP panel and the metallic fitting. The metallic grounding member provides an electrical grounding path extending from the metallic fitting to the metallic rib post.

The present disclosure relates to a connection structure for connecting a power cable and a conductor lead-out rod to minimize electrical resistance of a contact surface, and conductor connection device of a power cable.

A charging inlet includes a first terminal including a first terminal body and a bus bar. An inlet body accommodates the first terminal body. A retaining member is attached to the inlet body from a rear side. The first terminal body includes a circular rod shaped first terminal connector. The bus bar includes a bus bar body, a bus bar-side fastening portion, and a first wire fastening portion. The bus bar body electrically connects the bus bar-side fastening portion and the first wire fastening portion. The retaining member includes a retaining body and a protruding portion. The first terminal connector is inserted through a first terminal insertion hole of the retaining body. The protruding portion is disposed along the bus bar body to retain the bus bar.