A method for manufacturing a lighting button key is provided. The method includes forming a button body by processing a metal plate, attaching a thin film to the button body and performing double etching on a rear surface of the button body to process a symbol pattern. Additionally, the method includes press-forming the rear surface of the button body and an injection material of a transparent or translucent material into the rear surface of the button body to perform injection molding.

Embodiments describing a method of forming a multi-layered keycap structure are disclosed herein. The method includes forming a first polymer layer on a second polymer layer, wherein the first polymer layer includes a first color and the second polymer layer includes a second color, and coupling the first polymer layer and second polymer layer to a substrate layer such that the first polymer layer is closer to the substrate than the second polymer layer. The method may further include forming a third polymer layer on the second polymer layer; and etching the multi-layered keycap structure to form an opening having a bottom surface that exposes at least one of the first or second color.

The present invention provides a keycap, method for manufacturing a keycap, and keyswitch. The keycap comprises an inner keycap member, an outer keycap member, and a character layer. The inner keycap member comprises an inner body and an inner sidewall. The inner sidewall is disposed on the periphery of the inner body. The outer keycap member is disposed on the inner keycap member. The outer keycap member comprises an outer body and an outer sidewall. The outer sidewall is disposed on the periphery of the outer body. The outer body is corresponding to the inner body. The outer sidewall corresponds to the inner sidewall. The character layer is disposed between the inner keycap member and the outer keycap member. The character layer comprises a character pattern disposed between the outer body and the inner body.

A method of assembly of an open-cavity, wire-in-air fuse which provides improved manufacturing yield and fuse reliability, involving coiling, braiding or twisting a fusible element around a sacrificial member during the manufacturing process to provide support for the fusible element to prevent mechanical breakages and necking problems commonly encountered during manufacture.

Nanoelectromechanical systems (NEMS) devices/switches and methods for implementing and fabricating the same with conducting contacts are provided. A nanoelectromechanical system (NEMS) switch can include a substrate; a source cantilever formed over the substrate and configured to move relative to the substrate; a drain electrode and at least one gate electrode formed over the substrate; wherein the source cantilever, drain and gate electrodes comprises a metal layer affixed to a support layer, at least a portion of the metal layer at the contact area extending past the support layer; and an interlayer sandwiched between the support layer and substrate.

Systems and methods for forming a magnetostatic MEMS switch include a movable structure formed in a top surface of a substrate, wherein the movable structure is coupled to the substrate by a plurality of restoring springs anchored to the substrate, a stationary structure formed in the same top surface of the substrate, a conductive shunt bar having a characteristic dimension of about 100 um, wherein the shunt bar is disposed on the movable structure adjacent to the gap, an input electrode and an output electrode disposed on the stationary structure and separated by a distance of about 100 um; and a plurality of permeable magnetic features inlaid into the stationary and movable structures, wherein the movable structure is configured to move relative to the stationary structure by interaction of the permeable features with an applied magnetic field, thereby closing the gap and electrically coupling the input and output electrodes across the conductive shunt bar.

Nanoelectromechanical systems (NEMS) devices/switches and methods for implementing and fabricating the same with conducting contacts are provided. A nanoelectromechanical system (NEMS) switch can include a substrate; a source cantilever formed over the substrate and configured to move relative to the substrate; a drain electrode and at least one gate electrode formed over the substrate; wherein the source cantilever, drain and gate electrodes comprises a metal layer affixed to a support layer, at least a portion of the metal layer at the contact area extending past the support layer; and an interlayer sandwiched between the support layer and substrate.

Nanoelectromechanical systems (NEMS) devices/switches and methods for implementing and fabricating the same with conducting contacts are provided. A nanoelectromechanical system (NEMS) switch can include a substrate; a source cantilever formed over the substrate and configured to move relative to the substrate; a drain electrode and at least one gate electrode formed over the substrate; wherein the source cantilever, drain and gate electrodes comprises a metal layer affixed to a support layer, at least a portion of the metal layer at the contact area extending past the support layer; and an interlayer sandwiched between the support layer and substrate.

A symbol button for a vehicle includes: a button body; a button surface portion positioned at an upper portion of the button body; a symbol printing portion positioned on the button surface portion; an anti-plating portion positioned at a lower portion of the button body; and a metal plating layer positioned at the outside of a button excluding the symbol printing portion and the anti-plating portion.

A key mechanism including one or more butterfly hinges. Each butterfly hinge may include a double wing design operative to move between a depressed position and non-depressed position. Hinged coupling mechanisms couple respective arms of the wings together. Additionally or alternatively, a key mechanism can include one or more half-butterfly hinges. Each half-butterfly hinge includes a double wing design operative to move between a depressed position and non-depressed position. A hinged coupling mechanism couples one set of corresponding arms of the wings together, while the other set of corresponding arms are not coupled together.